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Deschamps Diesel Inverted V-12 Engine

Catalog Data

Designer:
D.J. Deschamps  Search this
Manufacturer:
Lambert Engine and Machine Company  Search this
Materials:
Steel, Aluminum, Paint, Rubber, Copper
Dimensions:
Length 266.7 cm (105 in.), Width 67.3 cm (26.5 in.), Height 125.9 cm (49.565 in.) (approximate dimensions)
Type:
PROPULSION-Reciprocating & Rotary
Country of Origin:
United States of America
Date:
Circa 1934
Physical Description:
Type: Reciprocating, 12 cylinders, V-type, Two-stroke cycle, Diesel, Inverted, Liquid cooled, supercharged
Power rating: 895 kW (1,200 hp) at 1,600 rpm
Displacement: 50 L (3,052 cu in)
Bore and Stroke: 152 mm (6 in.) x 229 mm (9 in.)
Weight (dry): 1,089 kg (2,400 lb)
Summary:
In 1929, D. J. Deschamps, formerly associated with a Belgian manufacturer, constructed a 2-cylinder Diesel test engine. Later, in early 1934, it was announced that Deschamps had designed a Diesel aircraft engine, designated V 3050 for its V-type and displacement. Built by the Lambert Engine and Machine Company in Moline, Illinois, as an experimental airship or trans-oceanic flying boat engine, it was one of the largest Diesel types for aircraft proposed up to that time.
Utilizing a liquid-cooled, two-stroke cycle, the inverted V-12 Diesel Deschamps engine also incorporated direct fuel injection and dual General Electric superchargers. Due to the narrow angle between its cylinder banks, it had a low frontal area. In order to accommodate airship requirements, the engine was fully reversible when operating. While a technically promising engine, financial difficulties prevented continued development and flight testing.
Credit Line:
Transferred from the U.S. Navy
Inventory Number:
A19710926000
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv9eecaf063-7aa5-4146-9112-679fd80385da
EDAN-URL:
edanmdm:nasm_A19710926000