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公开(公告)号：US12012227B2
公开(公告)日：2024-06-18
申请号：US18205842
申请日：2023-06-05
CPC分类号： B64F1/228 , B64C25/08 , B64D45/08 , B64D47/02 , B64F1/0297 , B64F1/0299 , B64F1/10 , B64D2205/00 , G08G5/065 , Y02T50/40
摘要： One variation of a tram system includes: a chassis; a latch configured to selectively engage a latch receiver mounted to an aircraft; an alignment feature adjacent the latch and configured to engage an alignment receiver mounted to the aircraft and to communicate acceleration and braking forces from the chassis into the aircraft; an optical sensor facing upwardly from the chassis; a drivetrain configured to accelerate and decelerate the chassis along a runway; and a controller configured to detect an optical fiducial arranged on the aircraft in optical images recorded by the optical sensor adjust a speed of the drivetrain to longitudinally align the alignment feature with the alignment receiver based on positions of the optical fiducial detected in the optical images, trigger the latch to engage the latch receiver once the aircraft has descended onto the chassis, and trigger the drivetrain to actively decelerate the chassis during a landing routine.
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公开(公告)号：US20240034484A1
公开(公告)日：2024-02-01
申请号：US18226747
申请日：2023-07-26
发明人： Mark R. Patey
IPC分类号： B64F1/22
CPC分类号： B64F1/228
摘要： This disclosure relates generally to aircraft tugs, which assist in the movement of small aircraft. More specifically, this disclosure relates to a remote power switch, which may also be referred to as an emergency tug shutoff (ETSO) switch, for remotely stopping movement of an aircraft tug. Systems that include such an aircraft tug and at least one remote power switch are also disclosed, as are methods for remotely stopping an aircraft tug.
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公开(公告)号：US20190019424A1
公开(公告)日：2019-01-17
申请号：US16026843
申请日：2018-07-03
申请人： Gregory M. Griffith
发明人： Gregory M. Griffith
CPC分类号： G08G5/045 , B64F1/228 , G01S13/86 , G01S13/931 , G01S2013/9335 , G01S2013/936 , G08B3/10 , G08G5/04 , G08G5/065
摘要： An aircraft collision avoidance system including (a) at least one separation monitoring device connectable to at least a portion of an aircraft and/or vehicle, the separation monitoring device comprising (1) at least one transmitter, (2) at least one receiver, and (3) an image sensor, and (b) a master unit.
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公开(公告)号：US09932129B2
公开(公告)日：2018-04-03
申请号：US14898128
申请日：2014-06-11
申请人： AIRBUS SAS
CPC分类号： B64F1/04 , B64C25/32 , B64F1/22 , B64F1/228 , Y02T50/826
摘要： A device for moving aircraft along the ground includes at least one runway and at least one aircraft. The aircraft is secured to a tractor element having a magnetic mass formed mainly of type II superconductor material and the runway includes stator coils arranged in the runway with at least one line of coils parallel to an axis of the runway. A command/control system supplies power to the stator coils to generate a magnetic field that levitates the tractor element, magnetized beforehand into a phase II superconducting state, above the runway.
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公开(公告)号：US20170057663A1
公开(公告)日：2017-03-02
申请号：US15246080
申请日：2016-08-24
申请人： AIRBUS (S.A.S.)
CPC分类号： B64F1/228 , B60L53/00 , B64F1/227 , G05D1/0011 , G05D1/0016 , G05D1/0022 , G05D2201/02
摘要： A device for maneuvering and immobilizing an aircraft on the ground. Included in the device is a moving apparatus and a remote control configured for remotely controlling the moving apparatus. The device allows a coupling of a single remote control with several moving apparatuses and/or of one moving apparatus with several remote controls. Also, the device allows an operator equipped with a remote control to remotely control several pushback maneuvers by successively using several moving apparatuses or several operators each equipped with a remote control to successively control the same moving apparatus.
摘要翻译： 用于在地面上操纵和固定飞机的装置。 设备中包括移动设备和配置为远程控制移动设备的远程控制。 该装置允许单个遥控器与多个移动装置和/或具有几个遥控器的一个移动装置的耦合。 此外，该装置允许配备有遥控器的操作者通过连续地使用多个移动装置或者每个配备有遥控器的几个操作器来连续地控制相同的移动装置来远程控制几个推回机动。
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公开(公告)号：US20160144981A1
公开(公告)日：2016-05-26
申请号：US14898128
申请日：2014-06-11
申请人： AIRBUS GROUP SAS
CPC分类号： B64F1/04 , B64C25/32 , B64F1/22 , B64F1/228 , Y02T50/826
摘要： A device for moving aircraft along the ground includes at least one runway and at least one aircraft. The aircraft is secured to a tractor element having a magnetic mass formed mainly of type II superconductor material and the runway includes stator coils arranged in the runway with at least one line of coils parallel to an axis of the runway. A command/control system supplies power to the stator coils to generate a magnetic field that levitates the tractor element, magnetized beforehand into a phase II superconducting state, above the runway.
摘要翻译： 用于沿着地面移动飞行器的装置包括至少一个跑道和至少一个飞机。 飞机被固定到具有主要由II型超导体材料形成的磁性质量的牵引器元件，并且跑道包括布置在跑道中的定子线圈，其中至少一条线圈平行于跑道的轴线。 指令/控制系统向定子线圈供电以产生使拖拉机元件悬浮的磁场，预先在跑道之上磁化成II级超导状态。
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公开(公告)号：US20120119018A1
公开(公告)日：2012-05-17
申请号：US13358659
申请日：2012-01-26
申请人： Arie PERRY , Ran BRAIER
发明人： Arie PERRY , Ran BRAIER
IPC分类号： B64C25/50
CPC分类号： B64F1/228 , B64F1/227 , Y02T50/826
摘要： An unmanned airplane transfer system, comprising: a transfer module adapted to transfer an airplane; a landing gear holder, adapted to firmly grip a landing gear of the airplane; wherein the landing gear holder is pivotally coupled to a structural element of the unmanned transfer system; and a controller, coupled to the transfer module, adapted to control the transfer module in response to a steering induced movement of the landing gear holder.
摘要翻译： 一种无人飞行器传输系统，包括：适于传送飞机的传送模块; 起落架保持器，适于牢固地抓住飞机的起落架; 其中所述起落架保持器枢转地联接到所述无人驾驶系统的结构元件; 以及耦合到所述传送模块的控制器，其适于响应于所述起落架保持器的转向引起的移动来控制所述传递模块。
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公开(公告)号：US20230303267A1
公开(公告)日：2023-09-28
申请号：US18110319
申请日：2023-02-15
申请人： Moonware, Inc.
发明人： Javier Vidal Rojas , Saunon Rod Malekshahi , Andrew Arnold , Dimitrios Bailas , Atanaz Bohlooli , Camille Carr , Orhan Elam , Dima Fayyad , Marc Jabbour , Lucas Liu , Berke Ozdemir , Vedant Singh , Philipp Haban , Matthew Derkach
CPC分类号： B64F1/228 , B60P3/11 , G05D1/0276
摘要： An autonomous vehicle includes a chassis for housing an aircraft ground contacting structure (GCS) and one or more GCS coupling and lifting mechanisms, GCS securing mechanisms, drivetrain, batteries and a sensor stack for performing autonomous navigation. Further, the vehicle incorporates multiple sensors, such as high-resolution machine vision cameras, GPS modules, Lidars, ultrasonic range sensors, and radars. The sensors deliver spatial perception capabilities to the vehicle and feed relevant data to onboard computing units to achieve location-based navigation, precision alignment with aircraft, obstacle detection and collision avoidance capabilities. A series of batteries deliver power to all components, including but not limited to, motors, electromechanical units, onboard computers, sensors and any other component requiring electrical input. External ports allow the vehicle to recharge batteries after each utilization cycle without replacement. The vehicle is capable of recognizing its power state and can autonomously navigate to a base station and dock itself for charging.
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公开(公告)号：US20230242265A1
公开(公告)日：2023-08-03
申请号：US18114346
申请日：2023-02-27
发明人： Oren TAL , Reuven TAL
摘要： A transportation system and method serve passenger-conveying VTOL air vehicles (AVs) at a vertiport. The vertiport has a flight deck including at least one landing pad, a passenger terminal, and a dynamic partition arrangement that defines a capsule for receiving one of the AVs at a time. The dynamic partition arrangement assumes a first open state in which it is open to the flight deck and closed to the passenger terminal and a second open state in which it is closed to the flight deck and open to the passenger terminal. A robotic system includes a handling robot that automatically approaches and docks with the AV after landing, and conveys the AV between the landing pad and the capsule via an opening provided by the first open state of the dynamic partition.
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公开(公告)号：US20190077520A1
公开(公告)日：2019-03-14
申请号：US16028353
申请日：2018-07-05
CPC分类号： B64F1/228 , B64C25/08 , B64D45/08 , B64D47/02 , B64D2205/00 , B64F1/02 , B64F1/10 , G08G5/065 , Y02T50/44
摘要： One variation of a tram system includes: a chassis; a latch configured to selectively engage a latch receiver mounted to an aircraft; an alignment feature adjacent the latch and configured to engage an alignment receiver mounted to the aircraft and to communicate acceleration and braking forces from the chassis into the aircraft; an optical sensor facing upwardly from the chassis; a drivetrain configured to accelerate and decelerate the chassis along a runway; and a controller configured to detect an optical fiducial arranged on the aircraft in optical images recorded by the optical sensor adjust a speed of the drivetrain to longitudinally align the alignment feature with the alignment receiver based on positions of the optical fiducial detected in the optical images, trigger the latch to engage the latch receiver once the aircraft has descended onto the chassis, and trigger the drivetrain to actively decelerate the chassis during a landing routine.
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