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公开(公告)号：US09663219B2
公开(公告)日：2017-05-30
申请号：US14807014
申请日：2015-07-23
发明人： Mathieu Carton , Pierre Debusschere , David Chabe
CPC分类号： B64C13/00 , B64D39/00 , G05D1/0607 , G05D1/0808
摘要： The system comprises at least one lift generator element that is able to modify directly the lift of the aircraft and means for defining a deflection instruction upon actuation by a pilot of the aircraft of a control column of the aircraft generating a vertical load factor control value and applying it to an elevator and simultaneously defining a command instruction and applying it to the lift generator element to generate a direct lift.
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22.发明申请公开(公告)号：US20160258750A1
公开(公告)日：2016-09-08
申请号：US14640878
申请日：2015-03-06
申请人： THE BOEING COMPANY
发明人： RICHARD GOLOB , JUSTIN CLEVE HATCHER , JUNG SOON JANG , KIMBERLY ANN HINSON , JEFFREY L. MUSGRAVE
CPC分类号： G01C9/005 , B64D39/00 , G01C9/02 , G01C25/005
摘要： An aerial refueling boom elevation estimation (“ARBEE”) system for estimating an elevation angle of an aerial refueling boom on an aerial refueling aircraft is described. The ARBEE system may include a data collector, storage unit, optimizer, and comparator.
摘要翻译： 描述了用于估计空中加油飞机上的空中加油站的仰角的空中加油站高程估计（“ARBEE”）系统。 ARBEE系统可以包括数据收集器，存储单元，优化器和比较器。
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公开(公告)号：US09334062B2
公开(公告)日：2016-05-10
申请号：US12792440
申请日：2010-06-02
摘要： An assisted in-flight refueling system having a tanker aircraft equipped with a drogue; a fuel take-on aircraft equipped with a probe; and a drogue-probe coupling assist system designed to determine a first distance between the drogue and the take-on aircraft/probe, a second distance between the tanker aircraft and the drogue, and a third distance between the tanker aircraft and the take-on aircraft. The drogue-probe coupling assist system is also designed to determine information relative to the necessary movement of the drogue and/or the necessary movement of the take-on aircraft to couple the drogue to the probe, as a function of the first, second, and third distance.
摘要翻译： 一个辅助的机上加油系统，具有配备有冷水的油轮飞机; 装有探头的燃油喷射飞机; 以及锥形探针联接辅助系统，其被设计用于确定锥套和接管飞行器/探针之间的第一距离，油罐飞机与锥套之间的第二距离，以及油轮飞机与接收器之间的第三距离 飞机。 锥形探针耦合辅助系统还被设计成根据第一，第二，第二，第二，第二，第二，第二，第二，第二和第二， 和第三距离。
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公开(公告)号：US20160023749A1
公开(公告)日：2016-01-28
申请号：US14807014
申请日：2015-07-23
发明人： Mathieu CARTON , Pierre DEBUSSCHERE , David CHABE
CPC分类号： B64C13/00 , B64D39/00 , G05D1/0607 , G05D1/0808
摘要： The system comprises at least one lift generator element that is able to modify directly the lift of the aircraft and means for defining a deflection instruction upon actuation by a pilot of the aircraft of a control column of the aircraft generating a vertical load factor control value and applying it to an elevator and simultaneously defining a command instruction and applying it to the lift generator element to generate a direct lift.
摘要翻译： 该系统包括至少一个提升发电机元件，该升降机发电机元件能够直接修改飞行器的升降机，以及用于在飞行器的飞行员致动之后定义偏转指令的装置，该飞行器的飞行器产生垂直载荷系数控制值， 将其施加到电梯并同时定义命令指令并将其施加到电梯发电机元件以产生直接电梯。
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公开(公告)号：US20150346344A1
公开(公告)日：2015-12-03
申请号：US14619405
申请日：2015-02-11
发明人： Patrick Gilliland , Robert W. Koseluk , Steve Penniman , Brad Short , Joseph Spagnolia , Roger Stettner
CPC分类号： G01S17/88 , B64D39/00 , B64D47/00 , B64G1/646 , G01S7/481 , G01S7/4863 , G01S7/4868 , G01S17/107 , G01S17/89
摘要： A system for landing or docking a mobile platform is enabled by a flash LADAR sensor having an adaptive controller with Automatic Gain Control (AGC). Range gating in the LADAR sensor penetrates through diffuse reflectors. The LADAR sensor adapted for landing/approach comprises a system controller, pulsed laser transmitter, transmit optics, receive optics, a focal plane array of detectors, a readout integrated circuit, camera support electronics and image processor, an image analysis and bias calculation processor, and a detector array bias control circuit. The system is capable of developing a complete 3-D scene from a single point of view.
摘要翻译： 用于着陆或对接移动平台的系统由具有具有自动增益控制（AGC）的自适应控制器的闪光灯LADAR传感器实现。 LADAR传感器中的范围门控穿透漫反射器。 用于着陆/逼近的LADAR传感器包括系统控制器，脉冲激光发射器，发射光学器件，接收光学器件，检测器的焦平面阵列，读出集成电路，照相机支持电子器件和图像处理器，图像分析和偏置计算处理器， 和检测器阵列偏置控制电路。 该系统能够从单一的角度开发完整的3-D场景。
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公开(公告)号：US09067689B2
公开(公告)日：2015-06-30
申请号：US14025542
申请日：2013-09-12
申请人： The Boeing Company
发明人： Kevin Julian Chang
IPC分类号： B64D39/00
CPC分类号： B64D39/00
摘要： An aircraft refueling system for use with a supplying aircraft is provided. The refueling system includes at least two strips of material coupled to a lower portion of the supplying aircraft. The at least two strips are separated by a distance and comprise a material that facilitates the at least two strips becoming progressively visible to a pilot of a receiving aircraft as the receiving aircraft approaches the supplying aircraft.
摘要翻译： 提供与供应飞机一起使用的飞机加油系统。 加油系统包括耦合到供应飞行器的下部的至少两条材料条。 所述至少两个条带分开一段距离，并且包括当所述接收飞行器接近所述供应飞机时便于所述至少两个条带对接收飞行器的飞行员逐渐可见的材料。
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公开(公告)号：US20150041591A1
公开(公告)日：2015-02-12
申请号：US13960614
申请日：2013-08-06
申请人： THE BOEING COMPANY
发明人： Aaron J. Kutzmann
IPC分类号： B64D39/00
CPC分类号： B64D39/00 , B64D39/04 , B64D39/06 , Y10T29/49826
摘要： Embodiments provide a flying boom that is capable of refueling both receptacle-equipped aircraft and probe-equipped aircraft. In one embodiment, a flying boom includes a refueling tube at an end of the flying boom that is adapted to extend from the end of the flying boom to refuel receptacle-equipped aircraft. The flying boom further includes a retractable hose and drogue assembly at the end of the flying boom that is adapted to extend from the end of the flying boom to refuel probe-equipped aircraft.
摘要翻译： 实施例提供了一种飞行吊杆，其能够对装有插座的飞机和装有探针的飞机进行加油。 在一个实施例中，飞行吊杆包括在飞行吊杆的端部处的加油管，其适于从飞行吊架的端部延伸至配备有加油装置的飞机。 飞行吊架还包括在悬臂的末端处的可伸缩软管和锥形组件，其适于从飞行架的末端延伸到加油探针配备的飞机。
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公开(公告)号：US08950708B2
公开(公告)日：2015-02-10
申请号：US13368431
申请日：2012-02-08
申请人： Christopher Mouskis , Georgios Filippos Papaioannou , Adrian Bedford , Richard John Foxwell , James Kemmitt
发明人： Christopher Mouskis , Georgios Filippos Papaioannou , Adrian Bedford , Richard John Foxwell , James Kemmitt
摘要： An air to air refuelling drogue assembly includes a reception coupling and a drogue canopy connected to the reception coupling by connection means which hold the canopy in an operative, drag producing, position relative to the reception coupling during refuelling. The drogue assembly is arranged to controllably fail so as to reduce the drag load produced by the drogue when a drag load on the canopy exceeds a predetermined threshold.
摘要翻译： 空气对空气加油锥套组件包括接收联接器和通过连接装置连接到接收联接器的锥套罩，所述连接装置在加油期间相对于接收耦合器将冠盖保持在可操作的，阻力产生位置。 锥形组件布置成可控制地失效，以便当在顶篷上的拖曳负载超过预定阈值时减小由锥套产生的牵引载荷。
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29.发明授权公开(公告)号：US08911236B2
公开(公告)日：2014-12-16
申请号：US12571962
申请日：2009-10-01
摘要： Training method for the simulation of an operation performed by at least one device which is part of a real apparatus, wherein the method comprises providing to display means overlaid images under controlled depth order of a virtual apparatus, and real images of said device, and providing a simulated response to control means, based on data of the position and behavior of said device and on data of the position and behavior of said virtual apparatus.
摘要翻译： 用于模拟由作为真实设备的一部分的至少一个设备执行的操作的训练方法，其中所述方法包括向显示装置提供在虚拟设备的受控深度顺序下重叠的图像以及所述设备的真实图像，以及提供 基于所述设备的位置和行为的数据以及所述虚拟设备的位置和行为的数据的对控制装置的模拟响应。
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公开(公告)号：US08876055B2
公开(公告)日：2014-11-04
申请号：US11727075
申请日：2007-03-23
申请人： Michael Crowley
发明人： Michael Crowley
CPC分类号： B64D37/20 , B64D37/16 , Y02T50/44 , Y10T137/3421 , Y10T137/7793
摘要： An aircraft refuelling system of an aircraft is provided. The refuelling system comprises a refuelling connector (34) mounted as part of the aircraft and configured to detachably connect to the fuel outlet (2) of a fuel supply apparatus separate from the aircraft, and a fuel pressure regulator (36) having an inlet in communication with a fuel inlet (35) of the refuelling connector (34) and having an outlet in communication with refuelling pipework (39) of the aircraft. The fuel pressure regulator (36), regulates the pressure of fuel in the refuelling pipework (39) when fuel is being passed into the refuelling pipework (39) from the fuel inlet (35) of the refuelling connector. A fuel pressure regulator apparatus for mounting in an aircraft, comprising a connector forming a fuel inlet to the fuel pressure regulator apparatus, configured to detachably connect to the fuel outlet of a fuel supply system, a fuel outlet for connection to the refuelling pipework of an aircraft and a fuel pressure regulator for regulating the pressure of fuel passing through the fuel outlet is also provided.
摘要翻译： 提供飞机的飞机加油系统。 加油系统包括作为飞行器的一部分安装的加油连接器（34），并被配置为可拆卸地连接到与飞行器分离的燃料供应装置的燃料出口（2），以及燃料压力调节器（36），其具有 与加油连接器（34）的燃料入口（35）连通并具有与飞行器的加油管道（39）连通的出口。 当燃料从加油连接器的燃料入口（35）进入加油管道（39）时，燃料压力调节器（36）调节加油管道（39）中的燃料压力。 一种用于安装在飞行器中的燃料压力调节器装置，包括形成燃料压力调节器装置的燃料入口的连接器，其构造成可拆卸地连接到燃料供应系统的燃料出口，用于连接到燃料供给系统的加油管道的燃料出口 还提供了用于调节通过燃料出口的燃料的压力的燃料压力调节器。
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