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词条 Rolls-Royce Gem
释义

  1. Design and development

  2. Applications

  3. Engines on display

  4. Specifications (Gem 42)

  5. See also

  6. References

     Notes  Bibliography 

  7. External links

{{Use dmy dates|date=January 2018}}{{Use British English|date=January 2018}}
name=Gemimage= Rolls Royce Gem HMW.JPGcaption= Rolls-Royce Gem at The Helicopter Museum (Weston)

}}{{Infobox Aircraft Engine

type= Turboshaftnational origin = United Kingdommanufacturer= Rolls-Royce Limitedfirst run=major applications= Westland Lynxnumber built =program cost =unit cost =developed from =developed into =variants with their own articles =
}}

The Rolls-Royce Gem is a turboshaft engine developed specifically for the Westland Lynx helicopter in the 1970s. The design started off at de Havilland (hence the name starting with "G") and was passed to Bristol Siddeley as the BS.360. When Rolls-Royce bought out the latter in 1966, it became the RS.360.[1]

Design and development

The Gem's three-shaft engine configuration is rather unusual for turboshaft/turboprop engines. Basic arrangement is a four-stage axial LP (Low Pressure) compressor, driven by a single stage LP turbine, supercharging a centrifugal HP (High Pressure) compressor, driven by a single stage HP turbine. Power is delivered to the load via a third shaft, connected to a two-stage free (power) turbine. A reverse flow combustor is featured.[2]

The Gem 42 develops {{convert|1000|shp|abbr=on}} at Take-off, Sea Level Static, ISA, but the Maximum Contingency Rating (MCR) is {{convert|1120|shp|abbr=on}}.

Until recently all versions of the Lynx have been Gem powered. However, now that Rolls-Royce own Allison, they have been marketing the more modern LHTEC T800, developed jointly with Honeywell.

Applications

  • Agusta A129 Mangusta
  • Westland Lynx

Engines on display

  • East Midlands Aeropark
  • Midland Air Museum
  • The Helicopter Museum (Weston)
  • 111 (Sunderland) Squadron ATC

Specifications (Gem 42)

{{jetspecs
|ref=Rolls-Royce[3]
|type=Triple-shaft two-spool turboshaft
|length= 43.4 in (1090 mm)
|diameter= 23.5 in (590 mm)
|weight=414 lb (187 kg)
|compressor=4-stage axial LP, single-stage centrifugal HP
|combustion=
|turbine=2-stage power turbine, single-stage LP, single-stage HP
|fueltype=
|oilsystem=
|power=1,000 shp (746 kW)
|thrust=
|compression=12:1
|aircon=7 lb/sec
|turbinetemp=
|fuelcon=
|specfuelcon=
|power/weight=
|thrust/weight=
}}

See also

{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
  • List of aircraft engines

|similar engines=
  • Bristol Siddeley Nimbus
  • Rolls-Royce Gnome

}}

References

Notes

1. ^Gunston 1989, p. 155.
2. ^Rolls-Royce Gem product page
3. ^Rolls-Royce Gem 42 factsheet {{webarchive|url=https://web.archive.org/web/20101217024018/http://www.rolls-royce.com/Images/Gem_tcm92-6705.pdf |date=17 December 2010 }} www.rolls-royce.com. Retrieved: 16 July 2009

Bibliography

{{refbegin}}
  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. {{ISBN|1-85260-163-9}}
{{refend}}

External links

{{commons category}}
  • Rolls-Royce Gem product page
  • "Rolls-Royce/Turbomeca BS.360" a 1972 Flight article
{{RRaeroengines}}{{Bristol aeroengines}}{{DHaeroengines}}

4 : Turboshaft engines 1970–1979|De Havilland aircraft engines|Rolls-Royce aircraft gas turbine engines|Mixed-compressor gas turbines

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