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Rolls-Royce Gem

Aircraft Engines

The Rolls-Royce Gem is a three-shaft turboshaft engine developed for the Westland Lynx helicopter in the 1970s. Its design began in the de Havilland engine division, which explains the G in the name, and passed to Bristol Siddeley as the BS.360. After Rolls-Royce bought Bristol Siddeley in 1966 and dropped that identity, the engine became the RS.360. A four-stage axial low pressure compressor, driven by a single-stage low pressure turbine, supercharges a centrifugal high pressure compressor with its own single-stage turbine, and a two-stage free power turbine delivers power to the load through a third shaft, behind a reverse-flow combustor. The Gem 42 develops 1,000 shaft horsepower at take-off, with a maximum contingency rating of 1,120. Besides the Lynx it powers the Agusta A129 Mangusta, and examples are displayed in several British museums.

Facts
Power (kW)
750 1
Connections

Of Make

Source Rolls-Royce Gem (Wikipedia)
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Source Rolls-Royce Gem (Wikipedia)Lead
Quote, Lead
Rolls-Royce bought out Bristol Siddeley in 1966 and after it dropped the Bristol Siddeley identity the engine became the RS.360.
Sources
1. Rolls-Royce Gem (Wikipedia)
  • Design and development, Gem 42
    The Gem 42 develops 1,000 shp (750 kW) at Take-off, Sea Level Static, ISA
  • Lead
    Rolls-Royce bought out Bristol Siddeley in 1966 and after it dropped the Bristol Siddeley identity the engine became the RS.360.
  • Part Of: Westland Lynx, Lead, Lynx
    developed specifically for the Westland Lynx helicopter in the 1970s
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