公开(公告)号：US12084180B2

公开(公告)日：2024-09-10

申请号：US17113896

申请日：2020-12-07

Applicant: Flirtey Holdings, Inc.

Inventor： Matthew Sweeny ,  John R Foggia ,  Jeremy Fries

IPC: B64C39/02 ,  B64D25/00 ,  B64U10/13 ,  B64U30/20 ,  B64U50/19

CPC classification number: B64C39/024 ,  B64D25/00 ,  B64D2201/00 ,  B64U10/13 ,  B64U30/20 ,  B64U50/19

Abstract: In an embodiment an unmanned aerial vehicle comprises a central body and a plurality of support structures extending outwards from the central body. Each support structure supports a rotor blade assembly and is provided with one or more deformable portions. The rotor blade assembly defines a rotational axis of one or more rotor blades associated with the rotor blade assembly.

公开(公告)号：US11851183B2

公开(公告)日：2023-12-26

申请号：US17077684

申请日：2020-10-22

Applicant: DASSAULT AVIATION

Inventor： Lionel Patrick Germe ,  Emmanuel Picut ,  Alain Levavasseur ,  Erwan Boulo ,  Jérémie Guerard

IPC: B64D11/06 ,  B64D41/00

CPC classification number: B64D11/0621 ,  B64D11/0601 ,  B64D11/0605 ,  B64D11/0638 ,  B64D41/00 ,  B64D2201/00

Abstract: An aircraft cabin includes at least one seat able to receive at least one passenger; at least one table arranged opposite the seat; and a safety device able to be mounted on the table, below the table or received in the table. The safety device includes a deployable protection assembly including an airbag deployable from a retracted idle configuration to a deployed safety configuration, and a system for controlling the deployment of the or each airbag, able to trigger the deployment of the airbag beyond a threshold deceleration value of the aircraft.

公开(公告)号：US20180370610A1

公开(公告)日：2018-12-27

申请号：US15632966

申请日：2017-06-26

Applicant: The Boeing Company

Inventor： Mithra Sankrithi

IPC: B64C1/06 ,  B64C1/18

CPC classification number: B64C1/061 ,  B64D11/06 ,  B64D13/06 ,  B64D2201/00

Abstract: Fuselage configurations in which window seats project into and partially occupy inter-frame spaces. In accordance with some embodiments, a frame in proximity to a window seat is equipped with a riser duct closure cover for defining a riser duct for passing a volume of air through a supply duct located below a floor of a passenger cabin through the riser duct and through a crown distribution duct located above a ceiling of the passenger cabin. In accordance with other embodiments, the frames in proximity to window seats are equipped with respective airbags. More specifically, for each pair of adjacent frames in which the forward frame of the pair is located forward of the window seat, the aft frame of the pair is located aft of the window seat, the forward frame is equipped with an airbag.

公开(公告)号：US09889937B2

公开(公告)日：2018-02-13

申请号：US14705915

申请日：2015-05-06

Applicant: AmSafe, Inc.

Inventor： William J. Gehret ,  Joshua Vyrostek ,  Kevin J. Keeslar ,  Daniel Nick Foubert

IPC: B60R21/16 ,  B64D11/06 ,  B60R21/20 ,  B60R21/231 ,  B60R21/26 ,  B60R21/00

CPC classification number: B64D11/0621 ,  B60R21/20 ,  B60R21/231 ,  B60R21/26 ,  B60R2021/0093 ,  B64D11/06 ,  B64D11/0604 ,  B64D11/06205 ,  B64D2201/00

Abstract: Structure mounted airbag assemblies and associated systems and methods are described herein. An airbag system configured in accordance with an embodiment of the present disclosure can include, for example, a housing having a cavity and an opening in communication with the cavity, an airbag assembly within the cavity, and an inflator operably coupled to the airbag assembly. The airbag assembly can include an airbag configured to deploy through the opening of the housing during a crash event. The airbag system can further include a door removably positioned across the opening and configured to move away from the opening during airbag deployment. The housing can be affixed to an interior portion of an aircraft, forward of and offset from an aircraft seat.

公开(公告)号：US20170210469A1

公开(公告)日：2017-07-27

申请号：US15476612

申请日：2017-03-31

Applicant: Piasecki Aircraft Corporation

Inventor： John W. Piasecki ,  Frederick W. Piasecki ,  Brian Geiger ,  Douglas Johnson ,  David Pitcairn

IPC: B64C37/00 ,  B60F5/02 ,  B64C11/00 ,  B64C27/08 ,  G05D1/10 ,  B64C27/22 ,  B64C27/57 ,  B64D17/80 ,  B64C39/02 ,  B64C3/56 ,  B64C29/00 ,  B64C27/20

CPC classification number: B64C37/00 ,  B60F5/02 ,  B64C3/385 ,  B64C3/56 ,  B64C11/001 ,  B64C25/58 ,  B64C27/08 ,  B64C27/20 ,  B64C27/22 ,  B64C27/32 ,  B64C27/52 ,  B64C27/57 ,  B64C29/00 ,  B64C29/0033 ,  B64C39/00 ,  B64C39/02 ,  B64D17/80 ,  B64D25/00 ,  B64D2201/00 ,  G05D1/102

Abstract: An air module may be attached to a ground module. The air module may be equipped with a center of gravity effector to change the relative locations and hence the center of gravity of the air and ground modules when the modules are attached. The center of gravity effector may be active or passive or a combination of active and passive. The center of gravity effector may be combined with a center of lift effector to change the relative locations of the center of gravity and center of lift.

公开(公告)号：US20170184524A1

公开(公告)日：2017-06-29

申请号：US15305063

申请日：2014-04-22

Applicant: SKYROBOT INC.

Inventor： RYOHEI UETAKI ,  DAISUKE KAIO

IPC: G01N25/72 ,  G01J5/04 ,  H04N5/33 ,  G06K9/00 ,  H02S50/10 ,  B64D47/08 ,  B64D17/80 ,  B64D45/00 ,  G05D1/10 ,  G01J5/00 ,  B64C39/02

CPC classification number: G01N25/72 ,  B64C39/024 ,  B64C2201/146 ,  B64D17/80 ,  B64D45/00 ,  B64D47/08 ,  B64D2201/00 ,  G01J5/0066 ,  G01J5/047 ,  G01J5/089 ,  G01J5/10 ,  G01J2005/0077 ,  G01J2005/0081 ,  G05D1/10 ,  G06K9/0063 ,  H02S50/10 ,  H04N5/33

Abstract: A solar power panel failure search and detect system to search and detect malfunctioning or failed sites of a solar power panel. A search unit is installed in a remotely controllable aerial vehicle. The search unit maintains a constant distance between a solar panel and a failure detector, and maintains the failure detector at an optimum angle. A control unit controls a flight path and a flight angle of the aerial vehicle and controls/regulates an angle of the failure detector, a receiver, a processor, and the search unit. The search unit has an angle sensor, the failure detector, an angle adjuster and an imaging device. The control unit has a transmitter to transmit the search result data.

公开(公告)号：US09643726B2

公开(公告)日：2017-05-09

申请号：US14801994

申请日：2015-07-17

Applicant: The Boeing Company

Inventor： John A. Lepore ,  Thomas E. Dowhower ,  Peter M. Heinrich

IPC: B60R21/01 ,  B60R22/00 ,  B64D11/00 ,  B64D25/00 ,  B64D11/06 ,  A44B11/25 ,  B60R21/18 ,  B60R22/02

CPC classification number: B64D11/06205 ,  A44B11/2526 ,  A44B11/2569 ,  B60R21/18 ,  B60R2021/01177 ,  B60R2022/021 ,  B64D25/00 ,  B64D2201/00

Abstract: A safety device for preventing accidental discharge of an airbag. A lower portion of the safety device includes two opposing sidewalls at least partially defining a cavity for holding a seat belt buckle assembly. An upper portion of the safety devices is hingedly coupled to the lower portion. The safety device also includes a mechanism for securely latching the upper portion to the lower portion and a mechanism for releasing the upper portion from the lower portion when the upper portion is securely latched to the lower portion to allow the upper portion to rotate away from the lower portion.

公开(公告)号：US09611045B2

公开(公告)日：2017-04-04

申请号：US14850642

申请日：2015-09-10

Applicant: Indemnis, Inc.

Inventor： Alan Jamal Erickson

IPC: B64D17/00 ,  B64D17/72 ,  B64D17/80 ,  B64C39/02

CPC classification number: B64D17/72 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/185 ,  B64D17/80 ,  B64D25/00 ,  B64D2201/00

Abstract: A system and method for resisting an uncontrolled descent or uncontrolled flight condition of an aerial vehicle. The system includes a control system, sensors, an inflation device, and a deployable, inflatable assembly. The control system detects an uncontrolled condition using the sensors, and subsequently initiates the inflation device to inflate the inflatable assembly. The assembly includes an inflatable cage stored on and deployed from the aerial vehicle upon detection of an uncontrolled condition. The inflatable cage includes a hub, a perimeter tube, and support tubes connected between the hub and perimeter tube. Fill tubes enable inflation of the support and perimeter tubes. The assembly includes a parachute-material enclosure connected to the inflatable cage and structured to create drag to reduce a velocity of the aerial vehicle when the inflatable assembly is deployed. The assembly includes weight distribution straps physically coupled between the vehicle and the enclosure or inflatable cage.

公开(公告)号：US20170057645A1

公开(公告)日：2017-03-02

申请号：US15349750

申请日：2016-11-11

Applicant: SZ DJI TECHNOLOGY CO., Ltd

Inventor： Mingyu Wang

IPC: B64D25/00 ,  B64C25/56 ,  B64C39/02 ,  B64C25/32

CPC classification number: B64D25/00 ,  B64C25/32 ,  B64C25/54 ,  B64C25/56 ,  B64C39/024 ,  B64C2201/027 ,  B64D45/00 ,  B64D2201/00

Abstract: An impact protection apparatus is provided, comprising a gas container configured to hold a compressed gas and an inflatable member configured to be inflated by the gas and function as an airbag of a movable object, such as an aerial vehicle. A valve controls flow of gas from the container to the inflatable member in response to a signal from a valve controller. The valve and valve controller are powered by an independent power source than one or more other systems of the movable object. A safety mechanism may also be provided that, unless deactivated, prevents inflation of the inflatable member.

Abstract translation: 提供了一种冲击保护装置，包括构造成保持压缩气体的气体容器和构造成由气体膨胀并充当诸如飞行器的可移动物体的气囊的充气构件。 响应于来自阀控制器的信号，阀控制气体从容器到可膨胀构件的流动。 阀和阀门控制器由与可移动物体的一个或多个其它系统相独立的电源供电。 还可以提供一种安全机构，除非被去激活，否则防止可膨胀构件的膨胀。

公开(公告)号：US09527468B2

公开(公告)日：2016-12-27

申请号：US14542887

申请日：2014-11-17

Applicant: Zodiac Seats France

Inventor： Alexandre Vasseur ,  Jean-Marc Obadia

IPC: B60R21/2155 ,  B60R21/237 ,  B60R21/231 ,  B60R21/216

CPC classification number: B60R21/2155 ,  B60R21/216 ,  B60R21/231 ,  B60R21/237 ,  B64D2201/00

Abstract: Embodiments of the present invention provide an airbag door assembly for use in a vehicle. The door assembly includes a moving door panel that deforms under pressure of an airbag as it deploys. The airbag system employing this airbag door assembly may be installed in a cavity in a structure on-board the vehicle, or it may be independently mounted to a vehicle structure.

Abstract translation: 本发明的实施例提供一种用于车辆的气囊门组件。 门组件包括移动的门板，其在展开时在气囊的压力下变形。 使用该安全气囊门组件的气囊系统可以安装在车辆上的结构中的空腔中，或者可以独立地安装在车辆结构上。