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公开(公告)号：US12036937B2
公开(公告)日：2024-07-16
申请号：US17535087
申请日：2021-11-24
发明人： Patrick Akoma , Manuel Marroquin , Kasey Garces
IPC分类号： B60R21/18 , B60R21/231 , B64D11/06 , B60R21/00 , B60R21/233
CPC分类号： B60R21/18 , B60R21/231 , B64D11/06205 , B60R2021/0004 , B60R2021/0009 , B60R2021/0093 , B60R2021/23107 , B60R2021/23308 , B64D2201/00
摘要： 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.
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公开(公告)号：US20180127102A1
公开(公告)日：2018-05-10
申请号：US15727985
申请日：2017-10-09
发明人： Charles W. Clarke
IPC分类号： B64D25/00
CPC分类号： B64D25/00 , B64C27/006 , B64D2201/00
摘要： An airbag system includes a VTOL aircraft fuselage having an airbag compartment defined within the fuselage. A protective cover defines a portion of the exterior surface of the fuselage. The protective cover encloses at least a portion of the airbag compartment. An airbag is folded within the airbag compartment secured to a point on the fuselage. A method for deploying an airbag in an aircraft includes sending a signal to a gas generator to inflate at least one airbag secured within an airbag compartment within a fuselage of an aircraft. The method includes jettisoning off a protective cover from the airbag compartment. The method includes inflating the airbag with the gas generator to extend outside of the airbag compartment to attenuate forces and cushion the aircraft upon ground impact.
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公开(公告)号：US09944389B2
公开(公告)日：2018-04-17
申请号：US15476612
申请日：2017-03-31
IPC分类号： B64C37/00 , B64C29/00 , B60F5/02 , B64C11/00 , B64C27/08 , B64C27/20 , B64C27/22 , B64C27/57 , B64D17/80 , B64C39/02 , B64C3/56 , G05D1/10
CPC分类号： B64C37/00 , B60F5/02 , B64C3/385 , B64C3/56 , B64C11/001 , B64C25/58 , B64C27/08 , B64C27/20 , B64C27/22 , B64C27/32 , B64C27/52 , B64C27/57 , B64C29/00 , B64C29/0033 , B64C39/00 , B64C39/02 , B64D17/80 , B64D25/00 , B64D2201/00 , G05D1/102
摘要： An air module may be attached to a ground module. The air module may be equipped with a center of gravity effector to change the relative locations and hence the center of gravity of the air and ground modules when the modules are attached. The center of gravity effector may be active or passive or a combination of active and passive. The center of gravity effector may be combined with a center of lift effector to change the relative locations of the center of gravity and center of lift.
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公开(公告)号：US20180009541A1
公开(公告)日：2018-01-11
申请号：US15513566
申请日：2015-11-20
申请人： Ngoc Quy Pham
发明人： Ngoc Quy Pham
CPC分类号： B64D25/00 , B64C1/14 , B64D2201/00
摘要： The invention is about a powered airbag for planes in case of uncontrollable falling which makes the plane fall vertically with the head up. The invention includes the bonnet cover of the head 1, the hinges of the bonnet cover 17, the head cover of the plane 12, the structural frame of the head the plane 13, the container of gas-creating material 8, Valve to activate the airbag 9. There is a difference that the structural frame of the head of the plane 13 has a powered airbag 11, the flexible soft tube 10 which connects the powered airbag 11 to the frame of the head of the plane 13
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5.发明申请公开(公告)号：US20170235018A1
公开(公告)日：2017-08-17
申请号：US15401999
申请日：2017-01-09
CPC分类号： G01V99/005 , B64C39/024 , B64C2201/123 , B64C2201/127 , B64D17/80 , B64D45/00 , B64D47/08 , B64D2201/00 , G05D1/0094 , G05D1/101 , G06F3/04817 , G06F16/5866 , G06T7/70 , G06T2207/10032
摘要： A method comprising receiving aerial images captured by one or more unmanned aerial vehicle; receiving metadata associated with the aerial images captured by the one or more unmanned aerial vehicle; geo-referencing the aerial images based on a geographic location of a surface to determine geographic coordinates of pixels of the aerial images; receiving a geographic location from a user; retrieving one or more of the aerial images associated with the geographic location based on the determined geographic coordinates; and displaying to the user one or more overview image depicting the geographic location and overlaid with one or more icons indicative of and associated with the retrieved aerial images associated with the geographic location.
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公开(公告)号：US09725177B2
公开(公告)日：2017-08-08
申请号：US15050866
申请日：2016-02-23
申请人： AMI Industries, Inc.
CPC分类号： B64D11/0647 , A47C27/10 , B60N2/914 , B64D2201/00
摘要： A pressure control system for an aircraft seat includes a base plate and a plurality of cells attached to the base plate, each cell having a bellows and a top inflatable diaphragm and defines a pressure chamber therein. Charging apertures are formed in the base plate such that each cell has an associated charging aperture such that each charging aperture is in fluid communication with a pressure chamber. Discharging apertures are formed in the base plate such that each cell has an associated discharging aperture such that each discharging apertures is in fluid communication a pressure chamber. A charging valve and a discharging valve is in fluid communication with the pressure chambers and configured to supply or extract air to or from the chambers through the apertures. A pump is configured to supply pressurized air to the at least one charging valve.
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7.发明申请公开(公告)号：US20170203847A1
公开(公告)日：2017-07-20
申请号：US15002237
申请日：2016-01-20
申请人： AmSafe, Inc.
CPC分类号： B64D25/02 , B60R2021/0093 , B64D11/0619 , B64D11/062 , B64D11/06205 , B64D2201/00
摘要： Various embodiments of vehicle occupant safety systems having extendable restraints for use with, for example, airbags are described herein. In one embodiment, for example, the disclosed technology includes a 2-point occupant restraint that secures an occupant in an aircraft seat. In this embodiment, the aircraft seat is positioned in a seating area that includes a forward monument housing a stowed airbag. In the event of a crash or other significant dynamic event that causes, for example, a rapid deceleration of the aircraft above a preset magnitude, the airbag deploys between the occupant and the monument as the dynamic forces cause the occupant to pitch forward. The forward momentum of the occupant's body creates a significant tension load in the 2-point restraint, which causes the restraint to extend by a preset amount, thereby allowing the occupant to move forward in the seat more than the occupant would have moved had the occupant been wearing a conventional, non-extending 2-point restraint. Although the occupant is allowed to move forward, the occupant remains secured to the extended restraint by means of non-extending webbing that is secured around the waist of the occupant. Allowing the occupant to move forward in this manner enables the occupant's upper torso to impact the airbag at a reduced or otherwise more favorable angle. This can reduce both the speed and the angle at which the occupant's head impacts the airbag, thereby reducing the likelihood of injury.
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公开(公告)号：US20160318612A1
公开(公告)日：2016-11-03
申请号：US15143201
申请日：2016-04-29
IPC分类号： B64D11/06
CPC分类号： B64D11/06205 , B64D11/0619 , B64D11/062 , B64D2201/00 , Y10T442/2656 , Y10T442/2672 , Y10T442/2721
摘要： The present invention discloses embodiments of an apparatus, systems and related methods for occupant protection in an aircraft during an abrupt stop - such as in a forward-facing crash event. Embodiments of the present invention disclose a two point lap belt that provide superior passenger comfort and retractability, due to inventive construction, by providing enhanced flexibility of the two point lap belt, and more specifically, the extensible (non-static) 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 lap belt 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 two point lap belt may be more easily stowed relative to the prior art.
摘要翻译： 本发明公开了一种在突然停止期间飞机中的乘员保护的装置，系统和相关方法的实施例，例如在面向前的碰撞事件中。 本发明的实施例公开了一种双点腰带，其由于本发明的结构，通过提供两点腰带的更大的灵活性，更确切地说，是可伸展的（非静止的）部分，提供优越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，使得其可以设置在搭接皮带中，同时保持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超过现有技术的增强的收缩能力，使得相对于现有技术，两点腰带可以更容易地收起。
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公开(公告)号：US20160075447A1
公开(公告)日：2016-03-17
申请号：US14948220
申请日：2015-11-20
发明人： Mingyu Wang
CPC分类号： B64D25/00 , B64C25/32 , B64C25/54 , B64C25/56 , B64C39/024 , B64C2201/027 , B64D45/00 , B64D2201/00
摘要： An impact protection apparatus is provided, comprising a gas container configured to hold a compressed gas and an inflatable member configured to be inflated by the gas and function as an airbag of a movable object, such as an aerial vehicle. A valve controls flow of gas from the container to the inflatable member in response to a signal from a valve controller. The valve and valve controller are powered by an independent power source than one or more other systems of the movable object. A safety mechanism may also be provided that, unless deactivated, prevents inflation of the inflatable member.
摘要翻译： 提供了一种冲击保护装置，包括构造成保持压缩气体的气体容器和构造成由气体膨胀并充当诸如飞行器的可移动物体的气囊的充气构件。 响应于来自阀控制器的信号，阀控制气体从容器到可膨胀构件的流动。 阀和阀门控制器由与可移动物体的一个或多个其它系统相独立的电源供电。 还可以提供一种安全机构，除非被去激活，否则防止可膨胀构件的膨胀。
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公开(公告)号：US09027886B1
公开(公告)日：2015-05-12
申请号：US13595373
申请日：2012-08-27
申请人： Roger J. Mechels
发明人： Roger J. Mechels
CPC分类号： B64D25/08 , A62B1/22 , B64D1/14 , B64D17/56 , B64D17/60 , B64D17/725 , B64D19/00 , B64D25/12 , B64D2201/00
摘要： A self inflating escape pod in the form of a vest to be worn by an individual to protect their body from a fall when they jump from a high rise building. The vest has a battery, altimeter, motion sensor, bladders and means for inflating the bladders. Removal of the vest from a storage cabinet activates the altimeter which activates the motion detector upon detecting a change in altitude. Upon sensing motion, the motion detector activates inflation of the bladders, forming a pod surround the individual's body. Air channels in the pod provide air to the individual and the pod is designed to accommodate different sizes of individuals. Beacons and reflectors on the pod assist in locating it, and one or more of the bladders will automatically deflate once the individual has stopped falling.
摘要翻译： 一个背包的形式的自充气逃生荚，由个人穿戴，以便在高层建筑物跳跃时保护身体免受摔倒。 背心具有电池，高度计，运动传感器，气囊和用于充气气囊的装置。 从存储柜中取出背心激活高度计，该高度计在检测到高度变化时激活运动检测器。 一旦检测到运动，运动检测器便激活囊的充气，形成围绕个人身体的容器。 荚中的空气通道为个人提供空气，荚被设计成适应不同大小的个体。 荚上的信标和反射器有助于定位，一旦个体停止坠落，一个或多个囊将自动放气。
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