Aircraft electrical system operating method
a technology of electrical system and operating method, which is applied in the direction of motor/generator/converter stopper, dynamo-electric converter control, instruments, etc., can solve the problems of engine shutdown, undemanded power drop, engine thrust control loss, etc., and achieve the effect of preventing fuel from leaking into the oil system
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[0026]FIG. 1 shows a passenger aircraft 2. The aircraft 2 is of conventional construction, having a fuselage 4, wings 6, and a pair of wing mounted engines 10.
[0027]FIG. 2 shows a cross sectional schematic view of one of the engines 10. The engine 10 comprises an air intake 12 and a propulsive fan 14 that generates two airflows A and
[0028]B. The gas turbine engine 10 comprises, in axial flow A, an intermediate pressure compressor 16, a high pressure compressor 18, a combustor 20, a high pressure turbine 22, an intermediate pressure turbine 24, a low pressure turbine 26 and an exhaust nozzle 28. The high pressure turbine 22 is mechanically coupled to the high pressure compressor 18 by a high pressure shaft 34, the intermediate pressure turbine 24 is mechanically coupled to the intermediate pressure compressor 16 by an intermediate pressure shaft 36, and the low pressure turbine 26 is mechanically coupled to the fan 14 by a low pressure shaft 38. A nacelle 30 surrounds the gas turbine...
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