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The General Electric T64 is a free-turbine turboshaft engine that was developed for use on helicopters. GE introduced the engine in 1964. The original engine design included technical innovations such as corrosion resistant and high-temperature coatings.[1] The engine features a high pressure ratio, yielding low specific fuel consumption. Later versions of the engine produce from 3,925 to 4,750 shp (2,927 to 3,542 kW).[2] The engine is also used in several turboprop fixed-wing applications.
[edit] VersionsHelicopter versions:
Turboprop versions:
Sources: Vectorsite,[3] Aviastar.org[4] [edit] Applications
[edit] Specifications (T64-GE-100)Data from [5] General characteristics
Components
Performance
[edit] References
[edit] External links
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