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公开(公告)号：US20200039667A1
公开(公告)日：2020-02-06
申请号：US16596885
申请日：2019-10-09
申请人： The Boeing Company
发明人： Justin G. Albright , John R. McCann
IPC分类号： B64G1/62
摘要： A landing inflation system may include a compressed gas source, an airbag assembly fluidly coupled to the compressed gas source and configured to receive compressed gas, and a command processor configured to: (1) generate an inflation initiation command signal in response to an initiation signal, (2) generate an inflation cessation command signal in response to a nominal fill pressure signal, and (3) generate a vent command signal in response to an impact pressure signal.
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公开(公告)号：US20160298948A1
公开(公告)日：2016-10-13
申请号：US14685585
申请日：2015-04-13
申请人： The Boeing Company
CPC分类号： F42B15/36 , B64D1/02 , F02K9/976 , F05D2260/311 , F42B15/10
摘要： A rocket comprises at least one propulsion unit including a pivotable rocket motor, a spring-assisted one-time deployment mechanism, and a release mechanism. The pivotable rocket motor is pivotable between a stowed position and a deployed position. The spring-assisted one-time deployment mechanism moves the rocket motor from the stowed position to the deployed position when the deployment mechanism is released by the release mechanism. Outer geometry of the rocket is changed as the rocket motor is moved to the deployed position.
摘要翻译： 火箭包括至少一个包括可枢转火箭发动机，弹簧辅助一次性部署机构和释放机构的推进单元。 可枢转的火箭发动机可以在收起位置和展开位置之间枢转。 当释放机构释放展开机构时，弹簧辅助的一次性部署机构将火箭发动机从收起位置移动到展开位置。 当火箭发动机移动到展开位置时，火箭的外部几何形状发生变化。
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公开(公告)号：US11155370B2
公开(公告)日：2021-10-26
申请号：US16596885
申请日：2019-10-09
申请人： The Boeing Company
发明人： Justin G. Albright , John R. McCann
摘要： A landing inflation system may include a compressed gas source, an airbag assembly fluidly coupled to the compressed gas source and configured to receive compressed gas, and a command processor configured to: (1) generate an inflation initiation command signal in response to an initiation signal, (2) generate an inflation cessation command signal in response to a nominal fill pressure signal, and (3) generate a vent command signal in response to an impact pressure signal.
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公开(公告)号：US10094646B2
公开(公告)日：2018-10-09
申请号：US14685585
申请日：2015-04-13
申请人： The Boeing Company
摘要： A rocket comprises at least one propulsion unit including a pivotable rocket motor, a spring-assisted one-time deployment mechanism, and a release mechanism. The pivotable rocket motor is pivotable between a stowed position and a deployed position. The spring-assisted one-time deployment mechanism moves the rocket motor from the stowed position to the deployed position when the deployment mechanism is released by the release mechanism. Outer geometry of the rocket is changed as the rocket motor is moved to the deployed position.
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公开(公告)号：US10479533B2
公开(公告)日：2019-11-19
申请号：US14668589
申请日：2015-03-25
申请人： The Boeing Company
发明人： Justin G. Albright , John R. McCann
摘要： A landing inflation system may include a compressed gas source, an airbag assembly fluidly coupled to the compressed gas source and configured to receive compressed gas, and a command processor configured to: (1) generate an inflation initiation command signal in response to an initiation signal, (2) generate an inflation cessation command signal in response to a nominal fill pressure signal, and (3) generate a vent command signal in response to an impact pressure signal.
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公开(公告)号：US20160280400A1
公开(公告)日：2016-09-29
申请号：US14668589
申请日：2015-03-25
申请人： The Boeing Company
发明人： Justin G. Albright , John R. McCann
IPC分类号： B64G1/62
CPC分类号： B64G1/62 , B64G2001/224
摘要： A landing inflation system may include a compressed gas source, an airbag assembly fluidly coupled to the compressed gas source and configured to receive compressed gas, and a command processor configured to: (1) generate an inflation initiation command signal in response to an initiation signal, (2) generate an inflation cessation command signal in response to a nominal fill pressure signal, and (3) generate a vent command signal in response to an impact pressure signal.
摘要翻译： 着陆充气系统可以包括压缩气体源，气体组合件，其流体耦合到压缩气体源并且被配置为接收压缩气体;以及命令处理器，其配置为：（1）响应于起始信号产生充气起始指令信号 ，（2）响应于标称填充压力信号产生通气停止命令信号，和（3）响应于冲击压力信号产生通气指令信号。
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