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21. 发明申请

WO2015135951A1 ROTATING-WING DRONE, WITH INTRINSICALLY PROTECTIVE AND ACCIDENT PREVENTION SUPPORTING STRUCTURE 审中-公开
标题翻译：旋转扶手，具有内在保护和意外防护支持结构
公开(公告)号：WO2015135951A1
公开(公告)日：2015-09-17
申请号：PCT/EP2015/054984
申请日：2015-03-10
申请人： G.A.M. PROGETTI DI GUZZARDI ANDREA E GUFFANTI MARCO SNC
发明人： GUZZARDI, Andrea , GUFFANTI, Marco , TARTARINI, Gian Luca , CANEPA, Guido
IPC分类号： B64C39/02
CPC分类号： A63H27/12 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/127 , B64F1/225
摘要： The invention relates to the structure of a rotating-wing drone (30), made of an expanded resin having a density of from 20 to 100 g/1, obtained through expansion of pre-expanded granules inside a mold. The structure comprises a supporting structure (20), a structure for protecting the propellers (35) and a base (22), as well as means (42,45) for fastening photographic equipment or the like.
摘要翻译：本发明涉及通过在模具内部膨胀预发泡颗粒而获得的由密度为20-100g / l的膨胀树脂制成的旋翼机（30）的结构。该结构包括支撑结构（20），用于保护螺旋桨（35）和基座（22）的结构以及用于紧固照相设备等的装置（42,45）。

22. 发明申请

WO2015097457A1 AIR CONDITIONING SYSTEM FOR AN AIRCRAFT MOVER 审中-公开
标题翻译：航空运输机空调系统
公开(公告)号：WO2015097457A1
公开(公告)日：2015-07-02
申请号：PCT/GB2014/053788
申请日：2014-12-19
申请人： TEXTRON GROUND SUPPORT EQUIPMENT UK LIMITED
发明人： KULKARNI, Tushar
IPC分类号： B60H1/00 , B60H1/32 , B64F1/22
CPC分类号： B60H1/00435 , B60H1/00378 , B60H1/3222 , B60H1/3226 , B64F1/225 , Y02T50/826
摘要： An air conditioning system (32) for an aircraft mover (10) motively powered by a driving engine (28). The air conditioning system (32) comprises a supplementary internal-combustion engine (62), a hydraulically powerable compressor (38),an evaporator (40) and a condenser (42) fed by the hydraulically powerable compressor (38), at least one fan (48) associated with the evaporator (40) and powerable by a first electrical output (70) associated with the driving engine (28) and a second electrical output (72) associated with the supplementary internal-combustion engine (62), and a controller (74) for activating the supplementary internal-combustion engine (62), under at least idling stop of the driving engine (28). The supplementary internal-combustion engine (62) hydraulically powers the compressor (38) at substantially constant speed. The invention further relates to an aircraft mover (10) having such an air conditioning system (32), and also to a method of reducing the fuel consumption of an aircraft mover (10).
摘要翻译：一种用于由驱动发动机（28）动力驱动的飞行器动子（10）的空调系统（32）。空调系统（32）包括辅助内燃机（62），液压可驱动压缩机（38），蒸发器（40）和由液压可驱动压缩机（38）供给的冷凝器（42），至少一个与所述蒸发器（40）相关联并且能够通过与所述驱动发动机（28）相关联的第一电输出（70）供电的风扇（48）和与所述辅助内燃机（62）相关联的第二电输出（72），以及在所述驱动发动机（28）的至少怠速停止下，用于启动所述辅助内燃机（62）的控制器（74）。补充内燃机（62）以基本恒定的速度液压地对压缩机（38）供电。本发明还涉及一种具有这种空调系统（32）的飞行器动子（10），并且还涉及一种降低航空器移动器（10）的燃料消耗的方法。

23. 发明申请

US20170294132A1 WEARABLE AIRCRAFT TOWING COLLISION WARNING DEVICES AND METHODS 有权
公开(公告)号：US20170294132A1
公开(公告)日：2017-10-12
申请号：US15092350
申请日：2016-04-06
申请人： Gulfstream Aerospace Corporation
发明人： Simón Colmenares
IPC分类号： G08G5/06 , G06T19/00 , G06K9/66 , G06K9/52 , G06K9/00 , G06T7/20 , B64F1/22 , G06T7/60
CPC分类号： G08G5/065 , B64F1/225 , G06K9/00671 , G06T7/75 , G06T19/00 , G06T2207/30241 , G06T2207/30261 , G06T2210/21 , G08G5/0026 , G08G5/045
摘要： The disclosed embodiments describe collision warning devices, controllers, and computer readable media. A collision warning device for towing vehicles includes a housing, a scanning sensor, a display, and a controller. The housing is configured to be secured to at least one of a tow operator and a tug during aircraft towing operations. The a scanning sensor is secured to the housing and is configured to scan an aircraft and to scan an object in an environment surrounding the aircraft. The controller is mounted to the housing and is operably coupled with the scanning sensor and the display. The controller is configured to generate a three dimensional (3D) model of the aircraft and the environment based on a signal output from the scanning sensor, and to calculate potential collisions between the aircraft and the object based on the 3D model.

24. 发明授权

US09783320B2 Airplane collision avoidance 有权
公开(公告)号：US09783320B2
公开(公告)日：2017-10-10
申请号：US15258913
申请日：2016-09-07
申请人： DM3 AVIATION LLC
发明人： Megan D. Barnes , Michael W. Delk , Richard L. Tutwiler , John R. Durkin , David E. Barnes, Jr.
IPC分类号： G08G5/04 , B64D47/08
CPC分类号： B64D47/08 , B64D2205/00 , B64F1/225 , G08G5/0021 , G08G5/045 , G08G5/065
摘要： A collision avoidance system for an airplane under tow may include a sensing device configured to capture image data of at least a portion of the airplane and an object while the airplane is being towed. The sensing device may be located remotely to both the airplane and the object. Positions of two or more features of the airplane may be determined based on the image data. A bounding box encompassing the airplane may be generated based, at least in part, on the positions of the two or more features. Additionally, based on a comparison of the position of an object relative to the bounding box, it may be determined whether the object is within a predetermined distance from the airplane.

25. 发明授权

US09561697B2 Single point disconnect in an aircraft pushback operation 有权
标题翻译：单点断开在飞机推回操作
公开(公告)号：US09561697B2
公开(公告)日：2017-02-07
申请号：US14644529
申请日：2015-03-11
申请人： Delta Air Lines, Inc.
发明人： Curtis Schramm , Brian Ardrey , Casey Aycock , Jim Heinzel
IPC分类号： B60D1/145 , B60Q9/00 , B64F1/22
CPC分类号： B60D1/145 , B60Q9/00 , B64F1/224 , B64F1/225 , Y02T50/826
摘要： A single point disconnect system useful for pushback of an aircraft using a tow bar and a vehicle includes a first sensor assembly that determines whether an angle of the tow bar respective to a surface of the vehicle to which the tow bar is coupled exceeds a threshold limit, a second sensor assembly that determines the direction of the wheels of the vehicle that are responsible for steering the vehicle, and an indicator panel. The indicator panel includes a first light module and a second light module that are coupled to the first sensor assembly and the second sensor assembly, respectively. The first light module emits light that indicates the angle of the tow bar respective to the surface of the vehicle and the second light module emits light that indicates the direction of the wheels of the vehicle.
摘要翻译：用于使用拖杆和车辆推回飞行器的单点断开系统包括第一传感器组件，其确定牵引杆的相应于牵引杆所耦接的车辆表面的角度是否超过阈限，确定负责转向车辆的车辆的车轮的方向的第二传感器组件和指示器面板。指示器面板包括分别联接到第一传感器组件和第二传感器组件的第一光模块和第二光模块。第一光模块发射指示拖杆相对于车辆表面的角度的光，而第二光模块发射指示车辆的车轮方向的光。

26. 发明授权

US09340303B2 Aircraft gate parking and servicing method 有权
标题翻译：飞机门停车和维修方法
公开(公告)号：US09340303B2
公开(公告)日：2016-05-17
申请号：US14329498
申请日：2014-07-11
申请人： Joseph J. Cox , Jan Vana , Rodney T. Cox , Isaiah W. Cox
发明人： Joseph J. Cox , Jan Vana , Rodney T. Cox , Isaiah W. Cox
IPC分类号： E01D15/00 , B64F1/22 , B64F1/315 , B64C25/40 , B64F1/305 , B64F1/00
CPC分类号： B64F1/22 , B64C25/405 , B64F1/00 , B64F1/225 , B64F1/305 , B64F1/315
摘要： An improved aircraft gate parking and servicing method is provided, wherein an aircraft is maneuvered into an airport terminal gate and parked in an optimum orientation at an angle that facilitates maximum access to aircraft front and rear doors. Boarding bridges are designed to facilitate connection to doors located rear of an aircraft wing without extending over the aircraft wing to maximize efficiency of passenger transfer. Passenger transfer and servicing of the aircraft may occur concurrently before the aircraft is maneuvered out of its optimum orientation in the parking space and driven to a takeoff runway for departure. Required safety margins are maintained at all times during aircraft maneuvers into and out of the optimum parking orientation. Stairs may be provided to simultaneously access aircraft doors not connected to boarding bridges. In a preferred embodiment, aircraft are moved to an optimum parking location by engines-off electric taxi systems.
摘要翻译：提供了一种改进的飞机门停车和维修方法，其中飞行器被操纵到机场终端门并且以有利于最大限度地进入飞机前门和后门的角度以最佳方向停放。登机桥设计用于方便连接到位于飞机机翼后方的门，而不延伸到飞机机翼上，以最大限度地提高乘客转移效率。飞机的乘客转机和维修可能会在飞机从停车位的最佳方向进行操纵之前同时出现，并被驱动到起飞跑道进行起飞。在飞机机动进出最佳停车方向时，始终保持所需的安全余地。可以提供楼梯以同时进入未连接到登机桥的飞机门。在优选实施例中，飞机通过发动机关闭的电动出租车系统移动到最佳停车位置。

27. 发明申请

US20160083113A1 SINGLE POINT DISCONNECT IN AN AIRCRAFT PUSHBACK OPERATION 有权
标题翻译：航空器按键操作中的单点断开
公开(公告)号：US20160083113A1
公开(公告)日：2016-03-24
申请号：US14644529
申请日：2015-03-11
申请人： Delta Air Lines, Inc.
发明人： Curtis Schramm , Brian Ardrey , Casey Aycock , Jim Heinzel
IPC分类号： B64F1/10 , B60D1/145 , B62D15/02 , B60Q9/00
CPC分类号： B60D1/145 , B60Q9/00 , B64F1/224 , B64F1/225 , Y02T50/826
摘要： A single point disconnect system useful for pushback of an aircraft using a tow bar and a vehicle includes a first sensor assembly that determines whether an angle of the tow bar respective to a surface of the vehicle to which the tow bar is coupled exceeds a threshold limit, a second sensor assembly that determines the direction of the wheels of the vehicle that are responsible for steering the vehicle, and an indicator panel. The indicator panel includes a first light module and a second light module that are coupled to the first sensor assembly and the second sensor assembly, respectively. The first light module emits light that indicates the angle of the tow bar respective to the surface of the vehicle and the second light module emits light that indicates the direction of the wheels of the vehicle.
摘要翻译：用于使用拖杆和车辆推回飞行器的单点断开系统包括第一传感器组件，其确定牵引杆的相应于牵引杆所耦接的车辆表面的角度是否超过阈限，确定负责转向车辆的车辆的车轮的方向的第二传感器组件和指示器面板。指示器面板包括分别联接到第一传感器组件和第二传感器组件的第一光模块和第二光模块。第一光模块发射指示拖杆相对于车辆表面的角度的光，而第二光模块发射指示车辆的车轮方向的光。

28. 发明授权

US2993549A Ground power system for jet type aircraft 失效
标题翻译：喷气式飞机地面动力系统
公开(公告)号：US2993549A
公开(公告)日：1961-07-25
申请号：US81226159
申请日：1959-05-11
申请人： CONS DIESEL ELECTRIC CORP
发明人： DAVIS JEROME I , STEINBACK JOHN E , ENYEART RAYMOND J
IPC分类号： B64F1/22
CPC分类号： B64C25/405 , B64F1/225 , Y02T50/823 , Y02T50/826 , Y10S180/904

29. 发明申请

US20170200380A1 AIRPLANE COLLISION AVOIDANCE 有权
公开(公告)号：US20170200380A1
公开(公告)日：2017-07-13
申请号：US15258913
申请日：2016-09-07
申请人： DM3 AVIATION LLC
发明人： Megan D. Barnes , Michael W. Delk , Richard L. Tutwiler , John R. Durkin , David E. Barnes, JR.
IPC分类号： G08G5/04 , G01S17/93 , G01S17/08 , B64F1/22
CPC分类号： B64D47/08 , B64D2205/00 , B64F1/225 , G08G5/0021 , G08G5/045 , G08G5/065
摘要： A collision avoidance system for an airplane under tow may include a sensing device configured to capture image data of at least a portion of the airplane and an object while the airplane is being towed. The sensing device may be located remotely to both the airplane and the object. Positions of two or more features of the airplane may be determined based on the image data. A bounding box encompassing the airplane may be generated based, at least in part, on the positions of the two or more features. Additionally, based on a comparison of the position of an object relative to the bounding box, it may be determined whether the object is within a predetermined distance from the airplane.

30. 发明申请

US20170174358A1 SYSTEMS AND METHODS FOR MULTILINGUAL AIRCRAFT TOWING COLLISION WARNING 审中-公开
公开(公告)号：US20170174358A1
公开(公告)日：2017-06-22
申请号：US14979052
申请日：2015-12-22
申请人： Gulfstream Aerospace Corporation
发明人： Thomas Landers
IPC分类号： B64D45/00
CPC分类号： B64D45/00 , B64F1/225 , G08G5/0013 , G08G5/0021 , G08G5/045 , G08G5/065
摘要： Collision warning systems, collision warning devices, and methods of operating collision warning systems are disclosed herein. A collision warning system includes, but is not limited to, a plurality of proximity sensors and a computer device. The plurality of proximity sensors are configured to mount on an aircraft and to generate a proximity signal. The computer device is communicatively coupled with the plurality of proximity sensors and is configured to determine a location in which the collision warning system is located, where the location includes at least one of a country and a region. The computer device is further configured to select an active linguistic profile based on the location, where the active linguistic profile includes at least one of a language and a dialect. The computer device is yet further configured to alert ground crew of potential collisions using the active linguistic profile and based on the proximity signal.

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