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:
Sep. 11, 2018

Filed:

May. 07, 2015
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Bellal Waissi, Moissy-Cramayel, FR;

Sébastien Chalaud, Moissy-Cramayel, FR;

Alain Pierre Garassino, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/00 (2006.01); F02C 7/275 (2006.01); F01D 19/00 (2006.01); F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
F02C 7/275 (2013.01); F01D 19/00 (2013.01); F02C 7/36 (2013.01); F05D 2220/32 (2013.01); F05D 2260/85 (2013.01);
Abstract

A multi-body gas turbine engine, especially an aircraft engine, comprising at least one low-pressure rotating body, a high-pressure rotating body, and a starter designed to rotate the high-pressure body in order to start the engine, wherein the starter is coupled to the low-pressure body and the engine comprises a first disengageable coupling device disposed between the low-pressure body and the high-pressure body, for rotatably connecting the high-pressure body to the low-pressure body so as to allow the starting of the engine by means of the starter.


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