| 摘要 |
A bypass turbojet engine has a body, subsonic intake, compressors of low, medium and high pressure, combustion chamber, turbines of low, medium and high pressure, outlet nozzles. The engine comprises an impeller connected to the drive shaft of the rotor of low pressure turbine, fixed guide apparatus by the first and the second contour connected to the engine body to which air intake and fixed guide apparatus of the second contour are rigidly attached. On the shaft of the medium pressure turbine an impeller of the rotor of medium pressure compressor is fixed. |
