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. 18, 2014

Filed:

May. 03, 2010
Applicants:

Guillaume Bulin, Blagnac, FR;

Severine Perret, Leguevin, FR;

Jean-michel Rogero, Toulouse, FR;

Inventors:

Guillaume Bulin, Blagnac, FR;

Severine Perret, Leguevin, FR;

Jean-Michel Rogero, Toulouse, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 11/44 (2006.01); F02C 7/32 (2006.01); H01L 35/32 (2006.01); B64C 11/48 (2006.01); F01D 15/10 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64C 11/48 (2013.01); F01D 15/10 (2013.01); F02C 7/32 (2013.01); B64D 2027/026 (2013.01); Y02T 50/66 (2013.01);
Abstract

An electrical energy generating device for a propfan-type aircraft propulsion unit rotor. 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 generates a flow of hot gases that exit via an annular hot vein, which is concentric with the moving annular crown, and defined for part of its surface by an inner wall of the moving annular crown, and includes, within the moving annular part, a mechanism to transform thermal energy into electrical energy, preferably by thermal diodes. Such a device, as an example, can find application to a device for controlling a pitch of rotors of a propfan-type propulsion unit.


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