Pratt & Whitney R-4360 Wasp Major: Difference between revisions
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|national origin= [[United States]] |
|national origin= [[United States]] |
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|first run= 1944 |
|first run= 1944 |
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|major applications= [[B-50 Superfortress]] <br> [[C-97 Stratofreighter]] <br> [[C-119 Flying Boxcar]] <br> [[Convair B-36]] |
|major applications= [[B-50 Superfortress]] <br> [[C-97 Stratofreighter]] <br> [[C-119 Flying Boxcar]] <br> [[Convair B-36]] <br> [[Hughes H-4 Hercules]] <br> |
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|number built = 18,697 |
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Revision as of 04:10, 6 June 2011
 | This article needs additional citations for verification. (January 2009) |
| R-4360 Wasp Major | |
|---|---|
| |
| Pratt & Whitney R-4360 Wasp Major (sectioned) | |
| Type | Four-row Radial engine |
| National origin | United States |
| Manufacturer | Pratt & Whitney |
| First run | 1944 |
| Major applications | B-50 Superfortress C-97 Stratofreighter C-119 Flying Boxcar Convair B-36 Hughes H-4 Hercules |
| Number built | 18,697 |
| Developed from | R-2180-A Twin Hornet |
| Developed into | R-2180 Twin Wasp E |
The Pratt & Whitney R-4360 Wasp Major was a large radial piston aircraft engine designed and built during World War II. It was the last of the Pratt & Whitney Wasp family and the culmination of its maker's piston engine technology, but the war was over before it could power airplanes into combat. It did, however, power the last generation of large piston-engined aircraft before the turbojet and turboprop took over.[1]
Design and development
The R-4360 was a 28-cylinder four-row air cooled radial engine. Each row of pistons was slightly offset from the previous, forming a semi-helical arrangement to facilitate efficient airflow cooling of the successive rows of cylinders, with the spiraled cylinder setup inspiring the engine's "corncob" nickname. A mechanical supercharger geared at 6.374:1 ratio to engine speed provided forced induction, while the propeller was geared at 0.375:1 so that the tips did not reach inefficient supersonic speeds.
Although reliable in flight, the Wasp Major was maintenance-intensive. Improper starting technique could foul all 56 spark plugs, which would require hours to clean or replace. As with most piston aircraft engines of the era, the time between overhauls of the Wasp Major was about 600 hours when used in commercial service.
Engine displacement was 4,362.50 in³ (71.5 L), hence the model designation. Initial models developed 3,000 hp (2,240 kW), and later models 3,500 hp but one model delivered 4,300 hp (3200 kW) using two large turbochargers in addition to the supercharger. Engines weighed 3,482 to 3,870 lb (1,579 to 1,755 kg), giving a power to weight ratio of 1.11 hp/lb (1.83 kW/kg), which was matched or exceeded by very few contemporary engines.
Wasp Majors were produced between 1944 and 1955; 18,697 were built.
A derivative engine, the 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 postwar Saab 90 Scandia airliner.
Applications
- Aero Spacelines Mini Guppy
- Aero Spacelines Pregnant Guppy
- Boeing 377 Stratocruiser
- Boeing B-50 Superfortress
- Boeing C-97 Stratofreighter
- Boeing KC-97 Stratotanker
- Boeing XF8B
- Boeing XB-44 Superfortress
- Convair B-36
- Convair XC-99
- Curtiss XBTC
- Douglas C-74 Globemaster
- Douglas C-124 Globemaster II
- Douglas TB2D Skypirate
- Fairchild C-119 Flying Boxcar
- Fairchild C-120 Packplane
- Goodyear F2G Corsair
- Hughes H-4 Hercules ("Spruce Goose")
- Hughes XF-11
- Lockheed R6V Constitution
- Martin AM Mauler
- Martin JRM Mars
- Martin P4M Mercator
- Northrop B-35
- Republic XP-72
- Republic XF-12 Rainbow
- SNCASE SE-2010 Armagnac
- Vultee A-41
Variants
- R-4360-4 - 2,650 hp (1,976 kW)
- R-4360-20 - 3,500 hp (2,610 kW)
- R-4360-25 - 3,000 hp (2,237 kW)
- R-4360-41 - 3,500 hp (2,610 kW)
- R-4360-51 VDT - "Variable Discharge Turbine" 4,300 hp (3,210 kW). Intended for B-36C. Used on Boeing YB-50C Superfortress. Turbo-supercharger exhaust used to augment thrust.
- R-4360-53 - 3,800 hp (2,834 kW)
- R-4360-B3 - 3,500 hp (2,610 kW)
Specifications (R-4360-51VDT)
General characteristics
- Type: 28-cylinder supercharged air-cooled four-row radial engine
- Bore: 5.75 in. (146.05 mm)
- Stroke: 6.00 in. (152.4 mm)
- Displacement: 4,362.5 in³ (71.49 L)
- Length: 96.5 in. (2 451 mm)
- Diameter: 55 in (1397 mm)
- Dry weight: 3,870 lb (1,755 kg)
Components
- Valvetrain: Poppet, two valves per cylinder
- Supercharger: Gear-driven single stage variable speed centrifugal type supercharger
- Turbocharger: General Electric CHM-2
- Fuel system: Bendix-Stromberg PR-100E2 pressure carburetor
- Fuel type: 108/135 octane gasoline
- Cooling system: Air-cooled
Performance
- Power output: 4,300 hp (3,210 kW)
- Specific power: 0.99 hp/in³ (44.9 kW/L)
- Compression ratio: 6.7 : 1
- Power-to-weight ratio: 1.11 hp/lb (1.83 kW/kg)
See also
Related development
- Pratt & Whitney Wasp series
- R-1830 Twin Wasp
- R-1535 Twin Wasp Junior
- R-2180 Twin Wasp E
- R-2800 Double Wasp
Comparable engines
Related lists
References
- ^ Pratt & Whitney web site
- Bridgman, Leonard, ed. Jane's All The World's Aircraft 1951–1952. London: Samson Low, Marston & Company, Ltd 1951.
- White, Graham (2006). R-4360: Pratt & Whitney's Major Miracle. North Branch, Minn.: Specialty Press. ISBN 1-58007-097-3.
External links
- Pratt & Whitney R-4360 page
- National Museum of the USAF– R-4360 fact sheet
- More info
- Information about the 4360 from the Aircraft Engine Historical Society includes photos of the VDT engine.
- Portrait of 3,500 Horses July 1947 cutaway illustration of Wasp Major