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Williams F107

From Wikipedia, the free encyclopedia
Turbofan engine for cruise missiles
F107 / WR19
An F107 engine on display at theSan Diego Air & Space Museum
TypeTurbofan
National originUnited States
ManufacturerWilliams International
First run1970s
Major applications
Developed intoWilliams F112

TheWilliams F107 (company designationWR19) is a smallturbofan engine made byWilliams International. The F107 was designed to propelcruise missiles. It has been used as the powerplant for theAGM-86 ALCM, andBGM-109 Tomahawk, as well as the experimentalKaman KSA-100 SAVER andWilliams X-Jet flying platform.

Applications

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Specifications (WR19)

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Data from Aircraft engines of the World 1970[1]

General characteristics

  • Type:
  • Length: 24 in (610 mm)
  • Diameter: 12 in (300 mm)
  • Dry weight: 67 lb (30 kg)

Components

  • Compressor: 2-stage fan, 2-stage axial IP compressor, 1-stage centrifugal HP compressor
  • Combustors: Annular combustion chamber
  • Turbine: 1-stage HP turbine, 2-stage LP turbine
  • Fuel type:JP-4 /JP-5 /JP-10
  • Oil system: Pressure system with return

Performance

  • Maximumthrust: 430 lbf (1.9 kN) Maximum continuous power
F107-WR-400 610 lbf (2.7 kN)
F107-WR-402 700 lbf (3.1 kN)
F107-WR-105/401 1,400 lbf (6.22 kN)

F122

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Williams F122
TypeTurbofan
National originUnited States
ManufacturerWilliams International
Major applicationsKEPD 350
Number built699 (as of August 2014)
Developed fromWilliams F107
VariantsWilliams F415

TheWilliams International F122 is a twin-shaft, axial-centrifugal-flow turbofan that is similar to the F107 in configuration but has a maximum thrust of 900 lbf (3.33 to 4.0 kN).

Design and development

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The F122 is used to power theKEPD 350 air-launchedcruise missile, and was the powerplant for the cancelledAGM-137 TSSAM air-launched cruise missile.[2] Although the AGM-137 was cancelled, the F122 was first used for the Taurus KEPD when it was flown aboard that missile in April 2002.

Applications

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See also

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References

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  1. ^Wilkinson, Paul H. (1970).Aircraft engines of the World 1970 (21st ed.). Washington D.C.: Paul H. Wilkinson. p. 120.
  2. ^"Designations Of U.S. Military Aero Engines".www.designation-systems.net.
  3. ^"Northrop AGM/MGM-137 TSSAM".www.designation-systems.net.

Further reading

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The initial version of this article was based on apublic domain article fromGreg Goebel's Vectorsite.

External links

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Wikimedia Commons has media related toWilliams F107.
Turbofans
United States military gas turbine aircraft enginedesignation system
Turbojets
Turboprops/
Turboshafts
Turbofans
Adaptive cycle engines
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