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The Bristol Hercules is a 14-cylinder two-row radial aircraft engine designed by Sir Roy Fedden and produced by the Bristol Engine Company starting in 1939. It was the most numerous of their single sleeve valve (Burt-McCollum, or Argyll, type) designs, powering many aircraft in the mid-World War II timeframe.
Following World War II, the sleeve valve became utilised less, Roy Fedden, very early involved in the S-V research, built some flat-six single sleeve-valve engines intended for general aviation around 1947; after this, just the French SNECMA produced some SSV engines under Bristol license that were installed in the Noratlas transport airplane ...
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 (67,875.2 cm 3) [6.25 in × 7.5 in (159 mm × 191 mm)], nearly as large as the American Pratt & Whitney R ...
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 Mercury model for that year, which shows that the sleeve system was being underexploited.
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The Bristol Hercules. The Bristol Engine Company was ... the division was renamed Bristol Aero Engines and then merged with Armstrong ... Sleeve-valve engines: ...
Pages in category "Sleeve valve engines" ... Bristol Centaurus; Bristol Hercules; Bristol Perseus; Bristol Taurus; D. Daimler Double-Six sleeve-valve V12; J.
The Hastings was powered by an arrangement of four wing-mounted Bristol Hercules 101 sleeve valve radial engines. [9] These engines were installed upon the leading edge of the wing via interchangeable power-eggs ; the air intakes and thermostatically -controlled oil coolers were also present within the wing.