Curtiss H-1640 Chieftain

H-1640
	H-1640 engine at the National Air and Space Museum
Type	Radial aero engine
Manufacturer	Curtiss Aeroplane and Motor Company
First run	1926

The Curtiss H-1640 Chieftain was an unusual American 12-cylinder radial aero engine designed and built by the Curtiss Aeroplane and Motor Company in the mid-1920s.^[1] In contrast to most multi-row radials, where the cylinders in the rows are staggered to present better airflow for cooling, the Chieftain used the inline radial arrangement with the cylinders behind each other to allow pairs of cylinders to share a cast cylinder head and camshafts. The design saw some use in the 1920s but was quickly passed by newer designs.

Design and development

The H-1640 was an air-cooled 12 cylinder two-row radial with the cylinder rows aligned rather than staggered as in most multi-row radials. One piece cylinder heads shared a single overhead camshaft and the propeller was directly driven. By aligning the cylinders the diameter of the engine was less than more conventional radial engines, and it was thought that the use of a Townend ring could make the engine more aerodynamically efficient than an inline engine. The engine first ran in 1927.

The H-1640 was the first airworthy 'inline radial' and was sponsored for flight testing in a range of aircraft by the U.S. Government. Among the types selected were the Thomas-Morse XP-13 and the Curtiss XO-18. Cooling problems with the rear cylinders caused the project to be canceled with few production engines being built.

A similar engine is the Bristol Hydra although this engine had 16 aligned cylinders, forming an octagon. Further similar engines are the Armstrong Siddeley Hyena and the much larger Armstrong Siddeley Deerhound.

Applications

A Thomas-Morse XP-13 Viper fitted with a Curtiss H-1640 Chieftain during testing

Specifications (H-1640)

Curtis H 1640 Engine - located at the Wings Over The Rockies museum, Denver, CO

Data from enginehistory.org^[2]

General characteristics

Type: 12-cylinder, two-row, air-cooled radial engine
Bore: 5⅝ in (142.9 mm)
Stroke: 5½ in (139.7 mm)
Displacement: 1,640 cu in (26.9 L)
Diameter: 45 in (1,143 mm)
Dry weight: 900 lb (408 kg)

Components

Valvetrain: Overhead camshaft
Fuel system: Single Stromberg NA-U8J carburetor
Cooling system: Air-cooled
Reduction gear: Direct drive, right-hand tractor

Performance

Power output: 615 hp (459 kW)
Specific power: 0.38 hp/cu in (17 kW/L)
Power-to-weight ratio: 0.68 hp/lb (1.13 kW/kg)

References

Notes

^ Gunston 1989, p. 46
^ Curtiss Chieftain www.enginehistory.org Retrieved: 17 September 2009

Bibliography

Gunston, Bill. World Encyclopaedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9

[1] Gunston 1989, p. 46

[2] Curtiss Chieftain www.enginehistory.org Retrieved: 17 September 2009

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