Bugatti U-16
http://dbpedia.org/resource/Bugatti_U-16 an entity of type: WikicatBugattiAircraftEngines
The Bugatti U-16 was a 16-cylinder water-cooled double-8 vertical in-line "U engine", designed by Ettore Bugatti in 1915-1916 and built in France in small numbers. The US Bolling Commission bought a license to build the engine in the US, and small numbers of a slightly revised version were built by the Duesenberg Motor Corporation as the King-Bugatti. Probably about 40 King-Bugattis were made before the end of World War I caused building contracts to be canceled.
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Le moteur Bugatti U-16 ou King-Bugatti U-16 ou Bugatti-Breguet U-16 est une série de moteurs d'avions du constructeur automobile Bugatti, conçu en 1916, pour la Première Guerre mondiale, et entre-deux-guerres, de 16 cylindres en U (2 × 8 cylindres en ligne) de 410 ch (et variantes démultipliées, couplés par 2 ou par 3 en H).
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Bugatti U-16
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King-Bugatti U-16
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24159214
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1106295828
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Split overhead camshaft per cylinder bank operating 3 valves per cylinder , driven by a shaft and bevel gers from the centre of the crankshaft.
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Ettore Bugatti and Col. Charles King
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about
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about
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at 2,000 rpm
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Jane's fighting aircraft of World War I, Jane's All the World's Aircraft 1919 except where indicated. Later specifications quote slightly varied detail dimensions and increased horsepower ratings.
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16
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about
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The Bugatti U-16 was a 16-cylinder water-cooled double-8 vertical in-line "U engine", designed by Ettore Bugatti in 1915-1916 and built in France in small numbers. The US Bolling Commission bought a license to build the engine in the US, and small numbers of a slightly revised version were built by the Duesenberg Motor Corporation as the King-Bugatti. Probably about 40 King-Bugattis were made before the end of World War I caused building contracts to be canceled.
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Le moteur Bugatti U-16 ou King-Bugatti U-16 ou Bugatti-Breguet U-16 est une série de moteurs d'avions du constructeur automobile Bugatti, conçu en 1916, pour la Première Guerre mondiale, et entre-deux-guerres, de 16 cylindres en U (2 × 8 cylindres en ligne) de 410 ch (et variantes démultipliées, couplés par 2 ou par 3 en H).
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4
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5
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Water-cooled
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1916
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4
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Petrol
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*List of aircraft engines
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Dry sump, one scavenging pump and one pressure pump each driven from the front ends of the camshafts
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0.42
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0.6666
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13008
