Hispano-Suiza 8

Origins At the beginning of World War I, 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. The resulting engine, called the Hispano-Suiza 8A (HS-31), made its first appearance in February 1915. The first 8A kept the standard configuration of Birkigt's existing design: eight cylinders in 90° Vee configuration, a displacement of 11.76 litres (717.8 cu in) and a power output of 140 hp at 1,900 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 cylinder blocks were cast aluminium and of monobloc type that is, in one piece with the SOHC cylinder heads. The inlet and exhaust ports were cast into the blocks, the valve seats were in the top face of the steel cylinder liners, which were screwed into the blocks. Using a rotating bevel gear-driven tower shaft 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, valve springs, magnetos, etc. The new engine was presented to the French Ministry of War in February 1915, and tested for 15 hours at full power. This was standard procedure for a new engine design to be admitted into military service. However, because of lobbying by French engine manufacturers, the Spanish-made engine was ordered to undergo a bench test that no French-made engine had yet passed: a 50-hour run at full speed. The HS-31 was therefore sent back to Chalais-Meudon on July 21, 1915, and tested for 50 hours, succeeding against all expectations. The design also promised far more development-potential than rotary engines. This was despite being the most common type, then in use, for most aircraft. French officials ordered production of the 8A to be started as soon as possible and issued a requirement for a new single-seat high-performance fighter aircraft using the new engine. The Louis Béchereau-designed SPAD VII was the result of this requirement and allowed the Allies to regain air superiority over the Germans. ==Production history==

The Hispano-Suiza 8 was the most produced aero engine series of World War I with 49,893 units manufactured during the conflict. The engine continued to be built in smaller numbers during the 1920s. Most of the engines were built under license in factories located in France, the United Kingdom, the United States and Italy. Small numbers of engines were also built in Japan, Spain, Switzerland and the Soviet Union. France In total 35,189 Hispano-Suiza 8 engines were produced in France during World War I. Fourteen French companies produced the engines under license including Ariès, Brasier, Chenard-Walcker, De Dion-Bouton, Peugeot and Voisin. The Hispano-Suiza 8 shared many common parts with the Peugeot 8Aa. Camshafts, piston rings and some bearings were interchangeable. United States In 1915 representatives from the Wright Company approached the French government to negotiate a license for the Hispano-Suiza 8 engine which was then under test. The French government refused to grant a license and instead offered the Peugeot 8Aa as an alternative. Ultimately the Wright company negotiated a license directly with Hispano-Suiza in Barcelona. The Wright company went on to produce 8,976 Hispano-Suiza engines during World War I. It powered the T-24 tank. ==Variants==

Some data from: British Piston Engines and their Aircraft Note: Hispano-Suiza company type numbers were prefixed by HS- or written in full as Hispano-Suiza Type 31, but military designations used the conventional system of Hispano-Suiza(engine manufacturer) 8(no of cylinders) A(engine series) b(variant) r(attribute), thus Hispano-Suiza 8Abr. ;8A (HS-31): , initial production and test engines, with few applications, including early Nieuport 14s. ;8Aa (HS-31) : at 2000 rpm, entered production in July 1915. Early HS-8A engines were plagued with various problems which required further work and was the standard powerplant for early-production SPAD VIIs and the Curtiss "Jenny" JN-4H variants. The demand for the Hispano-Suiza engine was such that other manufacturers began producing it under licence, in France, Great Britain (Wolseley Adder), Italy (Nagliati in Florence and Itala/SCAT in Turin) and Russia. Total production of the HS-8Aa amounted to some 6,000 engines. ;8Ab (HS-34) : at 2,100 rpm, increasing the compression ratio from 4.7 to 5.3, Birkigt was able to increase the power output . The 8Ab began replacing the 8Aa on SPAD VIIs in early 1917. ;8Ac : ;8Ad :(1929) bore x stroke, for take-off. ;8B (HS-35) : , compression ratio 5.3:1, geared at 0.75:1. The HS-36 was the 8B with a Lewis gun firing through the propeller boss. ;8B twin (HS-39):Coupled 8B engines ;8Ba : at 2,300 rpm, low compression ratio of 4.7:1, spur geared at 0.585:1. ;8Bb : , compression ratio of 4.8:1, reduction gear 0.75:1. However the reduction gear system was fragile, and often broke down, sometimes with spectacular results ending up with the entire propeller, driveshaft and driven gear parting company from the airframe. Progressive refinement of the engine brought the available power to by the end of 1917. The 8B, 8Ba and 8Bb were used (a) to power the earliest versions of the S.E.5a, (b) along with the 8Bd, the SPAD S.XIII, (c) front-line active versions of the Sopwith Dolphin, and (d) several other Allied aircraft types, with its gear reduction easily identifiable in vintage World War I photos, from its use of a clockwise (viewed from in front, otherwise known as a left hand tractor) rotation propeller. ;8Bc: , compression ratio of 5.3:1, reduction gear 0.75:1. ;8Bd: , compression ratio of 5.3:1, reduction gear 0.75:1. ;8Bda ;8Be: , compression ratio of 5.3:1, reduction gear 0.75:1. ;8BeC (HS-38): The 8Be fitted with the SAMC Model 37 cannon, or a similar weapon, as an engine gun firing through the propeller boss. A reduction gear equipped power-plant with a resultant clockwise rotation propeller like the 8B, produced at 2,100 rpm. Two known weapons fitted were the SAMC with a rifled barrel and a smooth-bore cannon firing canister ammunition. The moteur-canon could fire a single shot at a time through the hollow drive shaft without propeller interference. This cannon mount required an "elevated" intake manifold design, bringing the intake "runners" straight off the inner surfaces of the cylinder banks to the updraft carburetor's plenum chamber. The engine was used on the SPAD S.XII. ;8Ca/220: engine gun-equipped at 2,100 rpm with 5.3:1 compression. Given the company designation HS Type 38 ;8Cb/180: engine gun-equipped at 2,000 rpm with 4.7:1 compression. Given the company designation HS Type 44 ;8Cc/220: engine gun-equipped at 2,100 rpm with 5.3:1 compression. Given the company designation HS Type 44 ;Hispano-Suiza Type 40: (8E ?) ;Hispano-Suiza Type 41: (8A ?) ;8F (HS-42) : at 2,100 rpm (eq. 750 lb·ft torque). The direct drive 8F was a bored out version of the 8B, intended for use in bombers, with a displacement of . Despite the increased weight of , the 8F was also installed in fighters such as the Nieuport-Delage NiD 29 and Martinsyde Buzzard, and would have powered the never-produced Mk.II version of the Sopwith Dolphin. Engine speed being lower than that of the HS-8B, the reduction gear was deleted, thereby increasing engine reliability. ;8Fa :generally similar to the 8F. ;8Fb : , aka HS Type 42, compression ratio of 5.3:1, direct drive. ;8Fd Special :For the CAMS 38 Schneider Trophy racer developing ;8Fe (HS-42VS) :(1926) bore x stroke, for take-off. ;Wolseley W.4B Adder I :, compression ratio of 4.7 :1, reduction spur gear to 0.593:1. ;Wolseley W.4B Adder II :, compression ratio of 4.7 :1, reduction spur gear to 0.593:1. With stronger crankshaft webs. ;Wolseley W.4B Adder III :, compression ratio of 4.7 :1, reduction spur gear to 0.593:1. With balanced crankshafts. ;Wright-Hisso A:Wright-Martin built Type 34/HS8Aa at 1,400 rpm and 4.72:1 compression. ;Wright-Hisso B: 4-cyl in-line water-cooled ;Wright-Hisso C: geared A ;Wright-Hisso D: geared A with engine gun ;Wright-Hisso E: at 1,700 rpm and 5.33:1 compression(HC 'I') ;Wright-Hisso E-2: (HC 'E') ;Wright-Hisso F: ('D' without engine gun) ;Wright-Hisso H: , based on the Type 42/HS8F ;Wright-Hisso H-2: improved 'H' ;Wright-Hisso I: ;Wright-Hisso K: H with 37mm Baldwin engine gun ;Wright-Hisso K-2: ;Wright-Hisso M: experimental 300 hp ;Wright-Hisso T: ;Wright-Hisso 180 hp V-8: direct drive ;Wright-Hisso 220 hp V-8: geared drive ;Wright-Hisso 300 hp V-8: geared drive ;Wright-Hisso 300 hp V-8: geared drive ;Wright-Hisso V-720 ;M-4: Soviet produced 8Bb ;M-6: Soviet produced 8Fb ;Mitsubishi-Hispano-Suiza 300 hp engine: Imperial Japanese Army produced 8Fb ==Applications==

• Austin-Ball A.F.B.1 (single prototype) • Avia BH-21 (from 1925) • Avia BH-22 • Bartel BM-5 • Bernard SIMB AB 10 • Blanchard Brd.1 • Caudron R.11 (8Bba) • Caudron C.59 • Caudron C.61 (8Ac) • Curtiss JN-4H Jenny (rare subvariant) • De Bruyère C 1 • Descamps 27 (8Fb) • Dewoitine D.1 (8Fb) • Farman F.121 Jabiru (8Ac) • FBA Type H (8Aa) • Felixstowe F.1 • Fokker D.IX • Fokker D.X (8Fb) • Fokker D.XII (8F) initial design only • Fokker S.III • Gourdou-Leseurre GL.21 • Hanriot HD.5 • Hanriot HD.15 • Hanriot HD.20 • Itoh Emi 29 • Letord Let.1 (8A) • Letord Let.2 & Let.3 (8Ba) • Letov Š-7 (8Fb) • Letov Š-13 (8Fb) • Letov Š-14 (8Fb) • Levasseur PL.1 (8Ab) • Martinsyde F.4 Buzzard (8Fb) • Nieuport 14 (8A) • Nieuport-Delage NiD 29 (8Fb) • Nieuport-Delage NiD 38 (8Ab) • Nieuport-Delage Sesquiplan (8Fb) • Royal Aircraft Factory S.E.5 (8Aa) and S.E.5a (8B, 8Ba or 8Bb on earliest versions and the Wolseley Viper derivative on later models) • Sopwith Dolphin (8B) • Sopwith B.1 prototypes (8Ba) • SPAD S.VII (8A) • SPAD S.XI (8Be) • SPAD S.XII (8Cb) • SPAD S.XIII (8Be) • Standard J-1 (post-war modification) • Waco DSO (8a) • Wibault 1 (single prototype) Wright-Hispano E • Boeing NB-2 • AT-3 • Consolidated PT-1 • Cox-Klemin TW-2 • Curtiss AT-4 • Dayton-Wright TW-3 • Huff-Daland TW-5 • Loening M-8 • Naval Aircraft Factory TS-3 • Travel Air 3000 • Vought VE-7 • Waco DSO Mitsubishi "Hi"shiki ;200 HP (8B) • Yokosuka Ro-go Ko-gata • Hanza-shiki suijō teisatsuki (ハンザ式水上偵察機, Type Hansa Surveillance Floatplane) ;300 HP (8F) • Mitsubishi 1MF • Mitsubishi 2MR ==Comparative table==

• A Hispano-Suiza 8Aa Type 34, made in 1916, is on public display at Museo de Aeronáutica y Astronáutica at Madrid, Spain. • A Hispano-Suiza 8Ab, serial number 11934, is on public display at Vaasan Auto- ja moottorimuseo Vaasa Automobile and Motor Museum in Vaasa, Finland. • A Wright-Hisso 8A is on public display at the Aerospace Museum of California. • A Wright-Hisso 8A is on public display at the National Museum of the U.S. Air Force ==Specifications (Hispano-Suiza 8a)==