公开(公告)号：WO2011096833A8

公开(公告)日：2012-08-16

申请号：PCT/PL2011000009

申请日：2011-01-26

Applicant: MALICKI SLAWOMIR

Inventor： MALICKI SLAWOMIR

IPC: B64F1/22

CPC classification number: B64F1/22 ,  B64F1/227 ,  B64F1/228 ,  Y02T50/826

Abstract: 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.

Abstract translation: 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）的通过而闭合， 。 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：WO2018206983A1

公开(公告)日：2018-11-15

申请号：PCT/GB2018/051288

申请日：2018-05-11

Applicant: MCLAREN APPLIED TECHNOLOGIES LIMITED

Inventor： HELLIWELL, James Oliver ,  GLOVER, Anthony Richard ,  LAW, Anthony David

IPC: B64F1/22

CPC classification number: B64F1/227 ,  B64F1/228

Abstract: A shunt device for moving a wheeled vehicle by applying force to a ground wheel of the vehicle, the shunt device comprising: a first support wheel configured to support the shunt device on a surface and rotate about a first rotation axis so that the first support wheel has a first rotation centre on the first rotation axis within the first support wheel; and a roller configured to rotate about a second rotation axis and contact the ground wheel to push the wheeled vehicle in a shunt direction, the roller being positioned relative to the support wheel so that the second rotation axis within the roller is located behind a first plane perpendicular to the shunt direction and that passes through the first rotation centreand between (i) a second plane generally parallel to the surface and coincident with the first rotation centre and (ii) the surface; wherein contact between the shuntdevice and the ground wheel is via the roller from behind the ground wheel in the shunt direction.

公开(公告)号：WO2011096833A3

公开(公告)日：2011-10-13

申请号：PCT/PL2011000009

申请日：2011-01-26

Applicant: MALICKI STAVOMIR

Inventor： MALICKI STAVOMIR

IPC: B64F1/22

CPC classification number: B64F1/22 ,  B64F1/227 ,  B64F1/228 ,  Y02T50/826

Abstract: 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.

Abstract translation: 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）的通过而闭合， 。 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：WO2010141043A1

公开(公告)日：2010-12-09

申请号：PCT/US2010/000621

申请日：2010-03-02

Applicant: GRIFFITH, Gregory, M.

Inventor： GRIFFITH, Gregory, M.

IPC: G08G5/04 ,  G08G1/16

CPC classification number: G08G5/045 ,  B64F1/228 ,  G01S13/86 ,  G01S13/931 ,  G01S2013/9335 ,  G01S2013/936 ,  G08B3/10 ,  G08G5/04 ,  G08G5/065

Abstract: An aircraft collision avoidance system comprising (a) at least one separation monitoring device connectable to at least a portion of an aircraft, the separation monitoring device comprising (1) at least one transmitter and (2) at least one receiver and (b) a master unit.

Abstract translation: 1.一种飞机防撞系统，包括：（a）至少一个可连接到飞行器的至少一部分的分离监测装置，所述分离监测装置包括：（1）至少一个发射器和（2）至少一个接收器，以及（b） 主单位

公开(公告)号：WO2010046605A3

公开(公告)日：2010-06-17

申请号：PCT/FR2009052033

申请日：2009-10-22

Applicant: AIRBUS SOC PAR ACTION SIMPLIFI ,  AIRBUS OPERATIONS SAS ,  FRINGS CARSTEN ,  CROS CHRISTOPHE

Inventor： FRINGS CARSTEN ,  CROS CHRISTOPHE

IPC: B64F1/22 ,  G08G5/06

CPC classification number: G08G5/06 ,  B64F1/22 ,  B64F1/227 ,  B64F1/228 ,  Y02T50/826

Abstract: The invention relates to a method for controlling at least one appliance (12) for moving aircrafts (10): at least one appliance (12) connected to an aircraft is driven to a position (80) that is closer to an entry corridor (74) of a take-off runway (70) than an exit corridor (76) of the runway, and, once the appliance or each appliance is separated from the aircraft, the appliance (12) is driven to a position (82) that is closer to an exit corridor (76) of a landing runway (70) than an entry corridor (74) of said runway.

Abstract translation: 本发明涉及一种用于控制用于移动飞行器（10）的至少一个器具（12）的方法：连接到飞行器的至少一个器具（12）被驱动到更靠近入口通道（74）的位置（80） ）的跑道（70）比跑道的出口走廊（76）小，并且一旦器具或每个器具与飞机分离，器具（12）被驱动到位置（82） 更靠近所述跑道入口跑道（70）的出口走廊（76）而不是所述跑道入口走廊（74）。

公开(公告)号：WO2008038270A2

公开(公告)日：2008-04-03

申请号：PCT/IL2007/001172

申请日：2007-09-24

Applicant: ISRAEL AEROSPACE INDUSTRIES LTD. ,  PERRY, Arie ,  BRAIER, Ran

Inventor： PERRY, Arie ,  BRAIER, Ran

IPC: B64F1/22 ,  G08G5/06

CPC classification number: B64F1/22 ,  B64F1/227 ,  B64F1/228 ,  Y02T50/826

Abstract: A method for transferring airplanes and an unmanned airplane transfer system. The airplane transferring system includes: receiving a transfer signal responsive of a movement of an airplane control component; and transferring an airplane, by an unmanned airplane transfer system, in response to the transfer signal.

Abstract translation:

一种转移飞机的方法和一种无人飞机转移系统。 该飞机传送系统包括：响应于飞机控制部件的移动而接收传送信号; 并通过无人驾驶飞机转移系统转移飞机，以响应转移信号。

公开(公告)号：WO2014198746A3

公开(公告)日：2016-04-28

申请号：PCT/EP2014062072

申请日：2014-06-11

Applicant: AIRBUS GROUP SAS

Inventor： JOUBERT EMMANUEL ,  NESPOULOUS CHARLES ,  RECHAIN BRUNO ,  SMAOUI HICHEM

IPC: B64F1/04

CPC classification number: B64F1/04 ,  B64C25/32 ,  B64F1/22 ,  B64F1/228 ,  Y02T50/826

Abstract: A device (100) for moving aircraft along the ground comprises at least one runway (10, 18a, 18b, 18c) and at least one aircraft. The aircraft is secured to a tractor element (30) comprising a magnetic mass (31) formed mainly of type II superconductor material and the runway (10, 18a, 18b, 18c) comprises stator coils (12) arranged in the runway in at least one line of coils which is parallel to an axis (11) of the runway. A command/control system (13) supplies power to the stator coils in such a way as to create a magnetic field that levitates the tractor element (30), magnetized beforehand into a phase II superconducting state, above the runway.

Abstract translation: 用于沿着地面移动飞行器的装置（100）包括至少一个跑道（10,18a，18b，18c）和至少一个飞行器。 飞机被固定到牵引器元件（30）上，该拖拉机元件（30）包括主要由II型超导体材料形成的磁性体（31），并且跑道（10,18a，18b，18c）至少包括设置在跑道中的定子线圈 一条线圈，其平行于跑道的轴线（11）。 指令/控制系统（13）以这样的方式向定子线圈供电，以便产生使拖拉机元件（30）悬浮的磁场，预先磁化成在跑道上方的II级超导状态。

公开(公告)号：WO2011154952A1

公开(公告)日：2011-12-15

申请号：PCT/IL2011/000457

申请日：2011-06-09

Applicant: ISRAEL AEROSPACE INDUSTRIES LTD. ,  LEVY, Raphael, E. ,  BRAIER, Ran ,  PERRY, Arie

Inventor： LEVY, Raphael, E. ,  BRAIER, Ran ,  PERRY, Arie

IPC: B64F1/00

CPC classification number: B62D1/283 ,  B64F1/002 ,  B64F1/22 ,  B64F1/227 ,  B64F1/228 ,  Y02T50/826

Abstract: A vehicle for towing an airplane by receiving thereupon a nose landing gear of the airplane having an airplane longitudinal axis. The vehicle having a vehicle longitudinal axis and is configured to tow the airplane along a straight or curved path and comprises a controller for directing its operation, including maintaining the vehicle's in-phase position in which the vehicle longitudinal axis is parallel to the airplane longitudinal axis.

Abstract translation: 用于通过在其上接收具有飞机纵向轴线的飞机的起落架来牵引飞机的车辆。 车辆具有车辆纵向轴线并且被构造成沿着直线或弯曲路径拖动飞机，并且包括用于引导其操作的控制器，包括保持车辆的同轴位置，在该位置中车辆纵向轴线平行于飞机纵向轴线 。

公开(公告)号：WO2011096833A2

公开(公告)日：2011-08-11

申请号：PCT/PL2011/000009

申请日：2011-01-26

Applicant: MALICKI, Stavomir

Inventor： MALICKI, Stavomir

CPC classification number: B64F1/22 ,  B64F1/227 ,  B64F1/228 ,  Y02T50/826

Abstract: 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.

Abstract translation: 本发明解决了用于在发动机关闭的情况下将飞机机场围绕机场停机坪从停机位置运送到起飞跑道以及从停机位置运送到停机位置的系统的问题。 该系统由导向槽（5）组成，其中安装在对接站（8）中的导向销（9）移动并优选地卡锁到飞机（4）的前轮（10）上。 导向槽（5）从上方被可旋转的格栅形式的格栅（11）覆盖，所述格栅设计成打开让导向销（9）在导向槽（5）中滑动并在导向销（9）通过之后关闭， 。 开关装置（12）安装在导向槽（4）中的突变曲线位置以及方向改变的位置处。

公开(公告)号：WO2010012261A3

公开(公告)日：2010-07-15

申请号：PCT/DE2009000974

申请日：2009-07-09

Applicant: BECKER ANDREAS ,  BERGERHOFF ECKHARD

Inventor： BECKER ANDREAS

IPC: B64F1/22

CPC classification number: B64F1/22 ,  B64F1/227 ,  B64F1/228 ,  G08G5/06 ,  Y02T50/826

Abstract: The invention relates to an automatic system (1) for manoeuvring aircraft (2) on the ground, based on driverless towing vehicles, (hereafter AGTV's) (1), which can independently hold the undercarriage of the aircraft (2). In said system the AGTVs pull the aircraft from transfer areas (4) on the taxiways of the runways (3) to the stand (8) and vice versa, allowing the propulsion systems of the aircraft (2) to remain switched off during the taxiing process. The driverless AGTVs receive their driving jobs from a computer-aided guidance and management system (49) which controls the AGTV fleet (1) in a collision- and conflict-free manner.

Abstract translation: 自动系统（1），用于操纵（2）基于无人驾驶飞机拖拉机地，在下文中AGTVs（1）中提到的飞机，可容纳所述飞行器（2）独立地在底盘上。 所述AGTVs（1）拉所述飞行器（2）上的跑道（3）的滚动轨道上的转印面（4）到栅极（8）和背面在该系统中，使得飞机的各个驱动器（2）可以保持，而辊关闭 ， 无人驾驶AGTVs（1）由计算机控制和管理系统（49），其控制的AGTV得到他们的运动任务（1）舰队将碰撞和无冲突。