公开(公告)号：EP2460070A4

公开(公告)日：2013-03-06

申请号：EP09847898

申请日：2009-07-27

Applicant: BELL HELICOPTER TEXTRON INC

Inventor： HILL ANDREW T ,  SMITH MICHAEL R ,  COVINGTON CHARLES E ,  LAPPOS NICHOLAS ,  SONNEBORN WALTER

IPC: G06F7/70 ,  B64D25/00 ,  G05D1/00 ,  G06F19/00 ,  G06G7/00 ,  G06G7/76

CPC classification number: B64D25/00 ,  B64D2201/00

公开(公告)号：EP2527941A1

公开(公告)日：2012-11-28

申请号：EP12161935.7

申请日：2012-03-29

Applicant: AmSafe, Inc.

Inventor： Shields, Ronald A. ,  Settles, Peter A.

IPC: G05B23/02

CPC classification number: G07C5/0808 ,  B64D11/062 ,  B64D11/06205 ,  B64D25/02 ,  B64D2201/00 ,  G05B23/0256

Abstract: A system for testing a number of electronic module assemblies (EMAs) that control one or more personal restraint systems. A programmed processor with a computer system transmits signals that instruct the EMAs to perform a diagnostic self-test. The results of the self-test are received by the computer system and stored in a computer readable memory. In one embodiment, the computer system is a cabin management computer system for use on an aircraft.

Abstract translation: 用于测试控制一个或多个个人约束系统的多个电子模块组件（EMA）的系统。 具有计算机系统的编程处理器传送指示EMA执行诊断自检的信号。 自检结果由计算机系统接收并存储在计算机可读存储器中。 在一个实施例中，计算机系统是用于飞机上的舱室管理计算机系统。

公开(公告)号：EP2459443A1

公开(公告)日：2012-06-06

申请号：EP09847899.3

申请日：2009-07-27

Applicant: Bell Helicopter Textron Inc.

Inventor： HILL, Andrew, T. ,  SMITH, Michael, R. ,  LU, Zi ,  THO, Cheng-Ho

IPC: B64C25/56

CPC classification number: B64D25/00 ,  B64D2201/00

Abstract: A crash attenuation system for an aircraft includes an airbag carried by the aircraft that is inflatable generally adjacent an exterior of the aircraft. The airbag is in fluid communication with at least one vent passage for channeling gas from within the interior of the airbag to a region external to the airbag that allows the gas to escape without being obstructed by the airbag. A gas source is in fluid communication with the interior of the airbag for inflating the airbag. A vent valve is provided within the vent passage for controlling a flow of gas through the vent passage, thereby controlling deflation of the airbag. The vent valve is continuously adjustable to and between an open state, a closed state, and any number of partially open states.

公开(公告)号：EP2311730A1

公开(公告)日：2011-04-20

申请号：EP09804707.9

申请日：2009-08-03

Applicant: Japan Aerospace Exploration Agency ,  Daicel Chemical Industries, Ltd.

Inventor： SHOJI, Hirokazu ,  KATAYAMA, Kazuo ,  ENOMOTO, Norio ,  YUTANI, Hiroshi

IPC: B64D11/06 ,  B60N2/44

CPC classification number: B64D11/0619 ,  B60N2/4242 ,  B64D11/06 ,  B64D11/0647 ,  B64D25/04 ,  B64D2201/00

Abstract: The present invention provides a shock absorbing apparatus for an aircraft seat, that attenuates shock to passengers and crews.
The apparatus includes; an airbag 11 being expanded in a plate shape in a state of less than maximum expansion; an upper flat plate 12 arranged on one side of the airbag 11; a lower flat plate 13 arranged on another side of the airbag 11; a gas supply device 15 for supplying a gas to the airbag 11; and a detector sending a signal to activate the gas supply device 15 by a preset condition. The shock is absorbed by expanding the airbag 11 before the shock is applied to the passenger.

Abstract translation: 本发明提供一种用于飞机座椅的减震装置，其减轻对乘客和乘员组的冲击。 该装置包括： 气囊11在小于最大膨胀的状态下以板状膨胀; 布置在气囊11一侧的上平板12; 布置在气囊11的另一侧的下平板13; 用于向气囊11供给气体的气体供给装置15; 以及检测器，其通过预设条件发送信号以激活气体供应装置15。 在冲击应用于乘客之前，通过使气囊11膨胀来吸收冲击。

公开(公告)号：EP0680436B1

公开(公告)日：1998-11-18

申请号：EP94908602.9

申请日：1994-01-21

Applicant: FREEWING AIRCRAFT CORPORATION

Inventor： RUTAN, Elbert, L. ,  SCHMITTLE, Hugh, J.

IPC: B64C3/38 ,  B64C29/00

CPC classification number: B64C29/02 ,  B64C3/385 ,  B64C29/0033 ,  B64C39/024 ,  B64C39/04 ,  B64C2201/044 ,  B64C2201/046 ,  B64C2201/084 ,  B64C2201/086 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/182 ,  B64C2201/187 ,  B64D2201/00 ,  Y10S446/901

Abstract: A VTOL/STOL free wing aircraft (100) includes a free wing (110) having wings on opposite sides of a fuselage (102) connected to one another respectively adjacent fixed wing inboard or center root sections (117) fixedly attached to the fuselage (102) for free rotation about a spanwise axis (112). Horizontal and vertical tail surfaces (138, 140) are located at the rear end of a boom assembly (120) rotatably connected to the fuselage (102). A gearing (150) or screw rod (160) arrangement controlled by the pilot or remote control operator selectively relatively pivots the fuselage (102) in relation to the tail boom assembly (120) to enable the fuselage to assume a tilted or nose up configuration to enable VTOL/STOL flight.

公开(公告)号：EP0862001A1

公开(公告)日：1998-09-02

申请号：EP98100352.8

申请日：1998-01-12

Applicant: Daimler-Benz Aerospace Aktiengesellschaft

Inventor： Wagner, Adalbert, Dipl.-Ing.

IPC: F16K13/00 ,  B64G1/62 ,  B64D1/14

CPC classification number: B64G1/62 ,  B64C25/00 ,  B64D2201/00 ,  F16K13/06

Abstract: Das Sprengventil zur Freigabe von Öffnungen von Airbag-Landesystemen für Flug- und Raumfahrtgeräte weist eine Schneidladung mit Zündern auf und eine die Öffnung verschliessende Abdeckung, die bei Zündung der Schneidladung abgeschert wird. Die Abdeckung ist eine dünnwandige Scheibe oder eine Membran, die entweder in das Flug- und Raumfahrtgerät oder in das Airbag-Landesystem integriert ist.

Abstract translation: 爆炸阀由带有点火器（11）的楔形电荷（6）和封闭开口的盖（4）组成，当楔形电荷被点燃时，其被剪切。 盖子是一个薄壁盘。 楔形电荷具有第二次点火。 点火器和楔形电荷定位在搁置在盘上的安装环（5）中以被剪切。 盘的背离安装环的一侧具有限定切割点并围绕盘的支撑环（7）。 适配器（8）装配在安装环背离盘的一侧。

公开(公告)号：EP0680436A1

公开(公告)日：1995-11-08

申请号：EP94908602.0

申请日：1994-01-21

Applicant: FREEWING AIRCRAFT CORPORATION

Inventor： RUTAN, Elbert, L. ,  SCHMITTLE, Hugh, J.

IPC: B64C3 ,  B64C29 ,  B64C39

CPC classification number: B64C29/02 ,  B64C3/385 ,  B64C29/0033 ,  B64C39/024 ,  B64C39/04 ,  B64C2201/044 ,  B64C2201/046 ,  B64C2201/084 ,  B64C2201/086 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/182 ,  B64C2201/187 ,  B64D2201/00 ,  Y10S446/901

Abstract: A VTOL/STOL free wing aircraft (100) includes a free wing (110) having wings on opposite sides of a fuselage (102) connected to one another respectively adjacent fixed wing inboard or center root sections (117) fixedly attached to the fuselage (102) for free rotation about a spanwise axis (112). Horizontal and vertical tail surfaces (138, 140) are located at the rear end of a boom assembly (120) rotatably connected to the fuselage (102). A gearing (150) or screw rod (160) arrangement controlled by the pilot or remote control operator selectively relatively pivots the fuselage (102) in relation to the tail boom assembly (120) to enable the fuselage to assume a tilted or nose up configuration to enable VTOL/STOL flight.

公开(公告)号：EP0491017B1

公开(公告)日：1994-03-16

申请号：EP91911473.6

申请日：1991-05-17

Applicant: CARROT, Louis

Inventor： CARROT, Louis

IPC: B64C27/00 ,  B64C25/56 ,  B64D45/00

CPC classification number: B64C27/006 ,  B64C25/56 ,  B64D2201/00

Abstract: The device comprises an inflatable bag (1) attached to the underside (2.1) of the body of the helicopter (2), its upper portion being shaped to fit the whole of the underside (2.1) of said helicopter. When inflated and ready for use, said bag has the shape of a very large trapezoid and extends well beyond the space occupied by the helicopter itself, increasing the lift polygon. The sides of said bag are provided with anti-buckling reinforcing elements (4), and devices (3) for limiting controlling internal pressure.

公开(公告)号：EP0291355A2

公开(公告)日：1988-11-17

申请号：EP88304419.0

申请日：1988-05-16

Applicant: WOODVILLE POLYMER ENGINEERING LIMITED

Inventor： Broadhurst, Jeffrey Charles

IPC: B60V3/08

CPC classification number: B60V3/08 ,  B64D2201/00

Abstract: Auxiliary landing equipment for aircraft which comprises a plurality of inflatable cushions (4) arranged in a predetermined array relative to each other and means (10) for securing them to the aircraft (1) so that, in an inflated state, the cushions (4) can contact the ground during landing or on take-off and so that, in a deflated state, the equipment can closely follow the contour of the aircraft part to which it is attached.

Abstract translation: 用于飞机的辅助着陆设备，其包括相对于彼此以预定阵列布置的多个可充气垫子（4）和用于将其固定到飞行器（1）的装置（10），使得在充气状态下，垫子（4） ）可以在着陆或起飞时接触地面，从而在收缩状态下，设备可以紧密跟随其附接的飞机部件的轮廓。

公开(公告)号：US12036937B2

公开(公告)日：2024-07-16

申请号：US17535087

申请日：2021-11-24

Applicant: SCHROTH SAFETY PRODUCTS LLC

Inventor： Patrick Akoma ,  Manuel Marroquin ,  Kasey Garces

IPC: B60R21/18 ,  B60R21/231 ,  B64D11/06 ,  B60R21/00 ,  B60R21/233

CPC classification number: B60R21/18 ,  B60R21/231 ,  B64D11/06205 ,  B60R2021/0004 ,  B60R2021/0009 ,  B60R2021/0093 ,  B60R2021/23107 ,  B60R2021/23308 ,  B64D2201/00

Abstract: A lap expanding reactionary airbag apparatus includes separate expanding lap and chest portions of the airbag. When loaded in a frontal or oblique crash event, the two portions act as a reactionary surface against each other, reducing the chest velocity of a vehicle occupant, thereby reducing the forward movement of the occupant. This restriction in forward movement results in reduced lumbar injuries.