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111. 发明申请

US20160001894A1 SKEW SENSING ARRANGEMENT 有权
标题翻译： SKEW感应装置
公开(公告)号：US20160001894A1
公开(公告)日：2016-01-07
申请号：US14707575
申请日：2015-05-08
申请人： Goodrich Actuation Systems Limited
发明人： Tony JONES
IPC分类号： B64D45/00 , B64C9/16
CPC分类号： B64D45/0005 , B64C9/16 , B64D2045/001
摘要： A skew detection system for a high lift system for an aircraft, wherein pairs of sensors 4a, 4b provide an onboard determination of relative skew between the sensors of each pair as an indication of skew of a flap of the high lift system.
摘要翻译：用于飞行器的高升力系统的偏斜检测系统，其中成对的传感器4a，4b提供每对传感器之间的相对偏差的板上确定，作为高升程系统的翼片的偏斜的指示。

112. 发明授权

US09170092B2 System for detecting misalignment of an aero surface 有权
标题翻译：用于检测航空表面未对准的系统
公开(公告)号：US09170092B2
公开(公告)日：2015-10-27
申请号：US13996276
申请日：2011-12-19
申请人： Phillip Vincent Teague
发明人： Phillip Vincent Teague
IPC分类号： G01B11/14 , B64D45/00
CPC分类号： G01B11/14 , B64D45/0005 , B64D2045/001
摘要： A system for detecting misalignment of an aero surface relative to other aero surfaces during simultaneous deployment of the aero surfaces is disclosed. A generator configured to shine a laser through aligned apertures in a series of aero surfaces towards a reflector during deployment of the aero surfaces, a receptor to detect reflection of the laser from the reflector back through the apertures to the generator and, a controller operable to terminate further deployment of the aero surfaces in the event that no reflection is detected by the receptor, or if an actual time taken for the reflected beam of light to be detected by the receptor differs from a predetermined time.
摘要翻译：公开了一种用于在同时展开航空表面期间检测航空表面相对于其他航空表面的未对准的系统。一种发光器，被配置为在航空表面的展开期间将激光照射到一系列航空表面中的对准的孔朝向反射器;接收器，用于检测来自反射器的激光从反射器反射回到发生器的反射器;以及控制器，在受体没有检测到反射的情况下，或者如果受体的反射光束所需的实际时间与预定时间不同，则终止气动表面的进一步展开。

113. 发明申请

US20150268110A1 LOAD SENSING SYSTEM 有权
标题翻译：负载感应系统
公开(公告)号：US20150268110A1
公开(公告)日：2015-09-24
申请号：US14666955
申请日：2015-03-24
申请人： GOODRICH ACTUATION SYSTEMS SAS
发明人： Laurent Schwartz , Arnaud de la Chevasnerie
IPC分类号： G01L5/00
CPC分类号： G01L5/0061 , B64C13/24 , B64D45/0005 , B64D2045/0085 , F16C19/522 , F16H25/2021 , F16H2057/016 , G01L1/18 , G01L5/0009 , G01L5/0019 , G01L5/12
摘要： An actuator including a pair of load sensors arranged in the load path through the actuator. The load sensors are antagonistically preloaded and their outputs electrically connected to a processor for calculating a load in the actuator from the difference in loads measured by the respective load sensors.
摘要翻译：包括一对负载传感器的致动器，其布置在通过致动器的负载路径中。负载传感器是对抗性预加载的，并且其输出电连接到处理器，用于根据由各个负载传感器测量的负载差来计算致动器中的负载。

114. 发明申请

US20150191257A1 Aircraft nacelle comprising a device providing a visual warning of a locking fault of the cowls 有权
标题翻译：飞机机舱包括提供整流罩的锁定故障的视觉警告的装置
公开(公告)号：US20150191257A1
公开(公告)日：2015-07-09
申请号：US14575089
申请日：2014-12-18
申请人： Airbus Operations (SAS)
发明人： Jacques Herve Marche
IPC分类号： B64D45/00 , B64D29/06
CPC分类号： B64D45/0005 , B64D29/06 , E05B41/00 , F01D25/24 , F05B2240/14 , F05D2240/14
摘要： An aircraft nacelle comprising a first and a second cowl mounted pivotably about an axis substantially parallel to a longitudinal axis of the nacelle and lockable to one another by at least one locking mechanism. The nacelle further comprises a device for providing a visual warning of a locking defect of the cowls. The device comprises a movable bolt associated with the locking mechanism and a movable edge plate mounted on the nacelle in line with said bolt with which it is associated, the movable edge plate being movable under the action of an operator between a protruding position, in which the edge plate is protruding from the nacelle and a locking mechanism is in an unlocked position, and a retracted position, in which the edge plate is immobilized within the nacelle by the bolt and the action of the locking of a locking mechanism.
摘要翻译：一种飞机机舱，包括第一和第二整流罩，所述第一和第二整流罩围绕基本上平行于所述机舱的纵向轴线的轴线可枢转地安装，并且可通过至少一个锁定机构彼此锁定。机舱还包括用于提供整流罩的锁定缺陷的视觉警告的装置。该装置包括与锁定机构相关联的可移动螺栓和安装在机舱上的可移动边缘板，与其相关联的所述螺栓对齐，可动边缘板可在操作者的作用下在突出位置之间移动，边缘板从机舱突出并且锁定机构处于解锁位置，并且缩回位置，其中边缘板通过螺栓固定在机舱内以及锁定机构的作用。

115. 发明申请

US20150175273A1 WARNING SYSTEM OF AIRCRAFT AND AIRCRAFT 有权
标题翻译：警告飞机和飞机系统
公开(公告)号：US20150175273A1
公开(公告)日：2015-06-25
申请号：US14186137
申请日：2014-02-21
申请人： Mitsubishi Aircraft Corporation
发明人： Masaya MIYOSHI
IPC分类号： B64D45/00
CPC分类号： B64D45/0005 , B64C13/10
摘要： A warning system 10 that warns of saturation of the control capability for the moving surface such as an elevator 4 and a rudder 8 of an aircraft has a determination section 31 that determines whether or not the control capability for the moving surface is saturated, and a display 50 that issues a warning when the determination section 31 determines that the control capability for the moving surface is saturated. The determination section 31 determines that the control capability for the elevator 4 is saturated, when a control target position of the elevator 4 by, for example, a control stick (column) is larger than a first reference position indicating an operation limit of the elevator 4, and a present position of the column is smaller than a second reference position indicating an operation limit of the column.
摘要翻译：警告系统10，其对运动面的控制能力饱和，例如飞机的电梯4和方向舵8具有确定部31，其确定移动表面的控制能力是否饱和，当确定部分31确定移动表面的控制能力饱和时发出警告的显示器50。当电梯4的控制目标位置例如控制棒（列）大于指示电梯的操作限制的第一参考位置时，确定部31确定电梯4的控制能力饱和 4，并且列的当前位置小于指示列的操作限制的第二参考位置。

116. 发明申请

US20150108283A1 Wingtip Control System 有权
标题翻译： Wingtip控制系统
公开(公告)号：US20150108283A1
公开(公告)日：2015-04-23
申请号：US14056475
申请日：2013-10-17
申请人： The Boeing Company
发明人： Adam Marshall Thoreen , Joshua Jay Baer , Joseph Adam Sikora , Matthew August Lassen , Michael Edwin Foster , Timothy P. Gallagher
IPC分类号： B64C13/04 , B64C23/06
CPC分类号： B64D45/0005 , B64C3/38 , B64C3/56 , B64C9/00 , B64C13/04 , B64C23/065 , B64C23/072 , B64C2009/005 , B64D45/00 , Y02T50/14 , Y02T50/145 , Y02T50/164
摘要： A method and apparatus for a wingtip control system. The wingtip control system comprises a switch system for a flight deck of an aircraft and a controller. The switch system is configured to be placed into an armed state and generate an armed signal. The controller is in communication with the switch system. The controller is configured to receive the armed signal from the switch system, visually indicate a desired position for a wingtip of the aircraft in the switch system in response to an event occurring during operation of the aircraft, and generate a movement command to move the wingtip.
摘要翻译：一种翼尖控制系统的方法和装置。翼尖控制系统包括用于飞行器的驾驶舱和控制器的开关系统。开关系统被配置成被置于无效状态并产生一个布防信号。控制器与交换机系统通信。控制器被配置为响应于在飞行器的操作期间发生的事件，从开关系统接收布防信号，在视觉上指示飞行器在开关系统中的翼尖的期望位置，并且产生移动指令以移动翼尖。

117. 发明授权

US08989953B2 Method for predicting a trailing edge flap fault 有权
标题翻译：预测后缘襟翼故障的方法
公开(公告)号：US08989953B2
公开(公告)日：2015-03-24
申请号：US14065893
申请日：2013-10-29
申请人： GE Aviation Systems Limited
发明人： Christopher Joseph Catt , Julia Ann Howard
IPC分类号： B64F5/00 , B64C9/20 , B64C9/26 , B64C13/10 , B64D45/00
CPC分类号： B64F5/0045 , B64C9/16 , B64C9/20 , B64C9/26 , B64C13/10 , B64D45/0005 , B64D2045/001 , B64F5/60
摘要： A method of predicting a trailing edge flap failure, the method includes receiving a position signal from the position sensor indicative of the position of at least one of the trailing edge flaps, comparing the position signal to a reference position value to define a position comparison, defining a variation comparison and providing an indication of a prediction of a trailing edge flap failure based on the variation comparison.
摘要翻译：一种预测后缘襟翼故障的方法，所述方法包括从所述位置传感器接收指示所述后缘襟翼中的至少一个位置的位置信号，将所述位置信号与参考位置值进行比较以限定位置比较，定义变化比较并且基于变化比较提供后缘皮瓣失效的预测指示。

118. 发明申请

US20150066288A1 METHODS FOR PREDICTING A SPEED BRAKE SYSTEM FAULT 有权
标题翻译：用于预测速度制动系统故障的方法
公开(公告)号：US20150066288A1
公开(公告)日：2015-03-05
申请号：US14536898
申请日：2014-11-10
申请人： GE Aviation Systems Limited
发明人： Christopher Joseph Catt , Julia Ann Howard
IPC分类号： G07C5/08 , G01M17/00
CPC分类号： G07C5/0816 , B64C9/323 , B64C19/00 , B64D45/0005 , B64F5/60 , G01M17/00
摘要： Methods of predicting a speed brake fault in an aircraft having a speed brake system including multiple control surfaces, a handle for setting the position of the multiple control surfaces, and at least one control surface position sensor, the methods include receiving a position signal from the at least one position sensor, determining a variation in the position signal and predicting a fault in the speed brake system.
摘要翻译：在具有包括多个控制面的速度制动系统的飞行器中预测速度制动器故障的方法，用于设定多个控制面的位置的手柄以及至少一个控制面位置传感器，所述方法包括：接收位置信号至少一个位置传感器，确定位置信号的变化并预测速度制动系统中的故障。

119. 发明授权

US08909393B2 Methods for predicting a speed brake system fault 有权
标题翻译：预测速度制动系统故障的方法
公开(公告)号：US08909393B2
公开(公告)日：2014-12-09
申请号：US14065967
申请日：2013-10-29
申请人： GE Aviation Systems Limited
发明人： Christopher Joseph Catt , Julia Ann Howard
IPC分类号： G01C23/00 , G06F7/00 , B64C19/00
CPC分类号： G07C5/0816 , B64C9/323 , B64C19/00 , B64D45/0005 , B64F5/60 , G01M17/00
摘要： Methods of predicting a speed brake fault in an aircraft having a speed brake system including multiple control surfaces, a handle for setting the position of the multiple control surfaces, and at least one control surface position sensor, the methods include receiving a position signal from the at least one position sensor, determining a variation in the position signal and predicting a fault in the speed brake system.
摘要翻译：在具有包括多个控制面的速度制动系统的飞行器中预测速度制动器故障的方法，用于设定多个控制面的位置的手柄以及至少一个控制面位置传感器，所述方法包括：接收位置信号至少一个位置传感器，确定位置信号的变化并预测速度制动系统中的故障。

120. 发明申请

US20140347482A1 OPTICAL IMAGE MONITORING SYSTEM AND METHOD FOR UNMANNED AERIAL VEHICLES 审中-公开
标题翻译：光学图像监测系统和无人驾驶飞行器的方法
公开(公告)号：US20140347482A1
公开(公告)日：2014-11-27
申请号：US14299979
申请日：2014-06-09
申请人： Robert V. Weinmann , Joshua N. Gelinske , Robert M. Allen , Johan A. Wiig , Joseph A. Heilman , Jeffrey L. Johnson , Jonathan L. Tolstedt
发明人： Robert V. Weinmann , Joshua N. Gelinske , Robert M. Allen , Johan A. Wiig , Joseph A. Heilman , Jeffrey L. Johnson , Jonathan L. Tolstedt
IPC分类号： B64D43/00 , H04N5/247 , G06T7/00 , B64C39/02
CPC分类号： G06T7/0002 , B64C39/024 , B64C2201/146 , B64D45/00 , B64D45/0005 , G06K2209/03 , G06T2207/10032 , G06T2207/30252 , G07C5/0866 , H04N5/247
摘要： A system and method of acquiring information from an image of a vehicle in real time wherein at least one imaging device with advanced light metering capabilities is placed aboard a unmanned aerial vehicle, a computer processor means is provided to control the imaging device and the advanced light metering capabilities, the advanced light metering capabilities are used to capture an image of at least a portion of the unmanned aerial vehicle, and image recognition algorithms are used to identify the current state or position of the corresponding portion of the unmanned aerial vehicle.
摘要翻译：一种实时地从车辆图像获取信息的系统和方法，其中至少一个具有高级测光能力的成像装置放置在无人驾驶飞行器上，提供计算机处理器装置以控制成像装置和先进光高级测光功能用于捕获至少一部分无人驾驶飞行器的图像，并且使用图像识别算法来识别无人机的相应部分的当前状态或位置。

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