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Rolls-Royce RB.203 Trent

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Title: Rolls-Royce RB.203 Trent  
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Rolls-Royce RB.203 Trent

RB.203 Trent
Type Turbofan
Manufacturer Rolls-Royce Limited
First run December 1967
Major applications Fairchild Hiller FH-228 (intended)
Hawker Siddeley HS.136 (intended)
Convair 660 (intended)[1]

The Rolls-Royce RB.203 Trent was a British medium-bypass turbofan engine of around 10,000lb thrust designed for production in the late 1960s, bearing no relation to the earlier Rolls-Royce RB.50 Trent turboprop or the later high bypass Rolls-Royce Trent turbofan.[2]

The RB.203 was a private venture engine based around the core of the Rolls-Royce Turbomeca Adour turbofan used in the SEPECAT Jaguar and the later Hawker Siddeley Hawk.[3]

The RB.203, the first three-spool engine, was intended as a civilian replacement for the earlier Rolls-Royce Spey.[4]

Specifications

Data from Flight International.[2]

General characteristics

  • Type: Three-spool medium bypass turbofan
  • Length: 82.2 in (208.8 cm)
  • Diameter: 38.7 in (98.3 cm)
  • Dry weight: 1,751 lb (794 kg)

Components

  • Compressor: Single-stage fan, four-stage intermediate pressure, five-stage high pressure
  • Combustors: Annular chambers
  • Turbine: Single-stage high pressure, single-stage intermediate, two-stage low pressure

Performance

See also

Comparable engines
Related lists

References

  1. ^ Convair 660, Flight Global, retrieved 28 January 2012
  2. ^ a b - RB.203 TrentFlight International www.flightglobal.com Retrieved: 23 January 2011
  3. ^ Commercial Aircraft Survey, Flight Global, 23 November 1967, retrieved 28 January 2012
  4. ^ Aero Engines 1968, A "Flight" special review
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