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:
May. 12, 2020

Filed:

Jul. 20, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Baptiste Marie Aubin Pierre Jouy, Moissy-Cramayel, FR;

Bertrand Guillaume Robin Pellaton, Moissy-Cramayel, FR;

Sebastien Jean Laurent Prestel, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/30 (2006.01); F01D 9/06 (2006.01); F02C 3/13 (2006.01); F02C 9/18 (2006.01);
U.S. Cl.
CPC ...
F01D 25/30 (2013.01); F01D 9/065 (2013.01); F02C 3/13 (2013.01); F02C 9/18 (2013.01); F05D 2220/323 (2013.01); F05D 2250/314 (2013.01); F05D 2260/20 (2013.01); F05D 2260/941 (2013.01); F05D 2270/101 (2013.01); F05D 2270/114 (2013.01); F05D 2300/50212 (2013.01); Y02T 50/675 (2013.01);
Abstract

The invention relates to an exhaust casing for a turbine engine of an aircraft, including: a collar (), a hub (), hollow arms () connecting said collar () to said hub (), and an opening piece () which is located on the collar () and is suitable for being connected to an outlet tube () of a transient-operation valve of the turbine engine. In said exhaust casing, said opening piece () is attached onto the collar () and forms an extension of a hollow arm () such that an air flow () leaving the outlet tube () of the transient-operation valve penetrates the hollow arm () and flows into the hub ().


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