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A method of operating a gas turbine engine having a turbine and a compressor connected via a shaft, a main fuel supply line for supplying fuel to a combustor that is positioned to release expanding hot gases to the turbine, the engine further including a starter/generator connected to the shaft via

A method of operating a gas turbine engine having a turbine and a compressor connected via a shaft, a main fuel supply line for supplying fuel to a combustor that is positioned to release expanding hot gases to the turbine, the engine further including a starter/generator connected to the shaft via a gearbox assembly, the method is characterised the step of during engine start up fuel is circulated in a re-circulating fuel circuit positioned on the main fuel supply line and which has a first fuel/oil heat exchanger, for cooling the oil, and a fuel accumulator.

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1. A gas turbine engine comprising: a turbine;a compressor connected via a shaft to said turbine;a main fuel supply line for supplying fuel;a combustor for receiving said fuel that is positioned to release expanding hot gases to the turbine, a first fuel and oil heat exchanger associated with an eng

1. A gas turbine engine comprising: a turbine;a compressor connected via a shaft to said turbine;a main fuel supply line for supplying fuel;a combustor for receiving said fuel that is positioned to release expanding hot gases to the turbine, a first fuel and oil heat exchanger associated with an engine starter/generator that is connected to the shaft via a gearbox assembly;the engine is characterised by a re-circulating fuel circuit positioned on the main fuel supply line and that has a second fuel/oil heat exchanger and a fuel accumulator, the re-circulating fuel circuit thereby cooling the oil in the starter/generator via the first fuel and oil heat exchanger. 2. A gas turbine engine as claimed in claim 1 wherein the second fuel/oil heat exchanger is fluidly connected to an engine oil circuit. 3. A gas turbine engine as claimed in claim 1 wherein the first fuel/oil heater exchanger is fluidly connected to the starter/generator. 4. A gas turbine engine as claimed in claim 1 wherein the circuit comprises a fuel filter. 5. A gas turbine engine as claimed in claim 4 wherein fuel filter is positioned between the second fuel/oil heat exchanger and the combustor. 6. A gas turbine engine as claimed in claim 1 wherein the circuit comprises a shut off valve that is provided to stop fuel return flow during normal engine running. 7. A method of operating a gas turbine engine having a turbine and a compressor connected via a shaft, a main fuel supply line for supplying fuel to a combustor that is positioned to release expanding hot gases to the turbine, the engine further having a starter/generator connected to the shaft via a gearbox assembly, a first fuel/oil heat exchanger for cooling the oil in the starter/generator oil circuit, and a fuel accumulator, the method comprising the steps of: initiating engine start-up;circulating fuel in a re-circulating fuel circuit positioned on the main fuel supply line. 8. A method of operating a gas turbine engine as claimed in claim 7 wherein a further step comprises supplying the cooled fuel to the starter/generator for cooling.