Turbomeca Turmo IIIC4

E880719

The Turbomeca Turmo IIIC4 is a French turboshaft engine developed by Turbomeca for medium-lift helicopters.

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Statements (44)

Predicate Object
instanceOf turboshaft engine
airIntakeType turbine engine intake
application helicopter propulsion
belongsToIndustry aerospace
aviation
category aero engine
helicopter engine
combustionChamberType annular combustor
compressionType axial-centrifugal compressor
coolingType air-cooled
countryOfOrigin France
designFocus maintainability
power-to-weight ratio
reliability
designOrigin French aerospace industry
designPurpose provide reliable power for medium-lift helicopters
developedBy Turbomeca engineering team
engineConfiguration free-turbine turboshaft
engineCycle Brayton cycle NERFINISHED
engineMounting helicopter engine bay
engineType turboshaft
exhaustType turbine exhaust outlet
familyGeneration Turmo III series NERFINISHED
fuelType kerosene-based jet fuel
ignitionType continuous combustion
intendedPlatformType rotary-wing aircraft
intendedRole medium-lift utility helicopter engine
manufacturer Turbomeca NERFINISHED
marketedBy Turbomeca NERFINISHED
namingScheme Turmo series designation
operatorType civil helicopter operators
military helicopter operators
partOfFamily Turbomeca Turmo NERFINISHED
powerOutputForm mechanical shaft power
powerTransmission shaft power output
primaryUse air transport support
utility helicopter missions
propulsionType shaft-driven rotor
relatedEngineFamily Turbomeca Turmo IIIC NERFINISHED
targetMarket helicopter manufacturers
technologyType turbine engine
usageEnvironment aeronautical
usedFor rotorcraft lift and propulsion
usedIn medium-lift helicopters

Referenced by (1)

Full triples — surface form annotated when it differs from this entity's canonical label.

Aérospatiale SA 330J Puma engineModel Turbomeca Turmo IIIC4