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. 26, 2023

Filed:

Mar. 15, 2021
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Paco Maurer, Moissy-cramayel, FR;

Fabien Roger Gaston Caty, Moissy-cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/12 (2006.01); F01D 5/08 (2006.01); F01D 17/14 (2006.01); F01D 9/06 (2006.01); F02C 9/18 (2006.01); F02C 6/08 (2006.01); F02C 3/13 (2006.01);
U.S. Cl.
CPC ...
F01D 25/12 (2013.01); F01D 5/081 (2013.01); F01D 9/065 (2013.01); F01D 17/141 (2013.01); F01D 17/145 (2013.01); F02C 6/08 (2013.01); F02C 9/18 (2013.01); F02C 3/13 (2013.01); F05D 2260/20 (2013.01); F05D 2270/3015 (2013.01); F05D 2300/50212 (2013.01);
Abstract

A turbo machine including a device for ventilating and pressurising a turbine rotor of a turbomachine having an axis, the device including at least one collection pipe suitable for collecting a fraction of the air circulating in a high-pressure compressor of the turbomachine and conveying it to a first inner chamber inside the turbomachine that communicates with a second inner chamber delimited by the turbine rotor, the first and second chambers being at least partially separated by a stationary shroud having the axis, wherein it includes at least one injector passing through the stationary shroud and having a cross-section that varies in response to a pressure difference between the first and second chambers.


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