About: Lycoming XR-7755

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The Lycoming XR-7755 was the largest piston aircraft engine ever built in the United States, with 36 cylinders totaling about 7,750 in³ (127 L) of displacement and a power output of 5,000 horsepower (3,700 kilowatts). It was originally intended to be used in the "European bomber" that eventually emerged as the Convair B-36. Only two examples were built before the project was terminated in 1946.

Attributes	Values
rdf:type	software yago:WikicatLycomingAircraftEngines yago:WikicatWater-cooledRadialEngines yago:AircraftEngine102687423 yago:Artifact100021939 yago:Device103183080 yago:Engine103287733 yago:HeatEngine103507963 yago:Instrumentality103575240 yago:Internal-combustionEngine103579982 yago:Machine103699975 yago:Motor103789946 yago:Object100002684 yago:PhysicalEntity100001930 yago:RadialEngine104040373 yago:Whole100003553 yago:WikicatRadialEngines
rdfs:label	Lycoming XR-7755 (de) Lycoming XR-7755 (fr) Lycoming XR-7755 (en) Lycoming XR-7755 (pt)
rdfs:comment	Lycoming XR-7755 ist die Bezeichnung eines Flugmotors, der zwischen 1943 und 1946 durch den US-amerikanischen Hersteller Lycoming entwickelt wurde. Der XR-7755 markierte den Höhepunkt der Entwicklung von Sternmotoren als Flugmotoren. (de) Le Lycoming XR-7755 est un moteur à pistons pour avions, mis au point pendant la seconde guerre mondiale par l'entreprise américaine Lycoming. Resté à l'état de prototype, il est le plus puissant moteur à piston pour avion jamais testé aux États-Unis. (fr) The Lycoming XR-7755 was the largest piston aircraft engine ever built in the United States, with 36 cylinders totaling about 7,750 in³ (127 L) of displacement and a power output of 5,000 horsepower (3,700 kilowatts). It was originally intended to be used in the "European bomber" that eventually emerged as the Convair B-36. Only two examples were built before the project was terminated in 1946. (en) O Lycoming XR-7755 foi o maior motor aeronáutico a pistão construído nos Estados Unidos, com 36 cilindros, totalizando cerca de 127 L (7,750 in³) de deslocamento e uma potência de 5,000 hp (3,700 kilowatts). Foi originalmente desenhado para equipar o "Bombardeiro europeu" que eventualmente tornou-se o Convair B-36 Peacemaker. Apenas dois motores foram construídos antes do projeto ser cancelado em 1946. (pt)
foaf:depiction
dcterms:subject	Abandoned military aircraft engine projects of the United States Inline radial engines 1940s aircraft piston engines Lycoming aircraft engines Water-cooled radial engines
Wikipage page ID	2126954 (xsd:integer)
Wikipage revision ID	1111074200 (xsd:integer)
Link from a Wikipage to another Wikipage	Pratt & Whitney R-4360 Wasp Major Propeller (aircraft) Engine displacement List of aircraft engines Abandoned military aircraft engine projects of the United States Horsepower Cylinder (engine) United States United States Army Air Forces Radial engine Convair B-36 Contra-rotating propellers Armstrong Siddeley Hyena Inline radial engines Lycoming Engines Lycoming H-2470 Smithsonian Institution Zvezda M503 Fuel injection Ignition magneto Aviation Week & Space Technology 1940s aircraft piston engines Watt Distributor H engine Jet engine Aircraft engine Overhead camshaft Carburetor Crankshaft Hyper engine Armstrong Siddeley Deerhound Junkers Jumo 222 Wright R-2160 Tornado Dobrynin VD-4K Lycoming aircraft engines BMW 803 Water-cooled radial engines Camshaft Poppet valve Variable valve timing Lycoming O-1230 Inline engine (aviation) Vultee XP-54 Wright Field dbr:Yakovlev_M-501
Link from a Wikipage to an external page	http://www.enginehistory.org/ http://archive.aviationweek.com/issue/19461201%23!&pid=86%7Curl-access=registration http://generalaviationnews.com/2007/04/20/the-xr-7755-the-whole-story http://www.aviation-history.com/engines/xr-7755.htm
sameAs	Lycoming XR-7755 Lycoming XR-7755 Lycoming XR-7755 Lycoming XR-7755 Lycoming XR-7755 Lycoming XR-7755 Lycoming XR-7755 Lycoming XR-7755
similar engines	Armstrong Siddeley Hyena Armstrong Siddeley Deerhound Dobrynin VD-4K Wright R-2160 Tornado Junkers Jumo 222 BMW 803 * Pratt & Whitney R-4360 Wasp Major (en)
specfuelcon	* at takeoff power * at 70% power * at minimum cruise power (en)
supercharger	Impeller diameter , at 6:1 drive ratio (en)
valvetrain	Single overhead camshaft per bank with separate cams for takeoff and economical cruise (en)
dbp:wikiPageUsesTemplate	dbt:Cite_book dbt:Cite_magazine dbt:Commons_category dbt:Cvt dbt:Refimprove

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