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T64
A T64-GE-7 on a CH-53G
Type Turboshaft
National origin United States
Manufacturer GE Aviation
Major applications AH-56 Cheyenne
Alenia G.222
CH-53 Sea Stallion
CH-53E Super Stallion

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.

Contents

[edit] Versions

Helicopter 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)

Turboprop versions:

  • T64-GE-10 - 2,970 shp (2,214 kW)
  • CT64-820-1 - 2,850 shp (2,125 kW)
  • CT64-820-3/-4 - 3130 shp (2,400 kW)
  • T64/P4D - 3400 shp (2,600 kW)

Sources: Vectorsite,[3] Aviastar.org[4]

[edit] Applications

[edit] Specifications (T64-GE-100)

Data from [5]

General characteristics

  • Type: Turboshaft
  • Length: 79 in (201 cm)
  • Diameter: 20 in (51 cm)
  • Dry weight: 720 lbf (327 kg)

Components

  • Compressor: Axial, 14 stage high pressure compressor
  • Combustors: Annular
  • Turbine: Axial, 2 stage high pressure turbine, 2 stage low pressure turbine

Performance

[edit] References

  1. ^ GE T64 page, GlobalSecurity.org, accessed October 29, 2007.
  2. ^ T64 turboshaft page, GE Aviation, accessed October 29, 2007.
  3. ^ Sikorsky Giant Helicopters: S-64, S-65, & S-80. Vectorsite, 1 March 2008.
  4. ^ Sikorsky S-65 / CH-53 Sea Stallion. Aviastar.org.
  5. ^ Gas Turbine Engines. Aviation Week & Space Technology Source Book 2009. p 118.

[edit] External links




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