公开(公告)号：US09988143B2

公开(公告)日：2018-06-05

申请号：US14614330

申请日：2015-02-04

Applicant: General Atomics Aeronautical Systems, Inc.

Inventor： Michael Allwein ,  Joseph Moore ,  Aron Howard Daria

IPC: B64C25/30 ,  B64C25/20 ,  B64C25/24 ,  B64C25/34

CPC classification number: B64C25/20 ,  B64C25/24 ,  B64C25/30 ,  B64C25/34

Abstract: Some embodiments provide apparatuses configured to deploy a landing gear of an aircraft, comprising: a landing gear coupler configured to couple with the landing gear; a release link configured to cooperate the landing gear coupler with a drive shaft that is configured to drive the landing gear between a stowed position and a deployed position; an override driver cooperated with the landing gear coupler; wherein the release link is configured to releasably maintain a relative position of landing gear coupler relative to the drive shaft, and the release link is configured to disengage a coupling between the drive shaft and the landing gear coupler such that the landing gear coupler is configured to move independent of the drive shaft; and wherein the override driver is configured to drive the landing gear coupler to the deployed position.

公开(公告)号：US20150291278A1

公开(公告)日：2015-10-15

申请号：US14614330

申请日：2015-02-04

Applicant: General Atomics Aeronautical Systems, Inc.

Inventor： Michael Allwein ,  Joseph Moore ,  Aron Howard Daria

IPC: B64C25/20 ,  B64C25/34

CPC classification number: B64C25/20 ,  B64C25/24 ,  B64C25/30 ,  B64C25/34

Abstract: Some embodiments provide apparatuses configured to deploy a landing gear of an aircraft, comprising: a landing gear coupler configured to couple with the landing gear; a release link configured to cooperate the landing gear coupler with a drive shaft that is configured to drive the landing gear between a stowed position and a deployed position; an override driver cooperated with the landing gear coupler; wherein the release link is configured to releasably maintain a relative position of landing gear coupler relative to the drive shaft, and the release link is configured to disengage a coupling between the drive shaft and the landing gear coupler such that the landing gear coupler is configured to move independent of the drive shaft; and wherein the override driver is configured to drive the landing gear coupler to the deployed position.

Abstract translation: 一些实施例提供了构造成展开飞行器的起落架的装置，包括：起落架联轴器，被配置为与起落架联接; 释放连杆，其构造成将起落架联接器与驱动轴配合，所述驱动轴构造成在收起位置和展开位置之间驱动起落架; 与起落架联轴器配合的超驰驾驶员; 其中所述释放连杆构造成可释放地保持起落架联轴器相对于所述驱动轴的相对位置，并且所述释放连杆构造成使所述驱动轴和所述起落架联轴器之间的联接件脱离，使得所述起落架联接器被配置为 独立于驱动轴移动; 并且其中所述超驰驱动器被配置为将所述起落架联接器驱动到展开位置。