Ranger V-770

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V-770
Preserved Ranger V-770
Type Piston aero-engine
Manufacturer
Ranger Aircraft Engine Division
First run 1931
Major applications Curtiss SO3C Seamew

The Ranger V-770 was an American air-cooled inverted

Ranger Aircraft Engine Division of the Fairchild Engine & Aircraft Corporation in the early 1930s.[1]

Design and development

In 1931, the V-770 design was built, derived from the Ranger 6-440 series of inverted inline air-cooled engines, and test flown in the Vought XSO2U-1 Scout. In 1938 it was tested in the Curtiss SO3C Seamew but was found to be unreliable with a tendency to overheat in low-speed flight, but would still be the most produced aircraft to have the V-770, with 795 being built.[2][3] Its competitor Vought XSO2U also suffered from overheating problems that were never satisfactorily solved.[4] By 1941 a more developed V-770 was installed in the Fairchild XAT-14 Gunner prototype gunnery school aircraft, which went into limited production as the

Fairchild AT-21 Gunner, of which 174 were built, not including one radial engine prototype.[5]

Produced from 1941 to 1945, the V-770 featured a two-piece aluminum alloy crankcase, steel cylinder barrels with integral

Fairchild AT-21 twin-engine bomber trainer,[6] and in the two Bell XP-77
light-weight fighter prototypes.

Variants

V-770-7 in Bell XP-77 mockup
V-770-4
Installed in the
Vought XSO2U-1
scout aircraft
V-770-6
Installed in the
Ryan SOR-1
Scout
V-770-7
Installed in the Bell XP-77 lightweight fighter prototype
V-770-8
Installed in the Curtiss SO3C Seamew Scout.[3]
V-770-9
Installed in the
North American XAT-6E Texan prototype.[5]
V-770-11
Installed in the
Fairchild AT-21 Gunner.[5]
V-770-15
Installed in the
Fairchild AT-21 Gunner.[5]
V-770-17
Similar to V-770-8 but with raised hollow propeller shaft for mounting cannon or machine gun.
GV-770
Geared un-supercharged variants.[7]
SV-770
Supercharged direct-drive variants.[7]
SGV-770
Supercharged and geared variants.[7]
SGV-770C-1
Tested in the
Curtiss XF6C-7 Hawk fighter-bomber at 350 hp (260 kW).[3]
SGV-770C-1B
(V-770-11)
SGV-770C-2A
(V-770-8)
SGV-770C-B1
Installed in the Ikarus 214 prototype
SGV-770D-4
(V-770-17) Similar to C-2A but with raised hollow propeller shaft for mounting cannon or machine gun.
SGV-770D-5
Developed for post-war commercial use,[1] 700 hp (520 kW) at 3,600 RPM, weight 870 lb (390 kg), height 31.11 in (790 mm), length 74.92 in (1,903 mm), width 33.28 in (845 mm)

Applications

Engines on display

Specifications (SGV-770C-1)

The Ranger V-770 engine as viewed along the cylinders.

Data from Janes Fighting Aircraft of World War II (1989).[1]

General characteristics

  • Type: 12-cylinder inverted Vee piston engine
  • Bore: 4 in (102 mm)
  • Stroke: 5.125 in (130 mm)
  • Displacement: 773 cu in (12.7 L)
  • Length: 62 in (1,575 mm)
  • Width: 28 in (711 mm)
  • Height: 32.2 in (818 mm)
  • Dry weight
    :     730 lb (330 kg)

Components

  • Single overhead camshaft
    (SOHC) (1 shaft per bank), gear driven
  • Supercharger: Single-speed, single-stage, produced 45 inches of mercury (1.5 bar, 22 psi) at take-off
  • Fuel system: Holley non-icing carburetor
  • Fuel type: 87 octane gasoline
  • Oil system: Full pressure type
  • Cooling system: Air-cooled

Performance

See also

Comparable engines

Related lists

References

Wikimedia Commons has media related to Ranger V-770.
  1. ^
    ISBN 1-85170-493-0
  2. OCLC 14253144
  3. ^
    ISBN 978-0-7607-3432-2
  4. ISBN 0-89747-270-5
    .
  5. ^
    ISBN 0-85177-816-X
  6. ^ "Ranger V-770 Inverted". National Museum of the USAF. Archived from the original on 30 December 2008. Retrieved 7 November 2008.
  7. ^ a b c Bridgman, Leonard (1937). Grey, C.G. (ed.). Jane's all the World's Aircraft 1937. London: Sampson Low, Marston & Co. Ltd.
  8. ^ Blown Ranger
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