Continental R-670

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The Continental R-670 (factory designation W670) was a seven-cylinder four-stroke radial aircraft engine produced by Continental displacing 668 cubic inches (11 litres) and a dry weight of Script error: No such module "convert".. Horsepower varied from 210 to 240 at 2,200 rpm. The engine was the successor to Continental's first radial engine, the 170 hp Continental A-70. This engine was used on many aircraft in the 1930s and 1940s. The R-670 was widely used in the PT-17 Stearman primary training aircraft of the U.S. military.[1]

In addition to being used in aircraft, the R-670 was used in a number of light armored vehicles of World War II.

Variants

Data from: Jane's All the World's Aircraft 1938[2] Variants of the W670 included:

W670-K
carburetor, 5.4:1 compression, 65 Octane, front exhausts and Script error: No such module "convert".
W670-L
carburetor, 5.4:1 compression, 73 Octane, rear exhausts and Script error: No such module "convert".
W670-M
carburetor, 6.1:1 compression, 80 Octane, front exhausts and Script error: No such module "convert".
W670-N
carburetor, 6.1:1 compression, 80 Octane, rear exhausts and Script error: No such module "convert".
W670-K1
fuel injection, 5.4:1 compression, 73 Octane, front exhausts and Script error: No such module "convert".
W670-L1
fuel injection, 5.4:1 compression, 73 Octane, rear exhausts and Script error: No such module "convert".
W670-M1
fuel injection, 6.1:1 compression, 80 Octane, front exhausts and Script error: No such module "convert".
W670-N1
fuel injection, 6.1:1 compression, 80 Octane, rear exhausts and Script error: No such module "convert".

Applications

Aircraft

Armored fighting vehicles

Specifications (R-670-K)

File:ContinentalR-670.JPG
An R-670 fitted to a Boeing Stearman at the Imperial War Museum Duxford

Data from Jane's 1938[2]

General characteristics

  • Type: Seven cylinder air-cooled radial
  • Bore: Script error: No such module "convert".
  • Stroke: Script error: No such module "convert".
  • Displacement: Script error: No such module "convert".
  • Length: Script error: No such module "convert".
  • Diameter: Script error: No such module "convert".
  • Dry weight: Script error: No such module "convert".

Components

  • Valvetrain: 1 inlet and 1 exhaust valve per cylinder
  • Fuel system: 1 Stromberg NA-R6 Carburetor
  • Fuel type: 65 octane
  • Oil system: Dry sump, one pressure pump, one scavenge pump, enclosed valve-train
  • Cooling system: Air-cooled

Performance

See also

Comparable engines

Related lists

References

Notes

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  1. Gunston 1989, p.42.
  2. a b Script error: No such module "citation/CS1".

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Bibliography

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  • Gunston, Bill. World Encyclopaedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. Template:ISBN
  • Jane's Fighting Aircraft of World War II. London. Studio Editions Ltd, 1998. Template:ISBN
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External links

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Template:Teledyne Continental aeroengines Template:US military piston aeroengines