CT7-2

E1026177

CT7-2 is a specific variant of General Electric’s CT7 turboshaft engine series, designed for use in medium-lift helicopters and similar aircraft.

All labels observed (5)

Label Occurrences
CT7-2 canonical 1
CT7-5 1
CT7-6 1

How this entity was disambiguated

Statements (34)

Predicate Object
instanceOf gas turbine engine ⓘ
turboshaft engine ⓘ
applicationDomain civil aviation ⓘ
military aviation ⓘ
basedOnMilitaryModel T700 turboshaft ⓘ
category helicopter engines ⓘ
turboshaft engines of the United States ⓘ
configuration free-turbine turboshaft ⓘ
countryOfOrigin United States ⓘ
designedFor medium-lift helicopters ⓘ
rotorcraft ⓘ
turboprop and turboshaft applications ⓘ
developer General Electric Aviation ⓘ
linked to: GE Aviation
familyBasedOn GE T700 ⓘ
fuelType Jet-A ⓘ
Jet-A1 ⓘ
aviation kerosene ⓘ
hasAbbreviation GE CT7-2 ⓘ
linked to: GE CT7-2F1
hasFeature annular combustor ⓘ
axial-centrifugal compressor ⓘ
modular design ⓘ
two-stage power turbine ⓘ
intendedUse medium-lift utility helicopters ⓘ
transport helicopters ⓘ
manufacturer General Electric ⓘ
partOfSeries CT7 engine family ⓘ
General Electric CT7 ⓘ
powerClass 1,000–2,000 shp class ⓘ
relatedTo CT7-2A ⓘ
CT7-2E ⓘ
CT7-6 ⓘ
CT7-8 ⓘ
seriesRole early CT7 civil variant ⓘ
usedIn helicopters ⓘ

How these facts were elicited

Referenced by (5)

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

General Electric CT7 → familyMember → CT7-5 ⓘ
linked to: CT7-2
General Electric CT7 → familyMember → CT7-6 ⓘ
linked to: CT7-2
General Electric CT7 → familyMember → CT7-8 ⓘ
linked to: CT7-2
General Electric CT7 → familyMember → CT7-9 ⓘ
linked to: CT7-2