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71. 发明授权

US09598181B2 Device for fastening a fluid transport circuit to an element of the structure of an aircraft and related aircraft 有权
公开(公告)号：US09598181B2
公开(公告)日：2017-03-21
申请号：US13688851
申请日：2012-11-29
申请人： AIRBUS OPERATIONS
发明人： Robert Rossato , Alexis Courpet
IPC分类号： F16L3/12 , B64D47/00 , B64D45/02
CPC分类号： B64D47/00 , B64D45/02 , F16L3/1222 , F16L39/005
摘要： A fastening device (10) is disclosed for attaching a fluid transport circuit to an element of a structure of an aircraft, with the fluid transport circuit containing two portions (23, 42), each of which is made up of an external tube (22, 44) positioned around an internal tube (21, 43). The fastening device (10) is positioned at a connection (40) between the two portions (23, 42) of the fluid transport circuit, and contains a body (26) with a plate (27) to attach the fastening device (10) to an element (61) of the structure of the aircraft. The body (26) provides at least one sealed connection between the external tubes (22, 44) of the two portions (23, 42) and a support system provides a constant radial clearance between the internal tubes (21, 43) and the external tubes (22, 44) of the two portions (23, 42) of the fluid transport circuit.

72. 发明申请

US20160329705A1 Modular and reconfigurable electrical power conversion device 审中-公开
标题翻译：模块化和可重新配置的电力转换装置
公开(公告)号：US20160329705A1
公开(公告)日：2016-11-10
申请号：US14574852
申请日：2014-12-18
申请人： THALES
发明人： Frederic LACAUX , Christophe BRUZY , Jacques CASUTT
IPC分类号： H02J1/00 , B64D47/00 , H02M1/44 , H02M7/68 , H02M1/08
CPC分类号： H02J1/00 , B64D47/00 , H02M1/083 , H02M1/126 , H02M1/44 , H02M7/493 , H02M7/68 , H02M2001/123
摘要： A device for powering a plurality of loads from an electrical energy supply network, comprises a number of converters, supplied with electrical energy by the network, ensuring the conversion and the supply of electrical energy for at least one load. The device comprises a control member making it possible to associate a number of converters in parallel to power at least one load, in response to a power requirement from the at least one load. Each of the converters comprises distributed means for limiting recirculation currents generated by the parallel association of a number of converters.
摘要翻译：用于从电能供应网络供电多个负载的装置包括由网络提供电能的多个转换器，确保至少一个负载的电能的转换和供应。该装置包括控制构件，使得可以响应于来自至少一个负载的功率需求并联多个并联的转换器来对至少一个负载供电。每个转换器包括用于限制由多个转换器的并联产生的再循环电流的分布式装置。

73. 发明申请

US20160311531A1 High Altitude, Long Endurance, Unmanned Aircraft and Methods of Operation Thereof 有权
标题翻译：高海拔，长寿命，无人驾驶飞机及其操作方法
公开(公告)号：US20160311531A1
公开(公告)日：2016-10-27
申请号：US15082983
申请日：2016-03-28
申请人： AEROVIRONMENT, INC.
发明人： Edward Oscar Rios
IPC分类号： B64C39/02 , G01S19/11 , G01S19/21 , G05D1/10 , B64D47/00
CPC分类号： B64C39/024 , B64C2201/122 , B64C2201/145 , B64D43/00 , B64D47/00 , G01C21/00 , G01S19/11 , G01S19/21 , G05D1/0022 , G05D1/0027 , G05D1/104 , H04B7/18504
摘要： Embodiments include one or more high altitude, long endurance (HALE) unmanned aircraft capable of persistent station-keeping having one or more electromagnetic (IR/Visual/RF) sensor elements or suites for purposes of survey and/or signal gathering. Embodiments include one or more high altitude, long endurance (HALE) unmanned aircraft capable of persistent station-keeping having a directable laser. Embodiments include a group of four or more high altitude, long endurance (HALE) unmanned aircraft configured as GPS repeaters.
摘要翻译：实施例包括一个或多个能够持续驻留的具有一个或多个电磁（IR / Visual / RF）传感器元件或套件以用于测量和/或信号收集的高空，长寿命（HALE）无人飞行器。实施例包括能够持续驻留具有可定向激光的一个或多个高空，长寿命（HALE）无人飞行器。实施例包括配置为GPS中继器的一组四个或更多的高空，长寿命（HALE）无人飞行器。

74. 发明申请

US20160298765A1 METAL MESH WITH A LOW ELECTRICAL RESISTANCE CONVERSION COATING FOR USE WITH AIRCRAFT STRUCTURES 审中-公开
标题翻译：具有低电阻转换涂层的金属网与飞机结构一起使用
公开(公告)号：US20160298765A1
公开(公告)日：2016-10-13
申请号：US15094571
申请日：2016-04-08
申请人： AVIATION DEVICES & ELECTRONIC COMPONENTS, L.L.C.
发明人： JEFF BUSBY , KENT BOOMER , MATT BOOMER , EMILY SAMUELSON
IPC分类号： F16J15/02 , B64D37/00 , B64D47/00 , B64C1/14
CPC分类号： F16J15/022 , B64C7/00 , B64D37/005 , B64D47/00 , F16J15/122
摘要： A gasket is provided with a tacky polyurethane or polyurea gel body and a metallic mesh skeleton where the skeleton has been coated with a conversion coating. The conversion coating helps reduce corrosion in the gasket and corrosion on the parts that place the gasket under compression, especially where an environment conducive to galvanic corrosion is present. This gasket may then be used in assemblies which include aircraft parts, which parts may be subject to extreme environmental conditions.
摘要翻译：垫圈设置有粘性聚氨酯或聚脲凝胶体和金属网骨架，其中骨架已经涂覆有转化涂层。转换涂层有助于减少垫片中的腐蚀和将垫片压缩的部件上的腐蚀特别是存在有助于电腐蚀的环境时。然后，该垫圈可用于包括飞机部件的组件中，该部件可能经受极端的环境条件。

75. 发明申请

US20160297544A1 ELECTRIC POWER SUPPLY SYSTEM HAVING ACTIVE POWER CONTROL DEVICE 有权
标题翻译：具有主动功率控制装置的电力系统
公开(公告)号：US20160297544A1
公开(公告)日：2016-10-13
申请号：US15031933
申请日：2013-10-29
申请人： KOREA AEROSPACE RESEARCH INSTITUTE
发明人： Keun Bae KIM , Bo Hwa LEE , Poo Min PARK , Chun Taek KIM , Seok Min AHN , Soon Bae CHUNG , Dong Sung KIM
IPC分类号： B64D47/00 , H02J9/06 , H02J7/35 , H02J3/38
CPC分类号： B64D47/00 , B64D27/24 , B64D2041/005 , B64D2211/00 , B64D2221/00 , H02J1/00 , H02J3/383 , H02J3/387 , H02J7/0068 , H02J7/34 , H02J7/35 , H02J9/06 , H02J2001/004 , Y02E10/563 , Y02T50/64 , Y02T90/36
摘要： As a component of an aerial vehicle, a power management system having an active power control device is provided. The system includes a solar cell converting solar energy into electric energy; a fuel cell provided in the aerial vehicle and converting fuel energy into electric energy by electrochemical reaction; a battery compensating for a lack of electric power supplied from the solar cell and the fuel cell to the aerial vehicle and storing surplus electric power; and an active power control device connecting with all the solar cell, the fuel cell and the battery and combining and distributing electric power generated in the solar cell, the fuel cell and the battery to loads. The system efficiently distributes the power from the respective power sources through the controllable output of the fuel cell in accordance with power required by the aerial vehicle and the solar cell's performance depending on weather.
摘要翻译：作为飞行器的组件，提供了具有有功功率控制装置的电力管理系统。该系统包括将太阳能转换为电能的太阳能电池; 燃料电池，其设置在飞行器中并通过电化学反应将燃料能量转化为电能; 补偿从太阳能电池和燃料电池供给到飞行器的电力不足而存储剩余电力的电池; 以及与所有太阳能电池，燃料电池和电池连接并且将太阳能电池，燃料电池和电池中产生的电力组合和分配的有源电力控制装置负载。根据天气要求，系统根据飞行器所需的功率和太阳能电池的性能，有效地分配来自各个电源的功率通过燃料电池的可控输出。

76. 发明授权

US09459190B2 Fuel tank contaminant prediction 有权
标题翻译：燃油箱污染物预测
公开(公告)号：US09459190B2
公开(公告)日：2016-10-04
申请号：US13667669
申请日：2012-11-02
申请人： AIRBUS OPERATIONS LIMITED
发明人： Joseph K-W Lam , Franklin Tichborne , Simon Masters , David Parmenter
IPC分类号： G01N33/22 , G01F23/22 , B64D37/00 , B67D7/08 , B67D99/00 , B64D47/00 , G06F17/40 , G06F19/00 , G01N7/00 , G01N33/28 , B64D37/32 , G06F15/00
CPC分类号： G01N7/00 , B64D37/00 , B64D37/32 , B64D47/00 , B67D7/08 , B67D99/00 , G01F23/22 , G01N33/22 , G01N33/2835 , G06F15/00 , G06F17/40 , G06F19/00
摘要： A method for predicting a quantity of a contaminant in a fuel tank at the end of a time period, the method comprising the steps of: determining a quantity of the contaminant in the fuel tank at the start of the time period; determining at least one operating condition of the fuel tank during the time period; using information relating to the at least one operating condition of the fuel tank to generate a predicted quantity of the contaminant accumulated in the fuel tank during the time period; and calculating, based upon the quantity of the contaminant at the start of the time period and the predicted quantity of the contaminant accumulated during the time period, a predicted quantity of the contaminant at the end of a time period.
摘要翻译：一种用于在时间段结束时预测燃料箱中的污染物的量的方法，所述方法包括以下步骤：在所述时间段开始时确定所述燃料箱中的污染物的量; 在该时间段内确定燃料箱的至少一个操作状态; 使用与所述燃料箱的所述至少一个运转状态有关的信息，生成在所述时间段内累积在所述燃料箱中的污染物的预测量; 以及基于所述时间段开始时的所述污染物的量和所述时间段内累积的所述污染物的预测量，计算出在时间段结束时的所述污染物的预测量。

77. 发明授权

US09403593B2 Distributed unmanned aerial vehicle architecture 有权
公开(公告)号：US09403593B2
公开(公告)日：2016-08-02
申请号：US15019165
申请日：2016-02-09
申请人： Unmanned Innovation, Inc.
发明人： Jonathan Downey , Bernard J. Michini , Brian Richman
IPC分类号： G01C23/00 , B64C39/02 , B64D47/00
CPC分类号： H04L47/25 , B64C39/024 , B64C2201/126 , B64C2201/127 , B64C2201/128 , B64C2201/145 , B64D41/00 , B64D47/00 , B64D47/08 , G01C23/00 , G05D1/0022
摘要： Methods, systems, and apparatus, including computer programs encoded on computer storage media, for a distributed system architecture for unmanned air vehicles. One of the methods includes obtaining information identifying flight information of a UAV, with the flight information including flight phase information or a contingency condition associated with a flight critical module included in the UAV. The obtained information is analyzed, and one or more first payload modules are determined to enter a modified power state. Requests to enter the modified power state are caused to be transmitted to each determined payload module in the one or more first payload modules.

78. 发明授权

US09394058B2 Method for controlling an obstruction light and a wind park for carrying out such a method 有权
标题翻译：用于控制障碍物的方法和用于执行这种方法的风力发电场
公开(公告)号：US09394058B2
公开(公告)日：2016-07-19
申请号：US14359889
申请日：2012-11-09
申请人： Wobben Properties GmbH
发明人： Stephan Harms , Gerd Moller
IPC分类号： B64D47/06 , B64D45/00 , F03D7/04 , F03D11/00 , B64D47/00 , G08B5/22 , G08B1/08
CPC分类号： B64D45/00 , F03D7/048 , F03D80/10 , F05B2270/303 , F05B2270/333 , Y02E10/722 , Y02E10/723
摘要： The invention concerns a method of controlling the flight lighting arrangement of a wind park by means of acoustic monitoring or wind park comprising one or more wind power installations, wherein the wind park has an acoustic monitoring device having a microphone arrangement, wherein the microphone arrangement records sound signals, noises or the like from the environment of the wind park and said sound signals are processed in a signal processing device connected to the microphone arrangement, wherein there is provided a switching device for switching on a flight lighting arrangement of at least one wind power installation of the wind park and the switching device is coupled to and controlled by the signal processing device so that the signal processing device causes the switching device to switch on the flight lighting arrangement if a sound signal of a flying object, for example an aircraft or a helicopter, is detected by means of the acoustic monitoring device, and/or a predetermined sound signal (for example sine sound) is superposed and/or falsified by the noises of the flying object.
摘要翻译：本发明涉及一种通过包括一个或多个风力发电设备的声学监测或风力发电场来控制风力发电场的飞行照明装置的方法，其中风力发电场具有具有麦克风装置的声学监测装置，其中麦克风装置记录来自风力发电场环境的声音信号，噪声等，并且所述声音信号在连接到麦克风装置的信号处理装置中被处理，其中设置有用于接通至少一个风的飞行照明装置的开关装置风力发电场和开关装置的电力安装耦合到信号处理装置并由其控制，使得如果飞行物体（例如飞行器）的声音信号，则信号处理装置使开关装置接通飞行照明装置或直升机，通过声学监测装置和/或预定义来检测（例如正弦声）被飞行物体的噪声叠加和/或伪造。

79. 发明授权

US09394051B2 Modular pod system for aircraft 有权
标题翻译：飞机模块化吊舱系统
公开(公告)号：US09394051B2
公开(公告)日：2016-07-19
申请号：US13926953
申请日：2013-06-25
申请人： The Boeing Company
发明人： Craig C. M. Chun , Lyle E. Picard , Frank Dugger , Harold A. Koehler , Paul L. Wynns , George Hall , Glen W. Cunningham , Arthur Jules Rosenwach , Justin Kearns
IPC分类号： B64D47/00 , B64D7/00 , B64C7/00 , B64D9/00 , H01Q1/28
CPC分类号： B64D7/00 , B64C7/00 , B64D9/00 , B64D47/00 , H01Q1/28
摘要： A mission pod system for an aircraft set to perform a mission includes a fixed portion that is fixedly secured to an exterior surface of the aircraft. The mission pod system also includes a modular portion that is removably secured to the fixed portion and spaced away from the exterior surface of the aircraft via the fixed portion. The modular portion includes an entirety of mission-specific components.
摘要翻译：用于执行任务的飞行器的任务舱系统包括固定地固定在飞行器的外表面上的固定部分。任务舱系统还包括可拆卸地固定到固定部分并经由固定部分与飞机的外表面间隔开的模块化部分。模块化部分包括整个任务特定组件。

80. 发明申请

US20160198591A1 PASSIVE AIRCRAFT COOLING SYSTEMS AND METHODS 审中-公开
标题翻译：被动飞机冷却系统和方法
公开(公告)号：US20160198591A1
公开(公告)日：2016-07-07
申请号：US14322133
申请日：2014-07-02
申请人： EMBRAER S.A. , UNIVERSIDADE FEDERAL DE SANTA CATARINA (UFSC)
发明人： Ricardo Gandolfi , Luiz Gonzaga De Souza Ribeiro , Marcia Barbosa Henriques Mantelli , Jorge Luiz Goes Oliveira , Kleber Vieira De Paiva
IPC分类号： H05K7/20 , B64D47/00
CPC分类号： B64D47/00 , B64D2013/0614 , B64D2013/0625 , B64D2013/064 , B64D2013/0674 , B64D2013/0688 , F28D15/0266 , H05K7/20245 , H05K7/2029
摘要： Passive on-board aircraft cooling systems are provided with an evaporator/receiver in heat-exchange relationship with at least one heat source on board the aircraft, the evaporator/receiver containing a liquid phase working fluid which changes state to a vapor phase working fluid in response to heat transfer therefrom from the at least one heat source. First and second condensers are fluid-connected to the evaporator/receiver for receiving vapor phase working fluid from the evaporator/receiver. An aircraft-internal pressurized air supply stream is provided in heat-exchange relationship with the second condenser, and an aircraft-external unpressurized air supply stream is provided in heat-exchange relationship with the first condenser. At least a portion of the vapor phase working fluid transferred to the first and second condensers is thus condensed by heat transfer between the first and second condensers and the unpressurized and pressurized air supply streams, respectively, to thereby form liquid phase working fluid which returns to the evaporator/receiver by virtue of the fluid connection with the first and second condensers.
摘要翻译：被动机载飞机冷却系统设置有与飞机上的至少一个热源热交换关系的蒸发器/接收器，蒸发器/接收器包含将状态改变为气相工作流体的液相工作流体对来自至少一个热源的热量的响应。第一和第二冷凝器流体连接到蒸发器/接收器，用于从蒸发器/接收器接收气相工作流体。与第二冷凝器以热交换关系提供飞机内部加压空气供应流，并且与第一冷凝器以热交换关系提供飞机外部未加压空气供应流。因此，转移到第一和第二冷凝器的气相工作流体的至少一部分分别通过第一和第二冷凝器与未加压和加压的空气供应流之间的热传递而被冷凝，从而形成液相工作流体，其返回到该蒸发器/接收器借助于与第一和第二冷凝器的流体连接。

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