Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Small wind turbine wing type aerodynamic robust optimization design method suitable for turbulent working conditions

A robust optimization and design method technology, applied in the field of wind turbines, can solve the problems of decreased aerodynamic stability and wind energy capture efficiency, and achieve the effects of improving optimization efficiency, enhancing aerodynamic robustness, and improving wind energy capture efficiency

Active Publication Date: 2019-02-22
XIANGTAN UNIV
View PDF3 Cites 16 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the traditional wind turbine airfoil optimization design, the design variables, objective functions and constraint functions are all deterministic, and the influence of uncertain factors such as turbulence intensity on the design is not considered, so that the optimal solution of the optimal design is uncertain in practice. Under turbulent flow conditions, the efficiency of wind energy capture decreases and the aerodynamic stability of the system decreases

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Small wind turbine wing type aerodynamic robust optimization design method suitable for turbulent working conditions
  • Small wind turbine wing type aerodynamic robust optimization design method suitable for turbulent working conditions
  • Small wind turbine wing type aerodynamic robust optimization design method suitable for turbulent working conditions

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0047] The patent of the present invention will be further described below in conjunction with the accompanying drawings, taking the S809 airfoil as the research object, Reynolds number Re=3×10 5 , the design angle of attack is 6°, and the turbulence intensity TI is used as an uncertain design parameter to optimize the robustness of the airfoil, but the present invention is not limited to the specific form of the stated case.

[0048] (1) The improved Hicks-Henne function is used to parametrically represent the airfoil.

[0049] (2) The geometric parameter design variable is the airfoil characteristic function coefficient c k , and the value range is shown in Table 3.

[0050] Table 3 Range of design variables

[0051]

[0052]

[0053] (3) Within the range of geometric parameter design variables, 150 sets of geometric parameter design variable sample points were extracted through the Latin hypercube design method.

[0054] (4) Design variable sample points according ...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention discloses a small wind turbine wing type aerodynamic robust optimization design method suitable for turbulent working conditions, belonging to the technical field of wind turbines. The invention adopts the non-embedded probability collocation point method in the design to realize the quantitative characterization of the turbulence intensity of the uncertain parameter. Through the improved Hick-Henne type function parameterization method, Latin hypercube test method and CFD numerical calculation method, the kriging agent model between design variables, uncertain parameters and themaximum lift-to-drag ratio of the airfoil is established. On this basis, a robust optimization mathematical model is established to maximize the mean value of the maximum lift-to-drag ratio and minimize the standard deviation of the wind turbine wing under uncertain turbulent conditions. The non-embedded probabilistic configuration point method, the kriging proxy model, and the NSGA-II optimization algorithm are used to optimize the wind turbine airfoil. The invention improves the maximum lift-drag ratio of the airfoil, reduces the fluctuation range, improves the wind energy capture efficiency, and enhances the aerodynamic robustness under the turbulent condition. At the same time, the computational workload of robust optimization design is reduced, and the optimization efficiency is improved, which provides an important reference for the optimization design of wind turbine wing under turbulent conditions.

Description

technical field [0001] The invention relates to the technical field of wind turbines, in particular, it provides an aerodynamic robust design method for small wind turbine airfoils suitable for turbulent flow conditions. Background technique [0002] For small wind turbines, due to the low installation position of the hub, affected by the evolution of atmospheric turbulence, wind shear and surface roughness, they often operate under uncertain and highly turbulent flow conditions. Under the action of uncertain turbulent wind, the flow on the airfoil surface is extremely unstable, and the aerodynamic performance fluctuates greatly, which directly affects the stability of the wind turbine system. In the traditional wind turbine airfoil optimization design, the design variables, objective functions and constraint functions are all deterministic, and the influence of uncertain factors such as turbulence intensity on the design is not considered, so that the optimal solution of th...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
CPCG06F30/15G06F30/20G06F2111/10Y02E10/72
Inventor 唐新姿李鹏程王效禹袁可人
Owner XIANGTAN UNIV
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products