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:
Oct. 28, 2014

Filed:

Dec. 03, 2012
Applicant:

Aircelle, Gonfreville l'Orcher, FR;

Inventors:

Jean-Philippe Joret, Beuzeville, FR;

Peter Segat, Le Havre, FR;

Guy Bernard Vauchel, Harfleur, FR;

Georges Alain Bouret, Epouville, FR;

Assignee:

Aircelle, Gonfreville l'Orcher, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 1/80 (2006.01); F02K 1/70 (2006.01); B64D 29/06 (2006.01); F02K 1/76 (2006.01);
U.S. Cl.
CPC ...
F02K 1/70 (2013.01); F02K 1/766 (2013.01); B64D 29/06 (2013.01);
Abstract

A nacelle for a turbojet engine of an aircraft is provided that includes a fan case, an internal structure positioned upstream from the fan case, and a thrust reverser positioned downstream from the fan case. The thrust reverser includes a cowl delimiting an external line (LE) and including two removable half cowls. A device for absorbing circumferential stresses are shaped so as to lock the half cowls in the closed position when it occupies a locking configuration on the one hand and for allowing the opening of the half cowls when it occupies an unlocking configuration on the other hand. The stress absorbing device is positioned under an upstream portion of a pylon and is exclusively attached to the half cowls in order to allow the opening of the two half cowls independently of the opening/closing of an external fan cowl.


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