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:
Jul. 18, 2023

Filed:

Apr. 08, 2019
Applicant:

Airbus Operations Sas, Toulouse, FR;

Inventors:

Alain Porte, Colomiers, FR;

François Pons, Daux, FR;

Jonathan Carcone, Toulouse, FR;

Assignee:

AIRBUS OPERATIONS SAS, Toulouse, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 15/22 (2006.01); B64D 15/12 (2006.01); B64D 29/00 (2006.01); H05B 1/02 (2006.01); H05B 3/00 (2006.01); B64D 15/20 (2006.01); F02C 7/047 (2006.01); B64D 33/02 (2006.01);
U.S. Cl.
CPC ...
B64D 15/22 (2013.01); B64D 15/12 (2013.01); B64D 15/20 (2013.01); B64D 29/00 (2013.01); B64D 33/02 (2013.01); F02C 7/047 (2013.01); H05B 1/0236 (2013.01); H05B 3/0019 (2013.01); B64D 2033/0233 (2013.01);
Abstract

An aircraft engine nacelle comprising an icing protection system and an icing protection method for such an aircraft engine nacelle. The aircraft engine nacelle comprises an air inlet comprising a lip, a tubular air inlet piece and an icing protection system. The icing protection system comprises an icing prevention means powered continuously by a first electrical energy source and wholly or partly covering the lip, a de-icing means powered by a second electrical energy source covering the tubular air inlet piece and a controller configured to acquire a current total air temperature value, and control the second electrical energy source as a function of the current total air temperature value.


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