Multi-spool by-pass turbofan engine
A turbofan engine and multi-rotor technology, applied in engine manufacturing, engine components, machines/engines, etc., can solve complex problems and achieve the effect of reducing fuel consumption
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[0025] Detailed Description of Preferred Embodiments
[0026] As shown in FIG. 1 , a three-rotor bypass turbofan engine 6 is schematically shown, and includes a cylindrical casing 8 , the outermost portion of which defines the outer wall of an annular bypass passage 10 . A low pressure rotor 12 is rotatable about a central longitudinal axis 14 of the engine 6 and includes a shaft 16 having a fan 18 and a low pressure compressor 19 at the front end of the shaft and a low pressure turbine 20 at the rear end of the shaft.
[0027] An intermediate pressure rotor 22 is arranged coaxially about the shaft 16 of the low pressure stage 12 and also includes a shaft 24 , an intermediate compressor 26 and an intermediate turbine 28 .
[0028] A high-pressure rotor assembly 30 is telescopic on shafts 16 and 24 of the low-pressure and medium-pressure rotors 12 and 22, respectively, and includes a shaft 32 with a high-pressure compressor 34 at its front end and a high-pressure turbine at its...
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