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公开(公告)号：US20190217675A1
公开(公告)日：2019-07-18
申请号：US16359477
申请日：2019-03-20
申请人： The Boeing Company
CPC分类号： B60D1/486 , B60D1/07 , B60D1/145 , B60D1/248 , B60D1/26 , B60Y2410/102 , B64F1/227 , B64F5/60
摘要： An example apparatus is configured to couple to a trailer and a tow vehicle. The apparatus includes a frame; one or more clamps mounted to the frame and configured to couple the frame to an underplate of the trailer; and a shaft having a first end rotatably coupled to the frame and a second end configured to couple to at least one replicated element of a towed vehicle. The at least one replicated element is configured to engage the tow vehicle.
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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：US20170001511A1
公开(公告)日：2017-01-05
申请号：US15105012
申请日：2014-12-19
发明人： Tushar Kulkarni , Paul Channon
CPC分类号： B60K6/46 , B60K6/28 , B60L1/003 , B60L7/14 , B60L15/2045 , B60L50/10 , B60L50/40 , B60L58/12 , B60L58/20 , B60L2200/40 , B60L2220/44 , B60L2240/423 , B60L2240/441 , B60L2260/28 , B60W10/26 , B60W20/19 , B64F1/227 , Y02T10/6217 , Y02T10/645 , Y02T10/7005 , Y02T10/7022 , Y02T10/7044 , Y02T10/7066 , Y02T10/72 , Y02T10/7283 , Y02T50/826 , Y02T90/16
摘要： There is provided a method of moving an aircraft using an aircraft mover, in various instances, an aircraft tractor. The method comprises: a] accelerating the aircraft up to speed using one or more electric motors drivable by at least a fast-discharge electrical-energy storage and supply device during a high-power requirement of the aircraft mover; b] substantially maintaining a speed of the aircraft using a slow-discharge electrical-energy storage and supply device during a low-power requirement of the aircraft mover; c] monitoring a charge status of the slow-discharge and fast-discharge energy storage and supply devices and when a predetermined charge status is reached, automatically charging the slow-discharge and/or fast-discharge energy storage and supply devices via an onboard electricity generator; and d] regeneratively recharging the slow-discharge and/or fast-discharge electricity-energy storage and supply devices during at least deceleration of the aircraft coupled to the aircraft mover. There is also provided a method of controlling the power distribution to the motors within the aircraft mover, a dual electrical-energy storage and supply system and controller for implementing the method, a hybrid power delivery system for an aircraft mover incorporating the dual electrical-energy storage and supply system and controller, and an aircraft mover using the systems.
摘要翻译： 提供了一种在各种情况下使用飞机拖拉机的飞行器移动器来移动飞行器的方法。 该方法包括：a）在飞机移动者的大功率要求期间加速飞行器以加速使用可由至少快速放电电能存储和供应装置驱动的一个或多个电动马达; b）在飞机移动者的低功率要求期间使用缓慢放电的电能存储和供应装置实质上保持飞行器的速度; c]监测慢放电和快速放电能量存储和供应装置的充电状态，并且当达到预定充电状态时，通过车载电力自动对慢放电和/或快速放电能量存储和供应装置充电 发电机; 以及d]在联接到所述飞行器移动器的飞行器的至少减速期间，再次对所述慢放电和/或快速放电的电能存储和供给装置进行再充电。 还提供了一种控制对飞机移动器内的电动机的配电的方法，用于实施该方法的双电能存储和供电系统和控制器，用于包含双电能的飞行器动力的混合动力输送系统 存储和供应系统和控制器，以及使用该系统的飞行器动力。
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公开(公告)号：US20160185386A1
公开(公告)日：2016-06-30
申请号：US14981297
申请日：2015-12-28
发明人： Avitzur Oren
CPC分类号： B62D15/024 , B62D15/029 , B64F1/22 , B64F1/225 , B64F1/227
摘要： The subject matter disclosed herein includes, inter alia, a method and system which enables to determine the steering-angle between the longitudinal axis of a tractor and the longitudinal axis of an aircraft which is being led by the tractor (referred to herein as “steering-angle” in short). While an aircraft is being led, the steering-angle can be repeatedly calculated and compared to a threshold value defining a mechanical steering limit. In case the comparison complies with one or more predefined conditions (e.g. the steering-angle is equal or smaller the threshold value) a warning can be generated indicating to an operator that the steering-angle has reached (or is about to reach) its limit and should be adjusted accordingly.
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公开(公告)号：US09248920B2
公开(公告)日：2016-02-02
申请号：US14580474
申请日：2014-12-23
发明人： Avitzur Oren
CPC分类号： B62D15/024 , B62D15/029 , B64F1/22 , B64F1/225 , B64F1/227
摘要： The subject matter disclosed herein includes, inter alia, a method and system which enables to determine the steering-angle between the longitudinal axis of a tractor and the longitudinal axis of an aircraft which is being led by the tractor (referred to herein as “steering-angle” in short). While an aircraft is being led, the steering-angle can be repeatedly calculated and compared to a threshold value defining a mechanical steering limit. In case the comparison complies with one or more predefined conditions (e.g. the steering-angle is equal or smaller the threshold value) a warning can be generated indicating to an operator that the steering-angle has reached (or is about to reach) its limit and should be adjusted accordingly.
摘要翻译： 本文公开的主题尤其包括一种方法和系统，其能够确定拖拉机的纵向轴线和由拖拉机引导的飞行器的纵向轴线之间的转向角度（在本文中称为“转向 简而言之）。 当飞机正在引导时，可以重复计算转向角并将其与限定机械转向限制的阈值进行比较。 在比较符合一个或多个预定条件（例如，转向角等于或小于阈值）的情况下，可以产生警告，指示操作者转向角达到（或即将达到）其极限 并应相应调整。
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公开(公告)号：US09187185B2
公开(公告)日：2015-11-17
申请号：US14335220
申请日：2014-07-18
发明人： Ran Braier , Arie Perry , Laurent Decoux , Eric Enault , Nicholas Vermalle
IPC分类号： B64F1/22
CPC分类号： B64F1/22 , B64F1/227 , Y02T50/826
摘要： The invention relates to a plane tractor which grips the nose gear of a plane, including: a chassis; wheel modules connected to the chassis, each wheel module including at least one actuator for inducing a vertical movement of the module in relation to the chassis; a gripping platform for gripping the nose gear of a plane, the platform together with the chassis having freedom of movement substantially in circular translation; and a damping and actuating means connecting the platform and the chassis.
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公开(公告)号：US08967939B2
公开(公告)日：2015-03-03
申请号：US14082392
申请日：2013-11-18
发明人： Carl L. Hammonds
CPC分类号： B64F1/227 , B62D53/045
摘要： An apparatus for moving parked aircraft with a tractor via an aircraft lift dolly which includes a hinged gate to entrap the aircraft nose gear. The aircraft lift dolly may be removably detachably coupled to the tractor through two attachment points to an intermediate connecting towbar. The aircraft lift dolly includes a lift mechanism having a lift carriage which is selectively elevated. The lift carriage includes a fixed forward chock and a rear chock that it repositioned longitudinally with respect to the forward chock and is hingedly coupled. The chocks are positioned about the aircraft nose gear without movement of the aircraft. Elevating the lift cradle elevates the chocks and the nose gear cradled therebetween.
摘要翻译： 一种用拖拉机通过飞机升降台移动停放的飞机的装置，其包括铰接门以捕捉飞机前置档。 飞机升降台可以通过两个附接点可拆卸地联接到拖拉机到中间连接拖杆。 飞机升降台具有升降机构，该升降机构具有有选择地升高的提升滑架。 提升架包括固定的前部轴承座和后轴承座，其相对于前轴承座纵向重新定位并铰接连接。 轴承座定位在飞机前档，而不会飞行。 提升升降架提升了轴承座和起落架之间的起落架。
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公开(公告)号：US08607905B2
公开(公告)日：2013-12-17
申请号：US13415320
申请日：2012-03-08
申请人： Dan Johnson
发明人： Dan Johnson
IPC分类号： B62D49/06
摘要： Apparatus for moving a wheeled load comprising: a frame having a two end; at least one wheel attached to at least one frame end; drive wheel(s) between the ends; a drive means for providing drive wheel power; a power source; a load-lifting arm means, the lifting arm means having a proximal end rotatably attached to the frame and a distal end; affixed to the distal end is a locking pickup head having a multi-socket center adapted to receive a ball, and a sliding locking gate to releasably affix the head to the ball; extending outwardly from the second end is a handle; disposed on the handle is a control means for operating the apparatus; and drive disengagement means for mechanically disengaging the powered driving mechanism so that a user can manually move the apparatus in case of battery or other mechanical failure.
摘要翻译： 用于移动轮式载荷的装置，包括：具有两端的框架; 至少一个轮连接到至少一个框架端; 两端之间的驱动轮; 用于提供驱动轮功率的驱动装置; 电源; 提升臂装置，提升臂装置具有可旋转地附接到框架的近端和远端; 固定到远端的是具有适于容纳球的多中心中心的锁定拾取头和用于将头部可释放地固定到球的滑动锁定门; 从第二端向外延伸的是把手; 设置在手柄上的是用于操作该装置的控制装置; 并且驱动脱开装置用于机械地脱开动力驱动机构，使得用户可以在电池或其它机械故障的情况下手动地移动装置。
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公开(公告)号：US08544792B2
公开(公告)日：2013-10-01
申请号：US12619123
申请日：2009-11-16
申请人： Arie Perry , Ran Braier
发明人： Arie Perry , Ran Braier
IPC分类号： B64C13/20
摘要： Disclosed a towbarless airplane tug and method of operating thereof. The tug comprises a chassis mounted on a plurality of tug wheels, at least some of said tug wheels being steerable tug wheels and at least some of said tug wheels being drivable tug wheels; an airplane wheel support turret assembly, rotatably mounted in connection with said chassis and operative to support at least one wheel of a nose landing gear of an airplane; at least one rotation sensor connected to said wheel support turret assembly and operative to sense rotation of said wheel support turret assembly relative to said chassis, said rotation resulting at least from steering control induced movement of the nose landing gear caused by pilot-controlled ground steering of said airplane, and to generate an output indicating a direction of said pilot-controlled ground steering of said airplane; at least one tug wheel driver unit operative to drive said drivable tug wheels; at least one tug wheel steering mechanism operative to steer said steerable tug wheels thereby providing steering of said chassis; and at least one tug controller operative to control operation of at least said tug wheel steering mechanism at least in response to said output of said rotation sensor, so as to cause steering said steerable tug wheels such that said chassis moves in the direction indicated in said output of said rotation sensor.
摘要翻译： 公开了一种无牵引式的拖拉机及其操作方法。 拖轮包括安装在多个拖轮上的底盘，至少一些所述拖轮是可转向的拖轮，并且至少一些所述拖轮是可驱动的拖轮; 飞机轮支撑转塔组件，其可旋转地安装在与所述底盘相连并用于支撑飞机的起落架的至少一个轮; 至少一个旋转传感器，其连接到所述车轮支撑转塔组件并且可操作以感测所述车轮支撑转塔组件相对于所述底盘的旋转，所述旋转至少导致转向控制引起的由先导控制的地面转向引起的前起落架的运动 并且产生指示所述飞机的所述先导控制地面转向的方向的输出; 至少一个拖轮驱动器单元，用于驱动所述可驱动拖轮; 至少一个牵引轮转向机构，用于转向所述可转向拖轮，从而提供所述底盘的转向; 至少一个牵引控制器至少响应于所述旋转传感器的所述输出来控制至少所述拖轮转向机构的操作，以便使所述可转向的拖轮轮转向，使得所述底盘沿所述转向传感器的所述方向移动， 输出所述旋转传感器。
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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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