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About: Rolls-Royce Eagle (1944)     Goto   Sponge   NotDistinct   Permalink

An Entity of Type : yago:Whole100003553, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)

Type: mean of transportationyago:WikicatRolls-RoyceAircraftPistonEnginesyago:WikicatSleeveValveEnginesyago:AircraftEngine102687423yago:Artifact100021939yago:Device103183080yago:Engine103287733yago:Instrumentality103575240yago:Machine103699975yago:Motor103789946yago:Object100002684yago:PhysicalEntity100001930yago:Whole100003553 New Facet based on Instances of this Class

The Rolls-Royce Eagle Mk XXII is a British 24-cylinder, sleeve valve, H-block aero engine of 46 litre (2,807 cubic inches) displacement. It was designed and built in the early-1940s by Rolls-Royce Limited and first ran in 1944. It was liquid-cooled, of flat H configuration with two crankshafts and was capable of 3,200 horsepower (2,387 kW) at 18 psi boost.