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. 18, 2015

Filed:

Nov. 19, 2012
Applicant:

Aircelle, Gonfreville l'Orcher, FR;

Inventor:

Guy Bernard Vauchel, Harfleur, FR;

Assignee:

AIRCELLE, Gonfreville L'Orcher, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 1/56 (2006.01); F02K 1/62 (2006.01); F01D 11/00 (2006.01); F02K 1/72 (2006.01); F02K 1/76 (2006.01);
U.S. Cl.
CPC ...
F02K 1/62 (2013.01); F01D 11/005 (2013.01); F02K 1/72 (2013.01); F02K 1/56 (2013.01); F02K 1/566 (2013.01); F02K 1/625 (2013.01); F02K 1/763 (2013.01); F05D 2240/55 (2013.01); F05D 2250/34 (2013.01); F05D 2250/41 (2013.01);
Abstract

A cascade thrust reverser for an airplane dual flow jet engine nacelle is provided that includes a front frame holding a plurality of cascades, a cowling slidably mounted between a direct jet position and a reverse jet position. The cowl includes a substantially annular diaphragm that is placed edge-to-edge with the front frame and radially inside said cascades when said cowl is located in the direct jet position. Thrust reversal flaps are pivotably mounted onto the diaphragm, and cylinders for actuating the cowl are also provided. Upstream ends of the cylinders are mounted on a stationary portion of the nacelle, and the downstream ends of the cylinders are mounted on an upstream edge of the diaphragm.


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