Pear-shaped linear wing type blade based impact water turbine
An airfoil blade and water turbine technology, which is used in impact engines, hydroelectric power generation, mechanical equipment, etc., can solve the problems of unavailability of water energy resources, poor economy, and low blade efficiency, so as to solve the problem that fish are difficult to migrate and reduce production. cost, efficiency
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Embodiment 1
[0026] to combine Figure 1 to Figure 5 , an impact turbine based on pear-shaped airfoil blades proposed by the present invention, which includes an impeller, a rotating shaft 3, a water diversion channel 5, and a bearing support frame 6, wherein: the impeller includes a plurality of pear-shaped airfoils Blade 4, the impeller is fixed at the upper 1 / 3 of the inlet section 5 of the water diversion channel along the center line, the impeller is fixed at the tail of the transition section 7 of the water diversion channel, and the water flow passes through the water inlet 1 of the water diversion channel The inlet section 5 of the water diversion channel is introduced into the transition section 7 of the water diversion channel, which drives the impeller to rotate, and then flows to the water outlet 2 of the water diversion channel through the outlet section 8 of the water diversion channel; the pear-shaped airfoil blade 4 Centered on the rotating shaft 3, it is arranged on the bl...
Embodiment 2
[0032] to combine figure 1 , figure 2 and Figure 4 , the impeller includes 3 pear-shaped airfoil blades 4, the coordinates of the key points of the pear-shaped curve in the impeller on the axial section airfoil curve are expressed in the following manner, X represents the pear-shaped airfoil The spatial abscissa value of the key point on the blade 4-section airfoil curve, Y represents the space ordinate value of the key point on the pear-shaped airfoil blade 4-section airfoil curve, the parameters are shown in Table 2,
[0033] Table 2:
[0034] serial number
[0035] The mathematical equations for the parameters described in Table 2 are: x=1+sint; y=a·cost·(1+sint).
Embodiment 3
[0037] to combine Figure 1 to Figure 3 , The number of impellers arranged on the bearing support frame 6 of the present invention is 10-12.
[0038] The length L of the inlet section 5 of the diversion channel 0 The length L of the transition section 7 with the diversion channel 1 The ratio of 0.37 to 0.44; the length L of the outlet section 8 of the diversion channel 2 The length L of the transition section 7 with the diversion channel 1 The ratio of and is 1.62 to 1.69.
[0039] The diameter of the impeller D 1 and the diameter D of the rotating shaft 3 0 The ratio of 1.95 to 2.02; the diameter D of the bearing support frame 6 2 and the diameter D of the rotating shaft 3 0 The ratio is 9.39 to 9.46.
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