|Preserved Bristol Perseus|
|Type||Piston aircraft engine|
|Manufacturer||Bristol Aeroplane Company|
|Major applications||Westland Lysander
The Perseus was a British, nine-cylinder, single-row, air-cooled radial aircraft engine produced by the Bristol Engine Company starting in 1932. It was the first production sleeve valve aero engine.
Design and development
In late 1925 and early 1926, the RAE published a series of papers by Harry Ricardo on the sleeve valve principle. The main advantages over the traditional poppet valves was better volumetric efficiency, and the ability to operate at higher rotational speeds. This allowed a smaller engine to produce the same power as a larger one, leading to better fuel efficiency and compact design, particularly in multi-row radial engines.
Roy Fedden, Bristol's primary engine designer, became interested in the concept and by 1927 he had constructed a working two-cylinder V as a testbed, with the idea of developing it into a V-12. However several problems cropped up on the design, notably that the sleeves tended to burst during the power stroke and strip their driving gears. This led to a long series of tests and materials changes and upgrades that required six years and an estimated 2 million pounds to cure; however, by 1933 the problems had been worked out, and the Perseus went on to become the first sleeve valve aero-engine in the world to be put into large quantity production.
The result was a Bristol Mercury-sized engine adapted to the sleeve valve system, the Perseus, and its smaller cousin, the Bristol Aquila. The first production versions of the Perseus were rated at 580 horsepower (433 kW), the same as the same-year model Mercury, which shows that the sleeve system was being underutilised. However this was quickly uprated as improvements were introduced, and by 1936 the Perseus was delivering 810 hp (604 kW), eventually topping out at 930 hp (690 kW) in 1939, while the Perseus 100 with an increased capacity of 1,635 cu in (26.8 L) produced 1,200 hp (890 kW) at 2,700 rpm at 4,250 ft (1,296 m). This far outperformed even the most-developed versions of the Mercury.
The Perseus saw limited use in the civilian field, notably on the Short Empire flying-boats, but was more common in the then-expanding military field where it was found on the Westland Lysander, Vickers Vildebeest, Blackburn Botha, Skua and Roc bombers.
The main contribution of the Perseus is that its mechanicals were used as the basic piston and cylinder for the "twinned" versions, the tremendously successful Hercules and Centaurus. It was in these designs that the advantages of the sleeve valve were finally put to good use, and by war's end the Centaurus was one of the most powerful engines in the world.
Specifications (Perseus XII)
Data from Lumsden.
- Type: Nine-cylinder single-row supercharged air-cooled radial engine
- Bore: 5.75 in (146 mm)
- Stroke: 6.5 in (165 mm)
- Displacement: 1,520 in³ (24.9 L)
- Length: 49 in (1,245 mm)
- Diameter: 55.3 in (1,405 mm)
- Dry weight: 1,025 lb (465 kg)
- Valvetrain: Sleeve valve
- Supercharger: Single-speed centrifugal type supercharger
- Fuel system: Claudel-Hobson carburettor
- Fuel type: 87 Octane petrol
- Cooling system: Air-cooled
- Reduction gear: 0.5:1 turning a de Havilland variable pitch propeller
- Power output:
- 830 hp (619 kW) at 2,650 rpm for takeoff
- 905 hp (675 kW) at 2,750 rpm at 6,500 ft (1,980 m)
- Specific power: 0.59 hp/in³ (26.75 kW/l)
- Compression ratio: 6.75:1
- Specific fuel consumption: 0.43 lb/(hp·h) (261 g/(kW·h))
- Oil consumption: 0.28 oz/(hp·h) (11 g/(kW·h))
- Power-to-weight ratio: 0.88 hp/lb (1.45 kW/kg)
- Related development
- Related lists
|Wikimedia Commons has media related to Bristol Perseus.|
- Lumsden 2003, p.116.
- Bridgman (Jane's) 1998, p. 270.
- Bridgman (Jane's) 1998, p. 272.
- List from Lumsden, the Perseus may not be the main powerplant for these types
- Lumsden 2003, p.117.
- Bridgman, L, (ed.) (1998) Jane's Fighting Aircraft of World War II. Crescent . ISBN 0-517-67964-7
- Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
- Gunston, Bill. Development of Piston Aero Engines. Cambridge, England. Patrick Stephens Limited, 2006. ISBN 0-7509-4478-1
- Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.