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公开(公告)号：US08474753B2
公开(公告)日：2013-07-02
申请号：US13125884
申请日：2009-07-27
申请人： Andrew T. Hill , Michael R. Smith , Zi Lu , Cheng-Ho Tho
发明人： Andrew T. Hill , Michael R. Smith , Zi Lu , Cheng-Ho Tho
IPC分类号： B64C25/56
CPC分类号： B64D25/00 , B64C27/04 , B64D2201/00
摘要： 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.
摘要翻译： 用于飞行器的碰撞衰减系统包括由飞机携带的气囊，该气囊大体上邻近飞行器的外部可充气。 气囊与至少一个通气通道流体连通，用于将气体从气囊的内部引导到气囊外部的区域，允许气体逸出而不被气囊阻挡。 气体源与气囊的内部流体连通，以使气囊膨胀。 在排气通道内设有排气阀，用于控制通过通气通道的气体流，从而控制气囊的放气。 排气阀可连续调节到打开状态，关闭状态和任何数量的部分打开状态之间。
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公开(公告)号：US20130062465A1
公开(公告)日：2013-03-14
申请号：US13696970
申请日：2011-02-23
申请人： Andrew T. Hill , Zi Lu , Robert S. Lynds , Andrew R. Hansen
发明人： Andrew T. Hill , Zi Lu , Robert S. Lynds , Andrew R. Hansen
CPC分类号： B64D25/00 , B64C25/52 , B64C2025/325 , B64D2201/00
摘要： 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.
摘要翻译： 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。
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公开(公告)号：US20110204181A1
公开(公告)日：2011-08-25
申请号：US13125884
申请日：2009-07-27
申请人： Andrew T. Hill , Michael R. Smith , Zi Lu , Cheng-Ho Tho
发明人： Andrew T. Hill , Michael R. Smith , Zi Lu , Cheng-Ho Tho
IPC分类号： B64C25/56
CPC分类号： B64D25/00 , B64C27/04 , B64D2201/00
摘要： 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.
摘要翻译： 用于飞行器的碰撞衰减系统包括由飞机携带的气囊，该气囊大体上邻近飞行器的外部可充气。 气囊与至少一个通气通道流体连通，用于将气体从气囊的内部引导到气囊外部的区域，允许气体逸出而不被气囊阻挡。 气体源与气囊的内部流体连通，以使气囊膨胀。 在排气通道内设有排气阀，用于控制通过通气通道的气体流，从而控制气囊的放气。 排气阀可连续调节到打开状态，关闭状态和任何数量的部分打开状态之间。
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公开(公告)号：US20120101666A1
公开(公告)日：2012-04-26
申请号：US13380925
申请日：2009-07-27
CPC分类号： B64D25/00 , B64D2201/00
摘要： An occupant protection system for an aircraft comprising a sensor system for sensing flight condition information and a control system, which includes an impending crash detection system and an impact detection system. The impending crash detection system receives flight information from the sensors determines whether a crash is likely to occur. If an impending crash is detected, the impending crash detection system activates impact modes of a first group of aircraft systems. The impact detection system receives flight information from the sensor system and determines whether an impact has occurred or is occurring. If an impact is detected, the impact detection system activates impact modes of a second group of aircraft systems.
摘要翻译： 一种用于飞行器的乘员保护系统，包括用于感测飞行情况信息的传感器系统和包括即将发生的碰撞检测系统和冲击检测系统的控制系统。 即将发生的碰撞检测系统从传感器接收飞行信息，确定是否可能发生碰撞。 如果检测到即将发生的碰撞，即将发生的碰撞检测系统激活第一组飞行器系统的冲击模式。 冲击检测系统从传感器系统接收飞行信息，并确定影响是否发生或正在发生。 如果检测到冲击，冲击检测系统激活第二组飞行器系统的冲击模式。
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公开(公告)号：US5377940A
公开(公告)日：1995-01-03
申请号：US34347
申请日：1993-03-19
申请人： Carlton L. Cabe , Andrew T. Hill
发明人： Carlton L. Cabe , Andrew T. Hill
CPC分类号： F16L3/1233 , F16L3/23 , H02G3/32
摘要： A clamp for retaining electrical wires, fluid conduits or the like has restraining means adjacent to the inner ends of the clamp's legs. When the clamp is closed, the hook of a hook-shaped member adjacent to the upper leg passes through a slot adjacent to the lower leg and engages the outer surface of the clamp, thereby retaining the clamp in the closed position.
摘要翻译： 用于保持电线，流体管道等的夹具具有邻近夹具腿的内端的约束装置。 当夹子闭合时，与大腿相邻的钩状构件的钩通过与小腿相邻的狭槽，并与夹具的外表面接合，从而将夹具保持在关闭位置。
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公开(公告)号：US09045222B2
公开(公告)日：2015-06-02
申请号：US13699758
申请日：2011-03-30
申请人： Zi Lu , Cheng-Ho Tho , Michael R. Smith , Andrew T. Hill , Samgeeth Rajan
发明人： Zi Lu , Cheng-Ho Tho , Michael R. Smith , Andrew T. Hill , Samgeeth Rajan
CPC分类号： B64C27/006 , B64D25/00 , B64D2201/00
摘要： The external crash attenuation airbag includes an inflatable bladder which is inflatable to an exterior of an aircraft, so that the inflatable bladder is generally located between the aircraft and a crash surface when inflated. The airbag includes a vent configured to burst at a predefined burst pressure, the vent being located along a side portion of the inflatable bladder. The airbag also includes a vent support located approximate the vent, the vent support being configured to prevent deformation and therefore maintain the effectiveness of a venting area of the vent, and the vent support being rigid and annular and includes an upper portion and a lower portion that are hinged together around the vent.
摘要翻译： 外部碰撞衰减安全气囊包括可膨胀到飞机外部的可膨胀气囊，使得充气气囊通常位于飞行器和膨胀时的碰撞表面之间。 安全气囊包括通气孔，其构造成以预定的突发压力爆裂，所述排气口沿着可充气气囊的侧部分定位。 安全气囊还包括靠近通气口的通气支架，排气口支架构造成防止变形并因此保持通气口通气区域的有效性，并且排气支架是刚性和环形的并且包括上部和下部 它们围绕通风口铰接在一起。
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公开(公告)号：US08588996B2
公开(公告)日：2013-11-19
申请号：US13380925
申请日：2009-07-27
IPC分类号： G05D3/00
CPC分类号： B64D25/00 , B64D2201/00
摘要： An occupant protection system for an aircraft comprising a sensor system for sensing flight condition information and a control system, which includes an impending crash detection system and an impact detection system. The impending crash detection system receives flight information from the sensors determines whether a crash is likely to occur. If an impending crash is detected, the impending crash detection system activates impact modes of a first group of aircraft systems. The impact detection system receives flight information from the sensor system and determines whether an impact has occurred or is occurring. If an impact is detected, the impact detection system activates impact modes of a second group of aircraft systems.
摘要翻译： 一种用于飞行器的乘员保护系统，包括用于感测飞行情况信息的传感器系统和包括即将发生的碰撞检测系统和冲击检测系统的控制系统。 即将发生的碰撞检测系统从传感器接收飞行信息，确定是否可能发生碰撞。 如果检测到即将发生的碰撞，即将发生的碰撞检测系统激活第一组飞行器系统的冲击模式。 冲击检测系统从传感器系统接收飞行信息，并确定影响是否发生或正在发生。 如果检测到冲击，冲击检测系统激活第二组飞行器系统的冲击模式。
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公开(公告)号：US20130068883A1
公开(公告)日：2013-03-21
申请号：US13699758
申请日：2011-03-30
申请人： Zi Lu , Cheng-Ho Tho , Michael R. Smith , Andrew T. Hill , Samgeeth Rajan
发明人： Zi Lu , Cheng-Ho Tho , Michael R. Smith , Andrew T. Hill , Samgeeth Rajan
IPC分类号： B60R21/239 , B64C25/56
CPC分类号： B64C27/006 , B64D25/00 , B64D2201/00
摘要： The external crash attenuation airbag includes an inflatable bladder which is inflatable to an exterior of an aircraft, so that the inflatable bladder is generally located between the aircraft and a crash surface when inflated. The airbag includes a vent configured to burst at a predefined burst pressure, the vent being located a side portion of the inflatable bladder. The airbag also includes a vent support located approximate the vent, the vent support being configured to prevent deformation and therefore maintain the effectiveness of a venting area of the vent.
摘要翻译： 外部碰撞衰减安全气囊包括可膨胀到飞机外部的可膨胀气囊，使得充气气囊通常位于飞行器和膨胀时的碰撞表面之间。 安全气囊包括通气孔，其被构造成以预定的突发压力爆裂，通气口位于可膨胀气囊的侧部。 安全气囊还包括靠近通气口的排气口支架，排气口支撑件构造成防止变形并因此保持排气口通气区域的有效性。
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公开(公告)号：US09487301B2
公开(公告)日：2016-11-08
申请号：US13696970
申请日：2011-02-23
申请人： Andrew T. Hill , Zi Lu , Robert S. Lynds , Andrew R. Hansen
发明人： Andrew T. Hill , Zi Lu , Robert S. Lynds , Andrew R. Hansen
CPC分类号： B64D25/00 , B64C25/52 , B64C2025/325 , B64D2201/00
摘要： 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.
摘要翻译： 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。
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