Bristol Taurus

Bristol had originally intended to use the Aquila and Perseus as two of its major product lines in the 1930s, but the rapid increase in size and speed of aircraft in the 1930s demanded much larger engines. The mechanicals from both of these designs were then put into two-row configurations to develop much larger engines, the Aquila becoming the Taurus, and the Perseus becoming the Hercules.

The Taurus used sleeve valves, resulting in an uncluttered exterior and little mechanical noise. It offered high power with a relatively low weight, starting from {{cvt|1015|hp}} in the earliest versions. It was also compact, with a diameter of {{cvt|46|in|mm}} which made it attractive for fighters. Unfortunately, the engine was also described as "notoriously troublesome", with protracted development and a slow growth in rated power. After several years of development, power had only increased from {{cvt|1015|hp}} to {{cvt|1130|hp}}. As the most important applications of this engine was in aircraft that flew at low altitude, development efforts focused on low-altitude performance.

The first Taurus engines were delivered just before World War II, and was used primarily in the Fairey Albacore and Bristol's Beaufort. In April 1940, a suggestion was made to replace the Taurus engines of the latter with the Pratt & Whitney R-1830 Twin Wasp, which had a slightly larger {{cvt|48|in}} diameter, but this change was postponed to the autumn of 1941 while attempts were made to cure the Taurus's reliability problems, and later had to be temporarily reversed because of shortages of Twin Wasps. The Twin Wasp was, however, strongly preferred, especially for overseas postings, because of its better reliability. The reliability problems were mostly cured in later models of the Taurus engine by a change in the cylinder manufacturing process, although the engine reputation never recovered, and in the Albacore the Taurus engine was used until the end of that aircraft's production in 1943.Lumsden 2003, p.115.

There were no other operational applications of the Taurus engine, because its initial reliability problems discouraged development of Taurus-powered aircraft, and because later-war combat aircraft demanded more powerful engines. Production ended in favour of the Hercules engine.

• Taurus II (1940) – {{cvt|1140|bhp|kW}} maximum power with {{cvt|4.25|psi|kPa}} boost at 3,225 rpm for take off or one minute using 87 octane fuel. Medium supercharged.{{sfnp|Lumsden|1994|p=118}}
• Taurus III – {{cvt|935| hp|kW}} maximum continuous power, medium supercharged, compression ratio 7.2:1.{{sfnp|Lumsden|1994|p=119}}
• Taurus VI – {{cvt|985|hp|kW}} maximum continuous power, medium supercharged, compression ratio 7.2:1.{{sfnp|Lumsden|1994|p=119}}
• Taurus XII (1940) – {{cvt|985|hp|kW}} maximum continuous power, medium supercharged, compression ratio 7.2:1.{{sfnp|Lumsden|1994|p=119}}
• Taurus XVI (1940) – {{cvt|985|hp|kW}} maximum continuous power, medium supercharged, compression ratio 7.2:1.{{sfnp|Lumsden|1994|p=119}}
• Taurus XX – trials engine only, one built.{{sfnp|Lumsden|1994|p=119}}

Note:List from Lumsden, the Taurus may not be the main powerplant for these aircraft types

File:Gloster f9 37.jpg

• Bristol Type 148
• Bristol Beaufort
• Fairey Albacore
• Fairey Battle testbed only
• Gloster F.9/37

{{pistonspecs

|

|ref=Lumsden.Lumsden 2003, p.118.

|type=14-cylinder, two-row, supercharged, air-cooled radial engine with dual ignition

|bore={{convert|5|in|mm|0|abbr=on}}

|stroke={{convert|5.625|in|mm|0|abbr=on}}

|displacement={{convert|1,550|cuin|L|abbr=on}}

|length={{convert|49.2|in|mm|abbr=on}}

|diameter={{convert|46.25|in|mm|abbr=on}}

|width=

|height=

|weight={{convert|1,301|lb|kg}}

|valvetrain=Sleeve valve

|supercharger=Single-speed centrifugal type supercharger

|turbocharger=

|fuelsystem=Claudel-Hobson carburettor

|fueltype=87 Octane petrol

|oilsystem=

|coolingsystem=Air-cooled

|power=

• {{convert|1,140|hp|kW|abbr=on}} at 3,225 rpm for takeoff
• {{convert|1,050|hp|kW|abbr=on}} at 3,225 rpm at {{convert|5,000|ft|m|abbr=on}}

|specpower=0.68 hp/in³ (30.83 kW/L)

|compression=7.2:1

|fuelcon=

|specfuelcon=0.43 lb/(hp·h) (261 g/(kW·h))

|oilcon=

|power/weight=0.81 hp/lb (1.33 kW/kg)

|reduction_gear=Farman epicyclic gearing, 0.444:1

}}

{{aircontent

|see also=

|related=

• Bristol Aquila

|similar aircraft=

|lists=

• List of aircraft engines

|similar engines=

• Fiat A.74
• Gnome-Rhône 14N
• Mitsubishi Kinsei
• Nakajima Sakae
• Piaggio P.XIX
• Pratt & Whitney R-1830 Twin Wasp
• Shvetsov ASh-82
• Tumansky M-88

}}

{{Commons category|Bristol Taurus}}

{{reflist}}

• Gunston, Bill (2006). World Encyclopedia of Aero Engines: From the Pioneers to the Present Day. 5th edition, Stroud, UK: Sutton.{{ISBN|0-7509-4479-X}}
• {{cite book |last=Lumsden |first=Alec |date=1994 |title=British Piston Engines and Their Aircraft |location=Shrewsbury |publisher=Airlife Publishing Ltd |isbn=1-85310-294-6}}.
• White, Graham (1995). Allied Aircraft Piston Engines of World War II: History and Development of Frontline Aircraft Piston Engines Produced by Great Britain and the United States During World War II. Warrendale, Pennsylvania: SAE International. {{ISBN|1-56091-655-9}}

{{Bristol aeroengines}}

Category:Aircraft air-cooled radial piston engines

Taurus

Category:Sleeve valve engines

Category:1930s aircraft piston engines