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. 04, 2024

Filed:

Oct. 22, 2021
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Maeva Daphne Gros-Borot, Moissy-Cramayel, FR;

Clementine Charlotte Marie Mouton, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/06 (2006.01); F01D 25/16 (2006.01); F02C 7/06 (2006.01); F01D 5/02 (2006.01);
U.S. Cl.
CPC ...
F01D 25/16 (2013.01); F02C 7/06 (2013.01); F01D 5/026 (2013.01); F01D 5/06 (2013.01); F05D 2220/323 (2013.01); F05D 2240/50 (2013.01);
Abstract

A device for pressurizing a turbomachine downstream enclosure, the device being fed by means of a pressurizing air flow and including: a first shaft portion, a second shaft portion coupled to the first shaft portion via internal splines and external splines and extending, at a distance, inside the first shaft portion. The device includes at least a first passage made through the splines, and at least one orifice passing right through the second shaft portion, the orifice being arranged upstream of the first passage, in fluidic communication with the first passage, and opening out inside the second shaft portion so as to allow the pressurizing air flow to circulate from the first passage, between the first and second shaft portions, towards the downstream enclosure.


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