公开(公告)号：US20150183511A1

公开(公告)日：2015-07-02

申请号：US14141150

申请日：2013-12-26

Applicant: Honeywell International Inc.

Inventor： Joseph Ott ,  Keith Hughes ,  Robert E. De Mers ,  Olukayode Olofinboba

IPC: B64C19/00 ,  B64C25/40

CPC classification number: B64C19/00 ,  B64C25/405 ,  B64D31/04 ,  Y02T50/823

Abstract: A lever control system integrates taxi operation using an electric motor in an aircraft with speed control of a jet engine in the same aircraft. The lever control system provides a smooth transition between the electric motor system used for aircraft taxi operation, and a jet engine system used to fly the aircraft. The lever control system may include a reverse lockout mechanism to prevent unintended reverse taxi movement of the aircraft.

Abstract translation: 杠杆控制系统将飞机中的电动机的出租车操作与在同一架飞机上的喷气发动机的速度控制相结合。 杠杆控制系统提供用于飞机出租车操作的电动马达系统和用于飞行飞机的喷气发动机系统之间的平滑过渡。 杠杆控制系统可以包括反向锁定机构，以防止飞机的意外的反向出租车运动。