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. 25, 2019

Filed:

Mar. 17, 2015
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Frederic Jacques Eugene Goupil, Moissy Cramayel, FR;

Noel Joseph Camille Robin, Moissy Cramayel, FR;

Regis Eugene Henri Servant, Moissy Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/18 (2006.01); F01D 25/24 (2006.01); F02C 3/04 (2006.01); F02K 3/075 (2006.01); F16B 2/22 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); F01D 25/24 (2013.01); F01D 25/243 (2013.01); F02C 3/04 (2013.01); F02K 3/075 (2013.01); F16B 2/22 (2013.01); F05D 2230/64 (2013.01); F05D 2240/91 (2013.01); F05D 2260/36 (2013.01); F05D 2260/37 (2013.01); F05D 2260/38 (2013.01); Y02T 50/671 (2013.01);
Abstract

A unit including an intermediate turbojet casing formed by a hub including a downstream transverse endplate having formed therein at least one first opening putting the inside of the hub into communication with a duct extending downstream from the endplate and opening out at its downstream end via a second opening formed in an outer annular shroud extending downstream from the hub for defining the inside of an annular flow space for a secondary stream, is provided. The upstream end of the duct is fastened to the downstream endplate of the hub by releasable elastic engagement.


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