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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. 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.

  5. Rolls-Royce aircraft piston engines - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_Aircraft...

    A preserved Rolls-Royce Griffon 58, one of the last Rolls-Royce piston engines to be produced. The red and white "dumb bell" object to the left of the engine is an air raid siren exhibit Rolls-Royce produced a range of piston engine types for aircraft use in the first half of the 20th century.

  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. 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 ...

  8. Bristol Siddeley - Wikipedia

    en.wikipedia.org/wiki/Bristol_Siddeley

    [citation needed] The Maybach Diesel (MD) MD650, MD655 and MD870 series engines built by Bristol Siddeley were sophisticated in design, running at much higher speeds than normal diesels of their size and featured advanced construction such as a disc-webbed crankshaft that ran in large roller bearings, telescopic pipes to deliver cooling oil to ...

  9. Rolls-Royce T406 - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_T406

    In October 2021, Bell and Rolls-Royce jointly announced that the Bell V-280 Valor powerplant would switch from the General Electric T64 turboshaft used on the prototype to a derivative of the 1107C used on the Osprey which would be named the 1107F. At the same time as increasing power from 5,000 to 7,000 horsepower, the 1107C is a known element ...

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