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:
Nov. 02, 2021

Filed:

Nov. 14, 2018
Applicant:

Safran Landing Systems, Velizy Villacoublay, FR;

Inventors:

Florent Fortier, Velizy Villacoublay, FR;

Sébastien Dubois, Velizy Villacoublay, FR;

Assignee:

SAFRAN LANDING SYSTEMS, Velizy Villacoublay, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 25/58 (2006.01); B64C 25/20 (2006.01); B64C 25/24 (2006.01); B64C 25/14 (2006.01); B64C 25/26 (2006.01); B64C 25/30 (2006.01); F16F 9/22 (2006.01); F16F 9/34 (2006.01);
U.S. Cl.
CPC ...
B64C 25/58 (2013.01); B64C 25/14 (2013.01); B64C 25/20 (2013.01); B64C 25/24 (2013.01); B64C 25/26 (2013.01); B64C 25/30 (2013.01); F16F 9/22 (2013.01); F16F 9/3405 (2013.01); F16F 2222/12 (2013.01); F16F 2232/08 (2013.01);
Abstract

Methods of moving an aircraft undercarriage that is movable between a retracted position and a deployed position generally include: using a rotary electromechanical type drive actuator coupled to a portion of the aircraft undercarriage to raise it from the deployed position to the retracted position; disengaging the drive actuator during a descent of the undercarriage from the retracted position to the deployed position and using a hydraulic linear shock absorber coupled to a portion of the undercarriage to regulate the rate of descent and to absorb shock on arrival of the undercarriage in the deployed position; and neutralizing the shock absorber while raising the undercarriage.


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