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:
Jun. 24, 2025

Filed:

Apr. 11, 2022
Applicant:

Safran Landing Systems, Velizy-Villacoublay, FR;

Inventor:

Jean-Baptiste Kamis, Moissy-Cramayel, FR;

Assignee:

SAFRAN LANDING SYSTEMS, Velizy-Villacoublay, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/76 (2006.01); F15B 7/00 (2006.01); F15B 20/00 (2006.01);
U.S. Cl.
CPC ...
F02K 1/763 (2013.01); F15B 7/003 (2013.01); F15B 7/006 (2013.01); F15B 20/00 (2013.01); F15B 2211/20515 (2013.01); F15B 2211/20561 (2013.01); F15B 2211/40523 (2013.01); F15B 2211/426 (2013.01); F15B 2211/428 (2013.01); F15B 2211/7057 (2013.01);
Abstract

A thrust reverser device for an aircraft turbojet engine nacelle an electro-hydrostatic actuation system that includes a motor pump and a first actuation assembly. The first actuation assembly includes a series of at least two actuators configured to be attached to a movable cover of the thrust reverser and to move the movable cover or covers between a retracted position and a deployed position relative to the nacelle. The first electro-hydraulic actuation system further includes a volumetric flow divider with an inlet connected to the motor pump and at least two outlets, wherein each outlet is connected to an actuator. The volumetric flow divider is configured to receive a fluid and to supply the fluid to the actuators with an equal flow rate.


Find Patent Forward Citations

Loading…