公开(公告)号：US20170121012A1

公开(公告)日：2017-05-04

申请号：US14927873

申请日：2015-10-30

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： David Lazarovich ,  Nicolae Morcov ,  Marius Pleniceanu

IPC: B64C25/40 ,  B64C25/50 ,  B64D41/00 ,  B64C25/34

CPC classification number: B64C25/405 ,  B64C25/34 ,  B64C25/50 ,  B64D41/00 ,  B64D2221/00 ,  Y02T50/44 ,  Y02T50/823

Abstract: A gate departure system for an aircraft includes an electric traction motor for driving a wheel of a main landing gear assembly of the aircraft on only one side of the aircraft; and a controller selectively connected to a starter-generator of an auxiliary power unit (APU) and to the traction motor to control flow of electrical power to either the starter-generator for starting of the APU or the electric traction motor for driving the wheel.

公开(公告)号：US20150375854A1

公开(公告)日：2015-12-31

申请号：US14317112

申请日：2014-06-27

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Stephen Abel ,  David Lazarovich ,  Joseph Nutaro

IPC: B64C25/40 ,  G05D1/00

CPC classification number: B64C25/405 ,  Y02T50/823

Abstract: An aircraft taxi control system may include a left main gear (MG) drive motor, a right MG motor, a first motor drive controller configured to produce a left motor torque signal responsively to nose gear angle (NGA) and nose wheel speed (NGS), and a second motor drive controller configured to produce a right motor toque signal responsively to the NGA and the NGS. The left motor torque signal and the right motor torque signal may be coordinated to reduce lateral loading of the nose wheel during a turning maneuver.

Abstract translation: 飞机出租车控制系统可以包括左主齿轮（MG）驱动马达，右MG马达，第一马达驱动控制器，其构造成响应于前档角（NGA）和前轮速度（NGS）产生左电机转矩信号， 以及第二电动机驱动控制器，被配置为响应于NGA和NGS产生正确的电动机转矩信号。 可以协调左电动机转矩信号和右电动机转矩信号以减少转向操纵期间前轮的横向负载。

公开(公告)号：US09771149B2

公开(公告)日：2017-09-26

申请号：US14927873

申请日：2015-10-30

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： David Lazarovich ,  Nicolae Morcov ,  Marius Pleniceanu

IPC: G01C23/00 ,  G05D1/00 ,  G05D3/00 ,  B64C25/40 ,  B64C25/34 ,  B64C25/50 ,  B64D41/00

CPC classification number: B64C25/405 ,  B64C25/34 ,  B64C25/50 ,  B64D41/00 ,  B64D2221/00 ,  Y02T50/44 ,  Y02T50/823

Abstract: A gate departure system for an aircraft includes an electric traction motor for driving a wheel of a main landing gear assembly of the aircraft on only one side of the aircraft; and a controller selectively connected to a starter-generator of an auxiliary power unit (APU) and to the traction motor to control flow of electrical power to either the starter-generator for starting of the APU or the electric traction motor for driving the wheel.