TURBOSHAFT ENGINE COMPRISING CONTROLLED MECHANICAL COUPLING DEVICE, HELICOPTER EQUIPPED WITH SUCH TURBOSHAFT ENGINE, AND METHOD FOR OPTIMISING ZERO-POWER SUPER-IDLE SPEED OF SUCH HELICOPTER Russian patent published in 2018 - IPC F02C3/113 F02C3/10 

Abstract RU 2674861 C2

FIELD: internal combustion engines.

SUBSTANCE: invention relates to a turboshaft engine designed to equip a multi-engine, in particular a twin-engine, helicopter. Invention also relates to a twin-engine helicopter comprising at least one turboshaft engine, and to a method for optimising the zero-power super-idle speed of such a helicopter. Turboshaft engine comprises gas generator (5), designed to be rotated and free turbine (6) rotated by the gases from gas generator (5). Turboshaft engine also comprises device (40) for controlled mechanical coupling of gas generator (5) and said free turbine (6), said device being designed to connect gas generator (5) and said free turbine (6) mechanically, on command, once the rotation speed of gas generator (5) reaches a pre-determined threshold speed.

EFFECT: invention allows to reduce the temperature of the hot parts of the turboshaft engine, and to reduce fuel consumption.

13 cl, 3 dwg

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RU 2 674 861 C2

Authors

Marconi Patrick

Thiriet Romain

Serghine Camel

Dates

2018-12-13Published

2015-03-20Filed