公开(公告)号：US5335884A

公开(公告)日：1994-08-09

申请号：US54925

申请日：1993-04-28

Applicant: Rober C. Kalberer ,  Kevin W. Kreutzer

Inventor： Rober C. Kalberer ,  Kevin W. Kreutzer

IPC: B60R21/00 ,  B60R21/16 ,  B60R21/203 ,  B64D25/02 ,  B64D25/00

CPC classification number: B64D25/02 ,  B60R2021/0093 ,  B60R2021/23107 ,  B64D2201/00

Abstract: Airbags are positioned relative to an aircraft yoke so as to minimize undesired force application to that yoke upon actuation thereof. The airbag actuation is accomplished by sensors which are capable of responding to multiple traumatic forces upon the aircraft to either establish multiple actuation of a common airbag, or actuation of separate airbags, upon occurrence of each event. The airbags can assume a side lobe configuration so as to minimize the possibility of impact upon side posts, or the interior side of the aircraft cabin structure. The sensors are arranged in an array with common directional alignment for maximizing probability of appropriate actuation. Use of multiple sensors and majority voting circuitry enhances the reliability of the systems and process. The airbag container is mounted on the control yoke post to allow relatively free motion in a direction generally parallel to the direction of motion of the craft while retaining it against motion in any other direction thereby allowing the container to seek a balanced or neutral position independent of the position or movement of the yoke post.

Abstract translation: 安全气囊相对于飞机轭架定位，以便最小化对该轭架在致动时的不期望的力施加。 安全气囊致动由传感器完成，传感器能够响应飞机上的多次创伤力，以便在每次事件发生时建立公共安全气囊的多次致动或单独安全气囊的致动。 安全气囊可以采用旁瓣构造，以便最小化对侧柱或飞机机舱结构的内侧的冲击的可能性。 传感器以具有共同定向对准的阵列布置，以最大化适当致动的概率。 使用多个传感器和多数投票电路可以提高系统和过程的可靠性。 安全气囊容器安装在控制轭架上，以允许在大致平行于飞行器的运动方向的方向上相对自由运动，同时保持其抵抗任何其它方向的运动，从而允许容器寻求平衡或中立位置，独立于 轭架的位置或运动。

公开(公告)号：US5301902A

公开(公告)日：1994-04-12

申请号：US973798

申请日：1992-11-09

Applicant: Robert C. Kalberer ,  Kevin W. Kreutzer

Inventor： Robert C. Kalberer ,  Kevin W. Kreutzer

IPC: B60R21/00 ,  B60R21/16 ,  B60R21/203 ,  B64D25/02 ,  B64D11/06

CPC classification number: B64D25/02 ,  B60R2021/0093 ,  B60R2021/23107 ,  B64D2201/00

Abstract: Airbags are positioned relative to an aircraft yoke so as to minimize undesired force application to that yoke upon actuation thereof. The airbag actuation is accomplished by sensors which are capable of responding to multiple traumatic forces upon the aircraft to either establish multiple actuations of a common airbag, or actuation of separate airbags, upon occurrence of each event. The airbags can assume a side lobe configuration so as to minimize the possibility of impact upon side posts, or the interior side of the aircraft cabin structure. The sensors are arranged in an array with common directional alignment for maximizing probability of appropriate actuation. Use of multiple sensors and majority voting circuitry enhances the reliability of the systems and process.

Abstract translation: 安全气囊相对于飞机轭架定位，以便最小化对该轭架在致动时的不期望的力施加。 安全气囊致动由传感器完成，该传感器能够响应飞机上的多次创伤力，以在每次事件发生时建立普通气囊的多次致动或单独安全气囊的致动。 安全气囊可以采用旁瓣构造，以便最小化对侧柱或飞机机舱结构的内侧的冲击的可能性。 传感器以具有共同定向对准的阵列布置，以最大化适当致动的概率。 使用多个传感器和多数投票电路可以提高系统和过程的可靠性。

公开(公告)号：US5279199A

公开(公告)日：1994-01-18

申请号：US929356

申请日：1992-08-14

Applicant: Henry August

Inventor： Henry August

IPC: B64D7/08 ,  F41F3/06 ,  B64D1/04

CPC classification number: F41F3/06 ,  B64D7/08 ,  B64D2201/00

Abstract: A technique and apparatus for rearward launch of a missile. The inventive apparatus (10) includes a launch tube (12) in which the missile (14) is mounted with the forward end of the missile being mounted at the forward end (16) of the tube. The rearward end of the launch tube is sealed with a break-away material (18) prior to expulsion of the missile (14). An expulsion mechanism expels the missile in a rearward direction from the launch tube. The expulsion mechanism includes an airbag (20) and a pressurization mechanism (30). The airbag (20) includes a bra (22) for maintaining the orientation of the missile (14) during the expulsion thereof. The airbag (20) also includes a metallized enclosure (24) for sealing the launch tube (14) after the expulsion of the missile (14).

Abstract translation: 用于向后发射导弹的技术和装置。 本发明的装置（10）包括发射管（12），其中安装有导弹（14），其中导弹的前端安装在管的前端（16）处。 在排出导弹（14）之前，用分离材料（18）密封发射管的后端。 排出机构从发射管沿向后的方向排出导弹。 排出机构包括气囊（20）和加压机构（30）。 气囊（20）包括用于在排出导弹（14）的过程中保持导弹（14）的取向的胸罩（22）。 气囊（20）还包括用于在导弹（14）被驱逐之后密封发射管（14）的金属化外壳（24）。

公开(公告)号：US5162006A

公开(公告)日：1992-11-10

申请号：US716749

申请日：1991-06-18

Applicant: Sylvester E. Yandle, II

Inventor： Sylvester E. Yandle, II

IPC: A62B7/02 ,  A62B99/00 ,  B60R21/18 ,  B63C9/125 ,  B63C11/22 ,  B64D10/00 ,  B64D25/00

CPC classification number: A62B99/00 ,  A62B7/02 ,  B60R21/18 ,  B63C11/22 ,  B63C9/1255 ,  B64D10/00 ,  B64D25/00 ,  B64D2201/00 ,  B64D2231/025

Abstract: A portable safety vest (20) includes an inflatable collar (22) which functions as a personal floatation device, a transparent, inflatable air bag (50), and an air mask (60). A cylinder of compressed air (40) has a seal (41) and, when the seal (41) is broken by a triggering mechanism (42, 43, 44), the compressed air expands and fills the air bag (50) and the collar (22). The air bag (50) is preferably large enough to hold at least a two-minute supply of air to allow one time to escape from an area filled with smoke or noxious or toxic gas.

Abstract translation: 便携式安全背心（20）包括用作个人漂浮装置的充气套环（22），透明的可充气气囊（50）和空气罩（60）。 压缩空气（40）的气缸具有密封件（41），并且当密封件（41）被触发机构（42,43,44）打破时，压缩空气膨胀并填充气囊（50） 衣领（22）。 安全气囊（50）优选地足够大以容纳至少两分钟的空气供应，以允许一次从充满烟雾或有毒气体的区域逸出。

公开(公告)号：US4565535A

公开(公告)日：1986-01-21

申请号：US632049

申请日：1984-07-18

Applicant: Tomas Tassy

Inventor： Tomas Tassy

IPC: B60R21/18 ,  A62B35/00 ,  B60R21/00 ,  B60R21/16 ,  B60R21/207 ,  B60R21/231 ,  B64D25/02

CPC classification number: B60R21/207 ,  B60R21/16 ,  B64D11/06205 ,  B64D25/02 ,  B60R2021/0004 ,  B60R2021/0093 ,  B60R2021/23107 ,  B60R2021/23153 ,  B64D2201/00

Abstract: The improved device includes a hollow container with latched door, inside of which is coiled an inflatable, body contoured gas bag releasably connected to the container and gravity deployable through the door. The device includes valves, conduits and the like to automatically or manually inflate and deflate the bag. The container is adapted to fit into the back of an airliner seat and when in that position and inflated acts as an effective crash barrier for a passenger sitting behind the bag. A strap or the like is also provided for releasably securing the bag to a person as a flotation device when the need arises. Therefore, the bag serves a dual function. The bag, when inflated, includes an upper horizontal portion with head-receiving opening and a vertical lower portion with end panel sides adapted to receive a passengers upper torso. The bag can include two sections releasably secured front to back, both of which act as the crash barrier and one of which acts as an individual flotation device. The device is simple and effective.

Abstract translation: 改进的装置包括具有锁定门的中空容器，其内部卷绕有可释放地连接到容器的可膨胀的身体轮廓的气囊，并且可通过门重力展开。 该装置包括阀，管道等以自动或手动地使袋充气和放气。 该容器适于装配到客机座椅的后部，并且当处于该位置并且充气时，其作为座椅后面的乘客的有效碰撞障碍。 还提供了一种带子或类似物，用于在需要时可释放地将袋子固定到作为浮选装置的人身上。 因此，该袋具有双重功能。 袋子在膨胀时包括具有头部接纳开口的上部水平部分和具有适于接收乘客上部躯干的端部面板侧面的垂直下部部分。 该袋可以包括两个可拆卸地前后固定的部分，两个部分用作碰撞障碍物，其中一个部分充当单独的浮选装置。 该设备简单有效。

公开(公告)号：US1640270A

公开(公告)日：1927-08-23

申请号：US9282626

申请日：1926-03-06

Applicant: RUSSELL FURMAN WILLIAM

Inventor： RUSSELL FURMAN WILLIAM

IPC: B64D10/00

CPC classification number: B64D10/00 ,  A41D2400/14 ,  B64D2201/00 ,  Y10S128/20

公开(公告)号：US12116141B2

公开(公告)日：2024-10-15

申请号：US17545566

申请日：2021-12-08

Applicant: Eaton Intelligent Power Limited

Inventor： Jeffrey A. Baker ,  Mario F. Cruz ,  David R. Smit ,  Derek Paul Dougherty

IPC: B64D41/00

CPC classification number: B64D41/00 ,  B64D2201/00 ,  B64D2221/00

Abstract: An aircraft emergency power unit (EPU) includes a battery powered subsystem that replaces toxic hydrazine fuel use. The battery of the battery powered subsystem is utilized to supply power to an aircraft electrical system in the event of a failure of the EPU turbine-powered generator. The battery of the battery powered subsystem is also utilized to supply power to an electric hydraulic motor pump in the event of a failure of the EPU turbine-powered hydraulic pump (or to augment the output of the EPU-turbine-powered hydraulic pump). The battery of the battery powered subsystem is capable of simultaneously powering the electrical system and the electric hydraulic motor pump or of powering either one of the electrical system and electric hydraulic motor pump independently based upon aircraft fault conditions. Intermittent operation of the electrical system and/or the electric hydraulic motor pump in an intermittent fashion on an as-needed basis is also possible.

公开(公告)号：US12097964B2

公开(公告)日：2024-09-24

申请号：US16517119

申请日：2019-07-19

Applicant: Bertil Werjefelt ,  Alexander Werjefelt

Inventor： Bertil Werjefelt ,  Alexander Werjefelt

IPC: B64D25/00

CPC classification number: B64D25/00 ,  B64D2201/00

Abstract: An emergency vision system includes a housing; an inflatable main enclosure having an inflated state and a deflated state, the main enclosure in the deflated state is disposed in the housing, the main enclosure in the inflated state is configured to be stationarily disposed between a user and a source of information required to be seen by the user during a smoke emergency; and a movable hand-held enclosure having an inflated state and a deflated state, the hand-held enclosure in the deflated state is disposed in the housing, the hand-held enclosure in the inflated state is configured to be used by the user to view a second source of information not visible through the main inflatable enclosure.

公开(公告)号：US20240111301A1

公开(公告)日：2024-04-04

申请号：US17936476

申请日：2022-09-29

Applicant: International Business Machines Corporation

Inventor： Tushar Agrawal ,  Sarbajit K. Rakshit ,  Jeremy R. Fox

IPC: G05D1/10 ,  B64C39/02 ,  G06Q10/08

CPC classification number: G05D1/101 ,  B64C39/024 ,  G06Q10/0832 ,  B64C2201/128 ,  B64C2201/143 ,  B64D2201/00

Abstract: Managing a package delivery system deploying an unmanned vehicle including an inflatable unit for reducing package vibration in a transportation vehicle. Package data is received at a computer, and the package data includes package descriptions. Spatial positioning of the packages in the transport space is tracked to determine, spatial positioning changes between the packages in the transport space based on the package data received at the computer and the transport. One or more unmanned vehicles are delivered to the transport space based on the spatial positioning changes in the transport space, and the unmanned vehicles including inflatable units. The inflatable units are deployed in the transport space by inflating the inflatable units at locations in the transport space based on the spatial positioning changes to discourage package movement in the transport space.

公开(公告)号：US11780586B2

公开(公告)日：2023-10-10

申请号：US17009079

申请日：2020-09-01

Applicant: US Gov't as represented by Secretary of Air Force

Inventor： Jerry Provenza

IPC: B64D11/06 ,  B60R21/00 ,  B60R21/01 ,  B60R21/0132 ,  B60R21/0136 ,  B60R21/203 ,  B60R21/207 ,  B60R21/231 ,  B60R21/26 ,  B60R21/015

CPC classification number: B64D11/0621 ,  B60R21/0132 ,  B60R21/0136 ,  B60R21/01516 ,  B60R21/203 ,  B60R21/207 ,  B60R21/231 ,  B60R21/26 ,  B60R2021/0093 ,  B60R2021/01013 ,  B60R2021/01231 ,  B60R2021/2078 ,  B60R2021/23107 ,  B64D2201/00

Abstract: An adaptive force vehicle airbag (AFVA) system includes airbag(s) stowed in a compressed state within an interior of a vehicle. An impact sensor detects a change in motion of the vehicle indicative of a collision. Selectable force gas generator(s) (SFGGs) gas-generating propellant cells that are individually fired. The SFGGs have conduit(s) that receive gas from fired gas-generating propellant cells and direct the gas to inflate at least one of the airbag(s). A controller is communicatively coupled to the inflation initiating component and the gas-generating propellant cells of the SFGGs. The controller enables the AFVA system to: (i) receive an inflation signal from the impact sensor; and (ii) fire a selected number of the gas-generating propellant cells to at least partially inflate the at least one airbag.