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Curtiss V-1570 Conqueror

From Wikipedia, the free encyclopedia
(Redirected fromCurtiss V-1570-23 Conqueror)
American piston aircraft engine
V-1570
TypeV12piston engine
ManufacturerCurtiss Aeroplane and Motor Company
First run1926

TheCurtiss V-1570 Conqueror was aV12 liquid-cooled aircraft engine. Representing a more powerful version of theCurtiss D-12, the engine entered production in1926 and flew in numerous aircraft.[1]

Design and development

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Designed in 1924 as a military successor to theCurtiss D-12, initially named the Conqueror, it was later given the military designation of V-1570 based on itsdisplacement of 1,570 cubic inches (26 L). The engine featured open-ended cylinder liners (advanced technology for the period) and pressurizedliquid cooling. Developments including the use of asupercharger gradually increased power output until reliability problems due to overheating and coolant leaks became apparent. Military funding for further development of the Conqueror was cut in 1932, efforts by Curtiss to market the engine for civilairliners failed and the line was dropped from production.

Variants

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V-1570-1
V-1570-5
V-1570-7
GV-1570-7
geared -7
V-1570-9
V-1570-11
V-1570-13
V-1570-15
SV-1570-15
V-1570-17
V-1570-23
V-1570-25
V-1570-27
V-1570-29
V-1570-33
V-1570-53
V-1570-55
V-1570-57
V-1570-59
V-1570-61
V-1570-79
GIV-1570-FM
V-1570-C
V-1570-F
GIV-1570C

Applications

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Curtiss XP-10

Other applications

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Specifications (V-1570 direct drive)

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Side view of V-1570-53

Data fromGrey and Gunston.[2][1]

General characteristics

  • Type: V-12 liquid-cooled aircraft piston engine
  • Bore:5+18 in (130 mm)
  • Stroke:6+1132 in (161 mm)
  • Displacement: 1,570.4 cu in (25.7 L)
  • Length: 64 in (1,600 mm)
  • Width:26+516 in (668 mm)
  • Height:39+116 in (992 mm)
  • Dry weight: 835 lb (379 kg)

Components

  • Valvetrain: Inlet and exhaust overhead camshafts operating two exhaust and two inlet valves per cylinder, via 'T' head cam followers.
  • Fuel system: Two Stromberg NA-Y6-O carburetors
  • Oil system: Dry sump, pressure feed and spray with scavenge.
  • Cooling system: Liquid-cooled (water or chemical coolant)
  • Reduction gear: Direct-drive
  • Ignition system:One Scintilla magneto and two distributors

Performance

See also

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Related development

Comparable engines

Related lists

References

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Wikimedia Commons has media related toCurtiss V-1570.

Notes

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  1. ^abGunston 1989, p. 46.
  2. ^Grey 1931, p. 72.

Bibliography

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  • Gunston, Bill.World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989.ISBN 1-85260-163-9
  • Grey, C.G.Jane's all the World's Aircraft 1931 London, England. Sampson Low, Marston & Company Limited
Inline engines
Radial engines
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)
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