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Rolls Royce Exe

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The Rolls-Royce Exe, or Boreas, was a 24-cylinder air-cooled X block sleeve valve aircraft engine intended primarily for the new Fairey Fleet Air Arm aircraft, particularly the Fairey Barracuda. The Exe was under development in 1939, having been started in the 1930s, along with the Peregrine and Vulture. The Exe was named after the River Exe, although Rolls-Royce later transferred the use of river names to its gas turbine engines.

Contents

Work on the Exe was suspended in August 1939, and stopped about August 1940. In August 1940 Ernest Hives, head of the Rolls-Royce aero engine division, wanted to stop work on the Exe, Peregrine, and Vulture to concentrate on the Merlin and Griffon engines.

Applications

Originally intended for the Supermarine Type 322 and Fairey Barracuda the Exe was only test flown in a Fairey Battle, the first flight taking place on 30 November 1938. This aircraft continued in use for some time as a communications aircraft where the Exe was noted to be quite reliable in service.

Specifications (Exe)

Data from Gunston and Lumsden.

General characteristics

  • Type: 24-cylinder supercharged air-cooled 90-degree X layout aircraft piston engine
  • Bore: 4.225 in (107.3 mm)
  • Stroke: 4.0 in (101.6 mm)
  • Displacement: 1,348 cu in (22.1 L)
  • Dry weight: 1,530 lb (694 kg)
  • Components

  • Valvetrain: Sleeve valve
  • Supercharger: Gear-driven centrifugal type supercharger, single stage
  • Fuel type: Petrol
  • Cooling system: Pressure air-cooled
  • Reduction gear: 0.358:1, left hand tractor
  • Performance

  • Power output: 1,150 hp (856 kW) at 4,200 rpm, +4.5 psi boost at sea level
  • Compression ratio: 8:1
  • Power-to-weight ratio: 0.75 hp/lb (1.23 kW/kg)
  • References

    Rolls-Royce Exe Wikipedia


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