公开(公告)号：US09658621B2

公开(公告)日：2017-05-23

申请号：US14726048

申请日：2015-05-29

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： James Fusaro ,  Steven Newell

IPC: G05D1/02 ,  B64F1/00

CPC classification number: G05D1/0202 ,  B64C25/405 ,  B64C25/44 ,  B64F1/002 ,  Y02T50/823

Abstract: Apparatuses, systems and methods are provided for automatically pushing aircraft back from an airport gate and/or for automatically taxiing an aircraft. At least one engines-off drive is attached to at least one landing gear wheel to apply a rotational force and/or a rotation impeding force to the at least one landing gear wheel. At least one friction brake is attached to at least one landing gear wheel to apply a rotation impeding force to the at least one landing gear wheel.

公开(公告)号：US20160349752A1

公开(公告)日：2016-12-01

申请号：US14726048

申请日：2015-05-29

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： James Fusaro ,  Steven Newell

IPC: G05D1/02 ,  B64F1/00

CPC classification number: G05D1/0202 ,  B64C25/405 ,  B64C25/44 ,  B64F1/002 ,  Y02T50/823

Abstract: Apparatuses, systems and methods are provided for automatically pushing aircraft back from an airport gate and/or for automatically taxiing an aircraft. At least one engines-off drive is attached to at least one landing gear wheel to apply a rotational force and/or a rotation impeding force to the at least one landing gear wheel. At least one friction brake is attached to at least one landing gear wheel to apply a rotation impeding force to the at least one landing gear wheel.

Abstract translation: 提供了设备，系统和方法，用于自动将飞机从机场门口推回并/或用于自动滑行飞机。 至少一个发动机关闭驱动器连接到至少一个起落架齿轮以向所述至少一个起落架轮施加旋转力和/或旋转阻力。 至少一个摩擦制动器附接到至少一个起落架齿轮以向所述至少一个起落架轮施加旋转阻力。

公开(公告)号：US09417629B2

公开(公告)日：2016-08-16

申请号：US14532443

申请日：2014-11-04

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Joseph Nutaro ,  William D. Cromer ,  Daniel P. Johnson ,  Lee Davis ,  James Fusaro

IPC: G05D1/00 ,  B64C25/40 ,  B64C25/42 ,  B64C25/50

CPC classification number: G05D1/0011 ,  B64C25/405 ,  B64C25/42 ,  B64C25/50 ,  B64D13/06 ,  B64D41/00 ,  B64D2013/0611 ,  G05D1/0038 ,  G05D1/0083

Abstract: A ground remote control system for an aircraft includes a security pairing device configured to establish a first secure communication link and protocol between a remote control device and a ground remote control system controller; and establish a second secure communication link and protocol, using the first communication link and protocol between the remote control device and the ground remote control system controller. The ground remote control system controller is configured to receive drive command signals, brake command signals, steering command signals, and power command signals, from the remote control device and generate the electronic drive commands, the electronic brake commands, the electronic steering commands, and the electronic power commands.

Abstract translation: 一种用于飞行器的地面遥控系统包括：一个安全配对装置，配置成在遥控装置和地面遥控系统控制器之间建立第一安全通信链路和协议; 并建立第二个安全通信链路和协议，使用远程控制设备和地面遥控系统控制器之间的第一通信链路和协议。 地面遥控系统控制器被配置为从遥控装置接收驱动命令信号，制动指令信号，转向指令信号和电力命令信号，并产生电子驱动命令，电子制动指令，电子转向指令和 电子命令。

公开(公告)号：US20160124428A1

公开(公告)日：2016-05-05

申请号：US14532443

申请日：2014-11-04

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Joseph Nutaro ,  William D. Cromer ,  Daniel P. Johnson ,  Lee Davis ,  James Fusaro

IPC: G05D1/00 ,  B64C25/42 ,  B64C25/50 ,  B64C25/40

CPC classification number: G05D1/0011 ,  B64C25/405 ,  B64C25/42 ,  B64C25/50 ,  B64D13/06 ,  B64D41/00 ,  B64D2013/0611 ,  G05D1/0038 ,  G05D1/0083

Abstract: A ground remote control system for an aircraft includes a security pairing device configured to establish a first secure communication link and protocol between a remote control device and a ground remote control system controller; and establish a second secure communication link and protocol, using the first communication link and protocol between the remote control device and the ground remote control system controller. The ground remote control system controller is configured to receive drive command signals, brake command signals, steering command signals, and power command signals, from the remote control device and generate the electronic drive commands, the electronic brake commands, the electronic steering commands, and the electronic power commands.

Abstract translation: 一种用于飞行器的地面遥控系统包括：一个安全配对装置，配置成在遥控装置和地面遥控系统控制器之间建立第一安全通信链路和协议; 并建立第二个安全通信链路和协议，使用远程控制设备和地面遥控系统控制器之间的第一通信链路和协议。 地面遥控系统控制器被配置为从遥控装置接收驱动命令信号，制动指令信号，转向指令信号和电力命令信号，并产生电子驱动命令，电子制动指令，电子转向指令和 电子命令。