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:
Dec. 10, 2019

Filed:

Jul. 21, 2015
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Florence Irène Noëlle Leutard, Moissy-Cramayel, FR;

Thibault Jamon, Moissy-Cramayel, FR;

Olivier Renon, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/10 (2006.01); F01D 5/02 (2006.01); F01D 21/00 (2006.01); F01D 25/16 (2006.01); F01D 25/18 (2006.01); F02C 7/28 (2006.01); F01D 9/04 (2006.01);
U.S. Cl.
CPC ...
F01D 11/10 (2013.01); F01D 5/02 (2013.01); F01D 5/026 (2013.01); F01D 9/04 (2013.01); F01D 21/003 (2013.01); F01D 25/16 (2013.01); F01D 25/166 (2013.01); F01D 25/186 (2013.01); F02C 7/28 (2013.01); F05D 2220/30 (2013.01); F05D 2240/54 (2013.01); F05D 2260/83 (2013.01);
Abstract

A turbomachine element includes a stator, a rotor, and a first sealing means for sealing between the rotor and the stator. The element is arranged to be active when the rotor is in the operating position of same around the axis of rotation thereof. The element includes an auxiliary pressure sealing means, sealing between the rotor and the stator and is arranged so that the two sealing means are active when the rotor is placed along the axis of rotation thereof during an assembly operation in a test position. In the test position, the rotor and the stator form an enclosure between said two sealing means.


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