公开(公告)号：US09085374B2

公开(公告)日：2015-07-21

申请号：US14325513

申请日：2014-07-08

申请人： ISRAEL AEROSPACE INDUSTRIES LTD.

发明人： Laurent Decoux ,  Eric Enault ,  Nicholas Vermalle

IPC分类号： B64F1/10 ,  B62D6/00 ,  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.

摘要翻译： 本发明涉及一种夹住飞机前起落架的平面拖拉机，包括：底盘; 车轮模块连接到底盘，每个车轮模块包括用于引起模块相对于底盘的垂直运动的至少一个致动器; 用于夹紧平面的前齿轮的夹持平台，所述平台与所述底架一起基本上以圆形平移的自由度; 以及连接平台和底盘的阻尼和致动装置。

公开(公告)号：US20140328663A1

公开(公告)日：2014-11-06

申请号：US14335220

申请日：2014-07-18

申请人： ISRAEL AEROSPACE INDUSTRIES LTD.

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.

公开(公告)号：US20140321960A1

公开(公告)日：2014-10-30

申请号：US14325513

申请日：2014-07-08

申请人： ISRAEL AEROSPACE INDUSTRIES LTD.

发明人： 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.

摘要翻译： 本发明涉及一种夹住飞机前起落架的平面拖拉机，包括：底盘; 车轮模块连接到底盘，每个车轮模块包括用于引起模块相对于底盘的垂直运动的至少一个致动器; 用于夹紧平面的前齿轮的夹持平台，所述平台与所述底架一起基本上以圆形平移的自由度; 以及连接平台和底盘的阻尼和致动装置。

公开(公告)号：US08515594B2

公开(公告)日：2013-08-20

申请号：US13130364

申请日：2009-11-25

申请人： Arie Perry ,  Ran Braier

发明人： Arie Perry ,  Ran Braier

IPC分类号： B64F1/22

CPC分类号： G06F11/30 ,  B60S13/00 ,  B64F1/10 ,  B64F1/22 ,  B64F1/227 ,  F16H61/4043 ,  F16H61/42 ,  Y02T50/826

摘要： An airplane tug for receiving a landing gear of an airplane. Tug comprises a chassis for receiving the landing gear, a propulsion arrangement for moving tug, force sensor(s) for measuring a force exerted by the chassis on the gear due to a speed differential between tug and airplane, and a controller for altering movement parameter(s) of tug for maintaining the force below a value. Propulsion arrangement comprises a variable angle swash plate hydraulic pump coupled to a variable angle swash plate hydraulic motor and to a bypass path valve such that fluid circulates between the pump and motor to activate the arrangement to increase the speed and/or traction force when bypass path is in a closed state, and the fluid circulates across the motor via the valve to reduce a rotational speed and/or traction force of the tug when the path is in an opened state.

摘要翻译： 用于接收飞机起落架的飞机拖船。 拖轮包括用于接收起落架的底架，用于移动拖轮的推进装置，用于测量由于牵引车和飞机之间的速度差异而由底盘施加在齿轮上的力的力传感器以及用于改变运动参数的控制器 拖把的力量维持在一个值以下。 推进装置包括联接到可变角度旋转斜盘液压马达的可变角度斜盘液压泵和旁路通路阀，使得流体在泵和马达之间循环以启动该装置，以在旁路路径时增加速度和/或牵引力 处于关闭状态，并且当路径处于打开状态时，流体经由阀循环跨过马达，以减小拖轮的旋转速度和/或牵引力。

公开(公告)号：US20120298797A1

公开(公告)日：2012-11-29

申请号：US13575322

申请日：2011-01-26

申请人： Slavomir Malicki

发明人： Slavomir Malicki

IPC分类号： B64F1/22

CPC分类号： B64F1/22 ,  B64F1/227 ,  B64F1/228 ,  Y02T50/826

摘要： The invention solves the question of a system for transporting airplanes about airport apron from the parking location to the takeoff runway and from the landing location to the parking location with engines switched off. The system is made up of guiding grooves (5) in which guiding pins (9) installed in docking stations (8) move and are catch-fitted preferably to the front wheel (10) of the airplane (4). The guiding grooves (5) are covered from above by pivotable gratings (11) of a segmental design that open giving way to guiding pin (9) sliding in the guiding groove (5) and close following the passage of the guiding pin (9). Switching devices (12) are installed at locations of abrupt curves in the guiding grooves (4) as well as at locations of changes in direction.

摘要翻译： 本发明解决了关于机场停机坪的飞机从停车位运送到起飞跑道的系统的问题，以及关闭发动机的从着陆位置到停车位置的问题。 该系统由引导凹槽（5）组成，其中安装在对接站（8）中的引导销（9）移动并优选地卡配于飞机（4）的前轮（10）。 引导槽（5）由分段设计的可枢转的光栅（11）从上方覆盖，所述可转动的光栅（11）向导向槽（9）滑动的引导销（9）打开并且随着引导销（9）的通过而关闭， 。 切换装置（12）安装在引导槽（4）中的突然曲线的位置以及方向改变的位置处。

公开(公告)号：US20110127366A1

公开(公告)日：2011-06-02

申请号：US12737586

申请日：2009-07-09

申请人： Andreas Becker

发明人： Andreas Becker

IPC分类号： B64F1/04 ,  B64F1/22

CPC分类号： B64F1/22 ,  B64F1/227 ,  B64F1/228 ,  G08G5/06 ,  Y02T50/826

摘要： The invention relates to an automatic system for maneuvering aircraft on the ground, based on driverless towing vehicles, (hereafter AGTV's), which can independently hold the undercarriage of the aircraft. In said system the AGTVs pull the aircraft from transfer areas on the taxiways of the runways to the stand and vice versa, allowing the propulsion systems of the aircraft to remain switched off during the taxiing process. The driverless AGTVs receive their driving jobs from a computer-aided guidance and management system which controls the AGTV fleet in a collision- and conflict-free manner.

摘要翻译： 本发明涉及一种基于无人驾驶车辆（以下简称AGTV）在地面上操纵飞行器的自动系统，其可以独立地保持飞机的起落架。 在所述系统中，AGTV将飞机从跑道的滑行道上的转移区域拉到支架，反之亦然，从而允许飞机的推进系统在滑行过程中保持关闭。 无人驾驶的AGTV通过计算机辅助指导和管理系统接收驾驶工作，该系统以碰撞和无冲突的方式控制AGTV车队。

公开(公告)号：US06305484B1

公开(公告)日：2001-10-23

申请号：US09541039

申请日：2000-03-31

申请人： Edward L. Leblanc

发明人： Edward L. Leblanc

IPC分类号： B60T716

CPC分类号： B64F1/228 ,  B60T7/16 ,  B62D1/24 ,  B62D1/28 ,  B64F1/22 ,  Y02T50/826 ,  Y10S180/904

摘要： An automated aircraft towing vehicle system for use with aircraft is provided. When coupled to an aircraft the towing tractor vehicle facilitates the movement of the aircraft without the requirement for use of the aircraft's jet engines. The towing vehicle system comprises a towing tractor vehicle having remotely controllable steering, braking, and acceleration. The remote system controller is located in the aircraft being towed such that the pilot of the aircraft being towed is capable of controlling the starting, stopping and steering of the towing tractor vehicle. The towing tractor vehicle further includes a remotely controllable de-coupling means. When the aircraft is towed to the desired location, the decoupling of the aircraft from the towing tractor vehicle is controllable by the remote system controller.

摘要翻译： 提供了一种与飞机一起使用的自动化飞行器牵引车系统。 当联接到飞行器时，牵引拖拉机车辆有助于飞机的移动，而不需要使用飞机的喷气发动机。 牵引车辆系统包括具有可遥控转向，制动和加速的牵引拖拉机。 远程系统控制器位于被拖曳的飞行器中，使得被拖曳的飞机的飞行员能够控制拖曳拖拉机车辆的启动，停止和转向。 牵引拖拉机车辆还包括可远程控制的解耦装置。 当飞机被拖到所需的位置时，飞机与牵引拖拉机车辆的分离可由远程系统控制器控制。

公开(公告)号：US5259572A

公开(公告)日：1993-11-09

申请号：US940189

申请日：1992-09-03

申请人： Wilhelm Franken ,  Ernest Kretschmann ,  Gerhard Weigardt ,  Heinrich Goris ,  Torsten L. Michaelsen ,  Dieter Pohe

发明人： Wilhelm Franken ,  Ernest Kretschmann ,  Gerhard Weigardt ,  Heinrich Goris ,  Torsten L. Michaelsen ,  Dieter Pohe

IPC分类号： B64F1/10 ,  B64F1/22 ,  B64C25/50

CPC分类号： B64F1/227 ,  B64F1/22 ,  Y02T50/826 ,  Y10S180/904

摘要： A vehicle with its own traveling gear for towing an aircraft without draw tongue, has a U-shaped chassis frame recess that is open in the forward direction with a clamping and lifting device arranged therein for the nose wheels of an aircraft. The clamping and lifting device, which is oscillatingly suspended on the chassis frame 1, includes a pivoting and lifting ramp 8, as well as two parallel telescoping arms 10 arranged rigidly on the pivoting and lifting ramp 8, with telescoping cylinders 11 and with gripping arms 14, which can be pivoted in and whose nose wheel contact surfaces 18 are rigidly attached to the gripping arms 14, and of telescopingly adjustable holddown devices 12, 13, which are hinged to the support 7.FIG. 3 shows the clamping and lifting devices with the nose wheels 17 lifted.

摘要翻译： 具有自己的用于牵引飞行器而不用拉舌的行星齿轮的车辆具有U形的底盘框架凹槽，其在向前方向上是开放的，其中布置有用于飞机前轮的夹紧和提升装置。 振动悬挂在底盘框架1上的夹紧和提升装置包括枢转和提升斜坡8以及刚性地布置在枢转和提升斜坡8上的两个平行伸缩臂10，其中伸缩气缸11和夹持臂 其可以枢转并且其前轮接触表面18刚性地附接到夹持臂14，以及铰接到支撑件7的可伸缩调节的压紧装置12,13。 图3示出了抬起前轮17的夹紧和提升装置。

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

发明人： Emmanuel Joubert ,  Charles Nespoulous ,  Bruno Rechain ,  Hichem Smaoui

IPC分类号： B64F1/04 ,  B64C25/32 ,  B64F1/22

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.

公开(公告)号：US20170001511A1

公开(公告)日：2017-01-05

申请号：US15105012

申请日：2014-12-19

申请人： TEXTRON GROUND SUPPORT EQUIPMENT UK LIMITED

发明人： Tushar Kulkarni ,  Paul Channon

IPC分类号： B60K6/46 ,  B60L1/00 ,  B64F1/22 ,  B60L11/02 ,  B60L11/18 ,  B60L15/20 ,  B60K6/28 ,  B60L11/00

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。