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:
Mar. 08, 2022

Filed:

May. 12, 2020
Applicant:

Safran Landing Systems, Velizy-Villacoublay, FR;

Inventors:

Jean-Baptiste Kamis, Moissy-Cramayel, FR;

Jean-Charles Roger, Moissy-Cramayel, FR;

Assignee:

SAFRAN LANDING SYSTEMS, Velizy Villacoublay, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F15B 15/22 (2006.01); B64C 25/22 (2006.01); F01B 11/02 (2006.01);
U.S. Cl.
CPC ...
F15B 15/223 (2013.01); B64C 25/22 (2013.01); F01B 11/02 (2013.01); F15B 15/22 (2013.01); F15B 15/227 (2013.01);
Abstract

The invention relates to a hydraulic actuator comprising a cylinder () in which a piston () secured to a rod () is mounted so as to slide in a sealed manner in order to delimit in the cylinder a hydraulic extension chamber () and a hydraulic retraction chamber () that are connected to respective ports, the hydraulic actuator comprising means for slowing the piston when the piston approaches a retracted position. According to the invention, the slowing means comprise first and second hydraulic lines () extending between the extension port and the extension chamber, the first hydraulic line comprising a seat () while the piston bears a retractable finger () having an end () that comes to bear against the seat in order to close the first hydraulic line () when the piston approaches the retracted position, such that only the second hydraulic line () remains open while the piston completes its travel towards the retracted position. Landing gear and aircraft comprising such an actuator.


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