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Résultats pour
brevets
1.
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Re-Configurable VTOL Aircraft
Numéro d'application |
18621047 |
Statut |
En instance |
Date de dépôt |
2024-03-28 |
Date de la première publication |
2025-08-14 |
Propriétaire |
Delhivery Robotics LLC (USA)
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Inventeur(s) |
- Gibboney, Jeff
- Sinha, Pranay
- Forrette, Christopher
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Abrégé
A manned/unmanned aerial vehicle adapted for vertical takeoff and landing which is configured to be easily disassembled and reassembled. The aerial vehicle may be assembled with different wings based upon flight needs, which may be based upon cargo mass and flight duration, for example. The aerial vehicle may utilize structural booms within components, and may allow for decoupling of boom sections to facilitate disassembly. The aerial vehicle may utilize electric motors and store power in batteries. A method of customizing a configuration of an unmanned aerial vehicle based upon flight profile factors such as duration, stability, and maneuverability. A method of disassembling an aerial vehicle for storage and/or transport.
Classes IPC ?
- B64U 10/20 - Aéronefs à décollage et atterrissage verticaux [ADAV, en anglais VTOL]
- B64C 3/18 - LongeronsNervuresLisses
- B64F 5/10 - Fabrication ou assemblage d’aéronefs, p. ex. gabarits à cet effet
- B64U 20/50 - Véhicules aériens sans pilote pliables ou repliables
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2.
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RE-CONFIGURABLE VTOL AIRCRAFT
Numéro d'application |
US2024022108 |
Numéro de publication |
2024/248929 |
Statut |
Délivré - en vigueur |
Date de dépôt |
2024-03-28 |
Date de publication |
2024-12-05 |
Propriétaire |
DELHIVERY ROBOTICS LLC (USA)
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Inventeur(s) |
- Gibboney, Jeff
- Sinha, Pranay
- Forrette, Christopher
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Abrégé
A manned/unmanned aerial vehicle adapted for vertical takeoff and landing which is configured to be easily disassembled and reassembled. The aerial vehicle may be assembled with different wings based upon flight needs, which may be based upon cargo mass and flight duration, for example. The aerial vehicle may utilize structural booms within components, and may allow for decoupling of boom sections to facilitate disassembly. The aerial vehicle may utilize electric motors and store power in batteries. A method of customizing a configuration of an unmanned aerial vehicle based upon flight profile factors such as duration, stability, and maneuverability. A method of disassembling an aerial vehicle for storage and/or transport.
Classes IPC ?
- B64U 80/50 - Transport ou stockage spécialement adaptés aux véhicules aériens sans pilote les véhicules aériens sans pilote étant démontés
- B64C 1/30 - Éléments de fuselage mobiles l'un par rapport à l'autre pour réduire l'encombrement
- B64C 3/38 - Réglage des ailes complètes ou de certaines parties de ces ailes
- B64C 29/00 - Aéronefs capables d'atterrir ou de décoller à la verticale, p. ex. aéronefs à décollage et atterrissage verticaux [ADAV, en anglais VTOL]
- B64U 10/20 - Aéronefs à décollage et atterrissage verticaux [ADAV, en anglais VTOL]
- B64U 20/40 - Véhicules aériens sans pilote modulaires
- B64U 30/14 - Ailes variables ou détachables, p. ex. ailes à flèche réglable détachables
- B64U 30/291 - Rotors ou supports de rotor détachables
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3.
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Remotely controlled modular VTOL aircraft and re-configurable system using same
Numéro d'application |
16524008 |
Numéro de brevet |
11414191 |
Statut |
Délivré - en vigueur |
Date de dépôt |
2019-07-27 |
Date de la première publication |
2020-05-21 |
Date d'octroi |
2022-08-16 |
Propriétaire |
Delhivery Robotics, LLC (USA)
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Inventeur(s) |
- Gibboney, Jeffrey Kyle
- Sinha, Pranay
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Abrégé
A manned/unmanned aerial vehicle adapted for vertical takeoff and landing using the same set of engines for takeoff and landing as well as for forward flight. An aerial vehicle which is adapted to takeoff with the wings in a vertical as opposed to horizontal flight attitude which takes off in this vertical attitude and then transitions to a horizontal flight path. A tailless airplane which uses a control system that takes inputs for a traditional tailed airplane and translates those inputs to provide control utilizing non-traditional control methods.
Classes IPC ?
- B64C 39/08 - Aéronefs non prévus ailleurs à ailes multiples
- B64C 39/02 - Aéronefs non prévus ailleurs caractérisés par un emploi spécial
- B64C 3/54 - Variation de la surface alaire
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4.
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Remotely controlled modular VTOL aircraft and re-configurable system using same
Numéro d'application |
15143625 |
Numéro de brevet |
10377482 |
Statut |
Délivré - en vigueur |
Date de dépôt |
2016-05-01 |
Date de la première publication |
2018-09-20 |
Date d'octroi |
2019-08-13 |
Propriétaire |
DELHIVERY ROBOTICS LLC (USA)
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Inventeur(s) |
- Gibboney, Jeffrey Kyle
- Sinha, Pranay
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Abrégé
A manned/unmanned aerial vehicle adapted for vertical takeoff and landing using the same set of engines for takeoff and landing as well as for forward flight. An aerial vehicle which is adapted to takeoff with the wings in a vertical as opposed to horizontal flight attitude which takes off in this vertical attitude and then transitions to a horizontal flight path. An aerial vehicle system which has removable wing sections which allow for re-configuration with different wing section types, allowing for configurations adapted for a particular flight profile. A method of customizing a configuration of an unmanned aerial vehicle based upon flight profile factors such as duration, stability, and maneuverability.
Classes IPC ?
- B64C 39/08 - Aéronefs non prévus ailleurs à ailes multiples
- B64C 39/02 - Aéronefs non prévus ailleurs caractérisés par un emploi spécial
- B64C 3/54 - Variation de la surface alaire
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