A Hybrid Microlayer Turbine Combining Impulse Action and Boundary Layer Effect
An impulsive action, boundary layer technology, applied in the direction of engine components, machines/engines, blade support components, etc., can solve the problem of increased friction loss between fluid and blade surface, bladed turbine blades susceptible to cavitation corrosion, and blade penetration. Due to the complex design of the flat blade, the effect of easy flow of the working fluid, alleviation of transmission mechanical losses, and improved energy utilization
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[0023] The present invention provides a hybrid microlayer turbine that combines impulse action and boundary layer effects. The present invention will be described in detail below in conjunction with the accompanying drawings.
[0024] Such as figure 1 , 2 As shown in the sectional view and side view of the overall structure, the turbine disks 11 and spacers 10 are alternately arranged on the turbine shaft 5, and the distance between the turbine disks 11 is controlled by the spacers to form a rotor disk group. The disc group is fit with the turbine shaft 5 through the key 13; the entire rotor disc group is fixed on the turbine shaft 5 by the shaft shoulder 3 at one end and the round nut 12 at the other end; there are two ceramic bearings 7 respectively installed on the main body 1 and the rear end cover 14, the axial distance is controlled by the circlip 6, and the turbine shaft 5 and the bearing 7 are fixed with the casing by interference fit; the front end cover 2 and the r...
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