Object Details
Manufacturer
Curtiss Aeroplane and Motor Company
Physical Description
Type: Reciprocating, 6 cylinders, In-line, Liquid-cooled
Power rating: 298 kW (400 hp) at 1,450 rpm
Displacement: 30.2 L (1,847.26 cu. in.)
Bore and Stroke: 178 mm (7 in.) x 203 mm (8 in.)
Weight: 544 kg (1,200 lb)
Summary
Among the most successful early engines marketed in the United States were those designed and built by aviation pioneer and inventor Glenn Curtiss in his factory at Hammondsport, New York. Early Curtiss engines powered motorcycles, and were air cooled. Later, to achieve higher power, Curtiss began to develop liquid-cooled engines. Curtiss built this engine for the U.S. Navy in 1921 for experimental purposes. It incorporated the Ricardo supercharging system, designed to increase engine power at high altitude and decrease fuel consumption.
The piston and cylinder assembly were designed so the underside of the piston compressed air on the intake stroke of the piston. The compressed air then passed through an intercooler back into the cylinder above the piston during the compression stroke. The Navy did not consider the experiment successful, as the improvements that resulted did not offset the increased weight and mechanical complexity.
Credit Line
Transferred from the U.S. Navy
Date
Circa 1921
Inventory Number
A19710936000
Restrictions & Rights
CC0
Type
PROPULSION-Reciprocating & Rotary
Materials
Steel, Preservative coating, Wood, Rubber, Textile, Aluminum, Paint, Phonolic, Copper
Dimensions
Height 119.4 cm (47 in.), Width 55.9 cm (22 in.), Depth 233.7 cm (92 in.)
Country of Origin
United States of America
See more items in
National Air and Space Museum Collection
Data Source
National Air and Space Museum
Link to Original Record
Record ID
nasm_A19710936000