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:
Jan. 23, 2024

Filed:

Mar. 18, 2019
Applicant:

Airbus Operations S.a.s., Toulouse, FR;

Inventors:

Camil Negulescu, Toulouse, FR;

Jean-Michel Rogero, Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 33/02 (2006.01); F02K 3/077 (2006.01); B64C 7/02 (2006.01); F02K 3/12 (2006.01); B64D 29/00 (2006.01); F01D 25/24 (2006.01); F02K 3/04 (2006.01); B64D 33/04 (2006.01); B64D 27/10 (2006.01); B64D 27/16 (2006.01);
U.S. Cl.
CPC ...
B64D 33/02 (2013.01); B64C 7/02 (2013.01); B64D 27/10 (2013.01); B64D 27/16 (2013.01); B64D 29/00 (2013.01); B64D 33/04 (2013.01); F01D 25/24 (2013.01); F02K 3/04 (2013.01); F02K 3/077 (2013.01); F02K 3/12 (2013.01); B64D 2033/0266 (2013.01); F05D 2220/323 (2013.01);
Abstract

An aircraft propulsion assembly includes a first engine and a second engine that are adjacent and a nacelle in which the engines are installed. The nacelle includes a common air inlet lip for the first engine and the second engine, the air flow being divided between the first engine and the second engine by a median lip which extends, at least partly, set back from said common air inlet lip. The common are inlet lip includes, directly in line with the median lip, a bottom lobe and a top lobe extending forward of the nacelle. Such a configuration makes it possible to be able to provide a high aerodynamic form between the fairings of the engines, without the risk of generating overspeeds in the air flow.


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