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:
Oct. 03, 2023

Filed:

Jul. 06, 2020
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Philippe Gérard Chanez, Moissy-Cramayel, FR;

Jean-Michel Daniel Paul Boiteux, Moissy-Cramayel, FR;

Nicolas Jérôme Jean Tantot, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 21/06 (2023.01); B64D 27/20 (2006.01); B64D 29/04 (2006.01); B64C 1/16 (2006.01); B64D 33/02 (2006.01);
U.S. Cl.
CPC ...
B64C 21/06 (2013.01); B64C 1/16 (2013.01); B64D 27/20 (2013.01); B64D 29/04 (2013.01); B64D 2033/0206 (2013.01); B64D 2033/0286 (2013.01);
Abstract

Propulsion assembly for an aircraft, comprising a fuselage extending along a longitudinal axis and enclosing an inner enclosure, at least one ducted engine fixed to the fuselage and comprising an air inlet section, the air inlet section being disposed at least partly in the inner enclosure, at least one plenum chamber disposed in the inner enclosure upstream of the air inlet section and in fluid communication with said air inlet section, at least one air intake formed on an outer wall of the fuselage, the inlet of the air intake being partly delimited by said outer wall of the fuselage, the air intake being configured to ingest external air and deflect it towards the plenum chamber.


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