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. 29, 2025

Filed:

Jun. 15, 2021
Applicant:

Safran Helicopter Engines, Bordes, FR;

Inventors:

Bernard Claude Pons, Moissy-Cramayel, FR;

Alphonse Puerto, Moissy-Cramayel, FR;

Laurent Pierre Tarnowski, Moissy-Cramayel, FR;

Lois Pierre Denis Vive, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/08 (2005.12); F02C 3/08 (2005.12); F02C 3/10 (2005.12); B64C 27/12 (2005.12); F04D 29/42 (2005.12);
U.S. Cl.
CPC ...
F02C 3/103 (2012.12); F02C 3/08 (2012.12); F02C 7/08 (2012.12); B64C 27/12 (2012.12); F04D 29/4233 (2012.12); F05D 2220/329 (2012.12);
Abstract

Aircraft turbomachine including a centrifugal compressor, a combustion chamber, the combustion chamber being supplied by the compressor via a diffuser and via a straightener, and a heat exchanger, the exchanger including a first circuit, supplied with exhaust gas from the turbomachine, and a second circuit, which are connected by volutes on the one hand to an outlet of the diffuser and on the other hand to an inlet of the straightener, the volutes having reversed winding directions such that their connection ports to the exchanger are independent of one another and are substantially diametrically opposed, and such that the minimum cross section of each duct is situated at a larger cross section of the other duct.


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