Renault 70 hp

As with other Renault air cooled V-8s, the engine had an early form of reduction gearing where the propeller was fixed to the end of the camshaft and turned at half engine speed. This method of gearing allowed the engine and propeller to be run close to their optimum speeds without the additional weight penalty of a gearbox. Engines intended for pusher aircraft were fitted with a centrifugal blower which fed cooling air over the large finned cast iron cylinders.{{cite book |last1=Angle |first1=Glenn D. |url=https://archive.org/details/airplaneenginee00anglgoog |title=Airplane Engine Encyclopedia |date=1921 |publisher=The Otterbein Press |location=Dayton, Ohio, USA |pages=412-414}}

Compared to contemporary air cooled rotary engines built by Gnome, the 70 hp Renault had a worse power to weight ratio but better fuel economy.{{cite magazine |last=Laux| first=James M|title=Gnome et Rhône - An Aviation Engine Firm in the First World War: Le Rhône|magazine=Aerospace Historian|publisher=Air Force Historical Foundation |date=March 1980|volume=27|issue=1|page=19-26}} Aircraft powered by the Renault 70 hp set distance and duration records in 1912.

The first military orders were placed in 1911 with 81 engines delivered to the French army for use in Farman observation aircraft. In 1912 Farman aircraft powered by the Renault 70 hp equipped two out of the five French squadrons.

In the UK the 70 hp air cooled V8 model was manufactured by Renault’s UK subsidiary and their licensees; Rolls Royce, Wolseley and Airco. Renault refused to sell licenses to German firms in the years before WW1.

Data from Wolseley Motors's 1917 instruction manual. Weights shown include flywheel, exhaust branches, cowl and propeller boss.{{cite document |date=1917 |title=Instruction Manual for Wolseley Aero Engines (Wolseley-Renault Types)|location=United Kingdom |publisher=Wolseley Motors}}

Type W.B - Version with internal lube oil pump. Dry weight: {{convert|440|lb|kg|abbr=on|0}}

Type W.C - Version with external lube oil pump. Dry weight: {{convert|440|lb|kg|abbr=on|0}}

Both the W.B and W.C variants were available for pusher (propeller at back) and tractor (propeller at front) aircraft. Engines fitted to tractor aircraft had a cowl scoop which directed part of the propellers air steam across the cylinders. Engines fitted to pusher aircraft were equipped with a back mounted (opposite end from prop) centrifugal blower. The blower added an extra {{convert|50|lb|kg|abbr=on|1}} of weight and consumed {{convert|4|hp|kW|abbr=on|1}}.

Type W.X - 75 hp variant. Outwardly almost identical to the 70 hp models but with a larger 100mm cylinder bore and redesigned connecting rods. The connecting rods used the same side by side layout as the 70 hp model but had a two stud design and were interchangeable between left and right cylinder banks. Available in tractor configuration only. Dry weight: {{convert|455|lb|kg|abbr=on|0}}

• Airco DH.1
• Armstrong Whitworth F.K.2
• SS class airships
• Blackburn Type E
• Bristol B.R.7
• Central Centaur IVA
• Farman MF.7 Longhorn
• Farman MF.11 Shorthorn
• Flanders F.4
• Royal Aircraft Factory B.E.2
• Royal Aircraft Factory F.E.2
• Royal Aircraft Factory R.E.1
• White & Thompson Bognor Bloater

{{pistonspecs

|

|type=Inline air–cooled, upright, 90-degree, V-8 piston engine

|ref= Lumsden{{Cite book |last=Lumsden |first=Alec |title=British Piston Engines and their Aircraft |date=2002 |publisher=Airlife Publishing |isbn=1853102946 |pages=180 |language=en}} and Angle.

Note: Figures are for British built W.B variant designed to be mounted in tractor configuration.

|bore=3.78 in (96 mm)

|stroke=4.72 in (120 mm)

|displacement=423.76 cu in (7 L)

|length=45.5 in (1,156 mm)

|diameter=

|width=29.8 in (757 mm)

|height=32.8 in (833 mm)

|weight= 396 lb (180 kg)

|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.

|supercharger=

|turbocharger=

|fuelsystem=Single carburettor

|fueltype=40–50 octane petrol

|oilsystem=

|coolingsystem=Air-cooled

|power=70 hp (52 kW) at 1,750 rpm

|specpower=0.17 hp/cu in (7.4 kW/L)

|compression=4.12:1

|fuelcon= 7.25 gallon/hr (27.4 L/hr)

|specfuelcon={{cvt|0.64|lb/hph|kg/kWh|2}}

|oilcon= 6.5 pints/hr (3 L/hr)

|power/weight= 0.18 hp/lb (0.28 kW/kg)

|designer=

|reduction_gear=0.5:1, left hand tractor (there is no reduction gear as such; The reduction is achieved by mounting the propeller on the camshaft).

|general_other=

|components_other=

|performance_other=

}}

{{aircontent

|see also=

|lists=

• List of aircraft engines

|similar engines=

}}

{{reflist}}

{{Commons category}}

• [https://digitaltmuseum.no/021015546292 Photo "Flymotor Type 70 hk Renault" (side view)], Norsk Luftfartsmuseum
• [https://digitaltmuseum.no/021015546294 Photo "Flymotor Type 70 hk Renault" (front view)], Norsk Luftfartsmuseum

{{Renault aeroengines}}

Category:1910s aircraft piston engines

70