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.
Observed surface forms (4)
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 ⓘ |
Referenced by (5)
Full triples — surface form annotated when it differs from this entity's canonical label.
this entity surface form:
CT7-5
this entity surface form:
CT7-6
this entity surface form:
CT7-8
this entity surface form:
CT7-9