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- Renault_80_hp abstract "The Renault 80 hp, or Type WS in British service, was a V-8 aero engine that first ran in 1914. The engine was manufactured in Britain by Renault Limited of West Brompton, London between August 1914 and December 1918, seven other companies, including Rolls-Royce and Brazil Straker, also produced the engine. The Renault V-8 engines were noted as inefficient but reliable, the inefficiency being mainly due to the excessively rich fuel/air mixture used to assist cooling.".
- Renault_80_hp wikiPageID "24378829".
- Renault_80_hp wikiPageLength "4780".
- Renault_80_hp wikiPageOutDegree "25".
- Renault_80_hp wikiPageRevisionID "682577995".
- Renault_80_hp wikiPageWikiLink Airco_DH.6.
- Renault_80_hp wikiPageWikiLink Alliance_P.1.
- Renault_80_hp wikiPageWikiLink Avro_548.
- Renault_80_hp wikiPageWikiLink Brazil_Straker.
- Renault_80_hp wikiPageWikiLink Canada_Aviation_Museum.
- Renault_80_hp wikiPageWikiLink Canada_Aviation_and_Space_Museum.
- Renault_80_hp wikiPageWikiLink Category:Aircraft_piston_engines_1910–1919.
- Renault_80_hp wikiPageWikiLink Category:Renault_aircraft_engines.
- Renault_80_hp wikiPageWikiLink Caudron_G.3.
- Renault_80_hp wikiPageWikiLink Farman_MF.11.
- Renault_80_hp wikiPageWikiLink Gasoline.
- Renault_80_hp wikiPageWikiLink List_of_aircraft_engines.
- Renault_80_hp wikiPageWikiLink Octane_rating.
- Renault_80_hp wikiPageWikiLink RAF_1.
- Renault_80_hp wikiPageWikiLink Renault.
- Renault_80_hp wikiPageWikiLink Renault_70_hp.
- Renault_80_hp wikiPageWikiLink Renault_Limited.
- Renault_80_hp wikiPageWikiLink Rolls-Royce_Limited.
- Renault_80_hp wikiPageWikiLink Royal_Aircraft_Factory_S.E.5.
- Renault_80_hp wikiPageWikiLink Straker-Squire.
- Renault_80_hp wikiPageWikiLink V8_engine.
- Renault_80_hp wikiPageWikiLink Vickers_E.F.B.7.
- Renault_80_hp wikiPageWikiLink West_Brompton.
- Renault_80_hp wikiPageWikiLinkText "80 hp".
- Renault_80_hp wikiPageWikiLinkText "Renault 80 hp".
- Renault_80_hp wikiPageWikiLinkText "Renault 80hp 8Ca".
- Renault_80_hp wikiPageWikiLinkText "Renault engine".
- Renault_80_hp wikiPageWikiLinkText "Renault piston engine".
- Renault_80_hp bore "4.13".
- Renault_80_hp compression "4.16".
- Renault_80_hp coolingsystem "Air-cooled".
- Renault_80_hp developedFrom Renault_70_hp.
- Renault_80_hp displacement "548.9".
- Renault_80_hp fuelsystem "Single 32 mm Claudel-Hobson carburettor".
- Renault_80_hp fueltype "40".
- Renault_80_hp hasPhotoCollection Renault_80_hp.
- Renault_80_hp height "35.3".
- Renault_80_hp length "50.6".
- Renault_80_hp lists "*List of aircraft engines".
- Renault_80_hp majorApplications Airco_DH.6.
- Renault_80_hp majorApplications Royal_Aircraft_Factory_S.E.5.
- Renault_80_hp manufacturer Renault.
- Renault_80_hp nationalOrigin "France".
- Renault_80_hp numberBuilt "2216".
- Renault_80_hp power "80".
- Renault_80_hp weight "0.17".
- Renault_80_hp reductionGear "0.5".
- Renault_80_hp ref "Lumsden".
- Renault_80_hp related "*RAF 1 *Renault 70 hp".
- Renault_80_hp specpower "0.15".
- Renault_80_hp stroke "5.12".
- Renault_80_hp type "Air-cooled V-8 piston engine".
- Renault_80_hp type "Inline air-cooled, upright, 90-degree, V-8 piston engine".
- Renault_80_hp valvetrain "Single overhead exhaust valve, single side inlet valve per cylinder.Although this valve arrangement is cited as "one side and one overhead valve" it should be noted that both valves are situated in a lateral pocket from/to which gases flow. Therefore both valves are "side valves" one on top of this lateral pocket and on on its bottom. There are no valves on the combustion chamber or on the overhead position.".
- Renault_80_hp weight "463.0".
- Renault_80_hp width "35.5".
- Renault_80_hp wikiPageUsesTemplate Template:Aircontent.
- Renault_80_hp wikiPageUsesTemplate Template:Globalize.
- Renault_80_hp wikiPageUsesTemplate Template:Infobox_Aircraft_Engine.
- Renault_80_hp wikiPageUsesTemplate Template:Pistonspecs.
- Renault_80_hp wikiPageUsesTemplate Template:Refbegin.
- Renault_80_hp wikiPageUsesTemplate Template:Refend.
- Renault_80_hp wikiPageUsesTemplate Template:Reflist.
- Renault_80_hp wikiPageUsesTemplate Template:Renault_aeroengines.
- Renault_80_hp subject Category:Aircraft_piston_engines_1910–1919.
- Renault_80_hp subject Category:Renault_aircraft_engines.
- Renault_80_hp hypernym Engine.
- Renault_80_hp type Article.
- Renault_80_hp type Software.
- Renault_80_hp type Article.
- Renault_80_hp comment "The Renault 80 hp, or Type WS in British service, was a V-8 aero engine that first ran in 1914. The engine was manufactured in Britain by Renault Limited of West Brompton, London between August 1914 and December 1918, seven other companies, including Rolls-Royce and Brazil Straker, also produced the engine. The Renault V-8 engines were noted as inefficient but reliable, the inefficiency being mainly due to the excessively rich fuel/air mixture used to assist cooling.".
- Renault_80_hp label "Renault 80 hp".
- Renault_80_hp sameAs m.07s5p02.
- Renault_80_hp sameAs Q7312721.
- Renault_80_hp sameAs Q7312721.
- Renault_80_hp wasDerivedFrom Renault_80_hp?oldid=682577995.
- Renault_80_hp isPrimaryTopicOf Renault_80_hp.