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1. 发明授权

US08783625B2 Pneumatic control system for aerodynamic surfaces 有权
标题翻译：气动表面气动控制系统
公开(公告)号：US08783625B2
公开(公告)日：2014-07-22
申请号：US13267614
申请日：2011-10-06
申请人： Kevin R. Lutke , Aaron J. Kutzmann
发明人： Kevin R. Lutke , Aaron J. Kutzmann
IPC分类号： B64C3/44
CPC分类号： B64C3/46
摘要： A flight control system for an airfoil comprises a control surface, a chamber connecting the control surface to the airfoil, and a pneumatic mechanism fluidly connected to the chamber. The chamber may be comprised of at least two cells that may be fluidly separated by a membrane. The pneumatic mechanism is configured to provide differential pressure to the cells in order to alternately increase volume/pressure of the cells to cause deflection of the control surface. The cells may have a stretchable outer surface to allow for changes in the length of the outer surface in response to inflation/deflation of the cells. The outer surface of the cells may be substantially continuous with outer mold lines of the airfoil and of the control surface.
摘要翻译：用于翼型的飞行控制系统包括控制表面，将控制表面连接到翼型件的腔室以及与腔室流体连接的气动机构。腔室可以由至少两个细胞构成，这些细胞可被膜流体地分离。气动机构构造成为细胞提供差压以便交替地增加细胞的体积/压力以引起控制表面的偏转。细胞可以具有可拉伸的外表面，以允许响应于细胞的充气/放气而改变外表面的长度。电池的外表面可以与翼型件和控制表面的外部模具线基本上连续。

2. 发明授权

US08459591B2 Methods and apparatus for aerial recovery of flying apparatus 有权
标题翻译：飞行装置空中回收方法及装置
公开(公告)号：US08459591B2
公开(公告)日：2013-06-11
申请号：US13465220
申请日：2012-05-07
申请人： Kevin Reed Lutke , Aaron J. Kutzmann
发明人： Kevin Reed Lutke , Aaron J. Kutzmann
IPC分类号： B64F1/04
CPC分类号： B64C39/024 , B64C2201/021 , B64C2201/082 , B64C2201/127 , B64C2201/165 , B64C2201/182 , B64C2201/206
摘要： Methods and systems are provided which may allow a first vehicle to recover a second air vehicle while both are moving. The first vehicle and the second air vehicle may be traveling at different velocities. An attachment member of the second air vehicle may attach to a recovery member of the first vehicle while the first vehicle and the second air vehicle are traveling at different velocities. The recovery member attached to the second air vehicle may move relative to and along an exterior surface of the first vehicle in a direction substantially parallel to a direction of travel of the first vehicle.
摘要翻译：提供了方法和系统，其可以允许第一车辆在移动时都恢复第二空中车辆。第一车辆和第二空中车辆可以以不同的速度行驶。当第一车辆和第二空中车辆以不同的速度行驶时，第二空中车辆的附接构件可以附接到第一车辆的回收构件。附接到第二空气车辆的回收构件可以在与第一车辆的行进方向基本平行的方向上相对于第一车辆的外表面移动并沿其移动。

3. 发明申请

US20120104182A1 PNEUMATIC CONTROL SYSTEM FOR AERODYNAMIC SURFACES 有权
标题翻译：气动表面气动控制系统
公开(公告)号：US20120104182A1
公开(公告)日：2012-05-03
申请号：US13267614
申请日：2011-10-06
申请人： Kevin R. Lutke , Aaron J. Kutzmann
发明人： Kevin R. Lutke , Aaron J. Kutzmann
IPC分类号： B64C3/44
CPC分类号： B64C3/46
摘要： A flight control system for an airfoil comprises a control surface, a chamber connecting the control surface to the airfoil, and a pneumatic mechanism fluidly connected to the chamber. The chamber may be comprised of at least two cells that may be fluidly separated by a membrane. The pneumatic mechanism is configured to provide differential pressure to the cells in order to alternately increase volume/pressure of the cells to cause deflection of the control surface. The cells may have a stretchable outer surface to allow for changes in the length of the outer surface in response to inflation/deflation of the cells. The outer surface of the cells may be substantially continuous with outer mold lines of the airfoil and of the control surface.
摘要翻译：用于翼型的飞行控制系统包括控制表面，将控制表面连接到翼型件的腔室以及与腔室流体连接的气动机构。腔室可以由至少两个细胞构成，这些细胞可被膜流体地分离。气动机构构造成为细胞提供差压以便交替地增加细胞的体积/压力以引起控制表面的偏转。细胞可以具有可拉伸的外表面，以允许响应于细胞的充气/放气而改变外表面的长度。电池的外表面可以与翼型件和控制表面的外部模具线基本上连续。

4. 发明授权

US06926231B2 Vertical takeoff and landing aircraft 有权
标题翻译：垂直起降飞机
公开(公告)号：US06926231B2
公开(公告)日：2005-08-09
申请号：US10829757
申请日：2004-04-22
申请人： Richard P. Ouellette , Aaron J. Kutzmann
发明人： Richard P. Ouellette , Aaron J. Kutzmann
IPC分类号： B64C1/14 , B64C29/00 , B64D5/00 , B64D27/02 , B64D27/20 , F02K7/075
CPC分类号： F02K7/075 , B64C1/1415 , B64C29/0058 , B64D5/00 , B64D27/023 , B64D27/20 , Y02T50/44 , Y02T50/672
摘要： A method is provided for reducing vulnerability to hostile detection of and aggression towards an aircraft. The method includes adapting an aircraft fuselage to form an armored payload bay, wherein the armored payload bay includes a pair of sidewalls and a bottom. The method additionally includes adapting wings of the aircraft to allow the aircraft to be transported within a larger aircraft. For example, the wings could have a fixed wing span that allows the aircraft to transported within a larger aircraft or the wings could be adapted to fold so that the aircraft can transported within a larger aircraft. The method further includes disposing at least one pulse ejector thrust augmentor (PETA) bank within each sidewall. Each PETA bank is oriented such that a thrust exhaust produced is directed down and away from a centerline of the payload bay. Still further, the method includes adapting the bottom of payload bay to allow ingress and egress of cargo.
摘要翻译：提供了一种减少对飞机的敌对侦察和侵略的脆弱性的方法。该方法包括使飞行器机身适应形成装甲有效载荷舱，其中装甲有效载荷舱包括一对侧壁和底部。该方法还包括使飞行器的翼适应，以允许飞机在较大的飞机内运输。例如，机翼可以具有固定的机翼跨度，其允许飞机在更大的飞行器内运输，或者翼可以适应折叠，使得飞机可以在更大的飞机内运输。该方法还包括在每个侧壁内设置至少一个脉冲喷射推力增强器（PETA）组。每个PETA组被定向成使得产生的推力排气向下并远离有效载荷舱的中心线。此外，该方法包括调整有效载荷底部以允许货物的入口和出口。

5. 发明授权

US08366052B1 Detachable inflation system for air vehicles 有权
标题翻译：机动车可拆卸通货膨胀系统
公开(公告)号：US08366052B1
公开(公告)日：2013-02-05
申请号：US12582706
申请日：2009-10-20
申请人： Kevin R. Lutke , Aaron J. Kutzmann
发明人： Kevin R. Lutke , Aaron J. Kutzmann
IPC分类号： B64G1/00
CPC分类号： B64G1/641 , B64G1/002 , B64G1/58 , B64G1/62 , B64G2001/224
摘要： A detachable inflation system for use with an air vehicle having at least one inflatable structure. The detachable inflation system comprises a pallet structure. The detachable inflation system further comprises an initial inflation system, attached to the pallet structure, that provides one or more compressed fluids. The initial inflation system is connected to an inflation distribution system in the air vehicle for distributing the one or more compressed fluids into the inflatable structure to inflate the inflatable structure. The detachable inflation system further comprises a detachable parachute.
摘要翻译：一种用于具有至少一个可充气结构的机动车辆的可拆卸充气系统。可拆卸的充气系统包括托盘结构。可拆卸的充气系统还包括附接到托盘结构的初始充气系统，其提供一个或多个压缩流体。初始充气系统连接到空中车辆中的充气分配系统，用于将一个或多个压缩流体分配到可充气结构中以使可充气结构膨胀。可拆卸的充气系统还包括可拆卸的降落伞。

6. 发明授权

US08322655B1 Twin-boom empennage 有权
标题翻译：双臂繁荣尾翼
公开(公告)号：US08322655B1
公开(公告)日：2012-12-04
申请号：US12410865
申请日：2009-03-25
申请人： Max Kismarton , Aaron J. Kutzmann , Kevin Lutke
发明人： Max Kismarton , Aaron J. Kutzmann , Kevin Lutke
IPC分类号： B64C1/00
CPC分类号： B64C5/02
摘要： Apparatus and methods provide for an aircraft empennage that utilizes two torque tube members to create opposing sides of the empennage. The torque tube members are connected using a bridging member that is attached at opposing ends to the top portions of the torque tube members. The torque tube members and bridging member provide structural support for access cut-outs within the aircraft skin between the torque tube members for access to a payload space within. The torque tube members may include any number of walls, any of which may provide a pressure barrier to the payload space.
摘要翻译：装置和方法为飞行器尾翼提供了利用两个扭矩管构件来产生尾翼的相对侧面的装置和方法。扭矩管构件使用在相对端附接到扭矩管构件的顶部的桥接构件连接。扭矩管构件和桥接构件提供用于在扭矩管构件之间的用于进入有效载荷空间的飞行器皮肤内的通路切口的结构支撑。扭矩管构件可以包括任何数量的壁，其中任何一个可以为有效负载空间提供压力屏障。

7. 发明授权

US08231083B2 System and methods for airborne launch and recovery of aircraft 有权
标题翻译：机载发射和恢复飞机的系统和方法
公开(公告)号：US08231083B2
公开(公告)日：2012-07-31
申请号：US12062861
申请日：2008-04-04
申请人： Aaron J. Kutzmann , Kevin R. Lutke , Zachary C. Hoisington
发明人： Aaron J. Kutzmann , Kevin R. Lutke , Zachary C. Hoisington
IPC分类号： B64D1/10
CPC分类号： B64C39/024 , B64C2201/082 , B64C2201/182 , B64D3/00 , B64D5/00 , B65H75/425 , B65H75/44
摘要： A system and methods for airborne launch and recovery of aircraft. In one embodiment the system comprises a flexible tether configured to be towed behind an airborne mother ship. A drag device is secured to a distal end of the flexible tether to generate drag and maintain tension in the flexible tether. A reel associated with the mother ship anchors a proximal portion of the flexible tether and selectively lets out and takes up the flexible tether to adjust a length of the flexible tether. A capture mechanism associated with the aircraft engages the flexible tether to secure the aircraft to the flexible tether. In certain embodiments of the present methods, a flexible tether is deployed from an airborne mother ship. An aircraft translates forward and rearward along the flexible tether. Alternatively, the aircraft translates forward and rearward as the flexible tether taken up and let out from the mother ship. Prior to launch, the weight of the aircraft is transferred from the flexible tether to the wings. During recovery, the weight of the aircraft is transferred from the wings to the flexible tether.
摘要翻译：飞机机载发射和恢复的系统和方法。在一个实施例中，系统包括被配置为被拖到空中母舰后面的柔性系绳。牵引装置固定到柔性系绳的远端以产生阻力并保持柔性系绳中的张力。与母船相关联的卷轴锚定柔性系绳的近端部分，并且选择性地放出并吸收柔性系绳以调节柔性系绳的长度。与飞行器相关联的捕获机构接合柔性系绳以将飞行器固定到柔性系绳。在本方法的某些实施例中，柔性系绳从空中母舰部署。飞机沿着柔性系绳向前和向后平移。或者，飞机向前和向后平移，因为柔性系绳被从母船出来。在发射之前，飞机的重量从柔性系绳转移到机翼。在恢复期间，飞机的重量从翼转移到柔性系绳。

8. 发明授权

US08191828B2 Methods and apparatus for aerial recovery of flying apparatus 有权
标题翻译：飞行装置空中回收方法及装置
公开(公告)号：US08191828B2
公开(公告)日：2012-06-05
申请号：US12120065
申请日：2008-05-13
申请人： Kevin Reed Lutke , Aaron J. Kutzmann
发明人： Kevin Reed Lutke , Aaron J. Kutzmann
IPC分类号： B64F1/04
CPC分类号： B64C39/024 , B64C2201/021 , B64C2201/082 , B64C2201/127 , B64C2201/165 , B64C2201/182 , B64C2201/206
摘要： Methods and systems are provided which may allow a first vehicle to recover a second air vehicle while both are moving. The first vehicle and the second air vehicle may be traveling at different velocities. An attachment member of the second air vehicle may attach to a recovery member of the first vehicle while the first vehicle and the second air vehicle are traveling at different velocities. The recovery member attached to the second air vehicle may move relative to and along an exterior surface of the first vehicle in a direction substantially parallel to a direction of travel of the first vehicle.
摘要翻译：提供了方法和系统，其可以允许第一车辆在移动时都恢复第二空中车辆。第一车辆和第二空中车辆可以以不同的速度行驶。当第一车辆和第二空中车辆以不同的速度行驶时，第二空中车辆的附接构件可以附接到第一车辆的回收构件。附接到第二空气车辆的回收构件可以在与第一车辆的行进方向基本平行的方向上相对于第一车辆的外表面移动并沿其移动。

9. 发明授权

US06926235B2 Runway-independent omni-role modularity enhancement (ROME) vehicle 有权
标题翻译：跑道独立的全能模块化增强（ROME）车辆
公开(公告)号：US06926235B2
公开(公告)日：2005-08-09
申请号：US10600400
申请日：2003-06-20
申请人： Richard P. Ouellette , Aaron J. Kutzmann
发明人： Richard P. Ouellette , Aaron J. Kutzmann
IPC分类号： B64C1/00 , B64C29/00 , B64C39/02 , B64D7/00
CPC分类号： B64C1/00 , B64C29/0058 , B64C39/024 , B64C2201/046 , B64C2201/086 , B64C2201/088 , B64C2201/104 , B64C2201/121 , B64C2201/165 , B64C2201/167 , B64C2201/187 , B64D7/00
摘要： A modular component set is configurable to form a plurality of flight capable platforms. A plurality of end pieces each has contiguously connected curved outer portions each longitudinally expanding from a tip to terminate at a blunt attachment face. Body members have opposed ends to receive the end piece blunt attachment face, and a rectangular shaped mid-portion having opposed walls. A plurality of task specific panels are each releasably connectable to one of the opposed walls. At least one of the body members with the end pieces joined at the opposed ends, and at least one of the task specific panels connected to one of the opposed walls form a minimum component set for each of the flight capable platforms.
摘要翻译：模块化组件组可配置成形成多个具有飞行能力的平台。多个端片各自具有连续地连接的弯曲外部部分，每个端部从尖端纵向扩展以终止于钝的附接面。主体部件具有相对的端部以接收端部钝器附接面，以及具有相对壁的矩形中间部分。多个任务专用面板各自可拆卸地连接到相对的壁之一。至少一个具有端部件的主体部件在相对的端部连接，并且连接到相对的一个壁之一的任务专用面板中的至少一个为每个具有飞行能力的平台形成最小的部件组。

10. 发明授权

US08829401B1 Projectile and associated method for seeking a target identified by laser designation 有权
标题翻译：用于寻找通过激光识别识别的目标的弹丸和相关方法
公开(公告)号：US08829401B1
公开(公告)日：2014-09-09
申请号：US13162167
申请日：2011-06-16
申请人： Kevin Lutke , Aaron J. Kutzmann
发明人： Kevin Lutke , Aaron J. Kutzmann
IPC分类号： F42B15/01 , F41G7/00 , B64D7/08 , F42B15/00
CPC分类号： F42B15/01 , B64D7/08 , F41F3/065 , F41G3/02 , F41G3/145 , F41G7/346
摘要： A projectile and associated method are provided for seeking a target that has been laser designated even though the projectile does not include a laser receiver. A projectile includes an aerodynamic body and a GPS receiver configured to receive GPS signals indicative of a location of the aerodynamic body. The projectile also includes a radio receiver configured to receive radio signals from an offboard laser receiver that provide information relating to a location of the target based upon laser designation of the target. Further, the projectile includes a processor configured to direct flight of the aerodynamic body toward the target based upon the location of the aerodynamic body as determined from the GPS signals and the location of the target based upon the information provided by the offboard laser receiver.
摘要翻译：提供射弹和相关方法用于寻求已经被激光指定的目标，即使射弹不包括激光接收器。射弹包括空气动力体和GPS接收器，其被配置为接收指示空气动力体的位置的GPS信号。射弹还包括无线电接收器，其被配置为从外部激光接收机接收无线电信号，所述无线电信号基于目标的激光指定来提供与目标的位置有关的信息。此外，射弹包括处理器，其被配置为基于根据由GPS信号确定的空气动力学体的位置和基于由外侧激光接收器提供的信息的目标的位置来引导空气动力学体向目标的飞行。

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