Westinghouse J34

Turbojet engine From Wikipedia, the free encyclopedia

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.

TypeTurbojet
National originUnited States
ManufacturerWestinghouse Aviation Gas Turbine Division
First run11 January 1947
Quick facts J34, Type ...
J34
J34 on display at the Wright-Patterson Air Force Base Museum
TypeTurbojet
National originUnited States
ManufacturerWestinghouse Aviation Gas Turbine Division
First run11 January 1947
Major applications
Developed fromWestinghouse J30
Developed intoWestinghouse J46
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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.[3]

Variants

Thrust given in foot-pounds (lbf) and kilonewtons (kN).

J34-WE-2
3,000 lbf (13 kN)
XJ34-WE-4
3,000 lbf (13 kN), originally designated J45[4]
XJ34-WE-7
3,000 lbf (13 kN)
J34-WE-11
Similar to -42 with short afterburner
J34-WE-13
3,000 lbf (13 kN)
J34-WE-15
3,000 lbf (13 kN), with short afterburner, similar to -42
J34-WE-15
4,100 lbf (18 kN)
J34-WE-17
3,370 lbf (15.0 kN) / 4,850 lbf (21.6 kN) with long afterburner, similar to -42
J34-WE-19
3,250 lbf (14.5 kN)
J34-WE-22
(24C-4B) 3,000 lbf (13 kN)[5]
J34-WE-30
(24C-4C) 3,150 lbf (14.0 kN) / 4,200 lbf (19 kN) with afterburner[5]
J34-WE-30A
3,150 lbf (14.0 kN) / 4,200 lbf (19 kN) with afterburner[5]
J34-WE-32
3,370 lbf (15.0 kN) / 4,900 lbf (22 kN) with long afterburner, similar to -42[5]
J34-WE-34
(24C-4D) 3,250 lbf (14.5 kN)[5]
J34-WE-34A
3,000 lbf (13 kN)
J34-WE-36
(24C-4E) 3,400 lbf (15 kN)[5]
J34-WE-36A
3,400 lbf (15 kN)[5]
J34-WE-38
3,800 lbf (17 kN)[5]
J34-WE-40
3,000 lbf (13 kN)
J34-WE-42
3,400 lbf (15 kN) / 4,200 lbf (19 kN) with afterburner[5]
J34-WE-46
3,400 lbf (15 kN)[5]
J34-WE-48
Single stage turbine. Contract awarded 1959
W-340
Commercial version of the WE-36
24C-4B
company designation for WE-22.[6]
24C-4C
company designation for WE-30.[6]
24C-4D
company designation for WE-34.[6]
24C-8
company designation for WE-32.[6]

Applications

Aircraft

Curtiss-Wright XF-87 Blackhawk

Others

Engines on display

Specifications (J34-WE-36)

Data from www.flightglobal.com[7]

General characteristics

  • Type: Turbojet
  • Length: 112 in (2.84 m)
  • Diameter: 27 in (0.69 m)
  • Dry weight: 1,207 lb (547.5 kg)

Components

Performance

See also

Related development

Comparable engines

Related lists

References

External links

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