REMOVABLE PACK FOR REACTIVATING A TURBOSHAFT ENGINE, ARCHITECTURE FOR A MULTI-ENGINE SYSTEM FOR PROPELLING A HELICOPTER, PROVIDED WITH SUCH A PACK, AND CORRESPONDING HELICOPTER

REMOVABLE PACK FOR REACTIVATING A TURBOSHAFT ENGINE, ARCHITECTURE FOR A MULTI-ENGINE SYSTEM FOR PROPELLING A HELICOPTER, PROVIDED WITH SUCH A PACK, AND CORRESPONDING HELICOPTER

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 com...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: SEVE, Caroline, DARFEUIL, Pierre, SERGHINE, Camel, MARCONI, Patrick, THIRIET, Romain
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Beschreibung
Zusammenfassung: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.