Renault 70 hp

Design and development

As with other Renault air cooled V-8s, the engine has an early form of reduction gearing where the propeller is fixed to the end of the camshaft and turns 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.

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

Variants

Data from Wolseley Motors's 1917 instruction manual. Weights shown include flywheel, exhaust branches, cowl and propeller boss.

Type W.B - Version with internal lube oil pump. Dry weight: 440 lb

Type W.C - Version with external lube oil pump. Dry weight: 440 lb

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 50 lb of weight and consumed 4 hp.

Type W.X - 75 hp variant. Outwardly almost identical to the 70 hp models but with a larger 100 mm 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. Same external lube oil pump design as the type W.C. Dry weight: 455 lb. Nominal power output: 75 hp. Actual power output: 80 hp at 1,800 rpm.

Applications

• Airco DH.1
• Armstrong Whitworth F.K.2
• SS class airships
• Blackburn Type E
• Breguet Type IV
• 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
• Savary Hydroaéroplane
• White & Thompson Bognor Bloater

Survivors

• Norsk Teknisk Museum, Oslo

Specifications (70 hp)

| and start a new, fully formatted line with -- Note: Figures are for British built W.B variant designed to be mounted in tractor configuration. |power/weight= 0.19 lb/hp

References

References

1. Hartmann, Gerard. (2005). "Les moteurs d’aviation Renault".
2. Boyne, Walter J. (July 2011). "The Influence of Airpower on the Marne".
3. (1921). "Airplane Engine Encyclopedia". The Otterbein Press.
4. Laux, James M. (March 1980). "Gnome et Rhône - An Aviation Engine Firm in the First World War: Le Rhône". Air Force Historical Foundation.
5. (1917). "Instruction Manual for Wolseley Aero Engines (Wolseley-Renault Types)". Wolseley Motors.
6. (August 2014). "Norsk Teknisk Museum".
7. Lumsden, Alec. (2002). "British Piston Engines and their Aircraft". Airlife Publishing.