T34 Turbo-Wasp
AB-17 Flying Fortress testbed for the T-34 turboprop engine. This aircraft was later flown on airshow circuits as theLiberty Belle.[1]
Type	Turboprop
National origin	United States
Manufacturer	Pratt & Whitney
First run	ca. 1950
Major applications	Douglas C-133 Cargomaster

ThePratt & Whitney T34 (company designationPT2 Turbo-Wasp^[2]) is an Americanaxial flow^[2]turboprop engine designed and built byPratt & Whitney. Its only major application was on theDouglas C-133 Cargomaster.

In 1945, theUnited States Navy funded the development of a turboprop engine. The T34 was produced from 1951 to 1960, but never used in U.S. Navy aircraft production.^[3]

The YT34 engine with three wide-bladed propellers was made for two NavyLockheed R7V-2 Constellation (C-121s) variants, for testing. Flight tests were on 1 September 1954.^[4]

In September 1950, a testbedBoeing B-17 Flying Fortress flew with a T34 turboprop mounted in the nose of the bomber. The first application for the T34 was theBoeing YC-97J Stratofreighter, which later became theAero Spacelines Super Guppy. The next application for the engine was theDouglas C-133 Cargomaster.^[3]

T34-P-1

5,700 shp (4,300 kW) equivalent.

T34-P-2

Similar to -1.

T34-P-3

6,000 shp (4,500 kW) equivalent.

YT34-P-5

5,229 shp (3,899 kW) equivalent^[5]

T34-P-6

5,531 shp (4,124 kW) equivalent^[6]

T34-P-7

T34-P-7W

7,100 shp (5,300 kW) equivalent, w/water injection

T34-P-9W

7,500 shp (5,600 kW) equivalent, w/water injection

T34-P-12

YT34-P-12A

5,500 shp (4,100 kW) equivalent^[7]

PT2F-1

5,500 shp (4,100 kW) equivalent, unbuilt civilian version planned to power the Lockheed L-1249B.^[8]

PT2G-3

5,600 shp (4,200 kW) equivalent, unbuilt civilian version planned to power the Lockheed L-1449 and possibly the L-1549.^[8]

• Aero Spacelines Super Guppy
• Boeing YC-97J Stratofreighter (YT34-P-5)^[5]
• Douglas YC-124B Globemaster II^[9]
• Douglas C-133 Cargomaster
• Lockheed R7V-2 Constellation (YT34-P-12A)^[10]
• Lockheed YC-121F Constellation (T34-P-6)^[6]

• T34-P-3:National Air and Space Museum^[11] (NASM) inWashington, D.C.
• T34-P-6:Travis Air Force Base Heritage Center inFairfield, California
• T34-P-7W: NASM^[11]
• T34-P-7WA:Pacific Coast Air Museum (PCAM) inSanta Rosa, California

Data fromJane's All The World's Aircraft 1961–62.^[12]

• Type:Turboprop
• Length: 156.8 in (3,983 mm)
• Diameter: 33.75 in (857 mm)
• Dry weight: 2,590 lb (1,175 kg)

• Compressor: 13-stageaxial compressor
• Combustors: annular combustion chamber with eight flame tubes
• Turbine: three-stage axial-flow
• Fuel type: JP-4
• Oil system: closed circuit

• Maximum power output: 5,500 shp (4,103 kW) plus 1,252 lbf (5.57 kN) thrust, 6,000 ehp (4,476 kW) (take-off power)
• Overall pressure ratio: 6.7:1
• Power-to-weight ratio: 2.32 ehp/lb

Related development

• Pratt & Whitney T57

Comparable engines

• Allison T56
• Allison T61
• Rolls-Royce Tyne

Related lists

• List of aircraft engines

• Gunston, Bill (2006).World Encyclopedia of Aero Engines, 5th Edition. Phoenix Mill, Gloucestershire, England, UK: Sutton Publishing Limited. p. 79.ISBN 0-7509-4479-X.
• Taylor, John W. R. (1961).Jane's All The World's Aircraft 1961–62. London: Sampson Low, Marston & Company.
• Breffort, Dominique (2006).Lockheed Constellation: from Excalibur to Starliner Civilian and Military Variants. Paris: Histoire and Collecions. p. 176.ISBN 2-915239-62-2.

Wikimedia Commons has media related toPratt & Whitney T34.

• Pratt & Whitney's T34 page
• Pratt & Whitney T34 page on Shanaberger.com

• 1950s turboprop engines
• Pratt & Whitney aircraft engines

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