An end effector is presented. The end effector comprises a torque wrench and a first vacuum source. The torque wrench is configured to hold a collar and apply a single-sided clamp-up to a structure. The first vacuum source is pneumatically connected to the torque wrench and configured to supply a vacuum for the single-sided clamp-up.
Fastener storage is presented. The fastener storage comprises a disc with a plurality of apertures through a first face of the disc and arranged in a plurality of rings concentric with the disc, and a plurality of machine-readable identifiers on the first face of the disc.
An end effector is presented. The end effector comprises a housing, an actuated mechanical retainer, and a normalizing nosepiece assembly. The actuated mechanical retainer is connected to the housing and configured to selectively constrain and release the normalizing nosepiece assembly from the housing. The normalizing nosepiece assembly is moveable relative to the housing and having a nosepiece bushing configured to contact a workpiece.
An end effector is presented. The end effector comprises a torque wrench and a first vacuum source. The torque wrench is configured to hold a collar and apply a single-sided clamp-up to a structure. The first vacuum source is pneumatically connected to the torque wrench and configured to supply a vacuum for the single-sided clamp-up.
This application relates to a boarding pass processing device. In one aspect, the device includes a communication unit for communicating with a central server and a boarding pass recognition unit for recognizing a boarding pass held by a passenger. The device may also include a boarding processing unit for, if procedure information relating to whether a passenger holding a boarding pass recognized by the boarding pass recognition unit has gone through a procedure required for boarding an airplane is obtained from the central server through the communication unit, processing whether or not the passenger holding the recognized boarding pass has boarded the airplane, on the basis of the obtained procedure information.
G07C 9/28 - Enregistrement de l’entrée ou de la sortie d'une entité isolée comportant l’utilisation d’un laissez-passer le laissez-passer permettant le repérage ou signalant la présence
G07C 9/27 - Enregistrement de l’entrée ou de la sortie d'une entité isolée comportant l’utilisation d’un laissez-passer une station centrale gérant l’enregistrement
7.
Fixed temperature maintenance system for engine in unmanned aircraft having automatic throttle limiting device
A system for maintaining a constant temperature of an engine in an unmanned aerial system with an autothrottle limiting device comprises an autopilot for issuing a throttle command, an autothrottle limiting device for automatically limiting an upper limit of the throttle command issued by the autopilot, and a rotary engine for feeding an internal temperature of the engine back to the autothrottle limiting device. The system is applicable to all kinds of unmanned aerial systems employing an air-cooling rotary engine, uses the existing autopilot of the unmanned aerial system without modification, and improves the reliability and life of the engine.
B64D 31/06 - Dispositifs amorçant la mise en œuvre actionnés automatiquement
F02D 41/14 - Dispositions de circuits pour produire des signaux de commande introduisant des corrections à boucle fermée
F02D 9/02 - Commande des moteurs par étranglement des conduits d'amenée de l'air ou du mélange air-combustible ou par étranglement des conduits d'échappement par étranglement des conduits d'amenée
F02D 41/26 - Commande électrique de l'alimentation en mélange combustible ou en ses constituants caractérisée par l'utilisation de moyens numériques utilisant des calculateurs, p. ex. microprocesseurs
B64D 33/08 - Aménagement sur les aéronefs des éléments ou des auxiliaires des ensembles fonctionnels de propulsion, non prévu ailleurs des systèmes de refroidissement des ensembles fonctionnels de propulsion
F02D 41/00 - Commande électrique de l'alimentation en mélange combustible ou en ses constituants
B64C 39/02 - Aéronefs non prévus ailleurs caractérisés par un emploi spécial
The present application discloses a method of obtaining multi-lineage stem cells or progenitor cells by allowing a sample of cells to settle in a container; transferring supernatant from the container to another container; and eventually isolating a colony from the supernatant after several transfer/settle processes and expanding further, and optionally freezing the cells thus obtained.
The present application discloses a method of treating pancreatitis by administering to the patient mesenchymal stem cells that are obtained by manipulating a biological sample of cells, which includes multi-lineage stem cells, progenitor cells, other marrow stromal cells: allowing the sample of cells to settle in a container; transferring supernatant from the container to another container; and isolating cells from the supernatant, which has comparatively lower density in the sample.
A61K 35/28 - Moelle osseuseCellules souches hématopoïétiquesCellules souches mésenchymateuses de toutes origines, p. ex. cellules souches dérivées de tissu adipeux
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