An aircraft seat arrangement includes a first aircraft seat module delimiting an aircraft seat region, the aircraft seat module includes an aircraft seat configured to be mounted in the aircraft cabin at an angle of more than 30°, to be oriented away from a central aisle towards a window and to form an at least substantially planar lying-down surface, wherein the aircraft seat module includes at least one enclosure unit delimiting the aircraft seat region at least partially, and includes at least one further aircraft seat module arranged directly neighboring the first aircraft seat module and delimiting a further aircraft seat region, wherein the further aircraft seat module also includes an enclosure unit which delimits the aircraft seat region at least partially, is realized substantially identically to the enclosure unit of the first aircraft seat module, and separates the aircraft seat regions of the first and second aircraft seat modules.
The invention relates to a passenger seat device comprising a table leaf and/or support panel (22a; 22b; 22c; 22d), and comprising a PED holder (28a; 28b; 28c; 28d), which is integrated into the table leaf and/or support panel (22a; 22b; 22c; 22d) and comprises a movably, in particular pivotably, mounted main holding panel (50a; 50b; 50c; 50d), which can be frictionally and/or form-fittingly fixed in various angular positions relative to the table leaf and/or support panel (22a; 22b; 22c; 22d). According to the invention, the PED holder (28a; 28b; 28c; 28d) comprises a secondary holding panel (78a; 78b; 78c; 78d) which is arranged so as to be movable, in particular pivotable, relative to the main holding panel (50a; 50b; 50c; 50d) at a lower end of the main holding panel (50a; 50b; 50c; 50d), which secondary holding panel preferably extends over at least half the width of the main holding panel (50a; 50b; 50c; 50d) and is provided in order to be brought at least into a supporting position depending on a movement of the main holding panel (50a; 50b; 50c; 50d) or at least into a supporting position depending on a separate movement of the main holding panel (50a; 50b; 50c; 50d).
The invention relates to a passenger seat device having: a mounting unit (12a; 12b) for mounting on a mounting plane; two seat structure elements (26a, 28a; 26b, 28b), which are respectively arranged on one side of a sitting region (30a); two bearing elements (44a, 46a; 44b, 46b), wherein in each case one bearing element (44a, 46a; 44b, 46b) is fixedly connected to one of the seat structure elements (26a, 28a; 26b, 28b); a backrest (34a; 34b; 34c), which has at least one pivotable backrest element (36a; 36b; 36c) which is mounted pivotably on the seat structure elements (26a, 28a; 26b, 28b) via the bearing elements (44a, 46a; 44b, 46b); at least one restoring module (66a; 66b; 66c), which has at least one spring element (68a; 68b) for providing a restoring force for restoring the pivotable backrest element (36a; 36b) from a comfort position to an upright sitting position; and a locking device (70a; 70b), which is designed separate from the spring element (68a; 68b) and is intended to lock the pivotable backrest element (36a; 36b) steplessly.
B60N 2/20 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable le dossier étant rabattable, p. ex. pour faciliter l'accès
B60N 2/22 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable le dossier étant réglable
B64D 11/06 - Aménagements ou adaptations des sièges
4.
PASSENGER SEAT DEVICE HAVING A DISPLACEABLE HEAD-SUPPORT UNIT
The invention relates to a passenger seat device comprising: a backrest (16a; 16b) and a seat base (14a), wherein the backrest (16a; 16b) and the seat base (14a) can be adjusted between an upright seat position and a lying position; a head-support unit (40a; 40ab), which is attached to an upper end (18a; 18b) of the backrest (16a; 16b); and a mounting module (46a; 46b) for linearly displaceably mounting the head-support unit (40a; 40b) on the upper end (18a; 18b) of the backrest (16a; 16b), wherein the head-support unit (40a; 40ab) can be moved by means of the mounting module (46a; 46b) from a retracted position, over a maximum pull-out path (50a; 50b), into a maximum position. According to the invention, the mounting module (46a; 46b) is intended to limit the maximum pull-out path (50a; 50b) of the head-support unit (40a; 40ab) to different lengths depending on a backrest angle of the backrest (16a; 16b).
The invention relates to an aircraft seat system with an aircraft seat region (14) which has an aircraft seat (16a; 16b; 16c), which can be adjusted between a seated position and a reclined position, and a console (28a; 28b; 28c) arranged in front of the aircraft seat (16a; 16b; 16c), wherein the console (28a; 28b; 28c) forms an elevated footrest surface (34a; 34b; 34c) which is provided to form part of a reclining surface, wherein the console (28a; 28b; 28c) has a stowage module (46a; 46b; 46c) which has a stowage compartment (48a; 48b; 48c) arranged below the footrest surface (34a; 34b; 34c). According to the invention, the stowage compartment (48a; 48b; 48c) is arranged in a region behind the footrest surface (34a; 34b; 34c) and the stowage module (46a; 46b; 46c) has a cover wall (50a; 50b; 50c) which at least partially delimits the stowage compartment (48a; 48b; 48c) in the region behind the footrest surface (34a; 34b; 34c).
The invention relates to a seat device, in particular an airplane seat device, comprising a backrest (14a; 14b; 14c; 14d; 14e), preferably a backrest which is designed to be free of a swiveling table, with a rear face (16a; 16b; 16c; 16d; 16e); and an interface module (24a; 24b; 24d; 24c; 24d) for connecting additional units, said interface module having a support (28a; 28b; 28c; 28d; 28e) which runs in a transverse direction (100a; 100b; 100c; 100d; 100e). According to the invention, the support (28a; 28b; 28c; 28d; 28e) has an attachment region (52a; 52b; 52c; 52d; 52e), in which the support (28a; 28b; 28c; 28d; 28e) forms a gap (54a; 54b; 54c; 54d; 54e) together with the rear face (16a; 16b; 16c; 16d; 16e) of the backrest (14a; 14b; 14c; 14d; 14e), said gap having a depth extension (56a; 56b; 56c; 56d; 56e) of maximally 25.4 mm (1 inch).
B64D 11/06 - Aménagements ou adaptations des sièges
B60N 3/00 - Aménagements ou adaptations d'autres accessoires pour passagers, non prévus ailleurs
B60N 3/10 - Aménagements ou adaptations d'autres accessoires pour passagers, non prévus ailleurs de réceptacles pour nourriture ou boissons, p. ex. réfrigérés
The invention relates to a passenger seat device having a seat component (14a; 14b; 14c) and having a display support module (26a; 26b; 26c) for movably supporting a display element (18a; 18b; 18c) on the seat component (14a; 14b; 14c), the display support module (26a; 26b; 26c) having a fastening base element (28a; 28b; 28c) for fixed connection of the display element (18a; 18b; 18c) and a support unit (30a; 30b; 30c) by means of which the fastening base element (28a; 28b; 28c) is pivotably connected to the seat component (14a; 14b; 14c) and which has at least one rotary bearing (32a, 34a; 32b, 34b; 32c, 34c) for this purpose. According to the invention, the display support module (26a; 26b; 26c) has a holding unit (42a; 42b; 42c) which is provided for fixing the fastening base element (28a; 28b; 28c) in different positions in a positionally secure way and which is in the form of a hinge unit, said hinge unit comprising at least one frictional element (44a; 44b; 44c) for positionally secure fixing.
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
B60R 11/02 - Autres aménagements pour tenir ou monter des objets pour postes radio, de télévision, téléphones, ou objets similairesDisposition de leur commande
An aircraft seat arrangement includes a first aircraft seat device and a second aircraft seat device, wherein the second aircraft seat device has an enclosure which forms a backrest wall in a subregion of the enclosure of the second aircraft seat device, wherein the second aircraft seat device comprises in an aircraft seat region a seat bottom which has a seat bottom front edge, a main extension axis of the seat bottom front edge being oriented at an angle of at least 5 degrees with respect to an aircraft seat device transversal axis of the second aircraft seat device, wherein a lying-down direction of the aircraft seat region is oriented at an angle of at least 30 degrees with respect to an aircraft seat device longitudinal axis of the second aircraft seat device, the lying-down direction being directed away from an access region of the aircraft seat region.
The invention is based on an aircraft seat device having a seat divider, having an armrest, which is pivotable, with respect to the seat divider, between a position of use and a position of non-use and which has an armrest base body, and having an attachment module, which is configured to support the armrest in a pivotable manner with respect to the seat divider, wherein the armrest base body, in a fully installed state, is coupled with the seat divider via the attachment module.
The invention is based on an aircraft seat device having a seat divider, having an armrest, which is pivotable, with respect to the seat divider, between a position of use and a position of non-use and which has an armrest base body, and having an attachment module, which is configured to support the armrest in a pivotable manner with respect to the seat divider, wherein the armrest base body, in a fully installed state, is coupled with the seat divider via the attachment module.
It is proposed that the attachment module is pivotably connected to the seat divider and is configured, in an installation state in which the attachment module is connected to the seat divider, for coupling with the armrest base body, wherein the attachment module, in the fully installed state, is received at least substantially in an attachment space of the armrest.
An aircraft seat module, which forms an aircraft seat region, includes an aircraft seat that is configured to be mounted in an aircraft cabin at an angle α of 30 degrees to 80 degrees, preferably 45 degrees to 65 degrees, and that comprises at least a base frame and a cinematics unit, with an enclosure unit comprising a first enclosure element, which delimits the aircraft seat region at least partially in the region of the aircraft seat, and a second enclosure element, which delimits the aircraft seat region partially at least in a region in front of the aircraft seat, and includes an ottoman providing a footrest region, and with a console unit that forms at least one stowage and/or depositing region of the aircraft seat region, wherein the aircraft seat is combined in a separately realized 16G module and the second enclosure element, the ottoman and the console unit are combined in a separately realized 9G module, wherein the 16G module and the 9G module are configured to be fastened to a cabin floor separately from each other.
The invention relates to an aircraft seat device comprising: a seat divider (26, 28, 30); a fastening pin (44, 46, 48) which is attached to the seat divider (26, 28, 30) for conjoint rotation therewith and which is designed to connect a backrest unit (36, 42); an armrest (60, 62, 64) which has a fastening main body (66), the fastening main body (66) forming at least one fastening shell (76, 78) for connection to the fastening pin (44, 46, 48); and at least one fastening shell element (86, 96) which forms a fastening shell (88) and which, in order to connect the armrest (60, 62, 64) to the fastening pin (44, 46, 48), is designed to be connected to the fastening main body (66) in the regions of the fastening shell (76, 78) of the fastening main body (66), wherein the fastening shells (76, 78, 88) of the fastening shell element (86, 96) and of the fastening main body (66) at least substantially enclose the fastening pin (44, 46, 48) that is fixedly attached to the seat divider (26, 28, 30).
A seat device, in particular an aircraft seat device, includes a backrest having a base frame which includes two lateral frame elements, and a shell element which is connected to the lateral frame elements and at least partly forms a backrest support surface.
The invention is based on an aircraft seat device with a stand unit (12a; 12b; 12c; 12d; 12e; 12f; 12g), with an aircraft seat (10a; 10b; 10c; 10d; 10e; 10f; 10g) which is attached to the stand unit (12a; 12b; 12c; 12d; 12e; 12f; 12g) and forms an aircraft seat region, with a screen unit (42a; 42b; 42c; 42d; 42f; 42g), and with an adjustment module (46a; 46b; 46c; 46d; 46e; 46f; 46g) which is provided to mount the screen unit (42a; 42b; 42c; 42d; 42f; 42g) so as to be adjustable between a stowage position arranged in a stowage region (44a; 44b; 44c; 44d; 44e; 44f; 44g) next to the aircraft seat region and a use position arranged in the aircraft seat region and, for this purpose, has at least one adjustable bearing arm (48a; 48b; 48c; 48d; 48e; 48f; 48g). It is proposed that the screen unit (42a; 42b; 42c; 42d; 42f; 42g) has a flexible, in particular foldable and/or rollable display element (52a; 52b; 52c; 52d; 52f; 52g) which is provided to be changed in its form between a use position and at least one further position.
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
B60N 3/00 - Aménagements ou adaptations d'autres accessoires pour passagers, non prévus ailleurs
B60R 11/02 - Autres aménagements pour tenir ou monter des objets pour postes radio, de télévision, téléphones, ou objets similairesDisposition de leur commande
The invention relates to a passenger seat device having: two seat structure elements (26a-26h, 28a-28h), which are respectively arranged on one side of a sitting region (30a); two bearing elements (44a-44h, 46a-46h), wherein in each case one bearing element (44a-44h, 46a-46h) is fixedly connected to one of the seat structure elements (26a-26h, 28a-28h); a backrest (34a-34h), which has at least one pivotable backrest element (36a-36h) which is mounted pivotably on the seat structure elements (26a-26h, 28a-28h) via the bearing elements (44a-44h, 46a-46h); at least one restoring module (66a-66h), which has at least one spring element (68a-68h) for providing a restoring force for restoring the pivotable backrest element (36a-36h) from a comfort position into an upright sitting position; and a locking device (70a-70h), which is intended to lock the pivotable backrest element (36a-36h) at least in the upright sitting position. The invention proposes that the locking device (70a-70h) have at least one locking module (72a-72h, 74a-74h) which is arranged between the first seat structure element (26a-26h) and a supporting element (42a-42h) of the pivotable backrest element (36a-36h).
B60N 2/20 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable le dossier étant rabattable, p. ex. pour faciliter l'accès
B60N 2/22 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable le dossier étant réglable
B60N 2/427 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules à des fins particulières ou pour des véhicules particuliers le siège étant construit pour protéger son occupant des effets des forces d'accélération anormales, p. ex. sièges anticollision ou sièges de sécurité le siège ou ses parties constitutives se déplaçant lors d'une collision
B64D 11/06 - Aménagements ou adaptations des sièges
The invention relates to an aircraft-seat device comprising: a mount unit (12a; 12b; 12c; 12d; 12e; 12f; 12g; 12h), which is provided for mounting on a cabin floor and has at least one cross member (22a, 24a; 22b, 24b; 22c, 24c; 22d, 24d; 22e, 24e; 22f, 24f; 22g, 24g; 22h, 24h); two seat structural elements (26a, 28a; 26b, 28b; 26c, 28c; 26d, 28d; 26e, 28e; 26f, 28f; 26g, 28g; 26h, 28h), each of which is arranged on one side of a seat region (30a; 30b; 30c; 30d; 30e; 30f; 30g; 30h) and each of which has a bearing (38a, 40a; 38b, 40b; 38c, 40c; 38d, 40d; 38e, 40e; 38f, 40f; 38g, 40g; 38h, 40h); a backrest (34a; 34b; 34c; 34d; 34e; 34f; 34g; 34h), which is attached via the bearings (38a, 40a; 38b, 40b; 38c, 40c; 38d, 40d; 38e, 40e; 38f, 40f; 38g, 40g; 38h, 40h) of the seat structural elements (26a, 28a; 26b, 28b; 26c, 28c; 26d, 28d; 26e, 28e; 26f, 28f; 26g, 28g; 26h, 28h); and a bearing device (42a; 42b; 42c; 42d; 42e; 42f; 42g; 42h), which is provided for supporting the backrest (34a; 34b; 34c; 34d; 34e; 34f; 34g; 34h) so as to be pivotable between an upright seat position and a comfort position, wherein the backrest (34a; 34b; 34c; 34d; 34e; 34f; 34g; 34h) comprises a pivotable backrest element (36a; 36b; 36c; 36d; 36e; 36f; 36g; 36h). According to the invention, the aircraft-seat device comprises at least one restoring module (56a; 56b; 56c; 56d; 56e; 56f; 56g; 56h), which is provided at least in order to provide a restoring force to restore the backrest (34a; 34b; 34c; 34d; 34e; 34f; 34g; 34h) from the comfort position into the upright seat position and for this purpose is arranged at least substantially in a region above the bearings (38a, 40a; 38b, 40b; 38c, 40c; 38d, 40d; 38e, 40e; 38f, 40f; 38g, 40g; 38h, 40h) of the seat structural elements (26a, 28a; 26b, 28b; 26c, 28c; 26d, 28d; 26e, 28e; 26f, 28f; 26g, 28g; 26h, 28h).
B64D 11/06 - Aménagements ou adaptations des sièges
B60N 2/22 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable le dossier étant réglable
The invention relates to a passenger seat device with a stand unit (12a; 12b; 12c; 12d; 12e; 12f), which is intended for mounting on a cabin floor, having a backrest (34a, 34b; 34c; 34d; 34e; 34f), and having a mounting device (42a; 42b; 42c; 42d; 42e; 42f) which is intended for mounting the backrest (34a, 34b; 34c; 34d; 34e; 34f) relative to the stand unit (12a; 12b; 12c; 12d; 12e; 12f) such that said backrest can pivot between an upright seat position and a comfort position, wherein the backrest (34a, 34b; 34c; 34d; 34e; 34f) comprises a pivotable backrest element (36a, 36b; 36c; 36d; 36e; 36f). According to the invention, the passenger seat device has at least one restoring module (56a; 56b; 56c; 56d; 56e; 56f) that is intended to provide a restoring force for restoring the backrest (34a, 34b; 34c; 34d; 34e; 34f) from the comfort position into the upright seat position, and comprises at least one leaf-spring element (58a; 58b; 58c; 58d; 58e; 58f) for this purpose.
B64D 11/06 - Aménagements ou adaptations des sièges
B60N 2/427 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules à des fins particulières ou pour des véhicules particuliers le siège étant construit pour protéger son occupant des effets des forces d'accélération anormales, p. ex. sièges anticollision ou sièges de sécurité le siège ou ses parties constitutives se déplaçant lors d'une collision
B60N 2/22 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable le dossier étant réglable
The invention relates to a passenger seat device comprising a stand unit (14a; 14b), a leg support module (20a; 20b) which is pivotally mounted on the stand unit (14a; 14b), a bearing module (29a; 29b) which is designed to adjust the leg support module (20a; 20b) between a stowed position and a maximally deflected position, and an actuator (42a; 42b) which is designed to exert an adjustment force onto the leg support module (20a; 20b). According to the invention, the passenger seat device has an overload locking module (44a; 44b) which is designed to mechanically lock the leg support module (20a; 20b) in the event of an overload.
The invention is based on an aircraft seat control unit for an aircraft seat (10), having a function circuit unit (14) that has at least one function circuit (16, 18, 20, 22) for controlling the aircraft seat (10), and having a communication circuit unit (24) that has at least one communication circuit (28) and is provided for communication with at least one external control unit (26). According to the invention, the communication circuit unit (24) is separated from the function circuit unit (14) at least in terms of software, and the function circuit unit (14) is provided to monitor the communication circuit unit (24).
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
B64D 11/06 - Aménagements ou adaptations des sièges
B60N 2/02 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable
The invention relates to a train seat layout with a first train seat module (30), which has one passenger seat (40), and with a second train seat module (32), which has one passenger seat (60), wherein the train seat modules (30, 32) are arranged adjacently in a seat longitudinal row (26) on one side of an aisle (22) in a passenger compartment (12), with a table unit (70), which is intended to be attached on the sidewall-side and is arranged between the first train seat module (30) and the second train seat module (32). According to the invention, the passenger seats (40, 60) of the train seat modules (30, 32) are each intended to be pivotable between a first seat position oriented in a first direction (76) and a second seat position oriented in a second direction (78), wherein the passenger seat (40) of the first train seat module (30) is, in its first seat position, directly facing the table unit (70) for use, and the passenger seat (60) of the second train seat module (32) is, in its second seat position, directly facing the table unit (70) for use.
B60N 2/04 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable le siège entier étant mobile
An aircraft seat module has an enclosure unit which at least partially delimits a flight passenger seating area, and has a door unit which at least in an operating state is at least configured to close a passage region to the flight passenger seating area, has a bearing device which is configured to support the door unit so as to be movable between an open position and a closed position in relation to the enclosure unit, and has a locking device which is configured to lock the door unit in the open position, wherein the locking device has at least one electrically and/or electronically actuatable actuator device, which is at least configured to be electrically and/or electronically actuated for an unlocking of the door unit.
E05B 81/08 - Serrures de véhicule actionnées par une force motrice caractérisées par le type d´actionneur utilisé électrique par électroaimants ou solénoïdes
B64D 11/06 - Aménagements ou adaptations des sièges
E05B 81/70 - Contrôle ou détection, p. ex. par des interrupteurs ou des détecteurs de la position du battant
E05B 81/18 - Serrures de véhicule actionnées par une force motrice caractérisées par la fonction ou les fins des éléments d’actionnement pour déplacer des pênes
E05B 81/28 - Éléments à mouvement linéaire en va-et-vient
E05C 1/08 - Dispositifs d'immobilisation avec pênes se déplaçant de façon rectiligne avec action d'une clenche
E05C 17/60 - Dispositifs pour le maintien des battants coulissants en position d'ouverture
An aircraft seat module having a flight passenger seating area has a door unit which in at least one operating state is configured at least to close a passage region to the flight passenger seating area, and has a locking device for the door unit, which is configured to lock the door unit in an open position, in particular a maximally open stowage position, and to this end comprises at least one actuator device which has at least two movably supported locking elements, which are in each case adjustable between a locking position and an unlocking position,
wherein that the locking device has a locking state indication unit which at least in the maximally open position of the door unit is configured to detect and indicate incomplete locking of at least one of the two locking elements.
E05B 41/00 - Serrures à indication visible de la position de verrouillage ou de déverrouillage
B64D 11/06 - Aménagements ou adaptations des sièges
E05B 81/08 - Serrures de véhicule actionnées par une force motrice caractérisées par le type d´actionneur utilisé électrique par électroaimants ou solénoïdes
E05B 81/18 - Serrures de véhicule actionnées par une force motrice caractérisées par la fonction ou les fins des éléments d’actionnement pour déplacer des pênes
E05B 81/28 - Éléments à mouvement linéaire en va-et-vient
E05B 81/70 - Contrôle ou détection, p. ex. par des interrupteurs ou des détecteurs de la position du battant
E05C 1/08 - Dispositifs d'immobilisation avec pênes se déplaçant de façon rectiligne avec action d'une clenche
E05C 17/60 - Dispositifs pour le maintien des battants coulissants en position d'ouverture
An aircraft seat arrangement including a plurality of aircraft seat devices which are arranged in an aircraft cabin section and are designed to be at least partially different from one another and each have an aircraft seat which is designed as a full-flat seat, wherein the aircraft seat devices in the aircraft cabin section differ in at least one comfort category, wherein the aircraft seat devices for the at least one comfort category each have a mutually different value which is caused by a different arrangement of the aircraft seats and by the at least partially different design of the aircraft seat devices.
Aircraft passenger seat device includes an aircraft seat row, comprising having a mounting unit, and three or more neighboring seat areas. In the two outer seat areas, an aircraft seat with a seat bottom and a backrest is mounted to the mounting unit. In the middle seat area a backrest base body is mounted to the mounting unit. In one or more operating states a detachable center console is detachably mounted to the mounting unit in the middle seat area forming a separation between the two outer seats. The backrest base body has one or more functional elements on its rear side provided for the use by a passenger sitting behind.
The invention is based on an aircraft-seat arrangement (10a; 10b; 10c) having a seat divider (12a; 12b; 12c), having an armrest (22a; 22b; 22c), which can be pivoted between a use position (26a; 26b; 26c) and a not-in-use position (28a; 28c) in relation to the seat divider (12a; 12b; 12c) and has a main armrest body (30a; 30b; 30c), and having an attachment module (40a; 40b; 40c), which is provided so as to mount the armrest (22a; 22b; 22c) pivotably in relation to the seat divider (12a; 12b; 12c), wherein, in a fully installed state (48a; 48b; 48c), the main armrest body (30a; 30b; 30c) is coupled to the seat divider (12a; 12b; 12c) via the attachment module (40a; 40b; 40c). It is proposed that the attachment module (40a; 40b; 40c) should be pivotably connected to the seat divider (12a; 12b; 12c) and, in an installation state (44a), in which the attachment module (40a; 40b; 40c) is connected to the seat divider (12a; 12b; 12c), should be provided for coupling to the main armrest body (30a; 30b; 30c), wherein, in the fully installed state (48a; 48b; 40c), the attachment module (40a; 40b; 40c) is accommodated at least substantially in an attachment space (42a; 42b; 42c) of the armrest (22a; 22b; 22c).
An aircraft seat device has a multi-part backrest frame unit comprising at least one first side frame element, at least one second side frame element, which is arranged on a side of the backrest frame unit that is opposite from the first side frame element, and at least one transverse frame element which is realized separately from the side frame elements and connects the side frame elements, wherein the transverse frame element is realized at least substantially plate-shaped.
The invention proposes an aircraft-seat assembly (10a-e) having a first aircraft-seat arrangement (20a-e) and having a second aircraft-seat arrangement (22a-e), which is arranged directly behind the first aircraft-seat arrangement (20a-e) and is designed to be at least substantially identical to the first aircraft-seat arrangement (20a-e), wherein the second aircraft-seat arrangement (22a-e) has a housing (32a-e), which forms a backrest wall (34a-e) at least in a sub-region of the housing (32a-e) of the second aircraft-seat arrangement (22a-e), wherein, in an aircraft-seat region (36a-e), the second aircraft-seat arrangement (22a-e) comprises a seat base (52a-e), which has a front edge (54a-e), wherein a main-extent axis of the front edge (54a-e) of the seat base is oriented at an angle of at least 5 degrees in relation to a transverse axis (26a) of the second aircraft-seat arrangement (22a-e), wherein a reclining direction (46a) of the aircraft-seat region (36 a-e) is oriented at an angle of at least 30 degrees in relation to a longitudinal axis (24a) of the second aircraft-seat arrangement (22a-e), wherein the reclining direction (46a) is directed away from an access region (48a-e) of the aircraft-seat region (36a-e).
The invention relates to a seat device (12a; 12b; 12c), in particular an aircraft seat device, said seat device comprising a backrest (20a; 20b; 20c) having: a base frame (24a; 24b; 24c) which comprises two lateral frame elements (26a, 28a; 26b, 28b; 26c, 28c); and a shell element (30a; 30b; 30c) which is connected to the lateral frame elements (26a, 28a; 26b, 28b; 26c, 28c) and at least part of which forms a backrest support surface (22a; 22b; 22c).
An aircraft seat module includes an enclosure unit which delimits a flight passenger seating region at least partially, and includes a door unit which at least closes a passage region to the flight passenger seating region in one or more operation states. The aircraft seat module further includes a bearing device which supports the door unit movably relative to the enclosure unit and has for this purpose a bearing module having a first bearing element and a second bearing element which are supported such that they are movable relative to each other.
The invention relates to an aircraft seat module which forms an aircraft seat region (26, 30), comprising an aircraft seat (42) which is designed to be installed at an angle ɑ of 30° to 80°, preferably 45° to 65°, in an aircraft cabin (12) and which has at least one base frame (50) and a kinematic unit (52); a housing unit (58) that comprises a first housing element (60) which at least party delimits the aircraft seat region (26) in the region of the aircraft seat (42) and a second housing element (62) which at least partly delimits the aircraft seat region (26) at least in the region in front of the aircraft seat (42); an ottoman (68) which provides a foot rest region (70); and a console unit (64) which forms at least one stowing and/or storage region (74) of the aircraft seat region (26). According to the invention, the aircraft seat (42) is combined into a separate 16-G module (86), and the second housing element (62), the ottoman (68), and the console unit (64) are combined into a separate 9G module (88), wherein the 16G module (86) and the 9G module (88) are designed to be secured to a cabin floor (32) separately from each other.
The invention relates to an aircraft seat assembly comprising a first aircraft seat module (24) which delimits an aircraft seat region (26), said aircraft seat module (24) having an aircraft seat (34) which is designed to be installed at an angle ɑ of more than 30° in the aircraft cabin (12), to be aligned away from a central aisle (20) and towards a window (50) of an aircraft cabin (12), and to form an at least substantially flat lying surface (42), wherein the aircraft seat module (24) has at least one housing unit (52) which at least partly delimits the aircraft seat region (26); and at least one additional aircraft seat module (28) which is arranged directly adjacently to the first aircraft seat module (24) and delimits another aircraft seat region (30). The other aircraft seat module (28) likewise has a housing unit (60) which at least partly delimits the aircraft seat region (30), and the housing unit (60) of the other aircraft seat module (28) has substantially the same design as the housing unit (52) of the first aircraft seat module (24) and separates the aircraft seat region (26) of the first aircraft seat module (24) from the aircraft seat region (30) of the second aircraft seat module (28).
In a passenger seating arrangement in an aircraft cabin, the passenger seating arrangement has exactly two rows of seat units and exactly one aisle. A first row of seat units and a second row of seat units are separated by the aisle. The rows of seat units and the aisle all extend in a longitudinal direction parallel to a longitudinal axis of the aircraft cabin. Each seat unit includes a seat, an upper shell and a lower shell, the lower shell forming a footwell. The seats are arranged in parallel to each other in a seating direction. An upper shell of a first seat unit and a lower shell of a second seat unit, which, viewed in the longitudinal direction, is arranged behind the first seat unit, partially overlap in a vertical direction.
An aircraft seat device with at least one shell element, with at least one table unit, with at least one support device that is configured to obliquely connect the at least one table unit to the shell element at least in a stowage position, the support device comprising at least one rotational bearing unit, which is configured for pivoting the table unit between the stowage position and at least one intermediate position that is situated substantially in a horizontal plane, the support device comprising at least one linear bearing unit, which is configured for traversing the table unit between the intermediate position and at least one completely deployed usage position that is close to a seat.
An assembly kit for an aircraft seat comprising at least one mounting unit, at least one backrest which is fixedly coupled with the mounting unit in a state when assembled and ready for flight, and at least one connection module, via which the backrest is in particular oriented rigidly in a position relative to the mounting unit in the assembled and ready-for-flight state, and the connection module comprises at least one adjusting element, by means of which the backrest is orientable respectively in at least two different backrest adjustment angles relative to the mounting unit without requiring new approval, and/or comprises at least two connection elements, by means of which the backrest can be fixedly mounted respectively in at least two different backrest adjustment angles relative to the mounting unit, the at least two connection elements being mountable without requiring new approval.
The invention relates to an aircraft seat device (10a; 10b; 10c; 10d; 10e; 10f; 10g; 10h; 10i) comprising at least one aircraft seat (12a; 12b; 12c; 12d; 12e; 12f; 12g; 12h; 12i) which has a backrest (14a; 14b; 14c; 14d; 14e; 14f; 14g; 14h; 14i) and forms an aircraft seat region (24a; 24b; 24c; 24d; 24e; 24f; 24g; 24h; 24i) that is delimited in at least one direction by the backrest (14a; 14b; 14c; 14d; 14e; 14f; 14g; 14h; 14i). According to the invention, the aircraft seat device (10a; 10b; 10c; 10d; 10e; 10f; 10g; 10h; 10i) has at least one infection protection separating unit (32a; 32b; 32c; 32d; 32e; 32f; 32g; 32h; 32i) which is arranged on the backrest (14a; 14b; 14c; 14d; 14e; 14f; 14g; 14h; 14i) of the at least one aircraft seat (12a; 12b; 12c; 12d; 12e; 12f; 12g; 12h; 12i) and/or on a headrest (18a; 18b; 18c; 18g; 18i) of the at least one aircraft seat (12a; 12b; 12c; 12d; 12e; 12f; 12g; 12h; 12i) and which is designed to separate the aircraft seat region (24a; 24b; 24c; 24d; 24e; 24f; 24g; 24h; 24i) from the surroundings (34a; 34b; 34c; 34d; 34e; 34f; 34g; 34h; 34i) of the aircraft seat region (24a; 24b; 24c; 24d; 24e; 24f; 24g; 24h; 24i), in particular from another aircraft seat region (52b; 52e; 52f; 52g; 52h) and/or an aircraft cabin passageway region (94d), at least in a head region (30a; 30b; 30c; 30d; 30e; 30f; 30g; 30h; 30i).
The invention is based on an aircraft seat module having a passenger seat region (10a; 10b), having a door unit (22a; 22b), which is at least provided, at least in one operating state, to close a passage region (18a; 18b) to the passenger seat region (10a; 10b), having a locking device (28a; 28b) for the door unit (22a; 22b), which is provided to lock the door unit (22a; 22b) in an open position, in particular a maximum open stowage position, and for this purpose comprises at least one actuator device (28a; 28b), which has at least two movably mounted locking elements (42a, 44a; 42b, 44b) which are each adjustable between a locking position and an unlocking position. It is proposed that the locking device (28a; 28b) has a locking state indication unit (74a; 74b) which is provided, at least in the maximum open position of the door unit (22a; 22b), to detect and display incomplete locking of at least one of the two locking elements (42a, 44a; 42b, 44b).
The invention relates to an aircraft seat module comprising an enclosure unit (14a; 14b; 14c) at least partially delimiting a passenger seating area (10a; 10b; 10c), and a door unit (22a; 22b; 22c) provided at least to close, at least in one operating state, a passage area (18a; 18b) to the passenger seating area (10a; 10b), comprising supporting means (24a; 24b; 24c) adapted to support the door unit (22a; 22b; 22c) movably between an open position and a closed position relative to the enclosure unit (14a; 14b), and locking means (28a; 28b; 28c) adapted to lock the door unit (22a; 22b; 22c) in the open position. According to the invention, the locking device (28a; 28b; 28c) comprises at least one electrically and/or electronically controllable actuator device (56a; 56b; 56c), which is at least provided to be electrically and/or electronically controlled for unlocking the door unit (22a; 22b; 22c).
The invention relates to an aircraft seat assembly (14a; 14b; 14c; 14d) comprising at least one aircraft seat device (46a; 46b; 46c; 46d) and at least one additional aircraft seat device (48a; 48b; 48c; 48d) which are arranged at least partly next to one another in at least one common column of seats(36a; 36b; 36c; 36d) and each of which can be adjusted between a sitting position and a lying position. According to the invention, the lying direction (64a; 64b; 64c; 64d) of the at least one aircraft seat device (46a; 46b; 46c; 46d) is oriented in the opposite direction to another lying direction (96a; 96b; 96c; 96d) of the at least one other aircraft seat device (48a; 48b; 48c; 48d).
An airplane seat device includes at least one functional unit that is configured at least for a locking, a controlling and/or a movement of at least one airplane seat element, wherein the functional unit includes at least one actuatable shape-memory element.
The invention relates to an aircraft seat assembly (14a-g) comprising multiple aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g) arranged in an aircraft cabin section (26a-g), which are designed to be at least partially different from one another and each have an aircraft seat (120a-g, 220a-g, 320a-g, 420a-g, 520a-g, 620a-g, 720a-g, 820a-g, 1200f, 3200f, 4200g, 5200f, 7200f, 8200g), which is designed as a full-flat seat. According to the invention, the aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g) in the aircraft cabin section (26a-g) differ in terms of at least one comfort category, wherein the aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000t, 5000'f, 7000f, 7000'f, 8000g, 8000'g) each have a different value from one another for the at least one comfort category, resulting from a different arrangement of the aircraft seats (120a-g, 220a-g, 320a-g, 420a-g, 520a-g, 620a-g, 720a-g, 820a-g, 1200f, 3200f, 4200g, 5200f, 7200f, 8200g) and from the at least partially different formation of the aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g).
An aircraft seat fixation device for a fixation at least of a portion of an aircraft seat on at least one fixation rail that is fixated on an aircraft structure comprises a seat base structure which is configured such that at least the aircraft seat is mounted thereon at least partially, further comprises at least one seat foot which is connected to the seat base structure, and comprises at least one fitting element which is connected to the seat foot and is at least configured to be coupled with the fixation rail,
wherein the aircraft seat fixation device comprises at least one compensation unit, which is arranged on the seat base structure, the seat foot and/or the fitting element and which is configured to permit at least one compensation movement of the seat base structure at least in an overload case.
The invention relates to an aircraft seat device (46a-c) having a multi-part backrest frame unit (10a-c), the aircraft seat device comprising at least one first side frame element (12a-c), at least one second side frame element (14a; 14b), which is arranged on a side of the backrest frame unit (10a-c) opposite from the first side frame element (12a-c), and at least one transverse frame element (16a; 16'a; 16b; 16c), which is separate from the side frame elements (12a-c, 14a-c) and connects the side frame elements (12a-c, 14a-c). It is proposed that the transverse frame element (16a; 16'a; 16b; 16c) is at least substantially plate-shaped.
The invention relates to an aircraft seat apparatus having a backrest (12a; 12b; 12c; 12d) and a functional unit (16a; 1b; 16c; 16d), such as, in particular, a screen unit or a literature pocket, integrated in an upper region (18a; 18b; 18c; 18d) of the backrest (12a; 12b; 12c; 12d), and having a holding apparatus (30a; 30b; 30c; 30d) which is provided such that at least one object can be arranged in the upper region (18a; 18b; 18c; 18d) of the backrest (12a; 12b; 12c; 12d). According to the invention, the holding apparatus (30a; 30b; 30c; 30d) is arranged at least substantially above the integrated functional unit (16a; 1b; 16c; 16d).
A life vest device, for a fixation on one or more aircraft seats, with a life vest unit, which is embodied as a lift vest with a packaging unit for a sealed accommodation of the life vest unit and with an opening unit for an opening of the packaging unit, which features one or more pull straps. The opening unit is functionally connected with the life vest unit and the packaging unit comprises one or more fixation units for a fixation on an aircraft seat. For a retrieval of the life vest unit from the packaging unit, the opening unit is connected in a tear-proof manner with the life vest unit. The pull strap and the life vest are embodied integrally with each other.
The invention relates to a life vest container device, in particular aircraft seat life vest container device, for a life vest unit, with a life vest container comprising an accommodation unit that has an accommodation space as well as an access opening to the accommodation space, and with a monitoring device.
It is proposed that the monitoring device is at least configured to capture a change of at least one characteristic via at least one electric and/or electronic signal.
G08B 13/14 - Déclenchement mécanique par l'enlèvement ou les essais de déplacement d'articles portatifs
B64D 11/06 - Aménagements ou adaptations des sièges
G08B 29/12 - Vérification intermittente des systèmes de signalisation ou d'alarme
G08B 7/06 - Systèmes de signalisation selon plus d'un des groupes Systèmes d'appel de personnes selon plus d'un des groupes utilisant une transmission électrique
B63C 9/08 - Bouées de sauvetage, p. ex. en forme de couronneCeintures, gilets, vêtements ou équipements analogues pour le sauvetage
B64D 45/00 - Indicateurs ou dispositifs de protection d'aéronefs, non prévus ailleurs
B64F 5/60 - Test ou inspection des composants ou des systèmes d'aéronefs
The invention is based on an aircraft-seat module having an enclosure unit, which at least partially delimits a passenger-seat region, and having a door unit, which is provided at least so that, at least in an operating state, it closes a through-passage region to the aircraft-seat module having an enclosure unit (14a; 14b; 14c), which at least partially delimits a passenger-seat region (10a; 10b), and having a door unit (22a; 22b; 22c), which is provided at least so that, at least in an operating state, it closes a through-passage region (18a; 18b) to the passenger-seat region (10a; 10b), and having a bearing device (24a; 24b; 24c), which is provided so that it supports the door unit (22a; 22b; 22c) in a movable manner in relation to the enclosure unit (14a; 14b; 14c) and, for this purpose, has a bearing module (26a, 28a; 26b, 26c), which has a first bearing element (30a; 30b, 30'b; 30c) and a second bearing element (34a; 34b, 34'b; 34c), which are mounted in a movable manner in relation to one another. It is proposed that the bearing module (26a, 28a; 26b, 26c) should have a third bearing element (26a, 28a; 26b, 26c), which is provided so that, in an operating state other than a normal operating state, it supports the second bearing element (34a; 34b, 34'b; 34c) in a movable manner and/or the bearing module (28e) has an attachment element (104e) for the attachment of the second bearing element (68e), wherein the second bearing element (68e) is provided so that, in a normal operating state, it is coupled in a fixed manner to the attachment element (104e) and, in an operating state other than a normal operating state, it is uncoupled from the attachment element (104e).
The invention relates to an aircraft cabin device comprising at least one first aircraft seat row (12a; 12b; 12c; 12d; 12e; 12f; 12g; 12h), which comprises at least two aircraft seats (16a, 18a, 20a; 16b; 16c; 16d;16e, 18e; 16g, 18g, 20g; 16h) arranged next to one another, and comprising at least one second aircraft seat row (26a; 26b; 26c; 26d; 26e; 26f; 26g; 26h), which is arranged directly in front of the first aircraft seat row (12a; 12b; 12c; 12d; 12e; 12f; 12g; 12h) and which comprises at least one aircraft seat (28a, 30a, 32a; 28b, 30b; 28c, 30c; 28d; 28e; 28f, 30f, 28g, 30g, 32g, 74g; 30h), wherein the aircraft seats (16a, 18a, 20a, 28a, 30a, 32a; 16b, 28b, 30b; 16c, 28c, 30c; 16d, 28d;16e, 18e, 28e; 16g, 18g, 20g, 20g, 72g, 28g, 30g, 32g, 74g; 16h, 30h) of the first and second aircraft seat row (12a, 26a; 12b, 26b; 12c, 26c; 12d, 26d; 12e, 26e; 12f, 26f; 12g, 26g; 12h, 26h) have substantially the same seat direction. According to the invention, at least one sub-region (44a; 44b; 44c; 44d; 44e; 44f; 44g; 44h) of the front second aircraft seat row (26a; 26b; 26c; 26d; 26e; 26f; 26g; 26h) is designed to form a common use area (46a; 26b; 46c; 46d; 46e; 46f; 46g; 46h) together with the first aircraft seat (16a; 16b; 16c; 16d; 16e; 16f; 16g; 16h) of the rear first aircraft seat row (12a; 12b; 12c; 12d; 12e; 12f; 12g; 12h) arranged directly behind said sub-region.
The invention relates to an aircraft cabin device comprising at least one first aircraft seat row (12a; 12b; 12c; 12d), which has at least two aircraft seats (16a, 18a, 20a; 16b, 18b, 20b; 16c, 18c, 20c; 16d, 18d, 20d) that are aligned in the same seat direction, and comprising a separating wall (26a; 26b; 26c; 26d), which is arranged directly in front of the first aircraft seat row (12a; 12b; 12c; 12d). The aircraft cabin device has at least one common area (28a; 28b; 28c; 28d), which is at least partly arranged on the separating wall (26a; 26b; 26c; 26d) and has at least one seat element (30a; 30b; 30c; 30d) that is designed to form a seating area for at least one passenger.
The invention relates to a seat system, in particular an aircraft seat system, comprising at least one seat device (14, 16) having at least one seat (24, 26, 28, 38) and a system for additionally booking and/or removing a booking (42), wherein the system for additionally booking and/or removing a booking of a service (42) is at least partially provided to additionally book and/or remove the booking of at least one individual service and/or of at least one comfort property.
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
B64D 11/06 - Aménagements ou adaptations des sièges
G06Q 10/06 - Ressources, gestion de tâches, des ressources humaines ou de projetsPlanification d’entreprise ou d’organisationModélisation d’entreprise ou d’organisation
A seat device, particularly aircraft seat device, includes at least one head-support module, which device has a central cushion unit and at least one lateral cushion unit, wherein the lateral cushion unit is supported movably relative to the central cushion unit.
According to the invention, an aircraft seat device is provided, comprising at least one housing element (12a; 12b), at least one table unit (24a; 24b), and at least one support device (34a; 34b) which is designed to attach the at least one table unit (24a; 24b) to the housing element (12a; 12b) diagonally at least in a stowed position, wherein the support device (34a; 34b) has at least one rotational support unit (54a; 54b), which is designed to pivot the table unit (24a; 24b) between the stowed position and at least one intermediate position which lies substantially on a horizontal plane. The support device (34a; 34b) comprises at least one linear support unit (36a; 36b) which is designed to linearly move the table unit (24a; 24b) between the intermediate position and at least one completely extended operational position which is close to the seat.
The invention relates to an assembly kit for an aircraft seat (24a), having at least one stand unit (12a; 12b), at least one backrest (14a; 14b) which is fixed to the stand unit (12a; 12b) when in an assembled and ready-to-fly state, and at least one connection module (28a, 28b) by means of which the backrest (14a; 14b) is oriented, in particular rigidly, in a position relative to the stand unit (12a; 12b) when in the assembled and ready-to-fly state. According to the invention, the connection module (28a; 28b) has at least one adjustment element (30a; 30b), by means of which the backrest (14a; 14b) can be oriented at at least two different backrest angles relative to the stand unit (12a; 12b) without new approval, and/or at least two connection elements (34a, 36a, 38a; 34b; 34c, 36c; 34d, 36d, 38d; 34e, 36e, 38e), by means of which the backrest (14a; 14b) can be mounted fixedly relative to the stand unit at at least two different backrest angles (12a; 12b), wherein the at least two connection elements (34a, 36a, 38a; 34b; 34c, 36c; 34d, 36d, 38d; 34e, 36e, 38e) can be installed without new approval.
A table device for a seat, in particular for an aircraft seat, includes a table unit which is configured for being adjustable at least between a use position and a stowage position, and has at least one locking module which has at least one attachment unit which is configured for being at least in part fixedly connected to a seat component, wherein the table unit at least in the stowage position is lockable to the attachment unit. The locking module has at least two force-fit and/or form-fit elements, by means of which the table unit in a locked state is coupled in a form-fitting and/or force-fitting manner to the attachment unit.
An aircraft seat device for an aircraft seat includes at least one mounting unit, having at least one seat bottom which is coupled with the mounting unit and is configured to implement a seating region and to this end has at least one main unit and at least one sub-unit that in relation to the mounting unit is implemented so as to be adjustable between a stowage position and a use position. The at least one adjustable sub-unit is configured for enlarging the seating region in at least one position, and having at least one actuation mechanism by means of which the adjustable sub-unit of the seat bottom is adjustable between its stowage position and its use position.
B64D 11/06 - Aménagements ou adaptations des sièges
B60N 2/02 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable
The invention relates to an airplane seat device, comprising at least one stand unit (12a; 12b; 12c), at least one backrest (24a; 24b; 24c; 24d) which is coupled to the stand unit (12a; 12b; 12c), at least one seat base (28a; 28b; 28c; 28d) which is coupled to the stand unit (12a; 12b; 12c) and/or the backrest (24a; 24b; 24c; 24d), and at least one kinematic module (34a; 34b), which is designed to adjust the backrest (24a; 24b; 24c; 24d) and/or the seat base (28a; 28b; 28c; 28d) between at least one normal substantially upright seating position and a comfort position. The kinematic module (34a; 34b) is designed to adjust the backrest (24a; 24b; 24c; 24d) and/or the seat base (28a; 28b; 28c; 28d) into an additional special upright position, which differs from the upright seating position and in which the backrest (24a; 24b; 24c; 24d) is set forwards at least in a sub-region and/or the seat base (28a; 28b; 28c; 28d) is at least pivoted, in at least one operating state.
B64D 11/06 - Aménagements ou adaptations des sièges
B60N 2/22 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable le dossier étant réglable
B60N 2/30 - Sièges indémontables susceptibles d'être gardés dans une position de non-utilisation, p. ex. strapontins
B60N 2/02 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable
The invention is based on an aircraft seat fastening device for fastening at least part of an aircraft seat to at least one fastening rail (36a, 38a) fastened to a vehicle structure (12a; 12b; 12c; 12d; 12e), with a seat base structure (14a; 14b; 14c; 14d; 14e) which is provided for at least the aircraft seat to be at least partially mounted thereon, with at least one seat foot (28a, 30a; 28b; 28c; 28d; 28e) which is attached to the seat base structure (14a; 14b; 14c; 14d; 14e), and with at least one fitting element (40a, 42a; 40b; 40c; 40d; 40e) which is attached to the seat foot (28a, 30a; 28b; 28c; 28d; 28e) and is provided at least for coupling to the fastening rail (36a, 38a). It is proposed that the aircraft seat fastening device has at least one compensating unit (44a, 46a; 44b; 44c; 44d; 44e) which is arranged on the seat base structure (14a), the seat foot (28a, 30a; 28b; 28c; 28d; 28e) and/or the fitting element (40a, 42a; 40b; 40c; 40d; 40e) and is provided for permitting at least one compensating movement of the seat base structure (14a; 14b; 14c; 14d; 14e) at least in the event of an overload.
The invention relates to an airplane seat device comprising at least one functional unit (20a; 20b; 20c; 20d; 20e; 20g; 20h) which is provided at least for locking, controlling, and/or moving at least one airplane seat element (14a; 14b; 14c; 14e; 14g; 14h). The functional unit (20a; 20b; 20c; 20d; 20e; 20g; 20h) comprises at least one actuatable shape-memory element (22a, 24a, 26a, 28a; 22b, 24b, 26b; 22c; 22d; 22e; 22g; 22h, 24h).
B64D 11/06 - Aménagements ou adaptations des sièges
B60N 2/02 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable
The invention relates to an aircraft seat device system having more than two aircraft seats (10, 12, 14, 16) which are arranged one behind the other at least in a line (30), and having at least one server rack (18, 20), which is formed separately from the aircraft seats (10, 12, 14, 16) and which is provided at least for operating two aircraft seats arranged in the line (30). According to the invention, the server rack (18, 20) is arranged in a start region (26) and/or in an end region (28) of the line (30).
The invention relates to an aircraft seat fastening device for fastening at least a part of an aircraft seat to at least one fastening rail (18a, 20a) fastened to an aircraft structure, comprising at least one fitting element (28a, 28'a; 28b) which is provided for coupling to the at least one fastening rail (18a, 20a), and a limiter element (42a, 42'a; 42b) which is formed at least partially separately from the fitting element (28a, 28'a; 28b) and is provided for securing the installed fitting element (28a, 28'a; 28b) in the fastening rail (18a, 20a). According to the invention, the aircraft seat fastening device has at least one retaining element (58a, 58'a; 58b) which couples the fitting element (28a, 28'a; 28b) to the limiter element (42a, 42'a; 42b).
B60N 2/015 - Fixation des sièges directement aux châssis des véhicules
B64D 11/06 - Aménagements ou adaptations des sièges
B60N 2/427 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules à des fins particulières ou pour des véhicules particuliers le siège étant construit pour protéger son occupant des effets des forces d'accélération anormales, p. ex. sièges anticollision ou sièges de sécurité le siège ou ses parties constitutives se déplaçant lors d'une collision
The invention is based on an aircraft seat device with at least one backrest (10a; 10b), with at least one backrest bridge (16a; 16b), which at least substantially spans the backrest (10a; 10b) at least in a transverse direction, and with at least one flap element (14a; 14b) which is arranged so as to be pivotable in the region of the backrest bridge (16a; 16b). It is proposed that the at least one flap element (14a; 14b), at least in a closed state, covers at least one backrest region (46a; 46b) above the backrest bridge (16a; 16b).
The invention relates to an aircraft seat device comprising a backrest (12a; 12b; 12d) and at least one structural component (20a; 20b, 36b, 46b; 20c; 20d) coupled at least to the backrest (12a; 12b; 12d) and/or mounted outside a primary load path. According to the invention, at least one structural component (20a; 20b, 36b, 46b; 20c; 20d) is formed at least partially from a magnesium material.
An aircraft seat device with at least one support beam, which is configured to realize at least part of a mounting unit of an aircraft seat. In at least one partial region, viewed in a circumferential direction of the support beam, the at least one support beam has a changing wall thickness.
The invention relates to an aircraft seat device having at least one safety device (46a; 46b) which is provided for restraining a passenger (50a) in an aircraft seat (10a; 10b) and comprises at least one multi-point restraining unit (54a).
The invention relates to an aircraft seat device having at least one seat component (12a; 12b), at least one pocket (16a; 16b) coupled to the seat component (12a; 12b), said pocket comprising at least one spring unit (32a; 32b) which is intended to provide a closing force of the pocket (16a; 16b). It is proposed that the spring unit (32a; 32b) has a multi-part design.
The invention relates to a crash test method for aircraft seats, in which method a test sled (12a; 12b; 12c) is accelerated in order to simulate intense acceleration on aircraft seats and on passengers sitting on aircraft seats. According to the invention, at least two differently oriented target seats (16a, 18a, 20a, 22a; 16b, 18b, 20b; 16c, 18c, 20c) are arranged on the test sled (12a; 12b; 12c).
The invention relates to an aircraft seat device comprising at least one back rest (12a), at least one seat component (14a) coupled to the back rest (12a), and a back rest impact protection device (20a; 20b), which is provided for at least partially reducing impact forces on the back rest (12a) at least in the event of a crash, by partially uncoupling the back rest (12a) from the seat component (14a), and which also comprises at least one holding unit (42a, 44a; 42b) that locks the back rest impact protection device (20a; 20b) in a normal state of operation. According to the invention, the holding unit (42a, 44a; 42b) is designed to be elastically deformable in order to release the protection device when the holding unit (42a, 44a; 42b) is activated.
B64D 11/06 - Aménagements ou adaptations des sièges
B60N 2/42 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules à des fins particulières ou pour des véhicules particuliers le siège étant construit pour protéger son occupant des effets des forces d'accélération anormales, p. ex. sièges anticollision ou sièges de sécurité
B60N 2/427 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules à des fins particulières ou pour des véhicules particuliers le siège étant construit pour protéger son occupant des effets des forces d'accélération anormales, p. ex. sièges anticollision ou sièges de sécurité le siège ou ses parties constitutives se déplaçant lors d'une collision
The invention is based on a table device for a seat (10a; 10b; 10c; 10d), in particular for an aircraft seat, having a table unit (14a; 14b; 14c; 14d) which is intended to be adjustable at least between a use position and a stowed position, and having at least one locking module (20a; 20b; 20c; 20d) which has at least one attachment unit (28a; 28b; 28c; 28d) which is intended to be at least partially firmly connected to a seat component (12a; 12b; 12c; 12d), wherein, at least in the stowed position, the table unit (14a; 14b; 14c; 14d) can be locked on the attachment unit (28a; 28b; 28c; 28d). It is proposed that the locking module (20a; 20b; 20c; 20d) has at least two force-fitting and/or form-fitting elements (34a, 36a, 38a, 40a; 34b, 36b, 38b, 40b; 34c, 36c, 38c, 40c; 34d, 36d, 38d, 40d) by means of which the table unit (14a; 14b; 14c; 14d), in a locked state, is coupled to the attachment unit (28a; 28b; 28c; 28d) in a form-fitting and/or force-fitting manner.
An aircraft seat device includes at least one seat bottom unit, a mounting unit, and at least one carrier element. The at least one seat bottom unit at least partly implements a seat surface. The at least one carrier element couples the seat bottom unit with the mounting unit and transfers force from the seat bottom unit to the mounting unit.
A transport seat system, in particular aircraft seat system, includes at least one first seat, with at least one mounting module that is configured, for the purpose of mounting the seat, to be connected on a guide rail, and with at least one second seat, which is arranged behind the first seat with at least one mounting module that is configured, for the purpose of mounting the seat, to be connected on the same guide rail, the two seats being configured, for the purpose of implementing a usage position and a stowage position of at least one of the seats, to be displaced on the guide rail relative to one another, wherein
at least one mounting module of at least one of the seats includes a seat foot unit, which is movably supported relative at least to a portion of the mounting module.
B64D 11/06 - Aménagements ou adaptations des sièges
B60N 2/30 - Sièges indémontables susceptibles d'être gardés dans une position de non-utilisation, p. ex. strapontins
B60N 2/12 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable le siège entier étant mobile coulissant et basculant
An airplane seat device with at least one airplane seat is at least configured to be adjusted between a use position and a stowage position. In the stowage position, the airplane seat has a maximum height which is equal to or less than a maximum height in the use position.
An airplane seat device has a seat base module, comprising at least one main body which is at least substantially implemented from a rigid foam, at least one comfort element disposed on an upper side of the main body, at least one accommodating region for attaching to a tubular support, and at least one fastening element for attaching to the tubular support, wherein the main body has at least two coupling regions, via which the at least one fastening element can be selectively attached to the main body.
The invention is based on an aircraft seat device with at least two aircraft seats (12a, 14a, 16a) arranged next to one another and at least one armrest (28a, 30a; 28b; 28c; 28d; 28e; 28f; 28g; 28h, 28i) arranged between the two aircraft seats, wherein the armrest (28a, 30a; 28b; 28c; 28d; 28e; 28f; 28g; 28h, 28i) is movable between a stowage position and a use position. It is proposed that at least one separating element (38a, 40a; 38b; 38c; 38d; 38e; 38f; 38g; 38h, 38i) which is arranged on a lower side of the armrest (28a, 30a; 28b; 28c; 28d; 28e; 28f; 28g; 28h, 28i) and, in at least one stowage position of the armrest (28a, 30a; 28b; 28c; 28d; 28e; 28f; 28g; 28h, 28i), forms a supporting and/or private sphere element separates the seat regions of the two aircraft seats (12a, 14a, 16a) from each other.
A seating device comprises a seat bottom unit, in particular an aircraft seat bottom unit, having an accommodating region for receiving a module, in particular a lifejacket module, with at least one upper wall element which forms at least a support surface for a comfort element.
The invention relates to an airplane seat device comprising at least one stand unit (12a), a seat base (38a) which is connected to the stand unit (12a) and can be adjusted relative to the stand unit (12a) between a sitting position and at least one comfort position, a backrest (30a) which can be pivoted between a sitting position and a comfort position, and at least one lower backrest element (64a) which is arranged in a lower region of the backrest (30a) and can be pivoted at least relative to the backrest (30a) at least between a sitting position and at least one comfort position.
The invention relates to an aircraft seat device for an aircraft seat (10a; 10b; 10c; 10e), comprising at least one stand unit (12a; 12b; 12c: 12e), at least one seat base (30a; 30b; 30c: 30e) coupled to the stand unit (12a; 12b; 12c; 12e) and provided for forming a seating region (32a; 32b; 32c; 32e), as well as at least one main unit (34a; 34b; 34c; 34e) and at least one sub-unit (42a; 42b; 42c; 42d; 42e) designed such that it can be adjusted relative to the stand unit (12a; 12b; 12c; 12e) between a stowed position and a use position, wherein the at least one adjustable sub-unit (42a; 42b; 42c; 42d; 42e) is provided for enlarging the seating region (32a; 32b; 32c; 32e) in at least one position, as well as comprising at least one actuation mechanism (68a; 68b; 68c; 68e) by means of which the adjustable sub-unit (42a; 42b; 42c; 42d; 42e) of the seat base (30a; 30b; 30c; 30e) can be adjusted between the stowed position and the use position thereof.
B64D 11/06 - Aménagements ou adaptations des sièges
B60N 2/02 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable
The invention proceeds from a seat device, particularly an aircraft seat device, comprising at least one headrest module (18a; 18b; 18c; 18d) with a central cushion unit (20a; 20b; 20c; 20d) and at least one lateral cushion unit (32a; 32b; 32c; 32d). According to the invention, the lateral cushion unit (32a; 32b; 32c; 32d) is mounted such that it can move relative to the central cushion unit (20a; 20b; 20c; 20d).
An aircraft device includes at least one control and/or regulation unit which is configured for controlling an aircraft passenger seat unit, and of a PED in which at least one operating program is stored, wherein the control and/or regulation unit is configured to receive control signals from the PED for controlling the aircraft passenger seat unit.
B64D 11/06 - Aménagements ou adaptations des sièges
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
H04N 21/4363 - Adaptation du flux vidéo à un réseau local spécifique, p. ex. un réseau Bluetooth®
H04N 21/214 - Plate-forme spécialisée de serveur, p. ex. serveur situé dans un avion, un hôtel ou un hôpital
H04N 21/436 - Interfaçage d'un réseau de distribution local, p. ex. communication avec un autre STB ou à l'intérieur de la maison
H04N 21/41 - Structure de clientStructure de périphérique de client
B60N 2/02 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable
H04N 21/414 - Plate-formes spécialisées de client, p. ex. récepteur au sein d'une voiture ou intégré dans un appareil mobile
An aircraft seat device has a table module and a PED holder configured for supporting a PED in an operable position on the table module, wherein the PED holder comprises at least one holding element which is pivotally connected to the table module, wherein
the PED holder comprises a pivot bearing unit, which is configured for pivoting the holding element by more than 180 degrees.
A seating device, in particular a flight passenger seating device, includes at least one seat bottom unit and with a backrest unit that is connected to the seat bottom unit, wherein at least the backrest unit is positionable in a comfort position and in a further sitting position.
The comfort position is implemented as a base position that is optimized for a passenger comfort.
B60N 2/22 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable le dossier étant réglable
B60N 2/809 - Appuis-tête mobiles ou réglables coulissant verticalement
A flight passenger seating device with a flight passenger seat has at least one seat bottom and at least one leg support module comprising a leg support element that is embodied at least partly movably with respect to the seat bottom, wherein
the leg support module comprises at least two pivot bearing units and a linear bearing unit, by means of which the leg support element is supported movably with respect to the seat bottom.
A headrest device for a seat, in particular for an airplane seat, with a headrest implementing at least one head support zone.
The headrest device comprises at least one fixation module with at least one fixation means, which is configured to arrange at least one personal item in the head support zone.
The invention relates to an aircraft seat device having a supporting module (24a; 24b; 24c; 24d; 24e) that is designed as a headrest, a lumbar support, or a seat bottom, and which comprises at least one elastically deformable supporting element (26a; 26b; 26c; 26d; 26e). According to the invention, the elastically deformable supporting element (26a; 26b; 26c; 26d; 26e) is provided for the purpose of performing a bending-wave-like compensating movement in the event a user force is exerted.
The invention relates to a life vest bag, in particular a passenger seat life vest bag, comprising at least one receiving unit (10a; 10b; 10c: 10d; 10e; 10f; 10g; 10h; 10i; 10j; 10k) having at least one receiving space (12a; 12b; 12c; 12d; 12e; 12f; 12g; 12h; 12i; 12j; 12k) for at least one life vest (14a) and at least one access opening (16a; 16b; 16c; 16d; 16e; 16f; 16g; 16h; 16i; 16j; 16k) to the receiving space (12a; 12b; 12c; 12d; 12e; 12f; 12g; 12h; 12i; 12j; 12k), and comprising at least one closure unit (18a; 18b; 18c; 18d; 18e; 18f; 18g; 18h; 18i; 18j; 18k) which closes the access opening (16a; 16b; 16c; 16d; 16e; 16f; 16g; 16h; 16i; 16j; 16k) at least when properly closed.
The invention relates to a tray table device, in particular a passenger seat tray table device, with at least one table unit, and with at least one cup holder unit which is provided in at least one position of use to at least partly hold at least one drinking vessel. The cup holder unit is movably mounted to the table unit.
The invention relates to an aircraft seat device having at least one supporting tube (20a, 22a; 20b; 20c; 20d; 20e; 20f; 20g; 20h; 20i) provided to form at least one part of an elevating unit (12a; 12b; 12c; 12d; 12e; 12f; 12g; 12h; 12i) of an aircraft seat. According to the invention, the at least one supporting tube (20a, 22a; 20b; 20c; 20d; 20e; 20f; 20g; 20h; 20i) has a varying wall thickness (26a, 34a; 26b; 26c; 26d; 26d; 26i) in at least a partial region, viewed in the circumferential direction of the supporting tube (20a, 22a; 20b; 20c; 20d; 20e; 20f; 20g; 20h; 20i).
The invention relates to a transport seat system, in particular an aircraft seat system, with at least one first seat (10a; 10b; 10c) comprising at least one support module (28a, 30a) which is provided for supporting the seat (10a; 10b; 10c) in a transport means for the purpose of being connected to a guide rail (22a, 24a; 22b; 22c), and with at least one second seat (12a; 12b; 12c) arranged behind the first seat (10a; 10b; 10c) comprising at least one support module (68a, 70a; 68b; 68c) which is provided for supporting the seat (12a; 12b; 12c) in the transport means for the purpose of being connected to the same guide rail (22a, 24a; 22b; 22c), wherein the two seats (10a, 12a; 10b, 12b; 10c, 12c) are provided to form a use position and a stowed position of at least one of the seats (12a; 12b; 12c) for the purpose of being moved relative to one another on the guide rail (22a, 24a; 22b; 22c). According to the invention, at least one support module (68a, 70a; 68b; 68c) of at least one of the seats (12a; 12b; 12c) has a seat base unit (80a; 80b; 82c) which is mounted to be moveable relative to at least one part of the support module (68a, 70a; 68b; 68c).
B64D 11/06 - Aménagements ou adaptations des sièges
B60N 2/12 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable le siège entier étant mobile coulissant et basculant
The invention proposes an aircraft seat device with at least one seat base unit (28a; 28b; 28c; 28d; 28e) which forms at least in part a seat surface (30a; 30b; 30c), with a mounting unit (14a; 14b; 14c; 14e) which is intended to be mounted on a mounting plane, and with at least one support element (52a, 54a, 56a, 58a; 52b, 54b; 52c, 54c; 52d, 54d; 52e) which extends at least over a large part of a seat depth of the seat surface (30a; 30b; 30c) and is intended to connect the seat base unit (28a; 28b; 28c; 28d; 28e) to the mounting unit (14a; 14b; 14c; 14e).
B64D 11/06 - Aménagements ou adaptations des sièges
B60N 2/10 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable le siège entier étant mobile basculant
The invention relates to a transport seat device, in particular an aircraft seat device, comprising at least one backrest unit (18a; 18b; 18c; 18d; 8e; 18f) having at least one supporting shell (20a; 20b; 20c; 20d; 20e; 20f) formed at least substantially from a fibre composite material, and comprising an armrest device (26a; 26b; 26c; 26d; 26e; 26f) having at least one armrest (28a, 28b; 28b; 28c; 28d, 30d; 28e, 30e; 28f, 30f) connected to the supporting shell (20; 20b; 20c; 20d; 20e; 20f).
An airplane seat device having at least one backrest, at least one seat component coupled to the backrest and a backrest impact safety device which, by partially decoupling the backrest from the seat component, is provided to at least partly reduce impact forces on the backrest at least in the event of crash. The backrest impact safety device is provided to decouple the backrest from the seat component before the impact forces takes effect.
B64D 11/06 - Aménagements ou adaptations des sièges
B60N 2/427 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules à des fins particulières ou pour des véhicules particuliers le siège étant construit pour protéger son occupant des effets des forces d'accélération anormales, p. ex. sièges anticollision ou sièges de sécurité le siège ou ses parties constitutives se déplaçant lors d'une collision
An aircraft seat device includes at least one backrest, at least one seat component coupled to the backrest, and a backrest impact safety device, which is designed to rigidly connect the backrest and the seat component in a locking position in at least one normal operating state and which is designed to at least partially reduce impact forces on the backrest at least in the event of crash by at least partially decoupling the backrest from the seat component in at least one further operating state. The backrest is designed to be locked in a locking position again after the partial decoupling.
B64D 11/06 - Aménagements ou adaptations des sièges
B60N 2/427 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules à des fins particulières ou pour des véhicules particuliers le siège étant construit pour protéger son occupant des effets des forces d'accélération anormales, p. ex. sièges anticollision ou sièges de sécurité le siège ou ses parties constitutives se déplaçant lors d'une collision
The invention proceeds from a seating device having a seat base unit (18), in particular an aircraft seat base unit. According to the invention, the seat base unit (18) has a receiving region (32) for receiving a module, in particular a life jacket module (34), said module having at least one upper wall element (38) that forms at least one support surface for a comfort element (28).
An aircraft seat system has at least one first aircraft seat region, which includes a first aircraft seat, and at least one second aircraft seat region, which is arranged behind the first aircraft seat region and includes a second aircraft seat, wherein, in a mounted state, the aircraft seat of the second aircraft seat region is arranged, at least in a lying position, at least partially overlapping beneath the first aircraft seat region.
The invention relates to an airplane seat device with a seat base module (18) that has at least one main part (22), which is at least substantially made of a hard foam, at least one comfort element (88), which is arranged on an upper face (30) of the main part (22), at least one receiving region (40, 42) for attaching to a support pipe (14, 16), and at least one securing element (60, 62, 64, 66) for attaching to the support pipe (14, 16). The main part (22) has at least two coupling regions (68, 70, 72, 74, 76, 78, 80, 82) via which the at least one securing element (60, 62, 64, 66) can be selectively attached to the main part (22).
The invention relates to an airplane seat device with at least one airplane seat (10, 14, 16) which is provided at least for being adjusted between a use position and a stowed position. In the stowed position, the airplane seat (10, 14, 16) has a maximum height which is equal to or less than a maximum height in the use position.
An airplane seat device includes at least one airplane seat element implementing at least a portion of a table-less airplane seat, with at least one deposit and/or storage element which is embodied separate from the airplane seat element; the airplane seat element comprising at least one interface via which the deposit and/or storage element can be connected to the airplane seat element if required.
An aircraft seat mounting device with at least one carrier profile, with at least one aircraft seat element and with at least one intermediate element, which at least substantially encompasses the at least one carrier profile and is coupled to the at least one aircraft seat element.
The intermediate element is arranged rotatably with respect to the carrier profile at least in case of crash/deformation.
The invention relates to a flight passenger seating device, comprising a flight passenger seat (10; 10b), which has at least one seat base (12) and at least one leg-supporting module (24; 24b), which comprises at least one leg-supporting element (26; 26b), which is at least partially movable in relation to the seat base (12). According to the invention, the leg-supporting module (24; 24b) comprises at least two rotary bearing units (34, 36; 34b, 36b) and a linear bearing unit (38; 38b), by means of which bearing units the leg-supporting element (26; 26b) is supported in such a way that the leg-supporting element can be moved in relation to the seat base (12).
The invention relates to an aircraft seat device comprising a table module (10a; 0b; 10c; 10d) and comprising a PED holder (36a; 36b; 36c; 36d) provided to support a PED (38a; 38b; 38c; 38d) in an operating position on the table module (10a; 10b; 10c; 0d), wherein the PED holder (36a; 36b; 36c; 36d) comprises at least one retaining element (40a; 40b; 40c; 40d) which is pivotably connected to the table module (10a; 10b; 10c; 10d). According to the invention, the PED holder (36a; 36b; 36c; 36d) comprises a pivot support unit (42a; 42d), which is provided to pivot the retaining element (40a; 40b; 40c; 40d) through more than 180 degrees.
The invention relates to an aircraft module covering device, comprising at least one aircraft module (10, 44) and at least one panel (12, 46), which is provided for covering the aircraft module (10, 44) and, for this purpose, is firmly connected to the aircraft module (10, 44) in order to at least partially cover the aircraft module (10, 44) in a mounted state. According to the invention the panel (12, 46) is designed to be connected to the aircraft module (10, 44) by means of at least one frictional connection and, for this purpose, has at least one connection element (18, 20, 22, 24, 28), which is firmly arranged on an underside (28) of the panel (12, 46).
B64D 11/06 - Aménagements ou adaptations des sièges
F16B 2/24 - Clips, c.-à-d. dispositifs de fixation à serrage effectué uniquement par la résistance à la déformation inhérente au matériau dont est fait le dispositif en matériau élastique, p. ex. un matériau caoutchouteux métallique
F16B 5/12 - Fixation par clips de bandes ou de barres à des feuilles ou plaques, p. ex. bandes de caoutchouc, bandes décoratives pour véhicules à moteur
F16B 21/07 - Dispositifs de fixation largables à action rapide dans lesquels la douille a une partie élastique
100.
SYSTEM FOR CONTROLLING AN AIRCRAFT PASSENGER SEAT UNIT
The invention relates to a system of an aircraft device (10), comprising at least one control and/or regulating unit (38) provided for controlling an aircraft passenger seat unit (18, 20, 22), and comprising a PED (40, 62) in which at least one operating program is stored. According to the invention, the control and/or regulating unit (38) is designed to capture control signals from the PED (40, 62) for controlling the aircraft passenger seat unit (18, 20, 22).
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
B64D 11/06 - Aménagements ou adaptations des sièges
B60N 2/02 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable
H04N 21/00 - Distribution sélective de contenu, p. ex. télévision interactive ou vidéo à la demande [VOD]
brevets
