Like other Bristol sleeve valve engines, the Centaurus was based on the design knowledge acquired from an earlier design, in this case the Bristol Perseus cylinder. The Centaurus used 18 Perseus cylinders. The same cylinder was in use in the contemporary 14-cylinder Hercules, which was being brought into production when the design of the Centaurus started.^[1]

The Centaurus had a cylinder swept volume of 3,272 cu in (53.6 L), nearly as much as the American 3,347.9 cu in (54.9 L) Wright R-3350 Duplex-Cyclone large radial, making the Centaurus one of the largest aircraft piston engines to enter production, while that of the Hercules was 2,363 cu in (38.7 L). The nearly 40 per cent higher capacity was achieved by increasing the stroke from 6.5 to 7 inches (165 to 178 mm) and by changing to two rows of nine cylinders instead of two rows of seven. The diameter of the Centaurus was only just over 6 per cent greater than the Hercules in spite of its much greater swept volume.^[2]

The cylinder heads had an indentation like an inverted top hat, which was finned, but it was difficult to get air down into this hollow to adequately cool the head. During development, Bristol contacted ICI Metals Division, Birmingham, to enquire whether a copper-chromium alloy with higher thermal conductivity would have sufficient high temperature strength to be used for this purpose. With the same cylinder volume and using the new material, the horsepower per cylinder was raised from 110 hp (82 kW) to 220 hp (160 kW).

Bristol maintained the Centaurus from type-testing in 1938, but production did not start until 1942, owing to the need to get the Hercules into production and improve the reliability of the entire engine line.^[2] Nor was there any real need for the larger engine at this early point in the war, when most military aircraft designs had a requirement for engines of about 1,000 hp (746 kW). The Hercules power of about 1,500 hp (1,119 kW) was better suited to the existing airframes.

The Centaurus did not enter service until near the end of the war, first appearing on the Vickers Warwick. Other wartime, or postwar, uses included the Bristol Brigand and Buckmaster, Hawker Tempest and Sea Fury and the Blackburn Firebrand and Beverley. The engine also entered service after the war in a civilian airliner, the Airspeed Ambassador and was also used in the Bristol Brabazon I Mark 1 prototype aircraft until the Brabazon trans-Atlantic airliner programme was cancelled. The eight Centaurus engines were to be replaced with eight Bristol Proteus gas turbines on the Mark II giving a 100 mph faster cruising speed at 10,000 ft higher altitude.^[3] By the end of the war in Europe, around 2,500 examples of the Centaurus had been produced by Bristol.^[2]

The 373 was the most powerful version of the Centaurus and was intended for the Blackburn Beverley transport aircraft. Using direct fuel injection, it achieved a remarkable 3,220 hp (2,400 kW), but was never fitted.^[4] A projected enlarged capacity version of the Centaurus was designed by Sir Roy Fedden; cylinders were produced for this engine, but it was never built. Known as the Bristol Orion, a name used previously for a variant of the Jupiter engine and later re-used for a turboprop, this development was also a two-row, 18 cylinder sleeve valve engine, with the displacement increased to 4,142 cu in (67.9 L)} (6.25 in × 7.5 in (159 mm × 191 mm)), nearly as large as the American Pratt & Whitney R-4360 Wasp Major four-row, 28-cylinder radial, the largest displacement aviation radial engine ever placed in quantity production.^[5]

The Centaurus was produced in 34 variants, ranging from the 2,000 hp (1,500 kW) Centaurus I to the final 2,405 hp (1,793 kW) Centaurus 663 for the Airspeed Ambassador airliner. The most powerful variants to enter service were the 2,625 hp (1,957 kW) Centaurus 170, 173, 660, 661 and 662.^[6]

Note:^[7]

The Royal Navy Historic Flight operated a Hawker Sea Fury powered by a Bristol Centaurus engine^[8] until it was destroyed in an accident on 28 April 2021 whilst attempting a forced landing following a failure and seizure of its Bristol Centaurus XVIII engine:

https://assets.publishing.service.gov.uk/media/628cd96cd3bf7f1f47c65ebc/Hawker_Sea_Fury_T_Mk_20_G-RNHF_07-22.pdf

Preserved Bristol Centaurus engines are on public display at the following museums:

• Aerospace Bristol
• Aerospace Museum of California
• Fleet Air Arm Museum
• Imperial War Museum Duxford
• London Science Museum
• Midland Air Museum
• Shuttleworth Collection, Old Warden
• Dumfries and Galloway Aviation Museum
• San Diego Air & Space Museum

Data from Lumsden^[9]

General characteristics

• Type: 18-cylinder, air-cooled, two-row radial engine
• Bore: 5.75 in (146 mm)
• Stroke: 7.00 in (178 mm)
• Displacement: 3,270 cu in (53.6 L)
• Diameter: 55.3 in (1,400 mm)
• Dry weight: 2,695 lb (1,222 kg)

Components

• Valvetrain: Sleeve valve, four ports per sleeve
• Supercharger: Two-speed centrifugal, single stage
• Fuel system: Injection
• Fuel type: 100/130 Octane petrol
• Oil system: Direct-pressure lubrication
• Cooling system: Air-cooled

Performance

• Power output: 2,520 hp (1,880 kW) at 2,700 rpm
• Specific power: 0.77 hp/cu in (35.0 kW/L)
• Compression ratio: 7.2:1
• Power-to-weight ratio: 0.94 hp/lb (1.55 kW/kg)

Related development

• Bristol Hercules

Comparable engines

• Alfa Romeo 135
• Nakajima Homare
• Pratt & Whitney R-2800 Double Wasp
• Wright R-3350 Duplex-Cyclone
• Shvetsov ASh-73

Related lists

• List of aircraft engines

Notes edit

Bibliography edit

• Bridgman, L, (ed.) (1998) Jane's Fighting Aircraft of World War II. Crescent. ISBN 0-517-67964-7
• Gunston, Bill. Development of Piston Aero Engines. Cambridge, UK. Patrick Stephens, 2006. ISBN 0-7509-4478-1
• Gunston, Bill. World Encyclopedia of Aero Engines: From the Pioneers to the Present Day. 5th edition, Stroud, UK: Sutton, 2006.ISBN 0-7509-4479-X
• Lumsden, Alec. British Piston Engines and Their Aircraft. Marlborough, UK: Airlife Publishing, 2003. ISBN 1-85310-294-6.
• White, Graham. 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, 1995. ISBN 1-56091-655-9

• Period advertisement for the Bristol Centaurus - Flight, May 1949
• Video of a cutaway engine in motion illustrating its operation