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:
Sep. 28, 2021

Filed:

Dec. 20, 2018
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Emmanuel Pierre Dimitri Patsouris, Moissy-Cramayel, FR;

Quentin Matthias Emmanuel Garnaud, Moissy-Cramayel, FR;

Antoine Elie Hellegouarch, Moissy-Cramayel, FR;

Martial Alexandre Monseu, Moissy-Cramayel, FR;

Clementine Charlotte Marie Mouton, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/76 (2006.01); F02K 1/72 (2006.01); F16H 25/20 (2006.01);
U.S. Cl.
CPC ...
F02K 1/763 (2013.01); F02K 1/72 (2013.01); F02K 1/766 (2013.01); F05D 2260/57 (2013.01); F16H 25/2056 (2013.01);
Abstract

The turbojet includes, linking two of its parts as a main nacelle portion and a rear nacelle portion, a device which moves them relative to one another, for example in order to open a reverse gas thrust slot. The device includes a sleeve and two rods which are coaxial connected together by two screw links and two locking devices which may be engaged independently, such that the deployment of one of the rods results in the opening of the slot and the movement of the other rod, controlled by the same device, only occurs under specific turbojet maintenance circumstances.


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