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:
Jun. 18, 2019

Filed:

Aug. 25, 2014
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Ceddric Beljambe, Soignolles en Brie, FR;

Noel Robin, Villejust, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/02 (2006.01); B64D 27/26 (2006.01); B64D 29/06 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
B64D 29/06 (2013.01); B64D 27/26 (2013.01); F01D 9/02 (2013.01); F01D 25/243 (2013.01); F01D 25/246 (2013.01); B64D 2027/262 (2013.01); F05D 2220/323 (2013.01); F05D 2260/30 (2013.01);
Abstract

A casing structure interposed between the engine and the nacelle of an aircraft, the structure including a shroud surrounding the engine having an engine axis and including a stationary portion and a plurality of sectors; a radial arm providing the connection to the nacelle; fasteners for securing the plurality of shroud sectors to one another or to the radial arm; and the fasteners include two series of holes formed in two parallel side walls of the shroud sectors for the purpose of receiving two respective series of bolts, each passing through a corresponding set of orifices of an adjacent shroud sector or of an adjacent radial arm, a hinge arranged between each of the shroud sectors and the stationary portion of the shroud to enable the shroud sectors to be pivoted in individual manner about a common pivot axis perpendicular to the side walls arranged along the engine axis.


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