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A turbine blade and a turbine composed of the turbine blade

A turbine blade and blade technology is applied in the design field of turbine blades and turbines and paddle blades composed of the turbine blades, which can solve the problems of reducing the temperature in front of the vortex, reducing the wind speed, and difficult to transmit energy.

Inactive Publication Date: 2018-06-26
刘欧阳 +2
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

So this turbine technology using fluid reverse thrust inevitably brings considerable energy loss
Secondly, an unavoidable problem with the popular turbine technology is that the linear velocity varies with the rotation radius of each point of the blade, and even the difference is huge, especially for turbines with huge wheel diameters such as wind turbines for wind power generation.
For example, the speed of the blades close to the shaft of the wind rotor is very slow, the wind cannot push it, and it can only go around here, so it is difficult to transfer energy, while at the tip of the wind rotor, the speed is much faster than the wind speed and even produces back pressure, that is, the blades The back of the blade catches up with the airflow, and the angle of attack causes the air pressure on the back of the blade to be greater than the air pressure on the front, resulting in a large rotational resistance
Therefore, the difference in the rotating line speed will reduce the turbine efficiency to a considerable extent
Third, the popular turbine technology cannot avoid the energy loss caused by centrifugal force
Fourth, in applications such as gas turbines, the discharged fluid contains a large amount of waste heat, which is not effectively converted into mechanical energy, so the temperature before the vortex is also reduced, and the efficiency of the gas turbine is also reduced
The total projected area of ​​the wind rotor blades or the solidity of the wind rotor is an indicator that is difficult to improve. If the solidity of the wind rotor is not high, it will inevitably lead to the loss of wind energy
However, increasing the solidity of the wind rotor will increase the wind resistance, reduce the wind speed, and reduce the efficiency of the wind rotor.

Method used

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  • A turbine blade and a turbine composed of the turbine blade
  • A turbine blade and a turbine composed of the turbine blade
  • A turbine blade and a turbine composed of the turbine blade

Examples

Experimental program
Comparison scheme
Effect test

no. 1 example

[0042] Combine below Figure 1 to Figure 7 to characterize the blade surface. like figure 1 , figure 2 As shown, Z is the axis of rotation, the first curve AB is a smooth and non-inflection point concave curve that is coplanar with the axis of rotation and does not intersect, and its concave surface faces the axis of rotation, and one end point B is close to the axis of rotation, called the proximal end, and the other end point A away from the axis of rotation is called the distal end. Take any point P1 on the first curve as a tangent, the angle α between the tangent and the rotation axis is less than or equal to 90 degrees at the proximal end B, and greater than or equal to 0 degrees at the distal end A. Obviously, α equal to 0 degrees means that the tangent at the distal end A is parallel to the axis of rotation. As the point moves from the proximal end B to the distal end A, the angle α decreases monotonically. If the first curve AB can be represented by a function, i...

no. 2 example

[0062] like Figure 12 As shown, the single blade can also form a single blade turbine 2 . The single-blade turbine 2 only includes a turbine blade 21 composed of a curved surface of the third blade. The turbine blade 21 can be regarded as a multi-blade turbine with infinitely small gaps between the blades, which is a complete reference surface with thickness, in the form of an antenna pot-shaped surface. , there is a cavity near the rotating shaft 22, or a guide hole is provided for fluid flow.

no. 3 example

[0064] like Figure 13 As shown, a plurality of single-blade turbines 2 can form a coaxial laminated turbine 3, and the coaxial laminated turbine 3 can also be regarded as a multi-stage turbine formed by a plurality of single-blade turbines 31 in series around the rotating shaft 32, that is, the diameter Different single blades are coaxially stacked together, leaving a gap between them. The law of the gap still follows the general law of the blade gap, that is, along the blade surface from the rotation axis to the radial edge of the blade, the blade gap is getting smaller and smaller, but the smallest. Gap is greater than zero. Figure 13 The section view of some blades is shown, and the law of blade clearance can be seen. In practice, the leaf density may be much higher than Figure 13 shown. Under the premise of not significantly affecting the performance, some special nodes between the blades on the blade surface are also allowed to have mutually fixed structures to enha...

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PUM

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Abstract

The invention provides a turbine blade and a turbine composed of the same. A first blade curved surface and a second blade curved surface or a third blade curved surface are formed by virtue of smooth and non-inflection-point concave curved lines which are coplanar and do not intersect with a rotary shaft. The turbine blade structures of a single-blade curved surface, a multi-blade curved surface, a multi-stage-connected single-blade curved surface, a multi-stage-connected multi-blade curved surface, a multi-stage-connected composite-blade curved surface and the like are formed through combining the abovementioned blade curved surfaces. The turbine provided by the invention is driven by virtue of a vortex artificially formed in a fluid. According to the turbine blade and the turbine which are provided by the invention, the concept of a second-order curved surface is put forward, and the turbine and a turbine group are composed of the turbine blade formed by virtue of second-order blade curved surfaces; and a vortex field is manufactured through the coupling of a vortex flow field, that is, the rotational motion of the blade in the fluid, a Coriolis force is generated in the flow field and the blade is pushed to accelerate rotation through a boundary layer effect, and positive feedback is formed between the vortex and the blade, thus a high energy conversion rate is achieved. The heat efficiency can be additionally increased if the blade is used in the turbine group of a gas turbine engine.

Description

technical field [0001] The present invention relates to the field of fluid dynamics, in particular, to a turbine blade and a turbine composed of the turbine blade. This technology is also applicable to the design of paddle blades for ships and flying objects, etc. Background technique [0002] The surface of the turbine blade is a space curved surface with three-dimensional characteristics. In actual operation, the real flow inside the turbomachinery is very complex, which is three-dimensional flow in space and unsteady in time. Due to the characteristics of the boundary layer, turbulence such as boundary vortices will appear near the blade end face. The Navier-Stokes equations commonly used to analyze fluid motion are difficult to use in turbine design to solve such complex problems. Nonetheless, we can find common flaws in popular turbine technology from basic mechanics. First of all, the popular turbine technology basically uses turbine blades to change the direction o...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F01D5/14F01D5/02F03D3/06F03B3/12F04D29/18F04D29/26B63H1/26B64C11/20
CPCB63H1/26B64C11/20F01D5/02F01D5/141F03B3/12F03B3/121F03D3/061F03D3/062F04D29/18F04D29/185F04D29/26Y02E10/20Y02E10/74Y02P70/50
Inventor 彭晓耘刘欧阳张曙光
Owner 刘欧阳