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. 13, 2015

Filed:

May. 03, 2010
Applicants:

Guillaume Bulin, Blagnac, FR;

Jean-michel Rogero, Toulose, FR;

Christian Fabre, Tournefeuille, FR;

Inventors:

Guillaume Bulin, Blagnac, FR;

Jean-Michel Rogero, Toulose, FR;

Christian Fabre, Tournefeuille, FR;

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); B64C 11/48 (2006.01); B64D 15/04 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64C 11/48 (2013.01); B64D 15/04 (2013.01); B64D 2027/026 (2013.01); Y02T 50/66 (2013.01);
Abstract

A deicing device for propfan-type aircraft propulsion unit blades, wherein the propulsion unit includes a turbomachine that drives in rotation at least one rotor including a plurality of blades arranged around an annular crown moving with the blades, which forms with its outer wall part of an outer envelope of the propulsion unit, the outer envelope being subjected to atmospheric conditions outside the propulsion unit, the turbomachine generating a flow of hot gases that exit via an annular vein, which is concentric with the moving annular crown, and defined for part of its surface by the inner wall of the moving annular crown. The deicing device includes: a mechanism capturing thermal energy from the annular vein, within the moving annular part; a mechanism transferring thermal energy towards the rotor blades; and a mechanism distributing the thermal energy onto at least a part of the surface of the blades.


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