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Trent 700


Trent -700 engines are comprised of:

  • low pressure compressor stage (1 stage, the fan)
  • intermediate pressure compressor stage (8 stages)
  • high pressure compressor stage (6 stages)
  • combustion chamber (24 nozzles, 2 igniters)
  • high pressure turbine stage (1 stage)
  • intermediate pressure turbine stage (1 stage)
  • low pressure turbine stage (4 stages)

They are flat-rated at ISA+15°C to 71,100 lbs thrust.


The low speed rotor (N1) consists of a fan connected to a low pressure turbine. The intermediate speed rotor (N2) consists of an intermediate pressure compressor connected to an intermediate turbine. The high speed rotor (N3) consists of a high pressure compressor connected to a high pressure turbine.


At low rpm valves open to dump air into the fan stream to prevent stall during start.


Categories: Airbus A330 | Power Plant



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