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 NERFINISHED
category helicopter engines
turboshaft engines of the United States
configuration free-turbine turboshaft
countryOfOrigin United States of America
surface form: United States
designedFor medium-lift helicopters
rotorcraft
turboprop and turboshaft applications
developer General Electric Aviation NERFINISHED
familyBasedOn GE T700 NERFINISHED
fuelType Jet-A
Jet-A1
aviation kerosene
hasAbbreviation GE CT7-2 NERFINISHED
hasFeature annular combustor
axial-centrifugal compressor
modular design
two-stage power turbine
intendedUse medium-lift utility helicopters
transport helicopters
manufacturer General Electric NERFINISHED
partOfSeries CT7 engine family NERFINISHED
General Electric CT7 NERFINISHED
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 CT7-2
this entity surface form: CT7-5
General Electric CT7 familyMember CT7-2
this entity surface form: CT7-6
General Electric CT7 familyMember CT7-2
this entity surface form: CT7-8
General Electric CT7 familyMember CT7-2
this entity surface form: CT7-9