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Curtiss H-1640 Chieftain

 

Curt-H-1640-2

 

The H-1640 was an air-cooled, two-row 12-cylinder radial with the cylinders aligned fore and aft in a hexagonal layout. The cylinder banks were placed at 60° intervals. One piece cylinder heads shared a single overhead camshaft, the propeller was directly driven. It was thought that the use of a Townend ring would prove more aerodynamically efficient over an inline engine. The engine first ran in 1927, by aligning the cylinders the diameter of the engine was less than more conventional radial engines.

 

Curt-H-1640-3

 

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. Although the engine was also intended for civil use in the 600 horsepower class continued cooling problems with the rear cylinders caused the project to be canceled with few production engines being built.

 

  Curt-H-1640

 

Applications:
Curtiss XO-18
Curtiss XP-22 Hawk
Curtiss YP-20
Curtiss P-6 Hawk
Thomas-Morse XP-13 Viper

 

Specifications:


H-1640
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)
Valvetrain: Overhead camshaft
Fuel system: Single Stromberg NA-U8J carburetor
Cooling system: Air-cooled
Reduction gear: Direct drive, right-hand tractor
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)

 


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