Wright D-1, In-line 6 Engine

Object Details

Physical Description: Type: Reciprocating, 6 cylinders, In-line, Liquid-cooled; Power rating: 261 kW (350 hp) at 1,350 rpm; Displacement: 30.28 L (1,847.26 cu in); Bore and Stroke: 178 mm (7 in.) x 203 mm (8 in.); Weight: 599 kg (1,320 lb)
Summary: As the Wright Brothers naturally sought more powerful engines as their aircraft further developed, they turned to six-cylinder vertical engines around 1911. But later, after merging with another major manufacturer in 1916, the Wright-Martin Company produced Hispano-Suiza V-8 engines under license.; In 1920 Wright-Martin dissolved, with most becoming part of Mack Trucks, while the new Wright Aeronautical Corporation began developing original designs for aviation. These included a special six-cylinder vertical engine for airships which had characteristics of the Maybach dirigible engines used in German Zeppelins. In June 1921, the U.S. Navy placed an order for three of these engines known as the Model D-1. In March 1922, the D-1 completed a 50-hour endurance test. The engine was the largest of its type built up to that time, but never entered production.

Credit Line: Transferred from the U.S. Navy, Naval Supply Center, Cheatham Annex, Williamsburg, Virginia

Circa 1922

Materials: Steel, Aluminum, Copper, Rubber, Glass, Textile, Paint, Plastic, Preservative coating
Dimensions: Height 104.6 cm, 41.19 in., Length 180.6 cm, 71.13 in., Width 56.6 cm, 22.31 in.

National Air and Space Museum

GUID (Link to Original Record): http://n2t.net/ark:/65665/nv958a69f6e-bf4d-441d-b863-7ba0c67a4238