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. 26, 2020

Filed:

Mar. 13, 2017
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Julien Alexis Louis Ricordeau, Paris, FR;

Marc Missout, Montigny le Bretonneux, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 13/02 (2006.01); F04D 27/00 (2006.01); F02C 7/32 (2006.01); B64D 13/06 (2006.01); B64D 27/10 (2006.01); F02C 6/20 (2006.01); F02C 7/36 (2006.01); F04D 25/02 (2006.01); F04D 25/06 (2006.01);
U.S. Cl.
CPC ...
F04D 27/004 (2013.01); B64D 13/02 (2013.01); B64D 13/06 (2013.01); B64D 27/10 (2013.01); F02C 6/206 (2013.01); F02C 7/32 (2013.01); F02C 7/36 (2013.01); F04D 25/028 (2013.01); F04D 25/06 (2013.01); B64D 2013/0644 (2013.01); F05D 2260/40311 (2013.01); Y02T 50/56 (2013.01);
Abstract

An aircraft turboprop engine has at least one low-pressure body and one high-pressure body. The low-pressure body drives a thrust propeller using a gearbox. The turboprop engine further includes a means for supplying air to an air-conditioning circuit of an aircraft cabin. The supply means includes a load compressor and a rotor that is coupled to the low-pressure body by the gearbox. The supply means further includes a means for controlling the rotation speed of the rotor of the compressor, which means comprise an electric motor, and a mechanical differential for coupling a first output shaft of said electric motor to a second output shaft of said gearbox and to said compressor rotor, such that the rotation speed of said rotor depends on the respective rotation speeds of said first and second output shafts.


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