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:
Nov. 01, 2022

Filed:

May. 28, 2020
Applicants:

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

Airbus (S.a.s.), Blagnac, FR;

Inventors:

Jérôme Colmagro, Toulouse, FR;

Aurélien Mauconduit, Toulouse, FR;

Assignees:

Airbus Operations (S.A.S.), Toulouse, FR;

Airbus (S.A.S.), Blagnac, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 33/08 (2006.01); B64C 1/06 (2006.01); B64C 1/16 (2006.01); B64D 27/02 (2006.01); H02K 9/19 (2006.01);
U.S. Cl.
CPC ...
B64D 33/08 (2013.01); B64C 1/068 (2013.01); B64C 1/16 (2013.01); B64D 27/02 (2013.01); H02K 9/19 (2013.01); B64D 2027/026 (2013.01);
Abstract

An aircraft propulsion plant including an electric motor having a rotor and a stator mechanically linked to a base which can be mounted at the rear of an aircraft fuselage, a fan rotated by the rotor, a set of fixed blades located downstream of the fan, and a nacelle comprising an outer casing and a fan casing surrounding the fan and the set of fixed blades. The nacelle is mechanically linked to the base through the set of fixed blades. This configuration enables a cooling circuit to be formed for enabling the heat produced by the electric motor at the location of the stator to be evacuated towards the fixed blades and the nacelle where it is dissipated. Furthermore, this heat may be used for the de-icing of the nacelle lip.


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