Misplaced Pages

Pratt & Whitney T73

Article snapshot taken from Wikipedia with creative commons attribution-sharealike license. Give it a read and then ask your questions in the chat. We can research this topic together.
(Redirected from Pratt & Whitney JFTD12-4A) Turboshaft engine
T73/JFTD12
JFTD12-4A mounted on an Erickson S-64E Aircrane
Type Turboshaft
National origin United States
Manufacturer Pratt & Whitney
Major applications Sikorsky CH-54 Tarhe
Sikorsky S-64 Skycrane
Number built 352
Developed from Pratt & Whitney JT12

The Pratt & Whitney T73 (company designation JFTD12) is a turboshaft engine. Based on the JT12A, the T73 powered the Sikorsky CH-54 Tarhe and its civil counterpart Sikorsky S-64 Skycrane flying crane heavy-lift helicopters. Turboshaft versions for naval use are known as the FT12.

Variants

T73-P-1
Basic military model, rated at 4,500 horsepower (3,355 kW) takeoff power and 4,000 horsepower (2,982 kW) maximum continuous power
T73-P-700
Higher-power military model with improved internal components; rated at 4,800 horsepower (3,579 kW) takeoff power and 4,430 horsepower (3,303 kW) maximum continuous power
JFTD12A-3
JFTD12A-4A
Civilian equivalent of T73-P-1
JFTD12A-5A
Civilian equivalent of T73-P-700
FT12
Marine powerplant

Applications

Specifications (T73-P-1)

T73s on a Sikorsky CH-54 Tarhe

Data from FAA Type Certificate E15EA

General characteristics

  • Type: Turboshaft
  • Length: 107.0 in (2,718 mm)
  • Diameter: 30.0 in (762 mm) maximum
  • Dry weight: 966 lbs (438 kg)

Components

  • Compressor: nine stage axial compressor
  • Combustors: eight cans in annular configuration
  • Turbine: axial two stage gas generator turbine and axial two stage free turbine
  • Fuel type: aviation kerosene conforming to MIL-I-5161 E Grade I or II

Performance

  • Maximum power output: 4,500 horsepower (3,355 kW) takeoff, 4,000 horsepower (2,982 kW) maximum continuous; at sea level at or below -8°C (17°F)
  • Turbine inlet temperature: 688°C (1270°F)
  • Power-to-weight ratio: 4.66 hp/lb (7.66 kW/kg)

See also

Related development

Comparable engines

Related lists

References

  1. Connors, p.285
  2. Greg Goebel's Vectorsite
  3. Pratt & Whitney JT12 (United States), Aero-engines - Turbojet, Jane's Information Group, 2011.05.09
  4. ^ Type Certificate Data Sheet E15EA, US DoT - FAA, 2011.09.12

External links

Pratt & Whitney aircraft engines
Radial engines
H piston engines
Free-piston gas turbines
Turbojets
Turbofans
Turboprops/Turboshafts
Propfans
Rocket engines
Aeroderivative gas
turbine engines
Subsidiaries
Key people
Joint development aeroengines
See also: Pratt & Whitney Canada aeroengines
United States military gas turbine aircraft engine designation system
Turbojets
Turboprops/
Turboshafts
Turbofans
Adaptive cycle engines
This aircraft engine article is missing some (or all) of its specifications. If you have a source, you can help Misplaced Pages by adding them.
Categories: