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:
Dec. 08, 2020

Filed:

Oct. 14, 2015
Applicant:

Safran Helicopter Engines, Bordes, FR;

Inventors:

Patrick Marconi, Gelos, FR;

Romain Thiriet, Jurancon, FR;

Camel Serghine, Boeil-bezing, FR;

Caroline Seve, Pau, FR;

Pierre Darfeuil, Idron, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/277 (2006.01); F02C 7/32 (2006.01); F02C 7/275 (2006.01); F02C 7/268 (2006.01); B64C 27/14 (2006.01); B64D 27/10 (2006.01); F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
F02C 7/277 (2013.01); B64C 27/14 (2013.01); B64D 27/10 (2013.01); F02C 7/268 (2013.01); F02C 7/275 (2013.01); F02C 7/32 (2013.01); F02C 7/36 (2013.01); F05D 2220/329 (2013.01); F05D 2220/50 (2013.01); Y02T 50/60 (2013.01);
Abstract

The invention relates to a removable reactivation pack for a turboshaft engine of a helicopter, comprising a gas generator equipped with a drive shaft, said turboshaft engine () being capable of operating in at least one standby mode during a stable flight of the helicopter, said removable pack comprising: a removable gearbox comprising a gearbox output shaft; controlled means for rotating said gearbox output shaft, referred to as reactivation means of said turboshaft engine; mechanical means for reversibly coupling said gearbox output shaft to said drive shaft of said gas generator.


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