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91. 发明申请

US20130193272A1 EXPENDABLE AERIAL DELIVERY SYSTEM 有权
标题翻译：支付费用的送货系统
公开(公告)号：US20130193272A1
公开(公告)日：2013-08-01
申请号：US13747659
申请日：2013-01-23
申请人： Roy L. Fox, JR.
发明人： Roy L. Fox, JR.
IPC分类号： B64D1/12
CPC分类号： B64D1/12
摘要： Methods and systems for aerial delivery utilize expendable materials. An expendable aerial delivery system comprises wood, textile and/or other expendable materials, for example materials suitable for disposing via burning or crushing in a forward area. In this manner, valuable and/or expensive metal platforms can be eliminated from airdrops, thus preventing insurgent repurposing of these platforms into improvised explosive devices and other implements of warfare.
摘要翻译：航空运输的方法和系统使用消耗性材料。消耗性空中交付系统包括木材，纺织品和/或其他消耗性材料，例如适于通过在前部区域中燃烧或破碎处理的材料。以这种方式，可以从空投中消除有价值的和/或昂贵的金属平台，从而防止将这些平台叛乱地重新利用到简易爆炸装置和其他战争工具中。

92. 发明授权

US08418965B2 Mounting set, system and method 有权
标题翻译：安装套件，系统和方法
公开(公告)号：US08418965B2
公开(公告)日：2013-04-16
申请号：US12457120
申请日：2009-06-01
申请人： Israel Schnitzer
发明人： Israel Schnitzer
IPC分类号： B64D1/12
CPC分类号： B64D7/08 , B64D1/00 , B64D1/04 , B64D9/00 , F02K9/343 , F05D2240/90 , F05D2260/30 , F41F5/00 , F42B25/00
摘要： A mounting set for use in mounting an external stores to a mounting station of an aerospace vehicle includes a mounting bracket arrangement and a strap arrangement. The bracket arrangement is configured for selective reversible engagement with respect to the mounting station and for cooperating with the strap arrangement. The strap arrangement is configured for securing the bracket arrangement to the stores in load bearing abutment therewith to enable transfer of loads between the stores and the mounting station via said bracket arrangement, in operation of said mounting set. A mounting system is also provided for mounting an external stores to an aerospace vehicle having two or more mounting stations, including a mounting set for each mounting station. Mounting methods are also provided.
摘要翻译：用于将外部商店安装到航空航天车辆的安装台上的安装组件包括安装支架装置和带装置。支架装置构造成用于相对于安装台的选择性可逆接合并且用于与带装置配合。带状装置构造成用于将支架装置固定到与其承载的承载座处的商店中，以便在所述安装组的操作中通过所述支架装置在所述商店和所述安装工位之间传递负载。还提供了一种用于将外部商店安装到具有两个或更多个安装站的航空航天器的安装系统，包括用于每个安装站的安装组件。还提供了安装方法。

93. 发明申请

US20120261522A1 MODULAR EXTERNALLY ACCESSIBLE BATTERIES FOR AN AIRCRAFT 有权
标题翻译：用于飞机的模块化外部可访问电池
公开(公告)号：US20120261522A1
公开(公告)日：2012-10-18
申请号：US13524541
申请日：2012-06-15
申请人： Christopher K. Droney
发明人： Christopher K. Droney
IPC分类号： B64D1/08 , B64D1/12 , B64D33/00
CPC分类号： B64D27/24 , B64C7/02 , Y02T50/62
摘要： An aircraft comprises an airframe, an electric propulsion system, a number of battery pods, and an engagement system. The number of battery pods has a physical connector system. The engagement system is attached to the airframe and is capable of engaging the physical connector system to connect the number of battery pods to the airframe.
摘要翻译：飞机包括机身，电动推进系统，多个电池舱和接合系统。电池盒的数量有一个物理连接器系统。接合系统连接到机身，并且能够接合物理连接器系统以将电池盒的数量连接到机身。

94. 发明申请

US20120256045A1 AIRBORNE COOLING SYSTEM 有权
标题翻译： AIRBORNE冷却系统
公开(公告)号：US20120256045A1
公开(公告)日：2012-10-11
申请号：US13432482
申请日：2012-03-28
申请人： Steven Gagne
发明人： Steven Gagne
IPC分类号： B64D33/10 , B64D1/12
CPC分类号： B64D1/08 , B64D13/00 , B64D33/10 , B64D2013/0614 , B64D2013/0674 , F28D5/00 , F28D2021/0021 , F41H13/0043 , F42B15/34
摘要： An aircraft having a cooling system is disclosed. The cooling system can be used to cool a heat emitting component. In one form the cooling system is a refrigerant system and includes a relatively high temperature device such as, but not limited to, a condenser. The relatively high temperature component is placed in thermal communication with a passing air flow. In one embodiment the aircraft includes a pod in which at least a portion of the cooling system is disposed. For example, a condenser of a vapor cycle refrigerant system can be located in the pod and in thermal communication with the air flow. The cooling system can also include a device capable of delivering a cooling fluid into the air flow and/or to the relatively high temperature component. The cooling fluid can be evaporated to provided additional cooling.
摘要翻译：公开了一种具有冷却系统的飞机。冷却系统可用于冷却发热部件。在一种形式中，冷却系统是制冷剂系统，并且包括相对高温的装置，例如但不限于冷凝器。相对较高的温度部件被放置成与通过的空气流热连通。在一个实施例中，飞行器包括其中布置有冷却系统的至少一部分的舱。例如，蒸气循环制冷剂系统的冷凝器可以位于容器中并与气流热连通。冷却系统还可以包括能够将冷却流体输送到空气流和/或相对高温部件的装置。冷却液可以被蒸发以提供额外的冷却。

95. 发明申请

US20120132757A1 EJECTION SYSTEM AND A METHOD FOR EJECTING A PAYLOAD FROM A PAYLOAD DELIVERY VEHICLE 有权
标题翻译：喷射系统和从PAYLOAD传递车辆喷射PAYLOAD的方法
公开(公告)号：US20120132757A1
公开(公告)日：2012-05-31
申请号：US12955436
申请日：2010-11-29
申请人： Thomas A. Olden
发明人： Thomas A. Olden
IPC分类号： B64D1/12 , B64D1/04
CPC分类号： B64D1/02 , B64D1/12
摘要： An ejection system for ejecting a payload from a payload delivery vehicle is provided. The ejection system includes an airbag ejection system configured to eject the payload from the payload delivery vehicle, a payload separation system configured to selectively couple the payload to the airbag ejection system, and a controller configured to inflate the airbag ejection system and further configured to signal the payload separation system to release the payload from the airbag ejection system.
摘要翻译：提供了一种用于从有效载荷传送车辆弹出有效载荷的弹出系统。排出系统包括安全气囊排出系统，其构造成从有效载荷递送车辆弹出有效载荷;有效载荷分离系统，被配置为选择性地将有效载荷耦合到安全气囊排出系统;以及控制器，其构造成使安全气囊排出系统膨胀，有效载荷分离系统以从气囊排出系统释放有效载荷。

96. 发明授权

US08172184B2 Aerial transport apparatus 有权
标题翻译：空中运输装置
公开(公告)号：US08172184B2
公开(公告)日：2012-05-08
申请号：US12366530
申请日：2009-02-05
申请人： Ken Spencer , Todd Humbert
发明人： Ken Spencer , Todd Humbert
IPC分类号： B64D1/12
CPC分类号： B66C1/36
摘要： The invention provides a cargo hook apparatus for securing cargo external to an aircraft for transportation, the apparatus comprising, pendent sling means, an attachment for securing the pendent sling means to the aircraft, and a cargo hook assembly, where the cargo hook assembly comprises a high-strength, lightweight alloy, and where the cargo hook assembly weighs less than about 55 pounds.
摘要翻译：本发明提供一种用于固定飞机外部用于运输的货物的货物钩装置，该装置包括：悬吊吊装装置，用于将悬吊悬挂装置固定到飞行器的附件和货钩组件，其中货钩组件包括高强度，轻质合金，以及货钩组件的重量小于约55磅。

97. 发明授权

US08162263B2 Payload quick release for an aerial system 失效
标题翻译：空中系统的有效载荷快速释放
公开(公告)号：US08162263B2
公开(公告)日：2012-04-24
申请号：US12415463
申请日：2009-03-31
申请人： Kimberly Wong , Armand Losinski
发明人： Kimberly Wong , Armand Losinski
IPC分类号： B64D1/12
CPC分类号： B64C39/024 , B64C2201/027 , B64C2201/044 , B64C2201/108 , B64C2201/127 , B64D1/02 , F16B21/02
摘要： A payload quick release mechanism for an unmanned aerial vehicle is provided. This mechanism is affixed to a structure on the unmanned aerial vehicle, and allows for quick attachment and removal of a payload from the unmanned aerial vehicle. The attachment device includes a body with a perimeter and a plurality of arms that extend from the body perimeter. Each arm includes an indented section, within which a tab extending from the payload top may be placed. When the payload tab rests within the indented section, the payload is prevented from translation and is attached to the mechanism.
摘要翻译：提供了一种用于无人机的有效载荷快速释放机构。该机构固定在无人驾驶飞行器上的结构上，并允许从无人驾驶飞行器快速附接和移除有效载荷。附接装置包括具有周边的主体和从主体周边延伸的多个臂。每个臂包括一个缩进的部分，其中可以放置从有效载荷顶部延伸的突片。当有效载荷标签搁置在缩进部分内时，防止有效载荷平移并附着在机构上。

98. 发明授权

US07954765B2 System and method for in-flight adjustment of store ejector gas flow orificing 有权
标题翻译：存储喷射器气体流量调节的飞行调整系统和方法
公开(公告)号：US07954765B2
公开(公告)日：2011-06-07
申请号：US12019615
申请日：2008-01-24
申请人： Thaddeus M. Jakubowski, Jr. , Cameron D. Brown , Daniel S. Rymarz , John K. Foster
发明人： Thaddeus M. Jakubowski, Jr. , Cameron D. Brown , Daniel S. Rymarz , John K. Foster
IPC分类号： B64D1/12 , B64C19/00
CPC分类号： B64D1/04 , Y10T137/86895
摘要： A store ejector is adapted for in-flight adjustment of the pitch attitude imparted to a store by a pair of ejector pistons. The pitch attitude of the store is adjustable to correspond to a flight condition of the aircraft at time of store release. The aircraft has a flight computer that provides store release pitch data corresponding to the aircraft flight conditions. The store ejector includes an orificing assembly that varies the flow of pressurized gas to the ejector pistons by translating a mandrel within a bore formed in the orificing assembly. Orifices within the bore are adjusted to apportion the flow of pressurized gas to the ejector pistons in accordance with an optimum orifice setting corresponding to the desired pitch attitude of the store for the given flight condition.
摘要翻译：商店喷射器适用于通过一对喷射器活塞进行向店内传播的俯仰姿态的飞行中调整。商店的俯仰姿态是可调整的，以对应于飞机在商店释放时的飞行状况。该飞机有一台飞行计算机，提供对应于飞行器飞行条件的储存释放俯仰数据。商店喷射器包括一个喷射组件，该喷射组件通过在形成在喷孔组件中的孔内平移心轴来改变加压气体到喷射器活塞的流动。调节孔内的孔径，以根据对于给定的飞行条件对应于商店的期望的俯仰姿态的最佳孔设置来分配加压气体到喷射器活塞的流量。

99. 发明申请

US20110024548A1 LAUNCHING SYSTEM AND LAUNCHING APPARATUS 有权
标题翻译：启动系统和启动装置
公开(公告)号：US20110024548A1
公开(公告)日：2011-02-03
申请号：US12649808
申请日：2009-12-30
申请人： Yoshikatsu Kuroda , Yoshihiro Kawamata , Mika Shingo
发明人： Yoshikatsu Kuroda , Yoshihiro Kawamata , Mika Shingo
IPC分类号： B64D3/00 , B64C3/00 , B64F1/04 , B64C37/02 , B64D1/12 , B64G1/10
CPC分类号： B64D1/04 , B64D3/00 , B64G1/005
摘要： A flying object capable of being launched in air is detachably mounted on a wing body of a launching apparatus. The launching apparatus is towed by an aircraft through a cable so as to be run and taken off. After raising the launching apparatus to a launching height of the flying object by the aircraft, the flying object is released from the wing body in air and then the flying object is ignited and launched in air in a launching system. The system for launching in air can be developed without newly developing a platform as a mother ship so that a research cost can be remarkably reduced. In the case that a small artificial satellite is installed in a flying object, it is possible to develop an artificial satellite smoothly and quickly applicable to security matters and disaster observation.
摘要翻译：能够在空气中发射的飞行物体可拆卸地安装在发射装置的翼体上。发射装置由飞机通过电缆拖曳以便被运行和取下。在将发射装置升高到飞行器的飞行物体的发射高度之后，飞行物体在空中从翼体释放，然后飞行物体在发射系统中被点燃并在空气中发射。可以开发空气发射系统，而不需要开发作为母船的平台，从而大大减少研究费用。在飞行物体上安装有小型人造卫星的情况下，可以平稳，快速地开发人造卫星，从而可以安全地进行灾害观察。

100. 发明授权

US07861972B1 Release mechanism for a forward and aft restrained load in an aircraft 有权
标题翻译：飞机前后束缚载荷释放机构
公开(公告)号：US07861972B1
公开(公告)日：2011-01-04
申请号：US11970768
申请日：2008-01-08
申请人： Martinus M. Sarigul-Klijn , Nesrin Sarigul-Klijn
发明人： Martinus M. Sarigul-Klijn , Nesrin Sarigul-Klijn
IPC分类号： B64D1/12 , B64D1/10
CPC分类号： B64D1/04 , F41F3/06 , F41F5/00
摘要： An object is deployed from an aircraft using gravity extraction of the object with the aid of a small parachute. The object is restrained in the fore and aft directions on either side of the center of gravity by fore and aft loading chains which hold the object to a loading deck. The chains are attached to the object by pear shaped rings mounted to a load plate. The load plate is supported on a lower attachment plate mounted to the object and is attached by a pin to an upper attachment plate also mounted to the object. Pulling the pin causes the load plate to rotate about a hinge formed on the lower attachment plate followed by release of the load plate from the lower attachment plate and the object to be deployed.
摘要翻译：借助于小型降落伞，使用重力提取物体从飞机部署物体。该物体通过将物体保持在装载甲板上的前后装载链在重心两侧的前后方向上被约束。链条通过安装在负载板上的梨形环连接到物体上。负载板被支撑在安装到物体上的下部附接板上，并且通过销附接到也安装到物体的上部附接板。拉动销使得装载板围绕形成在下附接板上的铰链旋转，随后将负载板从下附接板和要部署的物体释放。

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