Renault 70 hp
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The Renault 70 hp or Type WB was a British V-8 aero engine that first ran circa 1913. The engine was manufactured by Renault Limited of West Brompton, London between August 1914 and December 1918, three other companies, including Rolls-Royce, also produced the engine. A variant known as the Type WC used an external oil pump as opposed to the internal pump of the Type WB.[1] 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.[2]
Applications
- Airco DH.1
- Armstrong Whitworth F.K.2
- Armstrong Whitworth S.S.27 airship
- Blackburn Type E
- Bristol B.R.7
- Caudron G.3
- Central Centaur IVA
- Farman MF.7 Longhorn
- Farman Shorthorn
- Flanders F.4
- HMA no.2 airship, short-lived modification
- Royal Aircraft Factory B.E.2
- Royal Aircraft Factory F.E.2
- Royal Aircraft Factory R.E.1
- White & Thompson Bognor Bloater
Specifications (70 hp)
Data from Lumsden [1]
General characteristics
- Type: Inline air–cooled, upright, 90-degree, V-8 piston engine
- Bore: 3.54 in (90 mm)
- Stroke: 4.72 in (120 mm)
- Displacement: 423.76 cu in (7 L)
- Length: 45.5 in (1,156 mm)
- Width: 29.8 in (757 mm)
- Height: 32.8 in (833 mm)
- Dry weight: 396 lb (180 kg)
Components
- Valvetrain: Single overhead exhaust valve, single side inlet valve per cylinder
- Fuel system: Single carburettor
- Fuel type: 40–50 octane petrol
- Cooling system: Air-cooled
- Reduction gear: 0.5:1, left hand tractor
Performance
- Power output: 70 hp (52 kW) at 1,750 rpm (takeoff power)
- Specific power: 0.17 hp/cu in (7.4 kW/L)
- Compression ratio: 4.12:1
- Power-to-weight ratio: 0.18 hp/lb (0.28 kW/kg)
See also
- Related development
- Related lists
References
Notes
Bibliography
- Gunston, Bill. World Encyclopaedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
- Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
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