Renault 80 hp
http://dbpedia.org/resource/Renault_80_hp an entity of type: Software
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 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.
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Renault 80 hp
xsd:integer
24378829
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1061093620
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*Curtiss OX-5
xsd:double
0.15
<inch>
5.12
rdf:langString
Single overhead exhaust valve, single side inlet valve per cylinder.Although this valve arrangement is cited as "one side and one overhead valve," 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 one on its bottom. There are no valves on the combustion chamber or on the overhead position.
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France
<inch>
35.3
<inch>
50.6
xsd:integer
80
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Lumsden
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*RAF 1
*Renault 70 hp
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Air-cooled V-8 piston engine
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Inline air-cooled, upright, 90-degree, V-8 piston engine
<pound>
463.0
<inch>
35.5
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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 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.
<inch>
4.13
xsd:double
4.16
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Air-cooled
xsd:double
548.9
xsd:integer
1914
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Single 32 mm Claudel-Hobson carburettor
xsd:integer
40
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*List of aircraft engines
xsd:integer
2216
xsd:double
0.17
xsd:double
0.5
xsd:nonNegativeInteger
5577