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  2. Rolls-Royce WR-21 - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_WR-21

    The turbine itself was designed primarily by Rolls-Royce with significant marine engineering and test facility input from DCN, with Northrop Grumman responsible for the intercooler, the recuperator and system integration. [1] [2] WR-21 development draws heavily on the technology of the successful Rolls-Royce RB211 and Trent families of gas ...

  3. Rolls-Royce Marine Olympus - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_Marine_Olympus

    Data from Rolls-Royce Heritage Trust General characteristics Type: Gas generator Length: Diameter: Dry weight: Components Compressor: 5-stage LP, 7-stage HP Combustors: 8 chamber, cannular Turbine: Single-stage LP and HP Performance Maximum power output: 28,500 shp (21.4 MW) Specific fuel consumption: 0.47 lb/hp/hr (0.287 kg/KWh) See also Related development Rolls-Royce Olympus References ^ a ...

  4. Rolls-Royce MT30 - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_MT30

    The Rolls-Royce MT30 (Marine Turbine) is a marine gas turbine engine based on the Rolls-Royce Trent 800 aero engine. The MT30 retains 80% commonality with the Trent 800, the engine for the Boeing 777. The maximum power rating is 40 MW and minimum efficient power 25 MW. [1] Rolls-Royce announced the MT30 program on 11 September 2001.

  5. Rolls-Royce Avon - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_Avon

    The Rolls-Royce Avon was the first axial flow ... gas generator that is rated at 21,000–22,000 shp (15.7–16.4 MW). ... system and single-stage turbine using ...

  6. Rolls-Royce Marine Spey - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_Marine_Spey

    The Rolls-Royce Marine Spey is a marine gas turbine based on the Rolls-Royce Spey and TF41 aircraft turbofan engines. [1] The Marine Spey currently powers seven ship classes including the Royal Navy's Type 23 frigates and provides a power output of 19.5 MW (about 26,150HP). The Marine Spey incorporates technology from the Tay and RB211.

  7. Rolls-Royce RR500 - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_RR500

    The Rolls-Royce RR500 is a family of small gas turbine engines developed by Rolls-Royce Corporation. The RR500TP turboprop variant was intended for use in small aircraft. The RR500TS was the turboshaft variant designed for light helicopters. Development of the RR500 was abandoned in 2012.

  8. Turbomeca Palouste - Wikipedia

    en.wikipedia.org/wiki/Turbomeca_Palouste

    Designed and built by Turbomeca, the Palouste was also built under license in Britain by Blackburn and Rolls-Royce.Originally conceived as an aircraft ground support equipment starter gas generator, it was used also as propulsion for the Sud-Ouest Djinn and other tip-jet powered helicopters.

  9. Category:Rolls-Royce aircraft gas turbine engines - Wikipedia

    en.wikipedia.org/wiki/Category:Rolls-Royce...

    Pages in category "Rolls-Royce aircraft gas turbine engines" The following 53 pages are in this category, out of 53 total. This list may not reflect recent changes .