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Napier Gazelle

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Napier Gazelle

The Napier Gazelle was a turboshaft engine manufactured by D. Napier & Son in the mid-1950s. In 1961 production was nominally transferred to a joint venture with Rolls-Royce called Napier Aero Engines Limited. But the venture closed two years later.

Contents

Variants

NGa.1
NGa.2
NGa.2(R)
NGa.2 series 2
NGa.13(R)
NGa.13 series 2
Mk.101
Mk.161
Mk.162
(NGa.13 series 2)
Mk.165
Gazelle 501
Gazelle 503
Gazelle 512
Gazelle 514
Gazelle E.219

Applications

These helicopter engines were used on the Westland Wessex HAS 1 and HAS 3 (other versions of the Wessex had two Rolls-Royce Gnome engines) and the Bristol Belvedere (later Westland Belvedere) transport helicopter.

Engines on display

A preserved Napier Gazelle is on display at the Royal Air Force Museum London. A preserved Napier Gazelle from a Westland Wessex helicopter is on display at the Queensland Air Museum, Caloundra, Australia.

Specifications (Gazelle 501 / Mk.101 / NGa.2(R))

Data from Jane's All the World's Aircraft 1962-63 and Flightglobal archive.

General characteristics

  • Type: Turboshaft
  • Length: 70 in (1,778 mm)
  • Diameter: 33.5 in (851 mm)
  • Dry weight: 830 lb (376.5 kg)
  • Components

  • Compressor: 11-stage axial flow
  • Combustors: 6 flame tubes
  • Turbine: 2-stage gas generator power turbine + 1-stage free power turbine
  • Fuel type: Aviation kerosene, (DERD 2482 / 2485 / 2486 / 2488 / 2494)
  • Oil system: Pressure spray / splash with gear pump and dry sump, oil grade DERD.2487
  • Performance

  • Maximum power output: 1,650 hp (1,230.4 kW) + 260 lbf (1.16 kN) thrust at 3,000 output shaft rpm, maximum rating for 2.5 minutes
  • Overall pressure ratio: 6.25:1
  • Air mass flow: 16.8 lb (8 kg)/s
  • Specific fuel consumption: 0.688 lb/(hp h) (0.4185 kg/(kW h))
  • Power-to-weight ratio: 1.458 hp/lb (2.397 kW/kg)
  • References

    Napier Gazelle Wikipedia