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. 29, 2021

Filed:

Jul. 23, 2018
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Jacky Novi Mardjono, Moissy-Cramayel, FR;

Norman Bruno André Jodet, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/045 (2006.01); F01D 1/02 (2006.01); F01D 9/06 (2006.01); F04D 29/54 (2006.01); F04D 19/02 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/045 (2013.01); F01D 1/02 (2013.01); F01D 9/06 (2013.01); F04D 19/02 (2013.01); F04D 29/547 (2013.01); F02K 3/06 (2013.01); F05D 2250/323 (2013.01); F05D 2250/324 (2013.01); F05D 2250/51 (2013.01); F05D 2260/60 (2013.01);
Abstract

A supply duct of a compressor of a turbine engine, formed from internal and external walls of revolution around an axis and opposite one another to define a circulation stream of a fluid, is provided. The stream allows the fluid to be routed from the inlet of the duct to the inlet of the compressor. The radius of the external wall at the inlet of the duct is greater than the radius of the duct at the inlet of the compressor. The duct includes a portion for which the radius of the external wall along the portion is less than the radius of the external wall at the inlet of the compressor, and the radius of the internal wall along the portion of the duct is less than the radius of the internal wall at the inlet of the compressor.


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