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. 08, 2020

Filed:

Mar. 20, 2015
Applicants:

Safran Helicopter Engines, Bordes, FR;

Safran Power Units, Toulouse, FR;

Inventors:

Fabien Mercier-Calvairac, Pau, FR;

Stéphane Beddok, Pau, FR;

Stéphane Chevalier, Colomiers, FR;

Sophie Humbert, Pau, FR;

Assignees:

SAFRAN HELICOPTER ENGINES, Bordes, FR;

SAFRAN POWER UNITS, Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/262 (2006.01); B64D 35/08 (2006.01); B64C 27/14 (2006.01); F02C 9/42 (2006.01); F02C 7/275 (2006.01); B64D 27/26 (2006.01); F02C 3/04 (2006.01); F02C 7/268 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64D 35/08 (2013.01); B64C 27/14 (2013.01); B64D 27/26 (2013.01); F02C 3/04 (2013.01); F02C 7/262 (2013.01); F02C 7/268 (2013.01); F02C 7/275 (2013.01); F02C 9/42 (2013.01); B64D 2027/026 (2013.01); F05D 2220/323 (2013.01); F05D 2220/329 (2013.01); F05D 2220/50 (2013.01); F05D 2220/76 (2013.01); F05D 2240/35 (2013.01); F05D 2260/85 (2013.01); Y02T 50/671 (2013.01);
Abstract

An architecture of a propulsion system of a multi-engine helicopter is disclosed, comprising turboshaft engines that are connected to a power transmission gearbox. It comprises: a hybrid turboshaft engine that is capable of operating in at least one standby mode during a stable flight of the helicopter; a pack for quickly restarting said hybrid turboshaft engine in order to bring said engine out of said standby mode and to reach a nominal operating mode; an auxiliary power unit that is connected to said electrotechnical restart pack by means of a first AC/DC converter and is capable of providing said restart pack, on demand, with power required for bringing said hybrid turboshaft engine out of said standby mode.


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