General Electric T64

From Wikipedia, the free encyclopedia

The General Electric T64 was a turboshaft engine developed for use on helicopters. GE introduced the engine in 1964. The engine featured technical innovations such as corrosion resistant and high-temperature coatings.^[1] The engine design featured 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.

Contents 1 Applications 2 Versions 3 References 4 External links

[edit] Applications

• XC-142A
• AH-56 Cheyenne
• CH-53 Sea Stallion
• MH-53 Pave Low
• H-53E Super Stallion
• Alenia G.222
• Lockheed/Kawasaki P-2J
• ShinMaywa US-1
• de Havilland Canada DHC-5 Buffalo

[edit] Versions

• T64-GE-1 - 3,080 shp (2,300 kW)
• T64-GE-6 - 2,850 shp (2,125 kW)
• T64-GE-7 - 3,925 shp (2,930 kW)
• T64-GE-16 - 3,485 shp (2,600 kW)
• T64-GE-412 - 3,695 shp (2,755 kW)
• T64-GE-413 - 3,925 shp (2,930 kW)
• T64-GE-415 - 4,380 shp (3,265 kW)
• T64-GE-416 - 4,380 shp (3,266 kW)
• T64-GE-423 - 3,925 shp (2,927 kW)

Source: Vectorsite,[1] Avia.Russian.ee[2]

[edit] References

[edit] External links

• GE Aviation T64 page
• GE Aviation Receives AHS Supplier Excellence Award (for T64 team)

v • d • e Lists relating to aviation General Timeline of aviation · Aircraft (manufacturers) · Aircraft engines (manufacturers) · Airports · Airlines Military Air forces · Aircraft weapons · Missiles · Unmanned aerial vehicles (UAVs) · Experimental aircraft Accidents/incidents General · Military · Commercial (airliners) · Deaths Records Airspeed · Distance · Altitude · Endurance · Most-produced aircraft