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. 26, 2016

Filed:

Mar. 28, 2011
Applicants:

Michel Gilbert Roland Brault, Quincy sous Senart, FR;

Philippe Pierre Vincent Bouiller, Samoreau, FR;

Inventors:

Michel Gilbert Roland Brault, Quincy sous Senart, FR;

Philippe Pierre Vincent Bouiller, Samoreau, FR;

Assignee:

SNECMA, Paris, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/18 (2006.01); F16L 37/14 (2006.01); F16L 21/08 (2006.01);
U.S. Cl.
CPC ...
F01D 25/18 (2013.01); F16L 21/08 (2013.01); F16L 37/14 (2013.01); F05D 2230/64 (2013.01); F05D 2230/642 (2013.01); F05D 2240/61 (2013.01); F05D 2260/30 (2013.01); F05D 2260/602 (2013.01); F05D 2260/6022 (2013.01); Y10T 29/49826 (2015.01);
Abstract

A venting pipe used to guide a gas stream in a turbojet including at least one hollow rotary shaft inside which the pipe is mounted, the pipe extending generally along an axis. The pipe includes at least two pipe segments configured to be aligned longitudinally and assembled to one another while retaining a degree of freedom in relative translation thereof, at least one of the segments including a deformable mechanism configured to deform radially as the pipe segments are tightened against one another in the shaft of the turbojet, to bear on the shaft. The pipe structure facilitates mounting of the pipe.


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