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.
Patent No.:
Date of Patent:
Jan. 29, 2019
Filed:
Aug. 31, 2015
Applicant:
Aircelle, Gonfreville l'Orcher, FR;
Inventors:
Patrick Boileau, Tournefeuille, FR;
Peter Segat, Courbevoie, FR;
Pierre Caruel, Le Havre, FR;
Sarah Tissot, Bois d'Arcy, FR;
Assignee:
AIRCELLE, Gonfreville l'Orcher, FR;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/72 (2006.01); F02K 1/09 (2006.01); F02K 1/82 (2006.01);
U.S. Cl.
CPC ...
F02K 1/72 (2013.01); F02K 1/09 (2013.01); F02K 1/827 (2013.01); F05D 2240/129 (2013.01); F05D 2240/90 (2013.01); F05D 2250/34 (2013.01);
Abstract
A thrust reverser device for an aircraft turbojet engine includes: a movable cowl, translating cascades connected to the movable cowl, a mast; and a front suspension to suspend the turbojet engine. The cascades translates between a direct jet position where the cascades are retracted in a fan casing, and an indirect jet position where the cascades are brought out of the fan casing. In particular, the cascades have a sliding connection with the mast by means of at least one spacer connected to the mast downstream of the front suspension.