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公开(公告)号：US09428132B2
公开(公告)日：2016-08-30
申请号：US13912937
申请日：2013-06-07
申请人： Zodiac Seats France
发明人： Jean-Marc Obadia , John Payne , Jeremy Cailleteau , Nick Lee , Nathan Kwok , Jean-Marie Daout , Jake Story , David Knox
CPC分类号： B60R21/20 , B60R2021/0093 , B64D11/00 , B64D25/02 , B64D2201/00
摘要： An airbag system assembly configured to be positioned in the interior of a vehicle that includes an aft wall configured to be positioned forward of a passenger seat and an airbag system. The aft wall includes front and aft surfaces and the aft wall includes a first flap that is formed by a plurality of weakness lines in at least the front surface thereof. The airbag system includes at least a first airbag module having a first airbag support plate with front and aft surfaces. The first airbag support plate is secured to the front surface of the aft wall, and the first airbag support plate includes a first airbag that is configured to deploy in the event of a crash condition and that is disposed on the aft surface of the first airbag support plate. The first airbag is positioned adjacent the first flap.
摘要翻译： 一种安全气囊系统组件，其构造成定位在车辆内部，所述气囊系统组件包括构造成位于乘客座椅前方的后壁和气囊系统。 后壁包括前表面和后表面，并且后壁包括在至少其前表面中由多条弱线形成的第一挡板。 所述安全气囊系统至少包括具有前后表面的第一气囊支撑板的第一气囊模块。 第一安全气囊支撑板固定在后壁的前表面上，第一安全气囊支撑板包括第一气囊，其构造成在碰撞状态下展开并且设置在第一气囊的后表面上 支撑板 第一安全气囊邻近第一挡板定位。
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公开(公告)号：US20160244173A1
公开(公告)日：2016-08-25
申请号：US15143090
申请日：2016-04-29
CPC分类号： B64D25/06 , B60R21/18 , B60R2021/0093 , B64D11/062 , B64D11/06205 , B64D2201/00 , Y10T442/2656 , Y10T442/2672 , Y10T442/2721
摘要： The present invention discloses embodiments of an apparatus, systems and related methods for side-facing occupant protection in an aircraft during an abrupt stop—such as in a forward-facing crash event. Embodiments of the present invention disclose a three point air belt that provide superior passenger comfort and retractability, due to inventive construction, by providing enhanced flexibility of the three-point air belt, and more specifically, the shoulder harness portion. The present invention first includes a new airbag material which contributes to the enhanced flexibility, namely, a polyester textile structure treated with a phosphate-phosphonate compound. In further embodiments the material is the coated in a polyurethane mixture. The present invention also includes a new method of compacting the airbag such that it may be disposed in a shoulder harness while remaining substantially unobtrusive and comfortable to a passenger. The invention also includes a new containment material, namely a tubular webbing, to further enhance the flexibility of the shoulder harness over the prior art which generally comprises leather or leather-approximations. The result of the invention also provides enhanced retractability over the prior art, such that the three-point harness may be more easily stowed relative to the prior art.
摘要翻译： 本发明公开了在突然停止期间（例如在前向碰撞事件中）在飞行器中侧面乘员保护的装置，系统和相关方法的实施例。 本发明的实施例公开了一种三点式气动带，其通过提供三点式气动带，更确切地说是肩带配件部分的增强的灵活性，由于本发明的结构，提供了出众的乘客舒适性和伸缩性。 本发明首先包括有助于提高柔性的新型气囊材料，即用磷酸酯 - 膦酸酯化合物处理的聚酯织物结构。 在另外的实施方案中，该材料被涂覆在聚氨酯混合物中。 本发明还包括一种压缩气囊的新方法，使得其可以设置在肩带上，同时对乘客基本上不引人注意并且舒适。 本发明还包括新的容纳材料，即管状织带，以进一步增强肩带的弹性，而现有技术通常包括皮革或皮革近似。 本发明的结果还提供了比现有技术更强的可缩回性，使得相对于现有技术，三点式线束可以更容易地收起。
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公开(公告)号：US09156558B2
公开(公告)日：2015-10-13
申请号：US13174659
申请日：2011-06-30
CPC分类号： B64D11/0621 , B64D11/062 , B64D11/06205 , B64D25/00 , B64D25/02 , B64D2201/00 , G07C5/0808 , G07C5/0841
摘要： An electronic module assembly (EMA) for use in controlling one or more personal restraint systems. A programmed processor within the EMA is configured to determine when a personal restraint system associated with each seat in a vehicle should be deployed. In addition, the programmed processor is configured to perform a diagnostic self-test to determine if the EMA and the personal restraint systems are operational. In one embodiment, results of the diagnostic self-test routine are displayed on a display included on the electronic module assembly. In an alternative embodiment, the results of the diagnostic self-test routine are transmitted via a wireless transceiver to a remote device. The remote device can include a wireless interrogator or can be a remote computer system such as a cabin management computer system.
摘要翻译： 一种用于控制一个或多个个人约束系统的电子模块组件（EMA）。 EMA内的编程处理器被配置为确定何时应该部署与车辆中的每个座椅相关联的个人约束系统。 此外，编程处理器被配置为执行诊断自检，以确定EMA和个人约束系统是否可操作。 在一个实施例中，诊断自检程序的结果被显示在包括在电子模块组件上的显示器上。 在替代实施例中，诊断自检程序的结果通过无线收发器传送到远程设备。 远程设备可以包括无线询问器，或者可以是诸如客舱管理计算机系统的远程计算机系统。
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公开(公告)号：US20100276540A1
公开(公告)日：2010-11-04
申请号：US12735176
申请日：2008-04-23
申请人： Camilo Garcia Rojo
发明人： Camilo Garcia Rojo
IPC分类号： B64D25/02 , B60R21/217
CPC分类号： B60R21/01 , B60R21/16 , B60R2021/0093 , B60R2021/23107 , B64D25/00 , B64D25/02 , B64D2201/00
摘要： The invention relates to an airbag system for aircraft, intended to protect crew and passengers. The system comprises: inflatable cushions; a supply of air from individual tanks, communal tanks and the aircraft APU; a connection to the landing gear and the altimeter; a manual switch; an approach and contact sensor enabling automatic activation; electric lines, electrovalves and air ducts. The system also includes a second version which is activated using electrochemical batteries which operate on the basis of sharp deceleration.
摘要翻译： 本发明涉及一种用于飞机的气囊系统，旨在保护船员和乘客。 该系统包括：充气垫; 来自各坦克，公共坦克和飞机APU的空气供应; 与起落架和高度计的连接; 手动开关; 一种能够自动激活的方法和接触式传感器; 电线，电动阀和风道。 该系统还包括使用基于急剧减速操作的电化学电池来激活的第二版本。
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公开(公告)号：US6073885A
公开(公告)日：2000-06-13
申请号：US72065
申请日：1998-05-04
CPC分类号： B64D25/02 , B64D11/0689 , B64D25/12
摘要： A crew systems module for providing normal ingress to and egress from an aircraft cockpit flight station includes a seat assembly for supporting a crew member and a shell which supports the seat assembly and is pivotally attached to the aircraft adjacent the cockpit. The shell is pivotal from a closed position placing the crew member in a flight-ready position to an ingress/egress position placing the crew member in a generally standing position. The shell in the ingress/egress position extends downward from the cockpit toward the ground. The shell preferably extends downward through the aircraft's wheel well which houses a folding or collapsible landing gear during flight. The crew systems module may be incorporated in a capsule which is separable from the aircraft in an emergency.
摘要翻译： 用于向飞行器驾驶舱飞行站提供正常进入和离开的船员系统模块包括用于支撑机组人员的座椅组件和支撑座椅组件的壳体，并且枢轴连接到与驾驶舱相邻的飞行器。 外壳从关闭位置枢转，将机组人员置于准备就绪的位置，将机组人员放置在大致站立的位置。 入口/出口位置的外壳从驾驶舱朝向地面向下延伸。 壳体优选地向下延伸穿过飞行器的车轮井，在飞行期间容纳折叠或可折叠起落架。 机组系统模块可以并入在紧急情况下可与飞行器分离的胶囊中。
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公开(公告)号：US5415366A
公开(公告)日：1995-05-16
申请号：US204860
申请日：1994-02-28
申请人： Bradley Mastrolia
发明人： Bradley Mastrolia
IPC分类号： B64D25/02 , B64D25/115
CPC分类号： B64D25/02
摘要： An arm restraint system for an ejection seat of an aircraft. The arm restraint system includes a pair of shrouds that are attached to the seat and each contain an outer channel. Extending through each outer channel is a corresponding strap that is coupled to the cockpit and fastened to a ring on the belt of the pilot. When the seat is ejected, the straps are pulled and the shrouds are deployed onto the arms of the pilot. The shrouds extend to a position which captures the wrists of the pilot, thereby preventing both sideward and upward movement of the arms.
摘要翻译： 一种用于飞机弹射座椅的手臂约束系统。 手臂约束系统包括一对护罩，其连接到座椅上并且各自包含外部通道。 通过每个外部通道延伸的是相应的皮带，其连接到驾驶舱并且紧固到飞行员皮带上的环上。 当座椅弹出时，带子被拉动，护罩部署在飞行员的臂上。 护罩延伸到捕获飞行员的手腕的位置，从而防止臂的侧向和向上移动。
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公开(公告)号：US5272422A
公开(公告)日：1993-12-21
申请号：US834878
申请日：1992-02-12
申请人： Raymond Beaussant
发明人： Raymond Beaussant
CPC分类号： A42B3/0473 , B64D10/00 , B64D25/02 , G02B23/16 , G02B27/0176 , G02B2027/0154 , G02B27/017
摘要： A head equipment comprises a component such as a helmet connectable to the head of a wearer and movable by the wearer in a limited field, with at least five degrees of freedom. It comprises an arm constituted by articulated segments giving the component at least five degrees of freedom with respect to the fixed structure and linking the component to a fixed structure.
摘要翻译： 头部设备包括诸如头盔的部件，其可连接到佩戴者的头部并且在有限的领域中可由穿着者移动，具有至少五个自由度。 它包括由铰接部分构成的臂，该部分相对于固定结构使组件具有至少五个自由度，并将部件连接到固定结构。
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公开(公告)号：US5026006A
公开(公告)日：1991-06-25
申请号：US313990
申请日：1989-02-22
CPC分类号： B64D25/00 , B64D2011/0046
摘要： Safety enclosures for use in high speed vehicles such as aircraft and high speed trains. The safety enclosures include an enclosure shell which preferably has two shell walls separated by a crash resistant intermediate material which also provides thermal insulation against fires and acoustic attenuation. The enclosures also advantageously include cooling systems which utilize a refrigerant which is expanded through tubes connected along the inner wall of the enclosure shell. A compressed air supply is provided which supplies breathing air to passengers and is used to expand a crash bag. Air is supplied through both the crash bag at passenger contacting panels and through supply lines which exhaust near the passengers' heads. A motor driven door assembly is controlled to close as the crash bag is being deployed. Exhaust ports having check valves allow positive pressure to be maintained in the cabin of the enclosures to exclude smoke and fire. Passenger seating is provided which includes a dual shoulder harness restraint which is supplemented by the crash bag system. Seating includes a number of features designed to reduce shock and inertial forces experienced by the passengers during crashes. The safety enclosures are provided in singular units and modular arrays having single rows and opposing muliple rows of passenger seats.
摘要翻译： 用于高速车辆如飞机和高速列车的安全外壳。 安全外壳包括外壳，其优选地具有由抗碰撞中间材料隔开的两个壳壁，其也提供防火和声衰减的热绝缘。 外壳还有利地包括利用通过沿着外壳的内壁连接的管而膨胀的制冷剂的冷却系统。 提供压缩空气供应，为乘客提供呼吸空气，并用于扩大碰撞袋。 空气通过乘客接触板上的碰撞袋和乘客头部附近排放的供应管线供应。 电动机驱动的门组件被控制为随着碰撞袋的展开而关闭。 具有止回阀的排气口允许在机壳的舱室内保持正压以排除烟雾和火灾。 提供乘客座椅，其中包括一个双肩带束缚，其由救护袋系统补充。 座椅包括许多功能，旨在减少乘客在碰撞期间遇到的冲击和惯性力。 安全外壳设置有单列和单排和相对的多排乘客座椅的模块阵列。
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公开(公告)号：US4923147A
公开(公告)日：1990-05-08
申请号：US249794
申请日：1988-09-27
CPC分类号： A42B3/0473 , B64D25/02 , B64D25/10
摘要： A seat insert insertable within the existing seat of a vehicle for maintaining a crew member of the vehicle in a forward posture during high G acceleration. An elongated head support member is provided for supporting the crew member's head during a forward leaning posture. A back plate assembly including at least one back plate is connected to the head support member for supporting the spine in its natural curvature. Means being connected to the back plate assembly are provided for pivoting the back plate assembly forward relative to the seat of the vehicle. Means are provided for transfering any G-induced weight from the spine to the back plate assembly and ultimately to the existing seat of the vehicle. The head support member is restrained in such a manner so as to maintain the crew member's head in an "eyes up" attitude during a forward lean. The seat insert reduces the risk of spinal injury by off-loading the pilot's spine and supporting the spine in its natural curvature, thereby preventing harmful bending of the spine and non-uniform load distribution across individual vertebrae interfaces.
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公开(公告)号：US4899961A
公开(公告)日：1990-02-13
申请号：US212572
申请日：1988-06-28
申请人： Gerald F. Herndon
发明人： Gerald F. Herndon
IPC分类号： A47C7/38 , B64D25/02 , B64D25/04 , B64D25/115
CPC分类号： B64D25/02
摘要： A lateral head restraint system providing support to a pilot's head during ejection or high-acceleration flight maneuvers. The lateral head restraint system includes inflating bladders positioned on opposite sides of a pilot's head. The bladders inflate from a compressed wedge position, sweeping through an arc on each side of the headrest structure. Inflation of the bladders centers the pilot's head into the correct control position and restricts lateral movement. When fully inflated, the bladders permit the pilot to lean forward or turn his head to either side. Further, an unobstructed field of vision is provided. The lateral head restraint system is incorporated into the ejection seat and remains fully operational during the ejection procedure to protect the pilot's head from injury.
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