The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jan. 16, 2018

Filed:

Aug. 20, 2014
Applicants:

Commercial Aircraft Corporation of China., Ltd, Shanghai, CN;

Commercial Aircraft Corporation of China, Ltd Shanghai Aircraft Design and Research Institute, Shanghai, CN;

Inventors:

Jun Lv, Shanghai, CN;

Qinggong Meng, Shanghai, CN;

Pu Zhang, Shanghai, CN;

Hao Jiang, Shanghai, CN;

Shangxin Yang, Shanghai, CN;

Hengkang Zhang, Shanghai, CN;

Jian Ma, Shanghai, CN;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 25/20 (2006.01); B64C 25/16 (2006.01); B64C 25/10 (2006.01);
U.S. Cl.
CPC ...
B64C 25/20 (2013.01); B64C 25/10 (2013.01); B64C 25/16 (2013.01);
Abstract

A linkage mechanism for controlling an aircraft landing gear hatch door includes a primary torsion tube having a first portion located inside a landing gear hatch and a second portion outside the landing gear hatch. A first drive apparatus transfer the driving force of a landing gear support column to the primary torsion tube. A secondary torsion tube has an inner end portion located inside the hatch and an outer end portion located outside the hatch. A second drive apparatus is located outside the landing gear hatch and connects the primary torsion tube and the secondary torsion tube outside the hatch. Two third drive apparatuses are connected between the inner end portion of the secondary torsion tube and one of the hatch doors.


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