Westinghouse J34 Explained
The Westinghouse J34, company designation Westinghouse 24C, was a turbojet engine developed by Westinghouse Aviation Gas Turbine Division in the late 1940s. Essentially an enlarged version of the earlier Westinghouse J30, the J34 produced 3,000 pounds of thrust, twice as much as the J30. Later models produced as much as 4,900 lb with the addition of an afterburner. It first flew in 1947. The J46 engine was developed as a larger, more powerful version of Westinghouse's J34 engine, about 50% larger.
Development
Built in an era of rapidly advancing gas turbine engine technology, the J34 was largely obsolete before it saw service, and often served as an interim engine.[1] For instance, the Douglas X-3 Stiletto was equipped with two J34 engines when the intended Westinghouse J46 engine proved to be unsuitable. The Stiletto was developed to investigate the design of an aircraft at sustained supersonic speeds. However, equipped with the J34 instead of its intended engines, it was seriously underpowered and could not exceed Mach 1 in level flight.[2]
Developed during the transition from piston-engined aircraft to jets, the J34 was sometimes fitted to aircraft as a supplement to other powerplants, as with the Lockheed P-2 Neptune and Douglas D-558-2 Skyrocket (fitted with radial piston engines and a rocket engine, respectively).
The afterburner was developed by Solar Aircraft, the first U.S. company to produce a practical afterburner.
Variants
- J34-WE-2: thrust
XJ34-WE-4: thrust; originally designated J45[3]
XJ34-WE-7: thrust
J34-WE-11: Similar to -42 with short afterburner
J34-WE-13: thrust
J34-WE-15: Similar to -42 thrust, with short afterburner
J34-WE-15: thrust
J34-WE-17: Similar to -42 thrust (thrust with long afterburner)
J34-WE-19: thrust
J34-WE-22: (24C-4B) thrust[4]
J34-WE-30: (24C-4C) thrust (thrust with afterburner)
J34-WE-30A: 3,150 lbf (14.01 kN) thrust (4,200 lbf (18.68 kN) thrust with afterburner)
J43-WE-32: Similar to -42 thrust (thrust with long afterburner)
J34-WE-34: (24C-4D) thrust
J34-WE-34A: thrust
J34-WE-36: (24C-4E) thrust
J34-WE-36A: thrust
J34-WE-38: thrust
J34-WE-40: thrust
J34-WE-42: thrust (thrust with afterburner)
J34-WE-46: thrust
J34-WE-48: Single stage turbine. Contract awarded 1959
W-340:Commercial version of the WE-36
24C-4B: company designation for WE-22.[5]
24C-4C: company designation for WE-30.[5]
24C-4D: company designation for WE-34.[5]
24C-8: company designation for WE-32.[5]
Applications
Aircraft
Others
Engines on display
References
Bibliography
- Gunston, Bill. World Encyclopedia of Aero Engines, 5th Edition. Phoenix Mill, Gloucestershire, England, UK: Sutton Publishing Limited, 2006. pp. 240–241. .
- Kay, Anthony L. Turbojet History and Development 1930-1960 Volume 2: USSR, USA, Japan, France, Canada, Sweden, Switzerland, Italy and Hungary (1st ed.). Ramsbury, UK: The Crowood Press, 2007. .
- Leyes, Richard A., II and William A. Fleming. The History of North American Small Gas Turbine Aircraft Engines (Library of Flight). Reston, Virginia: American Institute of Aeronautics and Astronautics, Inc, 1999. .
- Roux, Élodie. Turbofan and Turbojet Engines: Database Handbook. Raleigh, North Carolina: Éditions Élodie Roux, 2007. .
External links
- http://www.arkairmuseum.org/engines/engine-westinghouse.php
- http://www.globalsecurity.org/military/systems/aircraft/systems/j34.htm
Notes and References
- http://www.globalsecurity.org/military/systems/aircraft/f6u.htm "F6U Pirate."
- http://www.shanaberger.com/X-3.htm "Douglas X-3 Stiletto,"
- Web site: Designations of U.S. Military Aero Engines .
- Roux 2007, pp. 217–220.
- Book: Wilkinson, Paul H. . Aircraft engines of the World 1950 . 1950 . Sir Isaac Pitman & Sons Ltd. . London . 11th . 62–63.
