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  2. Allison Model 250 - Wikipedia

    en.wikipedia.org/wiki/Allison_Model_250

    The Allison Model 250, now known as the Rolls-Royce M250, (US military designations T63 and T703) is a highly successful turboshaft engine family, originally developed by the Allison Engine Company in the early 1960s. The Model 250 has been produced by Rolls-Royce since it acquired Allison in 1995.

  3. Rolls-Royce C range engines - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_C_range_engines

    The Rolls-Royce C range was a series of in-line 4, 6 and 8 cylinder diesel engines used in small locomotives, railcars, construction vehicles, and marine and similar applications. They were manufactured by the Rolls-Royce Oil Engine Division headed by William Arthur Robotham to 1963, initially at Derby and later at Shrewsbury , from the 1950s ...

  4. Rolls-Royce B range engines - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_B_range_engines

    The B range of engines were all of the inline configuration, with crossflow inlet-over-exhaust cylinder heads and were naturally aspirated.They were heavily rationalized engines, which made use of as many common parts across the range as possible, for example, the 8 cylinder versions used 2 sets of the oil bath air filters, exhaust manifolds and points components of the 4 cylinder, while using ...

  5. Allison Engine Company - Wikipedia

    en.wikipedia.org/wiki/Allison_Engine_Company

    In 1995 US authorities approved, with restrictions on Joint Strike Fighter Program, the purchase of Allison by Rolls-Royce. [9] The price was $525 million. [ 12 ] In the year 2000, some of these restrictions were alleviated, [ 13 ] and in 2001 the US government chose the F-35 with Rolls-Royce LiftFan and Pratt & Whitney F135 engines.

  6. Rolls-Royce RR300 - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_RR300

    Data from Rolls-Royce General characteristics Type: Twin-spool turboshaft/turboprop Length: 37.6 inches (96 cm) Diameter: 21.5 inches (55 cm) Dry weight: 201 pounds (91 kg) Components Compressor: Single-stage centrifugal Turbine: 2 stage GP, 2 stage PT Performance Maximum power output: 240–300 shaft horsepower (180–220 kW) Overall pressure ratio: 6.2 Power-to-weight ratio: 0.67 pounds per ...

  7. IOE engine - Wikipedia

    en.wikipedia.org/wiki/IOE_engine

    Yale IOE engine from 1911. The intake/inlet over exhaust, or "IOE" engine, known in the US as F-head, is a four-stroke internal combustion engine whose valvetrain comprises OHV inlet valves within the cylinder head and exhaust side-valves within the engine block.

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