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Hispano Suiza 18R

18R
Hispano-Suiza 18 Sbr (MAE).JPG
Hispano-Suiza 18Sbr W-18 engine on display in the Musée de l’Air et de l’Espace in Le Bourget, France.
Type W-18 high performance Aeor-engine
National origin France
Manufacturer Hispano-Suiza
First run 1929
Major applications
Developed from Hispano-Suiza 12N

The Hispano-Suiza 18R was an eighteen cylinder high performance water-cooled piston engine, in an 80° W or broad arrow layout, for use in racing aircraft, built in France during the latter half of the 1920s.

After failing to enter the Schneider Trophy seaplane race for several years, the French Ministère de l’Air decided to enter the 1929 competition. Two companies were tasked with designing and building floatplane racers to compete with the entries from Italy and Great Britain, resulting in the Nieuport-Delage NiD-450 and Bernard H.V.120, both of which were powered by the specially designed Hispano-Suiza 18R engines.

To power the racers Hispano-Suiza married three six cylinder blocks from the Hispano-Suiza 12Nb to a common crankshaft / crankcase, set at 80° to each other. Retaining the 150 mm (5.91 in) bore and 170 mm (6.69 in) stroke of the 12Nb, the 18R had the compression ratio increased from 6.25:1 to 10:1 with a total displacement of 54.075L (3,299.8ci). Each cylinder aspirated through two valves operated by single overhead cam-shafts with ignition from two spark plugs set on opposite sides of the combustion chamber supplied by magnetos at the rear of the engine. Fuel metering was carried out by nine carburetors each supplying two cylinders.

Construction of the 18R was largely of Elektron magnesium alloy for body components with high strength steels for highly loaded parts such as the crankshaft. In common with many multiple bank and radial engines the pistons were connected to the crankshaft via master and slave connecting rods; the central vertical bank was served by the master rod which housed the big-end bearing with connecting rods articulating from this to the other two banks. The 18R was available with or without a Farman (bevel planetary) reduction gear.

Development issues delayed production of the engine, with the first geared drive engine delivered to Nieuport-Delage in October 1929, a month after the 1929 Schneider Trophy race. Despite the effort put into its development the 18R proved to be unreliable and unable to achieve the expected power output. The poor performance of the 18R prompted the development of the 18S, a de-rated version intended for commercial use. Reducing the compression ratio to 6.2:1 at a maximum rpm of 2,000 and replacing the Elektron with aluminium alloy, the 18S was available with or without the Farman reduction gear, but was not a success, only powering the Ford 14A in the pylon mounted central nacelle.


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