Turbomeca Turmo IIIC4
E880719
The Turbomeca Turmo IIIC4 is a French turboshaft engine developed by Turbomeca for medium-lift helicopters.
All labels observed (1)
| Label | Occurrences |
|---|---|
| Turbomeca Turmo IIIC4 canonical | 1 |
How this entity was disambiguated
This entity first appeared as the object of triple T10695568 — resolving that mention is where its identity was fixed. The disambiguator weighed these candidate entities and picked the highlighted one (or “None”, minting a new entity). This is how homonymy is resolved: the same surface form can point to different entities.
NED1
Entity disambiguation (via context triple)
gpt-5-mini-2025-08-07
Target entity: Turbomeca Turmo IIIC4 Context triple: [Aérospatiale SA 330J Puma, engineModel, Turbomeca Turmo IIIC4]
-
A.
Turbomeca Artouste IIIB
The Turbomeca Artouste IIIB is a French turboshaft engine widely used in light helicopters, notably powering early variants of the Aérospatiale Alouette III.
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B.
Turbomeca Arrius 2B1
The Turbomeca Arrius 2B1 is a turboshaft helicopter engine variant in the Arrius family, designed to provide reliable, efficient power for light twin-engine rotorcraft.
-
C.
Turbomeca Arrius 2B2
The Turbomeca Arrius 2B2 is a turboshaft aircraft engine developed by Safran Helicopter Engines for light twin-engine helicopters, offering reliable performance and efficiency.
-
D.
Turbomeca Makila 2A1
The Turbomeca Makila 2A1 is a powerful turboshaft engine developed by Safran Helicopter Engines for medium- to heavy-lift helicopters, offering high performance and reliability in demanding military and civil operations.
-
E.
Turbomeca Astazou
The Turbomeca Astazou is a French-designed turboshaft and turboprop engine widely used in light helicopters and aircraft from the 1960s onward.
- F. None of above. chosen
- G. Unsure - the case is ambiguous/there is not enough information to decide.
NED2
Entity disambiguation (via description)
gpt-5-mini-2025-08-07
Target entity: Turbomeca Turmo IIIC4 Target entity description: The Turbomeca Turmo IIIC4 is a French turboshaft engine developed by Turbomeca for medium-lift helicopters.
-
A.
Turbomeca Artouste IIIB
The Turbomeca Artouste IIIB is a French turboshaft engine widely used in light helicopters, notably powering early variants of the Aérospatiale Alouette III.
-
B.
Turbomeca Arrius 2B1
The Turbomeca Arrius 2B1 is a turboshaft helicopter engine variant in the Arrius family, designed to provide reliable, efficient power for light twin-engine rotorcraft.
-
C.
Turbomeca Arrius 2B2
The Turbomeca Arrius 2B2 is a turboshaft aircraft engine developed by Safran Helicopter Engines for light twin-engine helicopters, offering reliable performance and efficiency.
-
D.
Turbomeca Makila 2A1
The Turbomeca Makila 2A1 is a powerful turboshaft engine developed by Safran Helicopter Engines for medium- to heavy-lift helicopters, offering high performance and reliability in demanding military and civil operations.
-
E.
Turbomeca Astazou
The Turbomeca Astazou is a French-designed turboshaft and turboprop engine widely used in light helicopters and aircraft from the 1960s onward.
- F. None of above. chosen
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 ⓘ |
How these facts were elicited
The pipeline generated the facts above by prompting gpt-5.1 with this entity's name + description and the instruction below.
Instruction
You are a knowledge base construction expert. Given a subject entity and a description of it, return factual statements that you know for the subject as a JSON list of dictionaries(triples), where keys must be "subject", "predicate" and "object". The number of facts may be very high, between 25 to 50 or more, for very popular subjects. For less popular subjects, the number of facts can be very low, like 5 or 10. # Requirements - If you don't know the subject at all, return an empty list. - If the subject is not a named entity, return an empty list. - Include at least one triple where predicate is "instanceOf". - Do not get too wordy. - Separate several objects into multiple triples with one object.
Input
Subject: Turbomeca Turmo IIIC4 Description of subject: The Turbomeca Turmo IIIC4 is a French turboshaft engine developed by Turbomeca for medium-lift helicopters.
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.