Title:
ターボシャフトエンジンのための取外し可能な再始動パック、そのようなパックが備えられた複数エンジンのヘリコプタの推進システムの構造、および、対応するヘリコプタ
Document Type and Number:
Japanese Patent JP6755860
Kind Code:
B2
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 (6) 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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| WO/2008/044973 | A DEVICE FOR AND A METHOD OF STARTING A GAS TURBINE ENGINE |
| JP5834173 | Gas turbine power generator |
| WO/1999/048187 | ELECTRIC MOTOR OR GENERATOR |
Inventors:
Cebu, Caroline
Darfeuille, Pierre
Marconi, Patrick
Sergine, Camel
Romance
Darfeuille, Pierre
Marconi, Patrick
Sergine, Camel
Romance
Application Number:
JP2017520897A
Publication Date:
September 16, 2020
Filing Date:
October 14, 2015
Export Citation:
Assignee:
Saffron Helicopter Engines
International Classes:
F02C7/268; B64C13/28; B64C27/12; B64D27/10; F02C7/36
Domestic Patent References:
| JP2013544329A | ||||
| JP2008190526A | ||||
| JP2012516407A |
Foreign References:
| WO2013160590A1 |
Attorney, Agent or Firm:
Kawaguchi International Patent Office