Misplaced Pages

Continental R-670

Article snapshot taken from Wikipedia with creative commons attribution-sharealike license. Give it a read and then ask your questions in the chat. We can research this topic together.
(Redirected from Continental R-670-A) Seven-cylinder four-cycle radial aircraft engine
R-670
Continental W670 on display
Type Piston aircraft engine
Manufacturer Continental Motors
First run 1934
Major applications PT-17 Stearman
M3 Stuart

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 465 lb (211 kg). 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.

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 Variants of the W670 included:

W670-K
carburetor, 5.4:1 compression, 65 Octane, front exhausts and 225 hp (168 kW)
W670-L
carburetor, 5.4:1 compression, 73 Octane, rear exhausts and 225 hp (168 kW)
W670-M
carburetor, 6.1:1 compression, 80 Octane, front exhausts and 240 hp (179 kW)
W670-N
carburetor, 6.1:1 compression, 80 Octane, rear exhausts and 240 hp (179 kW)
W670-K1
fuel injection, 5.4:1 compression, 73 Octane, front exhausts and 230 hp (172 kW)
W670-L1
fuel injection, 5.4:1 compression, 73 Octane, rear exhausts and 230 hp (172 kW)
W670-M1
fuel injection, 6.1:1 compression, 80 Octane, front exhausts and 250 hp (186 kW)
W670-N1
fuel injection, 6.1:1 compression, 80 Octane, rear exhausts and 250 hp (186 kW)

Applications

Aircraft

Armored fighting vehicles

Specifications (R-670-K)

An R-670 fitted to a Boeing Stearman at the Imperial War Museum Duxford

Data from Jane's 1938

General characteristics

  • Type: Seven cylinder air-cooled radial
  • Bore: 5+1⁄8 in (130.2 mm)
  • Stroke: 4+5⁄8 in (117.5 mm)
  • Displacement: 668 cu in (10.95 L)
  • Length: 34+3⁄16 in (868.4 mm)
  • Diameter: 42+1⁄2 in (1,079.5 mm)
  • Dry weight: 450 lb (204.1 kg)

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

  1. Gunston 1989, p.42.
  2. ^ Jane's All the World's Aircraft 1938. London: Sampson, Low & Martin company Limited. 1938.

Bibliography

  • Gunston, Bill. World Encyclopaedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
  • Jane's Fighting Aircraft of World War II. London. Studio Editions Ltd, 1998. ISBN 0-517-67964-7
  • Jane's All the World's Aircraft 1938. London: Sampson, Low & Martin company Limited. 1938.

External links

Continental Motors, Teledyne Continental, and Continental Aerospace Technologies aircraft engines
Opposed piston engines
(Gasoline)
By company
horsepower designation
By displacement
Aircraft Diesel engines
Radial engines
Inverted-V engines
Turboprops
United States military piston aircraft engine designation system
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)
Categories: