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SPECO XB-4070-2 Diesel 9 Barrel Engine

Air and Space Museum

Object Details

Manufacturer

Steel Products Engineering Corporation (SPECO)

Physical Description

Type: Reciprocating, 9 cylinders, barrel-type, two-stroke, supercharged, Diesel, liquid-cooled
Power rating: 1,491 kW (2,000 hp) at 1,750 rpm
Displacement: Unknown
Bore and Stroke: Unknown
Weight: 975.2 kg (2,150 lb)

Summary

In June 1939, the U.S. Navy placed a contract with the Steel Products Engineering Co. (SPECO) of Springfield, Ohio for one XB-4070-2 barrel engine, a concept also tried elsewhere, but never fully successful. In a barrel engine, the cylinders are parallel to the engine driveshaft and arranged radially around it; therefore producing a small frontal area. This version incorporated 9 cylinders having 18 opposed pistons, with the pistons rotating slowly to insure uniform heating and avoid thermal distortion. A swashplate (an inclined disc) located on the driveshaft in the center of the engine converted piston thrust to torque. This arrangement is inherently very compact and light in weight. However, the bearing problems involved in the swashplate mechanism were difficult to solve and did not result in a good high-output engine.

Credit Line

Transferred from the U.S. Navy

Date

Circa 1942

Inventory Number

A19710890000

Restrictions & Rights

Usage conditions apply

Type

PROPULSION-Reciprocating & Rotary

Materials

Steel
Non Magnetic Alloy
Paint
Rubber
Aluminum
Copper Alloy
Cadmium Plating
Masking Tape

Dimensions

Length 188 cm (74 in.), Diameter 88.9 cm (35 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

Metadata Usage

Not determined

Link to Original Record

http://n2t.net/ark:/65665/nv99381fe0d-30ec-4e62-a598-93f39b2b4bf9

Record ID

nasm_A19710890000

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