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:
May. 21, 2024

Filed:

Oct. 25, 2019
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Nicolas Jérôme Jean Tantot, Moissy-Cramayel, FR;

Anthony Binder, Moissy-Cramayel, FR;

Mario Antoine Lambey, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/10 (2006.01); B64C 11/30 (2006.01); B64C 11/48 (2006.01); B64D 27/24 (2006.01); F02B 61/04 (2006.01); F02C 3/067 (2006.01); F02C 7/36 (2006.01); B64D 27/00 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64D 27/10 (2013.01); B64C 11/306 (2013.01); B64C 11/48 (2013.01); B64D 27/24 (2013.01); F02B 61/04 (2013.01); F02C 3/067 (2013.01); F02C 7/36 (2013.01); B64D 2027/005 (2013.01); B64D 2027/026 (2013.01); F05D 2220/324 (2013.01); F05D 2220/325 (2013.01); F05D 2220/76 (2013.01);
Abstract

A turbomachine of an aircraft comprising an outer casing delimiting with an inner hub, a flow path of a gas stream in which is disposed a low-pressure turbine configured to rotationally drive a low-pressure shaft; said turbomachine comprising, in the direction of flow of the gas stream, a first propeller; and a second propeller downstream of the first propeller, the first propeller being rotationally driven by said low-pressure shaft and the second propeller being rotationally driven by an electric motor, the second propeller being further disposed at a distance between 1.5 and 4 cord lengths from the first propeller defined between the respective axes of shimming of each of the first and second propellers.


Find Patent Forward Citations

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Tantot, Nicolas Jérôme Jean. (2024). Turbomachine with unducted dual propellers (U.S. Patent No. 11987369). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/11987369

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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