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Gnome
Rolls-Royce Gnome at the Imperial War Museum Duxford
Type Turboshaft
Manufacturer Rolls-Royce
First run 5 June 1959
Major applications Westland Whirlwind
Westland Wessex
Westland Sea King
Developed from General Electric T58

The Rolls-Royce Gnome is a single spool turboshaft originally developed by the de Havilland Engine Company as a licence-built General Electric T58 - a mid 1950s design.[1] The Gnome came to Rolls-Royce after their takeover of Bristol Siddeley in 1966, Bristol having absorbed de Havilland Engines Limited in 1961.

Contents

[edit] Design and development

A two stage turbine drives the 10 stage all-axial compressor, whilst a single stage free power turbine drives the load. The combustor is annular. The engine was one of the first developed with an analogue computer as part of the fuel control system, specifically to control fuel flow during acceleration to prevent engine surge occurring.

[edit] Variants and applications

[edit] Engines on display

A Rolls-Royce Gnome is on display at the Imperial War Museum Duxford, another is part of the aero engine collection at the Science Museum (London).

[edit] Specifications (Gnome H1400-1)

Data from Flight[2]

General characteristics

  • Type: Turboshaft
  • Length: 54.8 in (1392 mm)
  • Diameter: 22.7 in (577 mm)
  • Dry weight: 334 lb (151.5 kg)

Components

  • Compressor: Ten-stage axial flow
  • Combustors: Annular
  • Turbine: Single stage compressor turbine, two-stage power turbine

Performance

[edit] See also

[edit] References

[edit] Notes

  1. ^ Gunston 1989, p.155.
  2. ^ Flightglobal archive - 1973 Retrieved: 9 November 2008

[edit] Bibliography

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

[edit] External links




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