公开(公告)号：US20120119018A1

公开(公告)日：2012-05-17

申请号：US13358659

申请日：2012-01-26

Applicant: Arie PERRY ,  Ran BRAIER

Inventor： Arie PERRY ,  Ran BRAIER

IPC: B64C25/50

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

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US20100096494A1

公开(公告)日：2010-04-22

申请号：US12619130

申请日：2009-11-16

Applicant: Ran BRAIER ,  Arie PERRY

Inventor： Ran BRAIER ,  Arie PERRY

IPC: B64C25/50 ,  G05D1/00

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

Abstract: Disclosed a method of transferring airplanes and an unmanned airplane transfer system. The transfer system comprises a transfer module adapted to transfer an airplane by moving a landing gear of the airplane; and a controller being assembled with the transfer system, coupled to the transfer module, and adapted to i) receive a transfer signal; ii) to control the transfer module in response to the transfer signal; and iii) to coordinate transferring the airplane by the unmanned airplane transfer system and at least one second unmanned airplane transfer system. The method of transferring an airplane by a plurality of unmanned airplane transfer systems comprises receiving by at least one unmanned airplane transfer system among said plurality of transfer systems a transfer signal, and in response to the transfer signal, coordinating the transfer of the airplane by at least two unmanned airplane transfer systems among said plurality of transfer systems.

Abstract translation: 公开了一种转移飞机和无人驾驶飞行器传输系统的方法。 传送系统包括：转移模块，其适于通过移动飞机的起落架来转移飞机; 以及与所述传送系统组装的控制器，耦合到所述传送模块，并且适于i）接收传送信号; ii）响应于传送信号来控制传送模块; 以及iii）协调由无人驾驶飞行器传送系统和至少一个第二无人飞行器传送系统传送飞机。 通过多个无人驾驶飞行器传输系统传送飞机的方法包括由所述多个传送系统中的至少一个无人驾驶飞行器传输系统接收传送信号，并且响应于传送信号，通过以下方式协调飞机的传送： 所述多个传送系统中的至少两个无人飞行器传送系统。

公开(公告)号：US20120061521A1

公开(公告)日：2012-03-15

申请号：US13238636

申请日：2011-09-21

Applicant: Arie PERRY ,  Ran BRAIER

Inventor： Arie PERRY ,  Ran BRAIER

IPC: G05D1/02

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

Abstract: An airplane transfer system for transferring an airplane comprising an airplane control component. The system comprises: a transfer module comprising at least one motor and adapted to transfer an airplane; and a controller coupled to the transfer module and configured to: i) receive a at least one transfer signal that is responsive to one or more commands provided via the airplane control component; and ii) control the transfer module in response to the transfer signal, wherein the commands are a priori capable of controlling the airplane or components thereof.

Abstract translation: 一种用于转移包括飞机控制部件的飞机的飞机传送系统。 该系统包括：传输模块，包括至少一个电动机并适于传送飞机; 以及耦合到所述传送模块并被配置为：i）接收响应于经由所述飞机控制部件提供的一个或多个命令的至少一个传送信号的控制器; 以及ii）响应于所述传送信号控制所述传送模块，其中所述命令是先验地能够控制所述飞机或其组件。

公开(公告)号：US20100140392A1

公开(公告)日：2010-06-10

申请号：US12619123

申请日：2009-11-16

Applicant: Arie PERRY ,  Ran BRAIER

Inventor： Arie PERRY ,  Ran BRAIER

IPC: B64C25/50

CPC classification number: B64F1/10 ,  B64C25/50 ,  B64F1/22 ,  B64F1/227

Abstract: 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.

Abstract translation: 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。