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:

Nov. 24, 2020
Applicants:

Safran Aircraft Engines, Paris, FR;

Safran Electrical & Power, Blagnac, FR;

Inventors:

Vincent Francois Georges Millier, Moissy-Cramayel, FR;

Loic Paul Yves Guillotel, Moissy-Cramayel, FR;

Philippe Delbosc, Moissy-Cramayel, FR;

Assignees:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H02K 5/22 (2006.01); F01D 9/06 (2006.01); F01D 15/10 (2006.01); H02K 7/18 (2006.01); H02K 15/00 (2006.01);
U.S. Cl.
CPC ...
H02K 5/225 (2013.01); F01D 9/06 (2013.01); F01D 15/10 (2013.01); H02K 7/1823 (2013.01); H02K 15/0006 (2013.01); F05D 2220/323 (2013.01); F05D 2220/76 (2013.01); F05D 2240/10 (2013.01);
Abstract

Disclosed is an electrically conductive rigid bar () for electrically connecting an electric machine () of an aircraft turbine engine, characterised in that it comprises: —an elongate body () made from electrically conductive material having a polygonal cross-section greater than or equal to 50 mm, and— an electrical insulation sheath () that surrounds the body, at least one of the longitudinal ends () of the body not being covered by the sheath and comprising a through-hole () in which a bolt () for fastening and electrically connecting this end is mounted.


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