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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.

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  • Renault 80 hp (en)
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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. (en)
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  • http://commons.wikimedia.org/wiki/Special:FilePath/Renault_80.jpg
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similar engines
  • *Curtiss OX-5 (en)
specpower
stroke
valvetrain
  • 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. (en)
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national origin
  • France (en)
height
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power
ref
  • Lumsden (en)
related
  • *RAF 1 *Renault 70 hp (en)
type
  • Air-cooled V-8 piston engine (en)
  • Inline air-cooled, upright, 90-degree, V-8 piston engine (en)
weight
width
has 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 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. (en)
bore
compression
coolingsystem
  • Air-cooled (en)
developed from
displacement
first run
fuelsystem
  • Single 32 mm Claudel-Hobson carburettor (en)
fueltype
lists
  • *List of aircraft engines (en)
major applications
number built
power/weight
reduction gear
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