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1. 发明申请

WO2017180392A1 MODULAR AIRCRAFT SYSTEM 审中-公开
标题翻译：模块化飞机系统
公开(公告)号：WO2017180392A1
公开(公告)日：2017-10-19
申请号：PCT/US2017/026146
申请日：2017-04-05
申请人： AL-SABAH, Nasser M. , 33100.81 PATENT TRUST
发明人： AL-SABAH, Nasser M.
IPC分类号： B64C3/38 , B64C3/34 , B64C9/00 , B64C9/32 , B64C13/00 , B64C13/20 , B64C39/02 , B64D15/00 , B64D27/02 , B64D27/14
CPC分类号： B64C3/38 , B64C1/26 , B64C3/34 , B64C5/06 , B64C9/00 , B64C9/326 , B64C13/00 , B64C13/20 , B64C39/024 , B64C2201/021 , B64C2201/048 , B64C2201/063 , B64C2201/104 , B64C2201/126 , B64C2201/141 , B64C2201/146 , B64C2201/16 , B64C2201/165 , B64C2211/00 , B64D15/00 , B64D27/02 , B64D27/14 , B64D27/20 , B64D37/00 , B64D39/00 , B64D47/08 , Y02T50/32
摘要： The modular aircraft system includes a single fuselage (10) having a permanently installed empennage (12) and plural sets of wing modules (46a, 46b, 66a, 66b, 68a, 68b) and engine modules (56, 60, 64), with each wing and engine module optimized for different flight conditions and missions. The fuselage (10) and each of the modules are configured for rapid removal and installation of the modules to minimize downtime for the aircraft. Short wings (46a, 46b) having relatively low aspect ratio are provided for relatively high speed flight when great endurance and/or weight carrying capacity are not of great concern. Long wings (68a, 68b) having high aspect ratio are provided for longer range and endurance flights where speed is not absolutely vital. A medium span wing module (66a, 66b) is also provided. Turboprop (56), single turbojet (60), and dual turbojet (64) engine modules are provided for installation depending upon mission requirements.
摘要翻译：模块化飞行器系统包括具有永久安装的尾翼（12）和多组翼模块（46a，46b，66a，66b，68a，68b）的单个机身（10）和发动机模块 56,60,64），每个机翼和发动机模块针对不同的飞行条件和任务进行了优化。机身（10）和每个模块被配置为用于模块的快速移除和安装以最小化飞行器的停机时间。当高度耐力和/或重量承载能力不受重视时，提供具有相对低纵横比的短翼（46a，46b）用于相对高速飞行。提供具有高纵横比的长翼（68a，68b）用于速度不是绝对重要的较长距离和耐力飞行。还提供了中跨翼模块（66a，66b）。根据任务要求，提供涡轮螺旋桨发动机（56），单涡轮喷气发动机（60）和双涡轮喷气发动机（64）发动机模块用于安装。

2. 发明申请

WO2016181116A1 AIRCRAFT DATA TRANSFER 审中-公开
标题翻译：飞机数据传输
公开(公告)号：WO2016181116A1
公开(公告)日：2016-11-17
申请号：PCT/GB2016/051313
申请日：2016-05-09
申请人： BAE SYSTEMS PLC
发明人： PESCOD, Christopher Ralph , SMITH, Andrew James
IPC分类号： B64D39/00 , H04B7/185 , B64C39/02
CPC分类号： B64D39/00 , B64C39/024 , B64C2201/063
摘要： Disclosed is a data transfer method comprising: performing a refuelling process including receiving, by an aircraft (104), aircraft fuel from a first entity (for example, a tanker aircraft (102)), the first entity being remote from the aircraft (104); and, during the refuelling process, sending data between the aircraft (104) and a second entity (for example, the tanker aircraft (102)), the second entity being remote from the aircraft (104). The data is sent as a radio frequency signal having a frequency in the range 50GHz to 70GHz. Preferably, the data is sent as a radio frequency signal having a frequency in the range 57GHz to 66GHz, for example 60GHz.
摘要翻译：公开了一种数据传输方法，包括：执行加油过程，包括由飞机（104）接收来自第一实体（例如，油轮飞机（102））的飞行器燃料，所述第一实体远离飞机（104 ）; 并且在加油过程期间，在飞机（104）和第二实体（例如，油罐飞机（102））之间发送数据，第二实体远离飞行器（104）。该数据作为具有在50GHz至70GHz范围内的频率的射频信号发送。优选地，数据作为具有在57GHz至66GHz范围内的频率（例如60GHz）的射频信号发送。

3. 发明申请

WO2014088680A3 SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS 审中-公开
标题翻译：长期航空运行的系统和方法
公开(公告)号：WO2014088680A3
公开(公告)日：2014-08-28
申请号：PCT/US2013060978
申请日：2013-09-20
申请人： HEPPE STEPHEN
发明人： HEPPE STEPHEN
IPC分类号： B64B1/06 , B64C37/02
CPC分类号： B64C37/02 , B64B1/06 , B64C2201/022 , B64C2201/063
摘要： In one example, a long endurance airship system includes a payload airship (210) and a first logistics airship (260) mechanically joined to the payload airship to form a first combined airship, the payload airship and the logistics airship having design capabilities differing by at least a factor of two with regard to at least one of: power generation capability, propulsion capability, endurance capability, and lift capability, in which the first combined airship is free flying, lighter-than-air, and configured to maintain aloft for greater than 30 days without physical connection to the ground. Illustrative methods for long endurance airship operations are also provided.
摘要翻译：在一个示例中，长期耐力飞艇系统包括有效载人飞艇（210）和机械地连接到有效载客飞艇上的第一物流飞艇（260），以形成第一组合飞艇，有效载运飞艇和后勤飞艇具有不同于关于发电能力，推进能力，耐力能力和提升能力中的至少一个，至少有两个因素，其中第一组合的飞艇是自由飞行的，比空气轻，并且被配置为保持更高的高度超过30天，没有物理连接到地面。还提供了长期耐力飞艇作业的说明性方法。

4. 发明申请

WO2012125639A1 SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS 审中-公开
标题翻译：长期航空运行的系统和方法
公开(公告)号：WO2012125639A1
公开(公告)日：2012-09-20
申请号：PCT/US2012/028931
申请日：2012-03-13
申请人： HEPPE, Stephen
发明人： HEPPE, Stephen
IPC分类号： B64B1/06 , B64C37/02
CPC分类号： B64B1/32 , B64B1/06 , B64C37/02 , B64C2201/022 , B64C2201/063
摘要： In one example, a long endurance airship system includes a payload airship and a first logistics airship mechanically joined to the payload airship to form a first combined airship, the payload airship and the logistics airship having design capabilities differing by at least a factor of two with regard to at least one of: power generation capability, propulsion capability, endurance capability, and lift capability, in which the first combined airship is free flying, lighter-than-air, and configured to maintain stationkeeping for greater than 30 days. Illustrative methods for long endurance airship operations are also provided.
摘要翻译：在一个例子中，长期耐力飞艇系统包括有效载运飞艇和与有效载客飞艇机械连接以形成第一组合飞艇的第一物流飞艇，有效载客飞艇和具有至少两倍的设计能力的物流飞艇，至少有以下至少一种：发电能力，推进能力，耐力能力和提升能力，其中第一组合飞艇自由飞行，轻于空中，并配置为维持停机时间超过30天。还提供了长期耐力飞艇作业的说明性方法。

5. 发明申请

WO2017147188A1 SYSTEMS AND METHODS FOR UNMANNED AERIAL VEHICLES 审中-公开
标题翻译：用于无人机的系统和方法
公开(公告)号：WO2017147188A1
公开(公告)日：2017-08-31
申请号：PCT/US2017/018951
申请日：2017-02-22
申请人： CULVER, Matthew
发明人： CULVER, Matthew
IPC分类号： B64D47/08 , B64F3/02
CPC分类号： B64D47/08 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/063 , B64C2201/108 , B64C2201/127 , B64D1/16 , B64D39/00 , B64F3/02 , Y02T50/53
摘要： An unmanned aerial system (UAS) may comprise an unmanned aerial vehicle (UAV), a portable power source, and a tether connecting a UAV to a portable power source. The tether may transmit power from the portable power source to the UAV. The UAS may be controlled by a remote control, which may command the UAV to surveil a location and transmit images back to the controller. The UAV may further include one or more components attached to the UAV, such as a camera, surveillance equipment, a Taser®, a LED strobe light, laser, or a claw. A remote control may control the flight of the UAV as well as the functionality of the one or more components. The UAS may be configured to, for example, surveil a location, intercept an intruder, inspect a building, and/or perform crowd control.
摘要翻译：无人机系统（UAS）可以包括无人飞行器（UAV），便携式电源以及将UAV连接到便携式电源的系绳。绳索可以将电力从便携式电源传输到无人飞行器。 UAS可以由遥控器控制，遥控器可以命令UAV监视位置并将图像传回控制器。无人飞行器可以进一步包括附接到无人飞行器的一个或多个部件，诸如照相机，监视设备，Taser＆reg;，LED频闪灯，激光器或爪。遥控器可以控制无人飞行器的飞行以及一个或多个部件的功能。 UAS可以被配置为例如监视位置，拦截入侵者，检查建筑物和/或执行人群控制。

6. 发明申请

WO2014088680A2 SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS 审中-公开
标题翻译：长期航空运行的系统和方法
公开(公告)号：WO2014088680A2
公开(公告)日：2014-06-12
申请号：PCT/US2013/060978
申请日：2013-09-20
申请人： HEPPE, Stephen
发明人： HEPPE, Stephen
IPC分类号： B64B1/06
CPC分类号： B64C37/02 , B64B1/06 , B64C2201/022 , B64C2201/063
摘要： In one example, a long endurance airship system includes a payload airship and a first logistics airship mechanically joined to the payload airship to form a first combined airship, the payload airship and the logistics airship having design capabilities differing by at least a factor of two with regard to at least one of: power generation capability, propulsion capability, endurance capability, and lift capability, in which the first combined airship is free flying, lighter-than-air, and configured to maintain aloft for greater than 30 days without physical connection to the ground. Illustrative methods for long endurance airship operations are also provided.
摘要翻译：在一个例子中，长期耐力飞艇系统包括有效载运飞艇和与有效载客飞艇机械连接以形成第一组合飞艇的第一物流飞艇，有效载客飞艇和具有至少两倍的设计能力的物流飞艇，至少有以下至少一个：发电能力，推进能力，耐力能力和升力能力，其中第一组合飞艇是自由飞行的，比空中轻，并且被配置为在没有物理连接的情况下保持高达30天以上到地面。还提供了长期耐力飞艇作业的说明性方法。

7. 发明申请

WO2017087399A1 MICRO HYBRID GENERATOR SYSTEM DRONE 审中-公开
标题翻译：微型混合发电机系统无人机
公开(公告)号：WO2017087399A1
公开(公告)日：2017-05-26
申请号：PCT/US2016/062060
申请日：2016-11-15
申请人： TOP FLIGHT TECHNOLOGIES, INC.
发明人： PHAN, Long N. , SARMA, Sanjay Emani , WOJCIK, Cody Miles , DAVIS, Eli M. , SENA, Benjamin Arthur , LEMUS, Julian
IPC分类号： B64C39/02 , B64D27/24
CPC分类号： B64C39/024 , B64C27/001 , B64C27/08 , B64C2201/027 , B64C2201/042 , B64C2201/044 , B64C2201/063 , B64C2201/066 , B64C2201/108 , B64D1/08 , B64D1/22 , B64D27/02 , B64D27/24 , B64D33/08 , B64D2027/026 , B64D2221/00 , B64F3/02 , G05D1/101 , Y02T50/44 , Y02T50/64
摘要： An unmanned aerial vehicle comprising at least one rotor motor. The rotor motor is powered by a micro hybrid generation system. The micro hybrid generator system comprises a rechargeable battery configured to provide power to the at least one rotor motor, a small engine configured to generate mechanical power, a generator motor coupled to the small engine and configured to generate AC power using the mechanical power generated by the small engine, a bridge rectifier configured to convert the AC power generated by the generator motor to DC power and provide the DC power to either or both the rechargeable battery and the at least one rotor motor, and an electronic control unit configured to control a throttle of the small engine based, at least in part, on a power demand of at least one load, the at least one load including the at least one rotor motor.
摘要翻译：包括至少一个转子电动机的无人驾驶飞行器。转子电机由微混合发电系统供电。微混合发电机系统包括：可充电电池，被配置为向至少一个转子电动机提供电力;小型发动机，配置成产生机械动力;发电机电动机，连接到小型发动机并配置为使用由小型发动机，被配置为将发电机马达产生的AC电力转换成DC电力并将DC电力提供给可再充电电池和至少一个转子电动机中的任一者或两者的桥式整流器，以及电子控制单元，小型发动机的节气门至少部分地基于至少一个负载的功率需求，所述至少一个负载包括至少一个转子电动机。

8. 发明申请

WO2015057832A1 MOTOR VEHICLE WITH CAPTIVE AIRCRAFT 审中-公开
标题翻译：具有主动飞机的电动车
公开(公告)号：WO2015057832A1
公开(公告)日：2015-04-23
申请号：PCT/US2014/060681
申请日：2014-10-15
申请人： ELWHA LLC , HYDE, Roderick A. , WOOD, Lowell L., Jr.
发明人： HYDE, Roderick A. , WOOD, Lowell L., Jr. , DUNCAN, William David , KARE, Jordin T. , MALASKA, Stephen L. , MYHRVOLD, Nathan P. , PETROSKI, Robert C. , WEAVER, Thomas Allan
IPC分类号： B62D63/02 , B62D63/04 , B64F3/02 , B64D39/00
CPC分类号： B64C39/024 , B64C39/022 , B64C2201/021 , B64C2201/042 , B64C2201/046 , B64C2201/063 , B64C2201/066 , B64C2201/12 , B64C2201/127 , B64C2201/145 , B64C2201/146 , B64C2201/208 , B64F1/00 , G05D1/0094
摘要： A motor vehicle system includes a motor vehicle including an aircraft landing portion, and an actively propelled unmanned aircraft configured to be supported on the aircraft landing portion. The vehicle and aircraft are configured such that the vehicle can provide at least one of fuel and electrical energy to the aircraft while the aircraft is supported on the aircraft landing portion.
摘要翻译：机动车辆系统包括包括飞行器着陆部分的机动车辆和被配置为被支撑在飞行器着陆部分上的主动推进无人飞行器。车辆和飞行器构造成使得当飞行器被支撑在飞行器着陆部分上时，车辆能够向飞机提供燃料和电能中的至少一种。

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