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About: Rolls-Royce Crecy     Goto   Sponge   NotDistinct   Permalink

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

Type: Thingyago:WikicatTurbo-compoundEnginesyago:WikicatTwo-strokeAircraftPistonEnginesyago:WikicatRolls-RoyceAircraftPistonEnginesyago:WikicatSleeveValveEnginesyago:AircraftEngine102687423yago:Artifact100021939yago:Device103183080yago:Engine103287733yago:Instrumentality103575240yago:Machine103699975yago:Motor103789946yago:Object100002684yago:PhysicalEntity100001930universityyago:Whole100003553 New Facet based on Instances of this Class

The Rolls-Royce Crecy was a British experimental two-stroke, 90-degree, V12, liquid-cooled aero-engine of 1,593.4 cu.in (26.11 L) capacity, featuring sleeve valves and direct petrol injection. Initially intended for a high-speed "sprint" interceptor fighter, the Crecy was later seen as an economical high-altitude long-range powerplant. Developed between 1941 and 1946, it was among the most advanced two-stroke aero-engines ever built. The engine never reached flight trials and the project was cancelled in December 1945, overtaken by the progress of jet engine development.