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Pratt & Whitney R-4360 Wasp Major

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(Redirected fromPratt & Whitney R-4360)
R-28 piston aircraft engine family
R-4360 Wasp Major
Pratt & Whitney R-4360 Wasp Major
TypeFour-rowRadial engine
National originUnited States
ManufacturerPratt & Whitney
First run1944
Major applicationsBoeing 377
Boeing B-50 Superfortress
Boeing C-97 Stratofreighter
Convair B-36
Fairchild C-119 Flying Boxcar
Number built18,697
Developed fromPratt & Whitney R-2180-A Twin Hornet
Developed intoPratt & Whitney R-2180-E Twin Wasp E

ThePratt & Whitney R-4360 Wasp Major is an American 28-cylinder four-rowradialpistonaircraft engine designed and built duringWorld War II. At 4,362.5 cu in (71.5 L), it is the largest-displacement aviation piston engine to be mass-produced in the United States, and at 4,300 hp (3,200 kW) the most powerful. First run in 1944, it was the last of thePratt & WhitneyWasp family, and the culmination of its maker'spiston engine technology.

The war was over before it could power airplanes into combat. It powered many of the last generation of large piston-engined aircraft beforeturbojets, but was supplanted by equivalent (and superior) poweredturboprops (such as theAllison T56).

Its main rival was the twin-row, 18-cylinder, nearly 3,350 cu in (54.9 L) displacement, up to 3,700 hp (2,800 kW)Wright R-3350 Duplex-Cyclone, first run some seven years earlier (May 1937).

Design and development

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The R-4360 was a 28-cylinder four-row air-cooled radial engine. Each row of seven air-cooled cylinders possessed a slight angular offset from the previous, forming a semi-helical arrangement to facilitate effective airflow cooling of the cylinder rows behind them, inspiring the engine's "corncob" nickname.[1] A mechanicalsupercharger geared at 6.374:1 ratio to engine speed provided forced induction, while thepropeller was geared at 0.375:1 so that the tips did not reach inefficientsupersonic speeds.

The engine was a technological challenge and the first product from Pratt and Whitney's new plant nearKansas City, Missouri.[2] The four-row configuration had severe thermal problems that decreased reliability, with an intensive maintenance regime involving frequent replacement of cylinders required.[citation needed] Large cooling flaps were required, which decreased aerodynamic efficiency, putting extra demands on engine power when cooling needs were greatest. Owing in large part to the maintenance requirements of the R-4360, all airplanes equipped with it were costly to operate and suffered decreased availability. Its commercial application in theBoeing Stratocruiser was unprofitable without government subsidy.[3] Abandonment of the Stratocruiser was almost immediate when jet aircraft became available, while aircraft with smaller powerplants such as theLockheed Constellation andDouglas DC-6 remained in service well into the jet era.

Engine displacement was 4,362.5 cu in (71.5 L), hence the model designation. Initial models developed 3,000 hp (2,200 kW), and later models 3,500 hp (2,600 kW). One model that used two largeturbochargers in addition to the supercharger delivered 4,300 horsepower (3,200 kW). Engines weighed 3,482–3,870 lb (1,579–1,755 kg), giving apower-to-weight ratio of 1.11 hp/lb (1.82 kW/kg).

Wasp Majors were produced between 1944 and 1955; 18,697 were built.

A derivative engine, thePratt & Whitney R-2180-E Twin Wasp E, was essentially the R-4360 "cut in half". It had two rows of seven cylinders each, and was used on the postwarSaab 90 Scandia airliner.[4]

Variants

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Sectioned R-4360 Wasp Major
  • R-4360-4 - 2,650 hp (1,980 kW)
  • R-4360-17 - 3,500 hp (2,600 kW) XB-35 and YB-35 outboard engines with 8-bladed contra-rotating propellers[5]
  • R-4360-20 - 3,500 hp (2,600 kW)
  • R-4360-21 - 3,500 hp (2,600 kW) XB-35 and YB-35 inboard engines with 8-bladed contra-rotating propellers[5]
  • R-4360-25 - 3,000 hp (2,200 kW)
  • R-4360-41 - 3,500 hp (2,600 kW)
  • R-4360-45 - 3,500 hp (2,600 kW) YB-35 outboard engines with 4-bladed propellers[5]
  • R-4360-47 - 3,500 hp (2,600 kW) YB-35 inboard engines with 4-bladed propellers[5]
  • R-4360-51 VDT - "Variable Discharge Turbine" 4,300 hp (3,210 kW). Intended for B-36C. Used on Boeing YB-50C Superfortress.[6]
  • R-4360-53 - 3,800 hp (2,800 kW)
  • R-4360-B3 - 3,500 hp (2,600 kW)
  • R-4360-B6 - 3,500 hp (2,600 kW)

Applications

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Engines on display

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R-4360 cutaway
R-4360-4 on display at theAir Zoo
R-4360 on display atMuseum of Aviation,Robins AFB

Specifications (R-4360-51VDT)

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Pratt & Whitney R-4360 Wasp Major (sectioned)

Data from White, 1995[21]

General characteristics

  • Type: 28-cylinder supercharged air-cooled four-rowradial engine
  • Bore: 5.75 in (146 mm)
  • Stroke: 6.00 in (152 mm).
  • Displacement: 4,362.5 cu in (71.489 L)
  • Length: 103 in (2,600 mm)
  • Diameter: 61 in (1,500 mm)
  • Dry weight: 3,720 lb (1,690 kg)

Components

Performance

See also

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Related development

Comparable engines

Related lists

References

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Notes

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  1. ^White 1995, p. 212.
  2. ^Gunston 2006, p. 132.
  3. ^"Ernest K. Gann's Flying Circus: Lady with a past". Ovi.ch. Retrieved2012-06-18.
  4. ^Gunston 2006, p. 164.
  5. ^abcdPape, Garry R.; Campbell, John M. (1995).Northrop Flying Wings : a history of Jack Northrop's visionary aircraft (1st ed.). Atglen: Schiffer Pub. pp. 116–193, 253.ISBN 0887406890.
  6. ^"Schematic Diagram of Wasp Major VDT Power Plant". Retrieved8 November 2023.
  7. ^"About the Museum".Mid America Museum of Aviation and Transportation. Retrieved18 February 2018.
  8. ^"Goodyear F2G-1 Super Corsair".The Museum of Flight. The Museum of Flight. Retrieved18 February 2018.
  9. ^abcdefghijklmnopHuff, Randy."Engines in North American Museums".Aircraft Engine Historical Society. Aircraft Engine Historical Society. Retrieved18 February 2018.
  10. ^"Pratt & Whitney R-4360 Wasp Major".Heritage Flight Museum. Avada. Retrieved18 February 2018.
  11. ^Yankee Air Museum archive records and display
  12. ^ab"ENGINES ON DISPLAY".Combat Air Museum. Combat Air Museum. Retrieved18 February 2018.
  13. ^""Wasp Major" Engine".Hill Air Force Base. United States Air Force. 20 January 2007. Archived fromthe original on October 19, 2016. Retrieved18 February 2018.
  14. ^"R-4360 Wasp Major".Air Victory Museum. Air Victory Museum. Archived from the original on August 19, 2015. Retrieved18 February 2018.
  15. ^"Pratt & Whitney Wasp Major R-4360-59B, Cutaway, Radial Engine".Smithsonian National Air and Space Museum. Smithsonian Institution. 2016-04-05. Retrieved18 February 2018.
  16. ^"Exhibits".SUN 'n FUN. SUN 'n FUN. Retrieved18 February 2018.
  17. ^"WELCOME TO THE MID-ATLANTIC AIR MUSEUM".www.maam.org. Retrieved2018-09-07.
  18. ^"Pratt & Whitney R-4360 "Wasp Major"".National Museum of the US Air Force™. Retrieved2018-09-07.
  19. ^"main exhibits".penngrovepower.org. Retrieved2019-07-11.
  20. ^Stoneberg, David (September 16, 2020)."A piece of military aircraft history sits in St. Helena, just waiting to put on a show".Napa Valley Register. St Helena, CA: Lee Enterprises, Inc. RetrievedSeptember 17, 2020.
  21. ^White 1995, p. 222.

Bibliography

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  • Bridgman, Leonard, ed.Jane's All The World's Aircraft 1951–1952. London: Samson Low, Marston & Company, Ltd 1951.
  • Gunston, Bill (2006).World Encyclopedia of Aero Engines: From the Pioneers to the Present Day (5 ed.). Stroud, UK: Sutton.ISBN 0-7509-4479-X.
  • White, Graham (1995).Allied Aircraft Piston Engines of World War II: History and Development of Frontline Aircraft Piston Engines Produced by Great Britain and the United States During World War II. Warrendale, Pennsylvania: SAE International.ISBN 1-56091-655-9.
  • White, Graham (2006).R-4360: Pratt & Whitney's Major Miracle. North Branch, Minn.: Specialty Press.ISBN 1-58007-097-3.

External links

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Wikimedia Commons has media related toPratt & Whitney R-4360.
Radial engines
H piston engines
Free-piston gas turbines
Turbojets
Turbofans
Turboprops/Turboshafts
Propfans
Rocket engines
Aeroderivative gas
turbine engines
Subsidiaries
Key people
H (four-bank
H-configuration inline)
IV (inverted-V inline)
L (single-bank inline)
O (opposed)
R (radial)
V (upright-V inline)
V (inverted-V inline)
VG (inverted-V inline)
W (three-bank
W-configuration inline)
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