 {|  |} the hispano-suiza 8 was a water-cooled v8 sohc aero engine introduced by hispano-suiza in 1914 and was the most commonly used engine in the aircraft of the entente powers during the first world war. the original hispano-suiza 8a was rated at 140&nbsp;hp (102&nbsp;kw) and the later hispano-suiza 8f reached 300&nbsp;hp (220&nbsp;kw). hs-8 engines and variants produced by hispano-suiza and other companies under licence were built in twenty-one factories in spain, france, britain, italy, and the u.s.browne, t.c. "retrospect: 1924 hispano-suiza h6c speedster", motor trend, 4/84, p.118. derivatives of the engine were also used abroad to power numerous aircraft types and the engine can be considered as the ancestor of another successful engine by the same designer, the hispano-suiza hs-12y (and soviet klimov v12 derivative aero-engines) which served in world war ii. ==design and development== ===origins=== when world war i began, the production lines of the barcelona based hispano-suiza automobile and engine company were switched to the production of war materiel. chief engineer marc birkigt led work on an aircraft engine based on his successful v8 automobile engine.one prototype of this aircraft engine is preserved in spanish museum "museo de aeronÃ¡utica y astronÃ¡utica" in madrid. the resulting engine, called the hispano-suiza 8a (or hs-8a), made its first appearance in february 1915. the first 8a kept the standard configuration of birkigt's existing design: eight cylinders in 90Â° vee configuration, a displacement of 11.76&nbsp;litres (717.8 cu in) and a power output of 140&nbsp;hp at 1,900&nbsp;rpm. in spite of the similarities with the original design, the engine had been substantially refined. the crankshaft was machined from a solid piece of steel. the cylinders were cast aluminium with steel liners. the sohc cylinder heads were also made of aluminium, using a rotary driveshaft (tower gear) coming up from the crankcase along the rear end of each cylinder bank, with the final drive for each cylinder bank's camshaft accommodated within a semicircular bulge at the rear end of each valve cover. aluminium parts were coated in vitreous enamel to reduce leakage. all parts subject to wear, and those critical for engine ignition were duplicated: spark plugs for dual ignition reliability
Aircraft_piston_engines_1910a1919 Hispano-Suiza_aircraft_engines