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:
Aug. 30, 2022

Filed:

Jun. 29, 2020
Applicant:

Safran Nacelles, Gonfreville l'Orcher, FR;

Inventors:

Loïc Grall, Gonfreville l'Orcher, FR;

Alexis Heau, Gonfreville l'Orcher, FR;

Benjamin Brebion, Gonfreville l'Orcher, FR;

Sébastien Michel Thierry Guillemant, Gonfreville l'Orcher, FR;

Mélody Seriset, Gonfreville l'Orcher, FR;

Patrick Boileau, Gonfreville l'Orcher, FR;

Assignee:

Safran Nacelles, Gonfreville l'Orcher, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/70 (2006.01); F02K 1/80 (2006.01); B64D 29/06 (2006.01); B64D 29/08 (2006.01);
U.S. Cl.
CPC ...
F02K 1/70 (2013.01); B64D 29/06 (2013.01); B64D 29/08 (2013.01); F02K 1/80 (2013.01); F05D 2220/323 (2013.01); F05D 2240/129 (2013.01);
Abstract

A grid-type thrust reverser for a turbojet engine includes a moving O-shaped thrust reverser body that is generally cylindrical in shape around a longitudinal central axis (A) and includes an inner wall configured to delimit a cold air stream, with an inner structure that surrounds the turbojet engine, the movable thrust reverser body being mounted so as to be able to slide along the longitudinal central axis (A) between a direct jet position in which the outer cowl covers the thrust reverser grids, and a thrust-reversal position in which the outer cowl uncovers the thrust reverser grids. The movable thrust reverser body includes a first half-portion and a second half-portion that are mounted so as to each pivot about a longitudinal pivot axis (B), between a closed position and an open gullwing position for removing the turbojet engine, via the cradle.


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