公开(公告)号：US20140244076A1

公开(公告)日：2014-08-28

申请号：US13781659

申请日：2013-02-28

Applicant: HONEYWELL INTERNATIONAL, INC., PATENT SERVICES M/S AB/2B

Inventor： MUTHUKUMAR MURTHY ,  MADASAMY SHUNMUGAVEL ,  BALAKRISHNA PEDDINENI ,  ROCCO DIVITO

IPC: B64C19/00

CPC classification number: B64C25/50

Abstract: Landing gear apparatus for an aircraft may include a steerable nosewheel assembly and left main landing gear wheels and right main landing gear wheels driven by motors. A controller may receive an angular position of the nosegear wheel assembly. The controller may respond to the angular position by transmitting wheel speed signals to one or more of the motors to maintain the center of gravity of the aircraft within a predetermined stability triangle and to perform short radii turning.

Abstract translation: 用于飞行器的起落架装置可包括由电动机驱动的可操纵的nosewhehele组件和左主起落架齿轮和右主起落架。 控制器可以接收鼻齿轮组件的角位置。 通过将车轮速度信号传送到一个或多个电动机来控制飞行器的重心，使飞行器的重心保持在预定的稳定三角形内并执行短的半径转动。