Rotor system and micro gas turbine
A rotor and shaft technology, applied in gas turbine devices, mechanical equipment, engine components, etc., can solve the problems of insufficient rigidity, difficult processing and manufacturing, high processing and manufacturing costs, etc., to improve dynamic performance and stability, and improve pneumatic lubrication. effect, the effect of improving the overall performance
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[0099] In order to better understand the technical solutions of the present invention, the present invention will be further described below in conjunction with specific embodiments and accompanying drawings.
[0100] According to one aspect of the invention, a rotor system is provided.
[0101] Such as figure 1 The rotor system shown includes a rotating shaft 110, the shaft body of the rotating shaft 110 is an integral structure, the rotating shaft 110 is arranged horizontally or vertically, and the rotating shaft 110 is sequentially sleeved with a thrust bearing 100, a first radial bearing 200, a motor 300, a second Radial bearing 400, compressor 500, turbine 600.
[0102] Such as figure 2 The rotor system shown includes a rotating shaft 110, the shaft body of which is an integral structure, the rotating shaft 110 is arranged horizontally or vertically, and the first radial bearing 200, the motor 300, and the second radial bearing 400 are sleeved on the rotating shaft 110...
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