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1. 发明授权

US5308212A Aircraft towing vehicle 失效
标题翻译：飞机牵引车
公开(公告)号：US5308212A
公开(公告)日：1994-05-03
申请号：US930537
申请日：1992-09-24
申请人： Jurgen Pollner , Gregor Trummer
发明人： Jurgen Pollner , Gregor Trummer
IPC分类号： B64F1/10 , B60P3/11 , B64F1/22
CPC分类号： B64F1/227 , B64F1/22 , Y10S180/904
摘要： An aircraft towing vehicle including a chassis formed with a recess receiving a towing device for securing a nose wheel of an aircraft and including a transversely tiltable bearing frame, a vertically displaceable and longitudinally swingable lifting cradle provided with a pair of telescopic traction arms having respective gripping devices on respective rearward ends, the arms being longitudinally displaceable and adapted to swing about respective transverse axes, bringing thereby the gripping devices upwardly to engage the circumference of the nose wheel above an axle thereof.
摘要翻译： PCT No.PCT / DE92 / 00057 Sec。 371日期：1992年9月24日 102（e）1992年9月24日PCT 1992年1月30日PCT PCT。 WO92 / 13762 PCT公开号日期：1992年8月20日。一种飞机牵引车辆，其包括形成有底座的底盘，该底盘形成有容纳用于固定飞行器前轮的牵引装置的凹部，并且包括横向可倾斜的轴承架，具有一对的可垂直移位和纵向摆动的升降架可伸缩的牵引臂在相应的后端具有相应的夹持装置，该臂可沿纵向移位并且适于围绕各自的横向轴线摆动，从而使夹持装置向上以与其轮轴上方的前轮的圆周接合。

2. 发明授权

US5219033A Tractor for aircraft 失效
标题翻译：飞机拖拉机
公开(公告)号：US5219033A
公开(公告)日：1993-06-15
申请号：US739383
申请日：1991-08-01
申请人： Jurgen Pollner , Gregor Trummer , Peter Molzer
发明人： Jurgen Pollner , Gregor Trummer , Peter Molzer
IPC分类号： B60K31/00 , B60K28/08 , B62D49/00 , B64F1/10 , B64F1/22 , F02D29/02 , F02D41/04
CPC分类号： B60K28/08 , B62D49/00 , B64F1/22 , Y10S180/904
摘要： An aircraft towing tractor has its acceleration limited to a predetermined limiting acceleration to reduce stresses upon the aircraft undercarriage by a computer-controlled regulator interposed between the gas pedal and the internal combustion engine. The regulator can also provide control of the speed increase of the engine below a predetermined limiting value thereof prior to control of the limiting acceleration.
摘要翻译：飞机牵引拖拉机的加速度受限于预定的极限加速度，以减少插入在油门踏板和内燃机之间的计算机控制的调节器在飞行器起落架上的应力。在控制限制加速度之前，调节器还可以将发动机的速度增加控制在其预定的极限值之下。

3. 发明授权

US4512560A Apparatus for mounting rails on a rigid rail beam 失效
标题翻译：用于将轨道安装在刚性轨道梁上的装置
公开(公告)号：US4512560A
公开(公告)日：1985-04-23
申请号：US419425
申请日：1982-09-17
申请人： Peter Molzer , Jurgen Pollner , Nicola Topic , Gregor Trummer , Rudolf Zurek
发明人： Peter Molzer , Jurgen Pollner , Nicola Topic , Gregor Trummer , Rudolf Zurek
IPC分类号： E01D21/00 , E01B25/00 , E01B25/30 , E01B25/32 , E01B35/00 , E01B37/00 , B25B11/02
CPC分类号： E01B25/32 , Y10T29/49998
摘要： An apparatus for mounting relatively small and deformable elongated rails on a relatively large, generally horizontal, and nondeformable elongated rail beam has a stiff but limitedly elastically deformable elongated jig. A plurality of clamps spaced longitudinally along the jig are engageable with the rail for locking onto the rail at respective longitudinally spaced locations. Respective vertical and horizontal jacks transversely engage between the clamps and the jig for elastically deforming the jig into a desired shape relative to the rail beam. Holders and the like are provided on the jig for securing the deformable rails to the rail beam in predetermined positions relative to the deformed jig. If the rail section is to be curved in any direction the jig is appropriately deformed relative to the rail beam so its various holders and mounting fixtures lie on the appropriate curve. Such elastic deformation of the jig therefore perfectly positions these rail holders. The clamps include respective horizontal and transverse clamp beams at the locations, respective jaws on the beams, and respective hydraulic actuators for locking the jaws on the rail beam at the respective locations and thereby solidly arresting the transverse beams on the rail beam at the respective locations.
摘要翻译：用于在较大的，大致水平的和不可变形的细长轨道梁上安装相对较小且可变形的细长导轨的装置具有刚性但有限地可弹性变形的细长夹具。沿着夹具纵向间隔开的多个夹具可与轨道接合，以在相应的纵向间隔的位置处锁定在轨道上。相应的垂直和水平千斤顶横向接合在夹具和夹具之间，用于使夹具弹性变形成相对于轨道梁所需的形状。夹具等设置在夹具上，用于将可变形轨道相对于变形夹具预定位置固定在轨道梁上。如果轨道部分在任何方向上都是弯曲的，则夹具相对于轨道梁适当地变形，因此其各种保持器和安装夹具位于适当的曲线上。因此，夹具的这种弹性变形完美地定位这些轨道支架。夹具包括位于各个位置处的相应的水平和横向夹持梁，梁上的相应夹爪以及相应的液压致动器，用于在相应位置处将轨道梁上的钳口锁定，从而在相应位置处将横梁牢固地阻挡在轨道梁上。

4. 发明授权

US4911604A Aircraft towing vehicle having steered nose wheel lifting mechanism 失效
标题翻译：具有转向前轮提升机构的飞机牵引车
公开(公告)号：US4911604A
公开(公告)日：1990-03-27
申请号：US250285
申请日：1988-09-28
申请人： Juergen Pollner , Gregor Trummer , Peter Moelzer
发明人： Juergen Pollner , Gregor Trummer , Peter Moelzer
IPC分类号： B64F1/10 , B64F1/22
CPC分类号： B64F1/227 , B64F1/22 , Y10S414/13
摘要： An aircraft towing vehicle is equipped with an aircraft nose wheel lifting and securing mechanism. The nose wheel is received in a U-shaped recess of the vehicle chassis, the lifting mechanism being constructed to grip the wheel from behind and underneath and to then push it up a ramp. The tilt angle of the lifting mechanism as it advances towards the wheel is controlled by a steering linkage such that the lower, freely movable segment of the lifting mechanism is tilted farther forward and beneath the nose wheel at the beginning of the nose wheel engaging operation, while conversely, a rigid upper segment is tilted farther forward as the engaging operation continues to completion.
摘要翻译：飞机牵引车配备有飞机前轮提升和固定机构。前轮被容纳在车辆底盘的U形凹部中，提升机构被构造成从后面和下面夹持车轮，然后将其推向斜坡。提升机构朝向车轮前进时的倾斜角度由转向联动器控制，使得提升机构的下部可自由移动的部分在前轮接合操作开始时向前倾斜并在前轮下方倾斜，而相反地，当接合操作继续完成时，刚性上部部分向前倾斜。

5. 发明授权

US4911603A Aircraft towing vehicle having swiveled nose wheel lifter 失效
标题翻译：飞机牵引车具有旋转的前轮升降机
公开(公告)号：US4911603A
公开(公告)日：1990-03-27
申请号：US250276
申请日：1988-09-28
申请人： Juergen Pollner , Gregor Trummer , Peter Moelzer
发明人： Juergen Pollner , Gregor Trummer , Peter Moelzer
IPC分类号： B64F1/10 , B64F1/22
CPC分类号： B64F1/227 , B64F1/22
摘要： An aircraft towing vehicle has a rearwardly opening recess adapted to receive the nose wheel of an aircraft to be towed. A nose wheel lifting and clamping mechanism has two nose wheel lifters which can be pivoted from a retracted position, in which they are parallel to sides of the vehicle frame, into an operative position, in which they extend into the recess for engaging the aircraft nose wheel. The lifters pivot on rocker arms which themselves pivot about a horizontal axis and are power driven by hydraulic actuators. A separate hydraulic swivel drive motor is provided for each lifter. The pressure increase which takes place when the swivel drive reaches the end of its path is used to initiate the delivery of pressurized fluid to the actuator. A crank arm driven by the hydraulic motor is connected to the support for the lifter with a low back pivot, self locking linkage to positively prevent even excessive forces generated during the nose wheel lifting process from unintentionally moving the lifters towards their retracted positions.
摘要翻译：飞机牵引车辆具有适于接收要拖曳的飞行器的前轮的向后开口凹部。前轮提升和夹紧机构具有两个前轮升降器，其可以从它们平行于车架的侧面的缩回位置枢转到操作位置，在该位置中，它们延伸到凹部中以接合飞机鼻部轮。升降器在摇臂上枢转，摇臂自身围绕水平轴线枢转，并由液压执行器驱动。为每个升降器提供单独的液压旋转驱动电机。当旋转驱动器到达其路径的端部时发生的压力增加用于启动加压流体传递到致动器。由液压马达驱动的曲柄臂与用于升降机的支撑件连接，该支撑件具有低的后部枢轴，自锁定联动装置，可以有效地防止在前轮提升过程中产生的过大的力量，从而无意中将升降机移动到其缩回位置。

6. 发明授权

US4917563A Aircraft towing vehicle having a mechanism for substantially preventing relative aircraft wheel movements 失效
标题翻译：具有用于基本上防止相对飞行器轮运动的机构的飞机牵引车辆
公开(公告)号：US4917563A
公开(公告)日：1990-04-17
申请号：US250286
申请日：1988-09-28
申请人： Juergen Pollner , Gregor Trummer , Peter Moelzer
发明人： Juergen Pollner , Gregor Trummer , Peter Moelzer
IPC分类号： B64F1/10 , B64F1/22
CPC分类号： B64F1/227 , B64F1/22
摘要： An aircraft towing vehicle has a frame with a rearwardly open, U-shaped recess for receiving the nose wheel of an aircraft and a lifting and securing mechanism for raising the nose wheel off the ground and securing it to the towing vehicle in the raised position. The lifting and securing mechanism, in particular a hold-down mechanism and/or a lifter mechanism secure the nose wheel after it has been fully engaged by applying a wheel clamping force of a predetermined magnitude to the periphery of the wheel. The clamping force is selected to substantially prevent relative nose wheel movements while the aircraft is being towed.
摘要翻译：飞机牵引车具有一个框架，该框架具有向后开口的U形凹槽，用于容纳飞行器的前轮，以及提升和固定机构，用于将前轮从地面上抬起并将其固定在牵引车辆处于升高位置。提升和固定机构，特别是压紧机构和/或升降机构，通过向车轮的周边施加预定大小的车轮夹紧力而使前轮完全啮合。选择夹紧力以在飞机被牵引的同时基本上防止相对的前轮移动。

7. 发明授权

US4836734A Ground vehicle for maneuvering aircraft 失效
标题翻译：机动飞机的地面车辆
公开(公告)号：US4836734A
公开(公告)日：1989-06-06
申请号：US174502
申请日：1988-03-28
申请人： Juergen Pollner , Gregor Trummer , Peter Moelzer
发明人： Juergen Pollner , Gregor Trummer , Peter Moelzer
IPC分类号： B64F1/10 , B64F1/22
CPC分类号： B64F1/227 , B64F1/22
摘要： A shunting vehicle for maneuvering aircraft on the ground equipped with an ascent and arresting device for the aircraft front undercarriages which overcomes the problem of the stepping out of the undercarriage in the upward direction and tilting off of the rear and, secondly, the problem of accepting front undercarriages equipped with stone guards. A pivoting ramp with automatically pivoting cams which pivot as a function of the pivoting motion of the ram is provided. Additional stationary and mobile elements of the arresting device prevent escape of the bow wheels in the upward or rearward directions. The ramp, and thus the cams, are actuated by a piston-cylinder unit, two toggle lever systems, and a sliding link guide.
摘要翻译：一种用于机动飞机的分流车辆，配备有用于飞机前底架的上升和制动装置，克服了起落架向上方向走出并向后倾斜的问题，其次，接受问题前起落架装备有石卫兵。提供了具有自动枢转凸轮的枢转斜面，该凸轮作为活塞的枢转运动而转动。止动装置的额外的固定和移动元件防止弓形轮沿向上或向后方向的逸出。斜坡，因此凸轮由活塞 - 气缸单元，两个肘节杆系统和滑动连杆导向器驱动。

8. 发明授权

US06283696B1 Aircraft towing vehicle 失效
标题翻译：飞机牵引车
公开(公告)号：US06283696B1
公开(公告)日：2001-09-04
申请号：US09424107
申请日：2000-02-07
申请人： Gregor Trummer , Hartmut Mann , Thomas Fuchs
发明人： Gregor Trummer , Hartmut Mann , Thomas Fuchs
IPC分类号： B64F122
CPC分类号： B64F1/227 , B62D49/02 , B64F1/22
摘要： An aircraft towing vehicle includes a lifting and locking device for the nose landing gear of the aircraft being towed. The device has two support elements which reach behind the nose wheels and can be displaced along straight-line guiding rails by a linear drive so as to pull the nose wheels of the aircraft onto a lifting platform and to lock it into place thereon. At the end of each guiding rail a guiding pin is provided which, in cooperation with a guiding track embodied in the support element, controls the rotation of the support element into a release position in which the nose landing gear is able to pass through. By a reverse movement, the rotation of the support elements are put into the operation position in which the support elements reach behind the nose landing gear.
摘要翻译：飞机牵引车辆包括用于被拖曳的飞机的起落架的提升和锁定装置。该装置具有两个支撑元件，它们到达前轮后面并且可以通过线性驱动器沿着直线导轨移位，以将飞行器的前轮拉到提升平台上并将其锁定在其上。在每个导轨的端部设置有引导销，该引导销与在支撑元件中实施的引导轨道配合地控制支撑元件旋转到其中前起落架能够通过的释放位置。通过反向运动，支撑元件的旋转被放入支撑元件到达起落架后面的操作位置。

9. 发明授权

US4923253A Braking system for aircraft towing vehicle 失效
标题翻译：飞机牵引车制动系统
公开(公告)号：US4923253A
公开(公告)日：1990-05-08
申请号：US250273
申请日：1988-09-28
申请人： Juergen Pollner , Gregor Trummer , Peter Moelzer , Karl Fichtner
发明人： Juergen Pollner , Gregor Trummer , Peter Moelzer , Karl Fichtner
IPC分类号： B64F1/10 , B60G17/016 , B60G17/0195 , B60T8/00 , B60T8/26 , B60T8/30 , B60T11/00 , B60T11/10
CPC分类号： B64F1/22 , B60G17/0164 , B60G17/0195 , B60T11/00 , B60T11/10 , B60T8/00 , B60T8/306 , B64F1/227 , B60G2300/00 , B60G2500/30 , Y02T50/826
摘要： A braking system for an aircraft towing vehicle which supports the nose wheel of an aircraft in a raised position and firmly clamps it to the vehicle. The braking force generated by the front wheels of the towing vehicle is greater by about 2:1 to 8:1 than the braking force at the rear wheels. The braking system has two hydraulic circuits employing identical braking cylinders at all four wheels of the vehicle. The number of cylinders per wheel are varied and different effective lever arms are used to generate like braking forces at each side of the vehicle, and the relatively greater braking force at the front wheels, even if one of the hydraulic circuits fails. The system limits the braking force at the front and rear wheels to maximum values to prevent excessive forces from damaging the nose gear of relatively smaller aircraft. The load carried by the vehicle is hydraulically sensed by tapping into the hydraulic leveling system to increase the braking forces that are generated when towing relatively heavier aircraft which is able to withstand such greater forces.
摘要翻译：一种用于飞机牵引车辆的制动系统，其支撑在升高位置的飞行器的前轮，并将其牢固地夹紧到车辆。牵引车辆的前轮产生的制动力比后轮的制动力大2:1〜8:1。制动系统具有在车辆的所有四个车轮处采用相同的制动缸的两个液压回路。每个车轮的缸数变化，并且使用不同的有效杠杆臂在车辆的每一侧产生相同的制动力，并且即使其中一个液压回路发生故障，前轮上的制动力也相对较大。该系统将前轮和后轮的制动力限制在最大值，以防止过大的力量损坏相对较小的飞机的前档。车辆承载的载荷通过进入液压调平系统进行液压感测，以增加在牵引能够承受更大力量的较重的飞机时产生的制动力。

10. 发明授权

US4917564A Hold-down system for an aircraft towing vehicle 失效
标题翻译：用于飞机牵引车的压紧系统
公开(公告)号：US4917564A
公开(公告)日：1990-04-17
申请号：US72502
申请日：1988-09-28
申请人： Juergen Pollner , Gregor Trummer , Peter Moelzer
发明人： Juergen Pollner , Gregor Trummer , Peter Moelzer
IPC分类号： B64F1/10 , B64F1/22
CPC分类号： B64F1/227 , B64F1/22
摘要： An aircraft towing vehicle has a frame with a rearwardly opening, U-shaped recess for receiving the nose wheel of an aircraft. A lifting and securing mechanism is disposed within the recess and includes a ramp and a stop plate carried by the frame, a lifter which pushes the nose wheel from behind up the ramp into abutment with the stop plate, and a pivotable hold-down mechanism mounted above the ramp. In its rest position the hold-down mechanism is set at a distance from the ground which is less than the diameter of the smallest nose wheel of the types of aircraft that can be towed. It contacts the periphery of the nose wheel being engaged at an upper forward guadrant of the wheel's periphery and passively moves in tandem with the nose wheel as it is being pushed up the ramp into its secured position. At the end of the engaging operation, the hold-down mechanism applied a downwardly directed force of a predetermined magnitude against the nose wheel, which is generated by a hydraulic actuator. The pressure remains sealed in the hydraulic actuator so that the clamping force is applied to the nose wheel throughout the towing operation. A sensor is provided for detecting any pressure drop in the hydraulic actuator and triggering a corresponding alarm signal.
摘要翻译：一架飞机牵引车具有一个带有向后开口的U形凹槽的框架，用于接收飞机的前轮。提升和固定机构设置在凹槽内，并包括一个斜面和一个由框架承载的止挡板，一个提升器，其将前轮从斜坡后面推压到止挡板上，以及一个可枢转的压紧机构，坡道上方在其静止位置，压紧机构设置在距离地面一定距离处，该距离小于可被牵引的飞行器类型的最小前轮的直径。它接触前轮的周边，该前轮的周边接合在车轮周边的上部前端，并且当其被向上推入斜坡进入其固定位置时被动地与前轮一起移动。在接合操作结束时，压紧机构施加预定大小的向下定向的力抵靠由液压致动器产生的前轮。压力保持密封在液压致动器中，使得夹紧力通过牵引操作施加到前轮。提供了用于检测液压致动器中的任何压降并触发相应报警信号的传感器。

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