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Turbomeca Artouste

From Alfawiki
Turbomeca
IndustryAerospace
Founded1938
Headquarters
France
ProductsAircraft engines, including the Artouste turboshaft engine
Template:Infobox aircraft engine

The Turbomeca Artouste represents one of the pioneering French turboshaft engines, with its inaugural operation dating back to 1947. Originally created to serve as an auxiliary power unit (APU), it was soon modified for primary aircraft propulsion roles, becoming a fundamental engine for turboshaft helicopters throughout the 1950s. Production under license was undertaken in the United Kingdom by Bristol Siddeley, in India by Hindustan Aeronautics Limited, and in the United States by Continental CAE under the designation Continental T51.

The engine was manufactured in two principal variants: the Artouste II series, which mainly powered the Aérospatiale Alouette II, featured a single-stage centrifugal compressor paired with a two-stage turbine, delivering power limited by gearbox constraints to approximately . The Artouste III series, predominantly installed in the Aérospatiale Alouette III and Aérospatiale Lama, incorporated a dual-stage axial-centrifugal compressor alongside a three-stage turbine, providing output up to , also limited by gearbox restrictions.

Variants

Artouste I
Artouste II
Artouste IIB, IIB1
takeoff power , continuous power
Artouste IIC series (IIC, IIC1, IIC2, IIC5, IIC6)
takeoff power , continuous power (gearbox-restricted); without gearbox limitation: takeoff power , continuous power
Artouste IIIB
takeoff power , continuous power (gearbox-restricted); without gearbox limitation: takeoff power , continuous power
Artouste IIIB1, IIID
takeoff power , continuous power (gearbox-limited); unrestricted ratings equal to IIIB
Continental T51
American licensed manufacture and further development of the Artouste
Turbomeca Marcadau
Turboprop variant derived from Artouste II, producing through a 2.3:1 reduction gearbox.

Applications

Artouste
Marcadau

Engines on display

Examples of the Turbomeca Artouste are on public exhibit at:

References

Notes
Bibliography