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:

Feb. 25, 2020
Applicant:

Safran Nacelles, Gonfreville l'Orcher, FR;

Inventor:

Thierry Jacques Albert Le Docte, Moissy-Cramayel, FR;

Assignee:

SAFRAN NACELLES, Gonfreville l'Orcher, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/047 (2006.01); B64C 7/02 (2006.01); B64D 15/04 (2006.01);
U.S. Cl.
CPC ...
F02C 7/047 (2013.01); B64C 7/02 (2013.01); B64D 15/04 (2013.01); F05D 2220/323 (2013.01); F05D 2250/25 (2013.01); F05D 2250/323 (2013.01); F05D 2250/73 (2013.01); F05D 2260/2212 (2013.01);
Abstract

The invention relates to a de-icing device for an air intake of an aircraft turbojet engine nacelle extending along an X-axis in which an air stream flows from upstream to downstream, the air intake having an inner cavity, extending annularly about the X-axis, which comprises an inner wall facing the X-axis and an outer wall which is opposite the inner wall, the walls being connected by a leading edge, the de-icing device comprising at least one injector for injecting a stream of hot air into the inner cavity, the injector comprising a nozzle extending along a nozzle axis, the nozzle being configured to inject a stream of hot air having a dissymmetry along the nozzle axis.


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