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:
Dec. 31, 2019

Filed:

Nov. 08, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/18 (2006.01); B64D 33/02 (2006.01); F02C 7/05 (2006.01); B64D 27/12 (2006.01); F02K 3/077 (2006.01); F02K 1/52 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
B64D 27/18 (2013.01); B64D 27/12 (2013.01); B64D 33/02 (2013.01); F02C 7/05 (2013.01); F02K 1/52 (2013.01); F02K 3/06 (2013.01); F02K 3/077 (2013.01); B64D 2033/0286 (2013.01); F05D 2240/40 (2013.01); F05D 2250/312 (2013.01);
Abstract

The invention relates to an aircraft propulsion assembly (), comprising a single gas generator () and two fans () drive in rotation by the gas generator () and offset on either side of a vertical plane passing through a longitudinal axis (X) of the gas generator, the rotational axes of the fans lying substantially in the same fan plane. According to the invention, the propulsion assembly () comprises an air inlet fairing formed upstream of a nacelle () connecting the fans, said fairing () having, between the fans (), an air inlet opening (') lying substantially perpendicular to the fan plane and on either side of this plane, the propulsion assembly further comprising an air supply device configured so as to supply the gas generator () with a part of the incoming air and to take off, from the remaining part of the incoming air, a cooling airflow intended to cool elements of the propulsion assembly and/or a wing supporting the propulsion assembly.


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