KR101730821B1 - Modeling method for wind blade and apparatus using thereof - Google Patents

Abstract

The present invention relates to a method of modeling a wind power blade and an apparatus for modeling using the same. The method of modeling a wind power blade by the modeling apparatus includes the steps of: receiving at least two pieces of airfoil data indicating a cross section of the wind power blade for each part; analyzing the inputted airfoil data to arrange the airfoil data for each part in the longitudinal direction of the wind power blade; generating a single wind power blade model according to a first modeling standard by collecting the arranged airfoil data for each part; and converting the generated wind power blade model into a second modeling standard adopted by a three-dimensional modeling software through a coordinate conversion operation.

Description

Technical Field [0001] The present invention relates to a modeling method for a wind turbine blade,

More particularly, the present invention relates to a modeling method for modeling a blade in conjunction with analysis and design of a wind turbine blade, a recording medium on which the method is recorded, and a modeling device according to the method.

Recently, as concerns about environmental pollution and depletion of fossil energy due to industrial development have increased, interest in environmentally friendly new and renewable energy has increased and development and investment have increased. In particular, wind power generation is one of the most active areas for research and development, and its technology and utilization rate are increasing each year. Such a wind turbine generator is a device for generating electric power by converting wind energy into electric energy by using a rotating body such as a rotor. It is effective in replacing fossil fuel and providing economical power supply in a backward region where electric facilities are difficult to supply And the application is expanding in the energy field.

Generally, the wind turbine generator is installed on the upper part of the support so that the position is changed according to the wind direction, and the rotor is rotatably installed at the tip of the fuselage. The induced electromotive force generated by the rotation of the rotor is stored in the battery . The rotor of the wind turbine is made up of a blade and a hub, and a driving device is provided on the hub to adjust the pitch angle of the blade. The blade has a cross section of an airfoil, and has a cross-sectional shape continuously from the root portion to the tip portion It has a changing shape.

Wind and drag force and drag force on the blade, the drag-based wind power generator based on the drag due to the wind can not exceed the wind speed, while the lift type wind power generator based on the lift generated from the wing Can be rotated at a speed faster than the wind speed, which is applied to the trend of high efficiency and large size of the wind power generator.

It is required to develop a blade shape capable of improving the performance of the wind turbine by changing the shape of the secondary flow region, vortex flow and radial flow generated during the rotation of the blade. In particular, according to the simulation result of the designed blade, A modeling methodology that is easy to change is also one of the major issues.

Although the prior art documents described below describe a technique relating to the airfoil structure of the blades in which the output efficiency of the blades at rated wind speed can be improved, it is still possible to easily reflect or modify such design methods in actual blade designs Technical measures are not presented.

Korean Patent Laid-Open Publication No. 2013-0097515, published on September 03, 2013, Chonbuk National University Industry-Academic Cooperation Foundation

SUMMARY OF THE INVENTION The present invention has been made in view of the above problems, and it is an object of the present invention to solve the problem that a modeling method for designing a wind turbine blade relies on a three-dimensional modeling implementation by a skilled worker, In order to overcome the limitations of productivity degradation in repetitive modeling process due to frequent changes of design due to inaccuracy with actual products, breakage of designed models, and adverse effects due to inadequacy of design changes due to modeling.

According to an aspect of the present invention, there is provided a method of modeling a wind turbine blade, the modeling device including at least one processor according to an embodiment of the present invention, Receiving at least two airfoil data representative of a cross-section of the airfoil; The modeling device analyzes the inputted airfoil data, arranges the airfoil data for each section in the longitudinal direction of the windpower blade, collects the arranged airfoil data for each section, and obtains one windblade blade model ; And converting the one wind turbine blade model generated by the modeling device into a second modeling standard adopted by the three-dimensional modeling software through a coordinate conversion operation.

In the method of modeling a wind turbine blade according to an embodiment, the airfoil data includes a geometry data set expressing a cross-section of a wind turbine blade of each section independently separated for each section, and the geometry data The dataset can be managed individually and selectively.

In one method of modeling a wind turbine blade according to an embodiment, a single wind turbine blade model according to the first modeling standard may have a cross section of a plurality of wind turbine blades arranged according to the coordinate analysis spatially along the longitudinal direction of the wind turbine blades Lt; / RTI >

In the method of modeling a wind turbine blade according to an embodiment, the airfoil data is geometry data expressing a cross section of a wind turbine blade for each section, including position information of each section with respect to the entire length of the wind turbine blade, The width information of each section and the twist angle. In addition, the positional information of each section and the width information of each section may be set as a relative ratio to the entire length of the wind turbine blade.

In the method of modeling a wind turbine blade according to an exemplary embodiment, the step of generating the one wind turbine blade model may include a step of receiving position information of a shear web indicating a structure inside the wind turbine blade, Step < / RTI > In addition, the number of the sheer webs can be adjusted according to the type of wind turbine blades.

The method of modeling a wind turbine blade according to an embodiment may further include reading the converted wind turbine blade model data through the three-dimensional modeling software.

In a method of modeling a wind turbine blade according to an embodiment, the 3D modeling software may be at least one of CATIA, UG NX, Inventor, and Solidworks.

Furthermore, a computer-readable recording medium on which a program for executing the method of modeling a wind turbine blade described above is stored in a computer is provided below.

According to an aspect of the present invention, there is provided an apparatus for modeling a wind turbine blade, comprising: an input unit for receiving at least two airfoil data expressing a cross section of each wind turbine blade; A memory for storing a modeling program for interpreting the airfoil data and performing a coordinate transformation operation; And at least one processor for driving the modeling program, wherein the modeling program stored in the memory analyzes the inputted airfoil data, arranges the airfoil data for each section in the longitudinal direction of the windpower blade, Dimensional wind turbine blade model according to the first modeling standard is collected by collecting the deployed airfoil data for each section and the generated windfoil blade model is collected by the second modeling standard, Convert to modeling specification.

In the modeling apparatus for a wind turbine blade according to an embodiment, the airfoil data includes a geometry data set expressing a cross-section of a wind turbine blade for each section independently separated for each section, and the geometry data The dataset can be managed individually and selectively.

In the modeling device of a wind turbine blade according to an embodiment, the modeling program stored in the memory spatially connects the cross sections of the plurality of wind turbine blades arranged in accordance with the coordinate analysis along the longitudinal direction of the wind turbine blades, Create one wind blade model according to the modeling standard.

In the modeling apparatus for a wind turbine blade according to an embodiment, the airfoil data is geometry data expressing a cross section of a wind turbine blade for each section, which includes position information of each section with respect to the entire length of the wind turbine blade, The width information of each section and the twist angle. The modeling program stored in the memory may set position information of each section and width information of each section as a ratio relative to the total length of the wind turbine blades.

In the modeling apparatus for a wind turbine blade according to an exemplary embodiment, the modeling program stored in the memory may receive position information of a shear web indicating a structure inside the wind turbine blade, and may be disposed inside the wind turbine blade. In addition, the modeling program stored in the memory can adjust the number of sheared webs according to the type of the wind blades.

In a modeling apparatus for a wind turbine blade according to an embodiment, the 3D modeling software may be at least one of CATIA, UG NX, Inventor, and Solidworks.

In the modeling device of the wind turbine blade according to the embodiment, the modeling program stored in the memory may be configured to interpret the input airfoil data to represent each set of geometric data expressing a cross section of each wind turbine blade as one row, And a UI (user interface) for displaying on the device and visualizing a cross section of the wind turbine blade defined by one row and displaying the cross section on a separate area. In addition, the modeling program stored in the memory may independently add, modify, or delete airfoil data for each set of geometry data that constitutes the one row.

According to the present invention, after a large amount of geometry information is input at a time in cooperation with a file format including a plurality of sets of geometry information, airfoil data and sheer web data are individually It is possible to manage the modeling configuration according to the history, and finally, by generating the blade model converted into the file format compatible with the general-purpose three-dimensional modeling software, Improves productivity through data sharing and collaboration.

1 is a flowchart illustrating a method of modeling a wind turbine blade according to an embodiment of the present invention.
FIG. 2 is a flowchart illustrating a process of generating one wind turbine blade modeling in the modeling method of FIG. 1 according to an embodiment of the present invention.
FIG. 3 is a diagram illustrating a GUI (software user interface) of a software prototype implementing a method of modeling a wind turbine blade according to an embodiment of the present invention.
4 is a diagram for explaining each item included in geometry data defining a cross section of a wind turbine blade for each section.
FIGS. 5 and 6 are views for explaining attributes of the geometry data of FIG. 4 represented through the blades.
7 is a diagram showing an example of a method of managing airfoil data in the GUI of Fig. 3. Fig.
8 is a diagram showing an example of a method of managing shear web data in the GUI of Fig.
FIG. 9 is a diagram for explaining attributes of each item constituting the share web data of FIG. 8 through a blade.
FIG. 10 is a diagram illustrating a three-dimensional blade model finally transformed through the GUI of FIG. 3. FIG.
11 is a block diagram illustrating a modeling apparatus for a wind turbine blade according to an embodiment of the present invention.

Prior to describing the embodiments of the present invention, the problems occurring in the existing modeling method related to the design of a wind turbine blade are briefly reviewed, and the technical means employed by the embodiments of the present invention to solve these problems are sequentially described Introduction.

In the field of conventional wind turbine blade modeling technology based on software, three-dimensional modeling of wind turbine blades has been carried out by a modeling expert through a three-dimensional commercial program. Modeling Experts gather blade geometry data for modeling and determine a coordinate system, angle, and position in a three-dimensional space based on the collected data, and use a loft or sweep function to create a linear surface geometry . Typical working time for this process takes about 1 ~ 2 days, and when the design is changed, this operation is repeatedly performed.

Another way to implement the blade shape is to use a three-dimensional measuring device (e.g., a three-dimensional scanner). This method requires the manufactured blade shape and scanner equipment and usually takes about 1-2 days. There must also be a skilled user, and the accuracy of the shape data is determined by the measurement angle and distance.

As described above, the 3D modeling implementation by a skilled worker is inefficient because it takes a lot of time, and problems such as inaccuracy with respect to actual products, breakage, and inadequacy in response to design changes may occur. Therefore, embodiments of the present invention described below are devised to solve the above-described problems, and it is an object of the present invention to provide a method and apparatus for generating bladed geometry data such as airfoil information, a twist angle, a shear web position, To provide software with speed, accuracy, and ease of shape change by automated programs.

To this end, embodiments of the present invention must satisfy the following functional requirements.

(1) Calling and interpreting large amounts of data: For example, it is necessary to be able to receive the blade's geometry data through interworking with a file that stores a large amount of data sets separated by delimiters, such as Excel.

(2) Management of airfoil data: The input airfoil data should be able to selectively input, modify, and delete the blade's section.

(3) Management of resting web data: It is interlocked with the mass data file, and it should be able to determine the number of webs according to the kind of blades, and to position and change them.

(4) Interworking with commercially available three-dimensional modeling program: Interoperating with commercially available three-dimensional modeling software such as CATIA, UG NX, Inventor, and Solidworks to design modeling data for each section, Loads must be able to implement accurate modeling.

BRIEF DESCRIPTION OF THE DRAWINGS The above and other objects, features and advantages of the present invention will be more apparent from the following detailed description taken in conjunction with the accompanying drawings, in which: FIG. In the following description and the accompanying drawings, detailed description of well-known functions or constructions that may obscure the subject matter of the present invention will be omitted. Incidentally, throughout the specification, " including " means not including other elements unless specifically stated to the contrary, it may include other elements.

Also, the terms first, second, etc. may be used to describe various components, but the components should not be limited by the terms. The terms may be used for the purpose of distinguishing one component from another. For example, without departing from the scope of the present invention, the first component may be referred to as a second component, and similarly, the second component may also be referred to as a first component.

The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. The singular expressions include plural expressions unless the context clearly dictates otherwise. In the present application, the terms "comprise", "having", and the like are intended to specify the presence of stated features, integers, steps, operations, elements, components, or combinations thereof, , Steps, operations, components, parts, or combinations thereof, as a matter of principle.

Unless defined otherwise, all terms used herein, including technical or scientific terms, have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. Terms such as those defined in commonly used dictionaries should be construed as meaning consistent with meaning in the context of the relevant art and are not to be construed as ideal or overly formal in meaning unless expressly defined in the present application .

FIG. 1 is a flowchart illustrating a method of modeling a wind turbine blade according to an embodiment of the present invention. In the method of modeling a wind turbine blade according to an embodiment of the present invention, at least one processor is used to perform a coordinate transformation operation Lt; / RTI > modeling device.

In step S110, the modeling apparatus receives at least two airfoil data expressing a cross section of the wind blade of each section. The airfoil can be designed in various forms depending on the purpose of use, and there are also a number of airfoils disclosed for a blade for wind power generation in which embodiments of the present invention are utilized. The airfoil data input through step S110 is not single data but consists of information about a plurality of blade cross sections constituting one wind turbine blade, Can be expressed as a set.

Particularly, in the airfoil data to which the embodiments of the present invention are input, a geometry data set expressing a cross section of each wind turbine blade is independently divided for each section, and a geometry data set for forming one section It is preferable to be individually and selectively managed.

In step S120, the modeling device analyzes the airfoil data input through step S110, arranges the airfoil data for each section in the longitudinal direction of the wind turbine blade, collects the arranged airfoil data for each section, Create one wind blade model according to the modeling standard. Here, one wind turbine blade model according to the first modeling standard generated through step S120 is generated by spatially connecting the cross sections of the plurality of wind turbine blades arranged according to the coordinate analysis along the longitudinal direction of the wind turbine blades . The first modeling standard is not a specification adopted by the general-purpose three-dimensional modeling software but a modeling method designed to easily define and manage the shape and position of a plurality of airfoil data sequentially arranged along the longitudinal direction of the wind- Standard, and the input of the raw data is performed through the above-described step S110.

In step S130, the modeling device converts the one wind turbine blade model generated in step S120 into a second modeling standard adopted by the three-dimensional modeling software through a coordinate transformation operation. Here, the second modeling standard is a modeling standard adopted by a general-purpose three-dimensional modeling software that is not specialized in the design of a wind turbine blade. Each of the nodes and position information for defining a three-dimensional model, Edge, and the cross section of each section in the longitudinal direction of one blade has an inconvenience that must be individually defined. Therefore, a modeling unit suitable for arranging and collecting the airfoil data in the longitudinal direction of the wind turbine blade through the steps S110 and S120 is necessary. One wind turbine blade model according to the first modeling standard generated through the above- Coordinate transformation should be done so that it can be utilized in 3D modeling software. This coordinate conversion operation is performed through this step S130.

FIG. 2 is a flowchart illustrating a wind turbine blade modeling process (S120) in more detail in the modeling method of FIG. 1 according to an embodiment of the present invention.

In step S121, the modeling device analyzes the airfoil data and arranges the airfoil data for each section in the longitudinal direction of the wind turbine blade. To this end, the software implemented in accordance with the present invention has the function of adding, selecting, releasing, and deleting individual airfoil data via a graphical user interface (GUI), and in particular, It is possible to do. Needless to say, the twist angle can be adjusted as necessary with respect to the arranged airfoil data.

In step S122, the modeling device receives the position information of the shear web indicating the structure inside the wind turbine blade and arranges the information on the inside of the wind turbine blade. Through this process, it is possible to specify the position of the web, or the number of the web, which is interlocked with the skin data of the blade or the sheared web.

The airfoil data and the sheer web data inputted through steps S121 to S122 are constructed in a separate database and the history information on the data set and the change is recorded and managed in the storage device, It can be used easily when modifying the model.

In step S123, the modeling device generates one wind turbine blade model according to the first modeling standard. In particular, one model data can be generated including the airfoil position, the twist angle and the section of the wind blade from the shear web data and the pressure skin data, It can be automatically created with 3D modeling software, for example CATIA file format.

FIG. 3 is a diagram illustrating a GUI (software user interface) of a software prototype implementing a method of modeling a wind turbine blade according to an embodiment of the present invention.

As illustrated in FIG. 3, the modeling program implemented in accordance with the modeling method of the wind turbine blade proposed in FIGS. 1 and 2 analyzes the inputted airfoil data and calculates the geometry representing the section of the wind turbine blade The user interface may further include a user interface (UI) that displays each data set as one row and displays the same on a display device, visualizes a cross section of the wind turbine blade defined by one row, and displays the data on a separate area.

Referring to the GUI screen of Fig. 3, a button 310 for initially inputting large amount of data including two or more airfoil information about the blade, a button (for managing individual airfoil data of the input large amount of data 320), a button (330) for receiving sheared web data, managing input individual sheared web data, and a blade model based on the geometry information of the finally disposed blade, And a button 340 for converting into a format of the modeling software.

3, the GUI screen includes a geometry information window 350 in which a series of geometry information read out through the mass data input button 310 is sequentially displayed for each section, an individual airfoil selected in the geometry information window 350, A coordinate window 370 for displaying coordinate values for each of the airfoils in sequence, and a control window 380. The coordinate window 370 displays the coordinates of the airfoil. Through the control window 380, whether or not to create an axis, whether to trim the tail of the blade shape, whether to fit the guide curve of the blade shape, As shown in FIG.

4 is a diagram for explaining each item included in geometry data defining a cross section of a wind turbine blade for each section. The airfoil data managed through FIG. 4 is geometry data expressing a cross section of a wind blade of each section. The data includes position information of each section with respect to the entire length of the wind turbine blade, width information of each section with respect to the entire length of the wind turbine blade, It is preferable to include a twist angle.

More specifically, 'Section No.' 401 represents the sequence number of the inputted series of geometry data, 'Blade Length' 402 represents the total length of the wind turbine blades, 'y / R' And the total length is defined as '1' in FIG. 5, the position of each section in the longitudinal direction of the entire blade is specified, and it can be seen that separate airfoil data should be placed for these sections. 6, the airfoil data for the section A-A in FIG. 5 will be described as an example.

Referring again to FIG. 4, 'c / R Chord' (404) represents the ratio of the chord length to the total length of the blade, and the total length is defined as '1' in FIG. The 'Twist Angle' 405 and the 'Center Ratio' 406 represent a twist angle and aero-cent from the tip to the center of the aero, respectively, and are specifically shown in FIG. 6, L / E means leading edge, T / E means trailing edge, and chord length means the width of the blade. The position information of each section and the width information of each section are set as relative ratios to the entire length of the wind turbine blades so that the physical characteristics of the blade modeled independently of the size of the wind turbine blades are preserved, Can be managed.

Referring again to FIG. 4, 'Airfoil No.' 407 represents the order of airfoils, 'Airfoil Type' 408 represents the type of airfoil, 'Plane Pos.' 409 represents' y / R 'BL Lead Pos.' 411 represents the absolute dimension (mm) for 'c / R Chord', 'Blade Width' 410 represents the absolute dimension (mm) (Mm), and 'Rotate Angle' (412) represents the absolute angle to 'Twist Angle'.

FIG. 7 is a diagram showing an example of a method for managing airfoil data in the GUI of FIG. 3, wherein a table is created through a separate database and individual airfoil data is inserted, modified, Management can be performed. That is, the modeling program illustrated in FIG. 7 is preferably capable of independently adding, modifying, or deleting airfoil data for each set of geometry data that constitutes a row.

FIG. 8 is a diagram illustrating an example of a method for managing shear web data in the GUI of FIG. 3. In FIG. 8, a table is generated through a separate database similarly to the case of FIG. 7, Insertion, modification, deletion, and the like can be performed.

The method of modeling a wind turbine blade proposed by embodiments of the present invention may further include a step of receiving position information of a shear web indicating a structure inside the wind turbine blade and arranging the received information on the inside of the wind turbine blade, The number of webs can be adjusted depending on the type of wind turbine blade. Referring to FIG. 8, 'fname' 801 represents the name of each position of the sheer web, 'num' 802 represents the assigned order, 'x' and 'y' Value.

FIG. 9 is a view for explaining the attributes of each item constituting the share web data of FIG. 8 through the blades. The name of each position illustrated in 'fname' 801 of FIG. a) It is indicated in the blade. In FIG. 9 (a), three sheer webs (sw1, sw2, sw3) are arranged as a structure inside the blade. Fig. 9 (b) shows the shape of the section b 'of Fig. 9 (a).

FIG. 10 is a diagram illustrating a three-dimensional blade model finally transformed through the GUI of FIG. 3. FIG.

It can be seen that the three-dimensional blade model converted by the blades modeling method proposed by the embodiments of the present invention has a shape as shown in (a) to (d), and the output file format is compatible with the general- . Therefore, it is possible for the user to load and utilize the converted wind turbine blade model data through the general-purpose three-dimensional modeling software. Here, the general purpose three-dimensional modeling software may be software such as CATIA, UG NX, Inventor, and Solidworks.

FIG. 11 is a block diagram illustrating a modeling apparatus 100 for a wind turbine blade according to an embodiment of the present invention. Referring to FIGS. 1 and 2, each process of modeling a wind turbine blade described in a time- . Therefore, in order to avoid duplication of description, only the function of each constitution is described here.

The input unit 10 receives at least two airfoil data expressing a cross section of the wind blade of each section.

The memory 30 stores a modeling program for interpreting the airfoil data and performing a coordinate transformation operation. Here, the modeling program stored in the memory analyzes the inputted airfoil data, arranges the airfoil data for each section in the longitudinal direction of the wind turbine blades, collects the airfoil data for each section, Generates a single wind turbine blade model, and converts the generated one wind turbine blade model into a second modeling standard adopted by the three-dimensional modeling software through a coordinate transformation operation.

In this airfoil data, a geometry data set expressing a cross section of each wind turbine blade is independently divided for each section, and a set of geometry data forming one section is preferably individually and selectively managed , The modeling program creates one wind turbine blade model according to the first modeling standard by spatially connecting the cross sections of the plurality of wind turbine blades arranged in accordance with the coordinate analysis along the longitudinal direction of the wind turbine blades. Particularly, the airfoil data is geometry data expressing a cross section of a wind turbine blade for each section, including position information of each section with respect to the entire length of the wind turbine blade, width information of each section with respect to the entire length of the wind turbine blade, And the modeling program preferably sets the position information of each section and the width information of each section as a ratio relative to the total length of the wind turbine blade. Further, the modeling program may be configured to receive the position information of the shear web indicating the structure inside the wind turbine blade, to arrange the wind turbine blade inside the wind turbine blade, and to adjust the number of the shear web according to the type of the wind turbine blade. have.

At least one processor 20 may be provided as a technical means for driving the modeling program. The processor 20 interprets a series of commands defined in the program and sequentially processes the data, Outputs a model wind turbine blade model.

According to the embodiments of the present invention described above, a large amount of geometry information is input at one time in cooperation with a file format including a plurality of sets of geometry information, and airfoil data and sheer web data are respectively input to the type of blade, design / It is possible to manage design changes easily and quickly by managing them individually according to the analysis result. It is also possible to manage the modeling configuration according to the history. Finally, by generating the blade model converted into the file format compatible with the general purpose three- Improves productivity by sharing and collaborating data associated with blade production.

Meanwhile, the embodiments of the present invention can be embodied as computer readable codes on a computer readable recording medium. A computer-readable recording medium includes all kinds of recording apparatuses in which data that can be read by a computer system is stored.

Examples of the computer-readable recording medium include ROM, RAM, CD-ROM, magnetic tape, floppy disk, optical data storage, and the like. In addition, the computer-readable recording medium may be distributed over network-connected computer systems so that computer readable codes can be stored and executed in a distributed manner. In addition, functional programs, codes, and code segments for implementing the present invention can be easily deduced by programmers skilled in the art to which the present invention belongs.

The present invention has been described above with reference to various embodiments. It will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the invention as defined by the appended claims. Therefore, the disclosed embodiments should be considered in an illustrative rather than a restrictive sense. The scope of the present invention is defined by the appended claims rather than by the foregoing description, and all differences within the scope of equivalents thereof should be construed as being included in the present invention.

100: Modeling device of wind turbine blade
10: Input unit
20: Processor
30: Memory

Claims (20)

CLAIMS 1. A method of modeling a wind turbine blade, the modeling device having at least one processor for performing a coordinate transformation operation,
Receiving at least two airfoil data representing a cross-section of a wind turbine blade of each section;
The airfoil data input by the modeling device is analyzed to arrange the airfoil data for each section in the longitudinal direction of the windpower blade, the airfoil data for each section arranged in accordance with the coordinate analysis is collected, Creating a single wind turbine blade model according to a first modeling standard by spatially connecting the plurality of wind turbine blades along a direction; And
Converting the one wind turbine blade model generated by the modeling device into a second modeling standard adopted by the three-dimensional modeling software through a coordinate transformation operation,
Wherein the airfoil data comprises:
The geometry data set expressing the section of each wind turbine blade is separated independently for each section,
Wherein a set of geometric data forming a section is individually and selectively entered, modified or deleted. delete delete The method according to claim 1,
The airfoil data includes:
The wind turbine blade according to any one of claims 1 to 3, wherein the geometric data expressing the cross section of the wind turbine blade for each section includes positional information of each section with respect to the entire length of the wind turbine blade, width information of each section with respect to the entire length of the wind turbine blade, . 5. The method of claim 4,
The position information of each section and the width information of each section are stored in a memory,
Is set as a ratio relative to the total length of the wind turbine blades. The method according to claim 1,
Wherein generating the one wind turbine blade model comprises:
Further comprising the step of receiving positional information of a shear web indicating a structure inside the wind turbine blade and arranging the received position information in the wind turbine blade. The method according to claim 6,
Wherein the number of the shear webs is adjusted according to the type of the wind turbine blades. The method according to claim 1,
And reading the converted wind turbine blade model data through the three-dimensional modeling software. The method according to claim 1,
The three-dimensional modeling software includes:
CATIA, UG NX, Inventor, and Solidworks. A computer-readable recording medium storing a program for causing a computer to execute the method according to any one of claims 1 to 9. An input unit for receiving at least two airfoil data expressing a cross section of each wind power blade;
A memory for storing a modeling program for interpreting the airfoil data and performing a coordinate transformation operation; And
And at least one processor for driving the modeling program,
A modeling program stored in the memory,
The input airfoil data is analyzed to arrange the airfoil data for each section in the longitudinal direction of the windpower blade, the airfoil data for each section arranged according to the coordinate analysis is collected, and the cross section of the windpower blade is spatially And converts the generated one wind turbine blade model into a second modeling standard adopted by the three-dimensional modeling software through a coordinate transformation operation,
Wherein the airfoil data comprises:
The geometry data set expressing the section of each wind turbine blade is separated independently for each section,
Wherein the set of geometric data forming a section is individually and selectively entered, modified or deleted. delete delete 12. The method of claim 11,
Wherein the airfoil data comprises:
The wind turbine blade according to any one of claims 1 to 3, wherein the geometric data expressing the cross section of the wind turbine blade for each section includes positional information of each section with respect to the entire length of the wind turbine blade, width information of each section with respect to the entire length of the wind turbine blade, Modeling device. 15. The method of claim 14,
A modeling program stored in the memory,
Wherein the position information of each section and the width information of each section are set as a ratio relative to the entire length of the wind turbine blade. 12. The method of claim 11,
A modeling program stored in the memory,
And position information of a shear web indicating a structure inside the wind turbine blade is received and arranged inside the wind turbine blade. 17. The method of claim 16,
A modeling program stored in the memory,
Wherein the number of the sheared webs is adjusted according to the type of the wind power blades. 12. The method of claim 11,
The three-dimensional modeling software includes:
CATIA, UG NX, Inventor, and Solidworks. 12. The method of claim 11,
A modeling program stored in the memory,
The input airfoil data is interpreted to represent a set of geometric data expressing a cross section of the wind turbine blade for each section as one row and displayed on a display device and a cross section of the wind turbine blade defined as one row is visualized, And a UI (user interface) for displaying the wind turbine blade in a region. 20. The method of claim 19,
A modeling program stored in the memory,
Wherein the airfoil data can be independently added, modified or deleted for each set of geometry data constituting the one row.

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