Novel blade used for ocean current power generation turbine
An ocean current power generation and turbine technology, applied in the field of turbine blades, can solve the problems of small self-weight, low efficiency, and large blade self-weight, and achieve the effects of small self-weight, high efficiency, and avoidance of cavitation.
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Embodiment 1
[0018] refer to Figure 1-3
[0019] A new type of blade for an ocean current power generation turbine, the blade 1 includes a wing root 11 close to the turbine rotor and a wing tip 12 away from the rotor, and the cross section of the blade 1 adopts NACA series airfoils; It is characterized in that: the chord length of the blade 1 gradually becomes shorter along the blade root 11 to the wing tip 12, and the thickness of the blade 1 gradually becomes thinner along the blade root to the wing tip.
[0020] The leading edge 13 of the blade 1 is straight, and the trailing edge 14 of the blade 1 is an elliptic curve of a quarter of the front concave.
[0021] The ratio of the length of the wing tip 12 of the blade 1 to the length of the wing root 11 is 1:3.
[0022] The concept of the present invention is: the blade 1 is gradually shortened along the wing root 11 to the wing tip 12 chord length 15, and the thickness is gradually thinned, so that the volume of the blade 1 is reduce...
Embodiment 2
[0025] refer to Figure 4 , 5 , in combination with the actual situation, this embodiment is described:
[0026] The specific implementation of the present invention will be further described below with the airfoil chord length c as the unit 1.
[0027] The cross section of the blade adopts NACA4415 airfoil, the maximum camber f is 4% of the chord length, and the maximum camber position x f The distance from the leading edge is 40% of the chord length, and the maximum thickness d is 15% of the chord length.
[0028] The blade adopts an elliptical airfoil whose length ratio between the wing tip and the wing root is 1:3 in the longitudinal section, the length a of the wing tip is about 0.333, the length b of the wing root is 1, the leading edge 1 is a vertical straight line, and the trailing edge gradient line 2 is a quarter elliptic curve x 2 0.66 7 2 ...
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