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. 21, 2012
Applicants:

Vincent Bourget, Jonquerettes, FR;

Serge Giordano, Marseilles, FR;

Nicolas Imbert, Marseilles, FR;

Charles Chuc, Marseilles, FR;

Inventors:

Vincent Bourget, Jonquerettes, FR;

Serge Giordano, Marseilles, FR;

Nicolas Imbert, Marseilles, FR;

Charles Chuc, Marseilles, FR;

Assignee:

Airbus Helicopters, Marignane Cedex, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H02K 7/14 (2006.01); B64D 15/12 (2006.01); B64C 27/18 (2006.01); H02K 7/18 (2006.01); H02K 19/16 (2006.01); H02K 41/03 (2006.01); H02K 35/02 (2006.01); H02K 1/27 (2006.01);
U.S. Cl.
CPC ...
B64D 15/12 (2013.01); H02K 7/14 (2013.01); B64C 27/18 (2013.01); H02K 7/1861 (2013.01); H02K 19/16 (2013.01); H02K 41/031 (2013.01); H02K 35/02 (2013.01); H02K 1/27 (2013.01);
Abstract

An electrical power supply device () for electrically powering equipment on a rotary rotor () of an aircraft (), which rotor is driven by a shaft (), said device () comprising a removable stick (). The stick () includes an upper alternator () and an upper tube () secured to said shaft () so as to be constrained in rotation therewith, said upper alternator () having a plurality of upper coils () fastened to an upper inside peripheral surface (') of said upper tube (), said stick () having a rod () carrying an upper permanent magnet (), said device () having a mechanism () so that said rod () and said upper tube () move with distinct rotary movements, said mechanism () having connection means () so as to be connectable to a reference member () of an aircraft ().


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