Seven-cylinder four-cycle radial aircraft engine
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 .[ 1]
In addition to being used in aircraft, the R-670 was used in a number of light armored vehicles of World War II .
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 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)
American Airmotive NA-75
Boeing-Stearman Model 75 (PT-17, N2S)
CallAir Model A
Cessna 190
Eagle Aircraft Eagle 220
Fairchild PT-23
Funk F-23
G class blimp
Grumman G-164 Ag Cat
Kellett K-2A, K-4
Morane-Saulnier MS.317
Timm N2T Tutor
Waco 240-A
Waco Standard Cabin series (UEC, UIC, UKC, UKC-S, UKS, VKS)
Waco Custom Cabin series (UOC, VQC)
Waco A series (UBA, ULA)
Waco F series (UBF, UMF, UPF)
Armored fighting vehicles [ edit ]
Specifications (R-670-K)[ edit ]
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 : 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
Comparable engines
Related lists
^ Gunston 1989, p.42.
^ a b Jane's All the World's Aircraft 1938 . London: Sampson, Low & Martin company Limited. 1938.
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.