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:
Apr. 28, 2020

Filed:

Mar. 08, 2017
Applicant:

Safran Nacelles, Gonfreville l'Orcher, FR;

Inventors:

Jean-Philippe Joret, Beuzeville, FR;

Emmanuel Lesteven, Triqueville, FR;

Vincent Peyron, Le Havre, FR;

Patrick Boileau, Tournefeuille, FR;

Assignee:

SAFRAN NACELLES, Gonfreville l'Orcher, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 29/06 (2006.01); F02K 1/76 (2006.01); B64D 27/16 (2006.01);
U.S. Cl.
CPC ...
B64D 29/06 (2013.01); F02K 1/763 (2013.01); B64D 27/16 (2013.01); F05D 2220/323 (2013.01); F05D 2230/72 (2013.01); F05D 2250/11 (2013.01); F05D 2260/57 (2013.01);
Abstract

A propulsion unit for an aircraft is provided. The propulsion unit includes a stationary unit having at least one cowl pivotally mounted on an axis collinear with a longitudinal axis of the propulsion unit between an operating position or a maintenance position allowing access to the turbojet engine for regular maintenance operations and irregular maintenance operations. The maintenance position for irregular maintenance operations includes an opening angle of the cowl that is greater than the opening angle of the cowl to carry out regular maintenance operations. The propulsion unit further includes at least one cylinder and at least one safety connecting rod secured to the cowl and stationary unit.


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