公开(公告)号：US2712913A

公开(公告)日：1955-07-12

申请号：US37580453

申请日：1953-08-21

Applicant: STANIEY AVIAT CORP

Inventor： STANLEY ROBERT M

IPC: B64D1/14

CPC classification number: B64D1/14 ,  B64D2201/00

公开(公告)号：US11993385B2

公开(公告)日：2024-05-28

申请号：US16960055

申请日：2018-11-12

Applicant: MATSUYA R&D., LTD.

Inventor： Hidetaka Goto

IPC: B64D25/00 ,  B64C39/02 ,  B64U10/13

CPC classification number: B64D25/00 ,  B64C39/024 ,  B64D2201/00 ,  B64U10/13

Abstract: To provide a drone with an airbag that can eliminate the danger of the drone injuring a person in the event of the drone crashing mid-flight including during takeoff and landing. The present invention is equipped with an airbag 3 for reducing the impact of a crashed drone 2 colliding with a person. Prior to the drone 2 taking off, the airbag 3 can be inflated by being supplied with gas. Once the drone 2 has taken off and reached a required altitude, the airbag 3 deflates due to the gas being exhausted. When the drone 2 is mid-flight and in danger of crashing, the airbag 2 can be inflated instantly by being supplied with gas. Prior to the drone 2 landing, the airbag 3 can be inflated by being supplied with gas.

公开(公告)号：US20230271703A1

公开(公告)日：2023-08-31

申请号：US17588237

申请日：2022-01-29

Applicant: AutoBotx, LLC

Inventor： David Kilzer ,  Craig Foster

IPC: B64D1/22 ,  G05D1/10 ,  B64D9/00 ,  B64D1/10 ,  B64C39/02 ,  B64D1/12 ,  B64F1/32

CPC classification number: B64D1/22 ,  B64C39/024 ,  B64D1/10 ,  B64D1/12 ,  B64D9/003 ,  B64F1/322 ,  G05D1/101 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/128 ,  B64C2201/141 ,  B64D2201/00

Abstract: An unmanned cargo loading and transport system adapted for operation with an unmanned aerial vehicle (UAV) comprising a payload pad comprising a plurality of support members movable from an extended mode to a retracted mode when exposed to a lateral force applied to the support members and a payload container adapted to attach to a UAV and pick up cargo from the payload pad by transferring the weight of the cargo from the payload pad to the payload container. The lower portion of the payload container comprises two generally opposed cargo doors movably mounted at opposed sides and movable inwardly to a closed position and outwardly to an open position to receive cargo when the payload container is positioned at the payload pad. The system further comprises a motive power mechanism coupled to the cargo doors for selectively moving the doors between their open and their closed positions.

公开(公告)号：US20170225788A1

公开(公告)日：2017-08-10

申请号：US15398977

申请日：2017-01-05

Applicant: AmSafe, Inc.

Inventor： Todd Joseph Humbert

IPC: B64D11/06 ,  B60R21/2338 ,  B60R21/276 ,  B60R21/235 ,  B60R21/237 ,  B60R21/239 ,  B60R21/18 ,  B60R21/2342

CPC classification number: B60R21/18 ,  B60R21/233 ,  B60R2021/0044 ,  B60R2021/0093 ,  B60R2021/23115 ,  B60R2021/23308 ,  B60R2021/23386 ,  B64D11/06205 ,  B64D2201/00

Abstract: Multi-chamber airbag systems for use in aircraft and other vehicles are described herein. In some embodiments, an occupant restraint system includes a multi-chamber airbag that deploys from an occupant restraint (e.g., a lap seat belt) in an aircraft. The multi-chamber airbag can include a first portion that inflates generally upward in front of the occupant's torso, and a second portion that inflates in front of the first portion. The first portion and/or the second portion can include multiple chambers (e.g., generally cylindrical-shaped chambers) that, when inflated, provide the airbag with a shape and/or contact surfaces which can help to maintain the position of the airbag between the occupant and a strike object or hazard. In other embodiments, multi-chamber airbags configured in accordance with the present disclosure can me mounted to a structure (e.g., a monument, console, seat back, etc.) positioned generally in front of the occupant. The structure-mounted airbag can deploy generally toward the occupant in the event of a vehicle impact or other potentially harmful event to protect the occupant from impact injury.

公开(公告)号：US20170096221A1

公开(公告)日：2017-04-06

申请号：US15205162

申请日：2016-07-08

Applicant: Piasecki Aircraft Corporation

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

IPC: B64C37/00 ,  B64D17/80 ,  B64C29/00 ,  B64C25/58 ,  B64C3/56 ,  B64C27/22 ,  B60F5/02 ,  B64D25/00

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 unmanned air module includes one or more rotors, engines, a transmission and avionics. Any of several different ground modules may be attached to the air module. The air module may fly with and without the ground module attached. The ground module may be manned. The air module may have two rotors, which may be ducted fans. The air module may include a parachute, an airbag and landing gear.

公开(公告)号：US20170015424A1

公开(公告)日：2017-01-19

申请号：US14801959

申请日：2015-07-17

Applicant: The Boeing Company

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

IPC: B64D11/06

CPC classification number: B64D11/06205 ,  B60R2021/01177 ,  B60R2022/021 ,  B64D11/0621 ,  B64D25/00 ,  B64D2201/00

Abstract: A safety device has a lower portion and an upper portion. The lower portion defines a cavity for receiving a seat belt buckle assembly and has at least one rear wall portion extending between opposing sidewalls that partially define the cavity. The rear wall portion forms a slot area to permit a strap attached to the seat belt buckle assembly to extend from the cavity when the seat belt buckle assembly is positioned in the cavity. The rear wall portion is configured to prevent the seat belt buckle assembly from moving laterally out of the cavity. The upper portion is hingedly coupled to the lower portion such that the upper portion completely covers the cavity of the lower portion when the upper portion is rotated into engagement with the lower portion.

Abstract translation: 安全装置具有下部和上部。 下部限定用于接纳安全带扣环组件的空腔，并且具有至少一个后壁部分，该后壁部分在部分地限定空腔的相对侧壁之间延伸。 后壁部分形成狭槽区域，以允许当安全带扣组件定位在空腔中时，连接到安全带扣组件的带从空腔延伸。 后壁部分构造成防止安全带扣环组件横向移出空腔。 上部部分铰接地联接到下部，使得当上部部分与下部部分旋转接合时，上部完全覆盖下部的空腔。

公开(公告)号：US20170008641A1

公开(公告)日：2017-01-12

申请号：US15204140

申请日：2016-07-07

Applicant: AIRBUS HELICOPTERS

Inventor： Tomas SANTANA-GALLEGO

IPC: B64D45/00 ,  B64D25/04 ,  B64D25/06 ,  B64D11/06

CPC classification number: B64D45/00 ,  B64D11/0619 ,  B64D11/0621 ,  B64D25/04 ,  B64D25/06 ,  B64D2201/00 ,  B64D2221/00

Abstract: A control device including at least one control member for measuring an acceleration of an aircraft, for generating an inflation order, and for transmitting the inflation order to an inflation member, the inflation member serving to inflate at least one inflatable safety bag, the control device, the inflation member and the inflatable bag being arranged together on a single seat of the aircraft. Such a control device includes at least one readying system connected to the at least one control member, the readying system comprising: at least a first sensor suitable for continuously measuring a first current acceleration of the aircraft relative to at least one axis; and at least one switch that is controllable as a function of the first current acceleration of the aircraft as measured by the first sensor.

Abstract translation: 一种控制装置，包括至少一个用于测量飞行器的加速度的控制构件，用于产生膨胀顺序，以及用于将膨胀顺序传送到充气构件，膨胀构件用于使至少一个充气安全袋充气，所述控制装置 ，充气构件和可充气袋一起布置在飞机的单个座椅上。 这种控制装置包括连接至至少一个控制构件的至少一个准备系统，所述准备系统包括：至少第一传感器，其适用于相对于至少一个轴线连续地测量飞机的第一当前加速度; 以及至少一个可由第一传感器测量的作为飞行器的当前加速度的函数来控制的开关。

公开(公告)号：US09493250B2

公开(公告)日：2016-11-15

申请号：US14948220

申请日：2015-11-20

Applicant: SZ DJI TECHNOLOGY CO., LTD.

Inventor： Mingyu Wang

IPC: B64D45/00 ,  B64C25/32 ,  B64D25/00 ,  B64C25/56 ,  B64C25/54

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.

公开(公告)号：US09487301B2

公开(公告)日：2016-11-08

申请号：US13696970

申请日：2011-02-23

Applicant: Andrew T. Hill ,  Zi Lu ,  Robert S. Lynds ,  Andrew R. Hansen

Inventor： Andrew T. Hill ,  Zi Lu ,  Robert S. Lynds ,  Andrew R. Hansen

IPC: B64D25/00 ,  B64C25/52 ,  B64C25/32

CPC classification number: B64D25/00 ,  B64C25/52 ,  B64C2025/325 ,  B64D2201/00

Abstract: An external airbag for an aircraft includes an inflatable bladder having a top portion and a bottom portion, the top portion being generally adjacent to an exterior of the aircraft. A widthwise panel divides the inflatable bladder into a first cylindrical portion and a second cylindrical portion. The widthwise panel acts to restrict outward bulging of the inflatable bladder. An aperture in the widthwise panel may be used for allowing gas communication between the first cylindrical portion and a second cylindrical portion.

Abstract translation: 一种用于飞行器的外部安全气囊包括具有顶部和底部的可膨胀气囊，所述顶部大体上邻近飞行器的外部。 横向面板将可充气气囊分成第一圆柱形部分和第二圆柱形部分。 横向面板用于限制可膨胀囊的向外膨胀。 宽度方向面板上的孔可以用于允许第一圆柱形部分和第二圆柱形部分之间的气体连通。

公开(公告)号：US09452843B1

公开(公告)日：2016-09-27

申请号：US14711230

申请日：2015-05-13

Applicant: Bell Helicopter Textron Inc.

Inventor： Zi Lu ,  Michael Seifert ,  Cheng-Ho Tho

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

CPC classification number: B64D25/00 ,  B64C25/32 ,  B64C25/56 ,  B64C2025/325 ,  B64D2201/00

Abstract: An aircraft airbag inflation system includes an airbag mounted on an external surface of an aircraft. The airbag is configured to inflate in one of multiple stages prior to the aircraft crashing, and each stage is associated with a respective pressure. The system also includes multiple sensors disposed on-board the aircraft and configured to sense aircraft velocities and an aircraft attitude. The system also includes a controller disposed on-board the aircraft and configured to receive multiple signals from the sensors, the multiple signals representing the aircraft velocities and the aircraft attitude sensed by the sensors, determine a crash event for the aircraft based on the received multiple signals, the crash event including an aircraft sink rate, an aircraft attitude at crash time, and an aircraft distance from the impact surface, and determine a stage at which the airbag is to be inflated based on the crash event.

Abstract translation: 飞机安全气囊充气系统包括安装在飞行器的外表面上的安全气囊。 气囊被构造成在飞机撞击之前的多个阶段中的一个中膨胀，并且每个阶段与相应的压力相关联。 该系统还包括布置在飞行器上的多个传感器并且被配置成感测飞行器速度和飞行器姿态。 该系统还包括设置在飞行器上的控制器，并被配置为从传感器接收多个信号，表示飞行器速度的多个信号和由传感器感测到的飞行器姿态基于接收到的多个飞行器确定飞机的碰撞事件 信号，碰撞事件包括飞机下沉速率，飞机在碰撞时的姿态，以及与撞击表面的飞行器距离，以及基于碰撞事件确定气囊膨胀的阶段。