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:
Sep. 03, 2024

Filed:

Dec. 11, 2020
Applicants:

Safran Aircraft Engines, Paris, FR;

Safran Transmission Systems, Colombes, FR;

Inventors:

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

Gilles Alain Marie Charier, Moissy-Cramayel, FR;

Matthieu Bruno François Foglia, Moissy-Cramayel, FR;

Caroline Marie Frantz, Moissy-Cramayel, FR;

Adrien Louis Simon, Moissy-Cramayel, FR;

Assignees:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 3/06 (2006.01); F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
F02K 3/06 (2013.01); F02C 7/36 (2013.01); F05D 2240/52 (2013.01); F05D 2260/40311 (2013.01);
Abstract

An aero-propulsion system includes a drive shaft, a low-pressure compressor, a fan shaft driving a fan, a reduction device that couples the drive shaft and the fan shaft, and an inlet channel which extends between the fan and the low-pressure compressor, the inlet having a predetermined mean radius, a ratio between a mean radius of the inlet channel and the mean radius of the low-pressure compressor, on the one hand, and the reduction ratio of the reduction mechanism, on the other hand, being less than 0.35.


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