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CN105822510A - Blade tip serialization segmentation blade and design method thereof - Google Patents

Blade tip serialization segmentation blade and design method thereof Download PDF

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Publication number
CN105822510A
CN105822510A CN201610221174.XA CN201610221174A CN105822510A CN 105822510 A CN105822510 A CN 105822510A CN 201610221174 A CN201610221174 A CN 201610221174A CN 105822510 A CN105822510 A CN 105822510A
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China
Prior art keywords
blade
tip
design
section
blade tip
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CN201610221174.XA
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Chinese (zh)
Inventor
叶婷婷
王同光
李慧
陈程
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WUXI WIND POWER INSTITUTE Co Ltd
Nanjing University of Aeronautics and Astronautics
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WUXI WIND POWER INSTITUTE Co Ltd
Nanjing University of Aeronautics and Astronautics
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Priority to CN201610221174.XA priority Critical patent/CN105822510A/en
Publication of CN105822510A publication Critical patent/CN105822510A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/20Rotors
    • F05B2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50Manufacturing or production processes characterised by the final manufactured product

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  • Wind Motors (AREA)

Abstract

The invention relates to a blade tip serialization segmentation blade and a design method thereof. Firstly, fan blade pneumatic design is carried out, an efficient low-resistance wing section is selected, high-precision performance of a wind turbine flow field is analyzed, and a foundation blade is generated; the foundation blade is subject to structural laying-up design, structure attribute calculation is carried out, a BLADED model is built, and blade loads are obtained; and through manual iterative modification of air operation-structure-loads, the final structure of the foundation blade is determined, according to the size of safety coefficients, the position with the minimum influence of the loads on the blade structure is judged and segmented, and the blade is divided into a blade main body segment and blade tip segments. Blade tip serialization design is carried out, the aim that one blade has multiple lengths is achieved, and the blade is suitable for various kinds of wind fields. Wind energy can be developed and used to the maximum limit, and the electric generation amount is improved; and the design cost, the production cost and the manufacturing cost of the blade are reduced.

Description

一种叶尖系列化分段叶片及其设计方法A kind of blade tip series segmented blade and its design method

技术领域technical field

本发明涉及风力机叶片技术领域,具体涉及到一种叶尖系列化分段叶片设计概念及工艺实施。The invention relates to the technical field of wind turbine blades, in particular to a design concept and process implementation of serialized and segmented blades with blade tips.

背景技术Background technique

刚刚结束的巴黎气候大会要求各参与国进一步提高自主贡献的减排目标,提出在本世纪尽早达到温室气体“净零”排放,预计最快2050年左右有望全面实现可再生能源对化石能源的替代。我国政府承诺,2020年非化石能源占一次能源消费比重15%,2030年左右二氧化碳排放达到峰值并争取尽早实现,2030年单位国内GDP二氧化碳排放比2005年下降60%-65%,非化石能源占一次能源消费的20%。风电被公认为技术最成熟、最具开发前景的可再生能源。我国风资源丰富。据中国气象局《中国风能资源的详查和评估》,70米度层风能资源技术可开发量有26亿千瓦,在当前的经济技术水平下开发量至少是10亿千瓦级,随着技术进步,发展空间和潜力还将被进一步挖掘。The just-concluded Paris Climate Conference required all participating countries to further increase the emission reduction targets of their nationally determined contributions, and proposed to achieve "net zero" greenhouse gas emissions as early as possible in this century. It is expected that renewable energy will fully replace fossil energy by around 2050 at the earliest. . The Chinese government promises that non-fossil energy will account for 15% of primary energy consumption in 2020, and carbon dioxide emissions will peak around 2030 and strive to achieve it as soon as possible. 20% of primary energy consumption. Wind power is recognized as the most mature technology and the most promising renewable energy. my country is rich in wind resources. According to the China Meteorological Administration's "Detailed Investigation and Evaluation of Wind Energy Resources in China", the technically exploitable capacity of wind energy resources in the 70-meter layer is 2.6 billion kilowatts. Under the current economic and technological level, the development capacity is at least 1 billion kilowatts. With technological progress , the development space and potential will be further tapped.

风力机叶片作为风力机发电的关键零部件,有着越做越大,越做越长的发展趋势。叶片外形的加大增长,使得制造过程变难,表现在对厂房空间要求更大,模具制造成本上升,工人工艺操作便利性降低,叶片质量难于控制。由于大型叶片一般都安装在沿海岛屿、山区、高原地带,这使得风场地理位置偏远、交通不便,运输异常困难。叶片叶尖系列化分段叶片除了解决以上难题,还可以有效的降低叶片成本,叶尖段便于安装拆卸,可以更有效的捕捉风能,降低载荷。As a key component of wind turbine power generation, wind turbine blades have a development trend of becoming larger and longer. The increase of the shape of the blade makes the manufacturing process more difficult, which is reflected in the greater requirement for the workshop space, the increase of the mold manufacturing cost, the reduction of the convenience of the worker's process operation, and the difficulty of controlling the blade quality. Because large blades are generally installed in coastal islands, mountainous areas, and plateaus, the wind farms are located in remote locations, with inconvenient transportation, and transportation is extremely difficult. In addition to solving the above problems, the segmented blade tip series can also effectively reduce the cost of the blade. The blade tip section is easy to install and disassemble, which can capture wind energy more effectively and reduce the load.

目前,国内尚无低风速叶尖系列化分段叶片。本发明依据目前行业的现在,提出一种新型的叶尖系列化分段叶片设计。At present, there is no low-wind-speed blade-tip series segmented blades in China. According to the current state of the industry, the present invention proposes a novel blade tip serialized and segmented blade design.

发明内容Contents of the invention

本发明的目的是提出一种适用于各类型风场的风机叶片设计新概念——叶尖系列化分段叶片设计概念,在降低叶片设计成本,制造成本的同时,提高风电机组发电量。The purpose of the present invention is to propose a new concept of fan blade design applicable to various types of wind farms—the design concept of blade tip serialization and segmented blades, which can increase the power generation of wind turbines while reducing blade design costs and manufacturing costs.

本发明公开了一种叶尖系列化分段叶片设计方法,包括如下步骤:The invention discloses a blade tip serialization and segmentation blade design method, comprising the following steps:

步骤1:首先进行风机叶片气动设计,通过选用高效低阻的翼型,采用CFD软件并对风力机流场高精度性能进行数值模拟,包括二维翼型数值模拟和三维叶片数值模拟,分析,生成一款基础叶片,规格:发电功率1.5MW及其以上,叶片长度大于40m,叶片气动效率cp值大于0.48;Step 1: First, carry out the aerodynamic design of the fan blade. By selecting an airfoil with high efficiency and low resistance, CFD software is used to simulate the high-precision performance of the wind turbine flow field, including two-dimensional airfoil numerical simulation and three-dimensional blade numerical simulation, analysis, Generate a basic blade, specifications: generating power 1.5MW and above, blade length greater than 40m, blade aerodynamic efficiency cp value greater than 0.48;

步骤2:对该基础款叶片进行结构铺层设计,结构属性计算,建立BLADED模型,获取叶片载荷;Step 2: Design the structural layup of the basic blade, calculate the structural properties, establish the BLADED model, and obtain the blade load;

步骤3:通过气动-结构-载荷的相互迭代修改,依据气动外形进行初步结构设计,依据结构设计结果计算载荷,载荷反馈结构设计,对结构安全系数低的位置进行铺层修改或者是气动外形修改,在反馈计算载荷,如此反复迭代,确定基础叶片最终结构,。Step 3: Carry out preliminary structural design based on the aerodynamic shape through mutual iterative modification of aerodynamic-structure-load, calculate the load based on the structural design results, load feedback structure design, and modify the layup or aerodynamic shape of the position with a low safety factor of the structure , in the feedback calculation load, so repeated iterations, to determine the final structure of the basic blade,.

步骤4:并依据结构校核最终结果,生成叶片各截面各部件安全系数。以叶片尖部为起点,在叶尖点至叶片总长度10%截面的范围内选取安全系数大于1.5且距离叶尖最远处作为叶尖分段截面大小判断载荷对叶片结构影响较小的位置进行分段,将叶片分为叶片主体段和叶尖段。之后依据不同风场风况,综合考虑弦长分布函数,扭角分布函数,相对厚度分布函数,对叶尖段进行进一步的气动结构优化,生成三款以上不同长度叶尖段。Step 4: And according to the final result of the structure check, generate the safety factor of each section and each part of the blade. Taking the tip of the blade as the starting point, within the range from the tip point to the 10% section of the total length of the blade, select the position with a safety factor greater than 1.5 and the furthest distance from the tip as the segmental section size of the tip to determine the position where the load has less influence on the blade structure For segmentation, the blade is divided into a blade body segment and a blade tip segment. Afterwards, according to the wind conditions of different wind fields, the aerodynamic structure of the blade tip section is further optimized by comprehensively considering the chord length distribution function, twist angle distribution function, and relative thickness distribution function, and more than three types of blade tip sections with different lengths are generated.

本发明还公开了一种叶尖系列化分段叶片,采用上述的方法设计叶片,叶片分为两段:叶片主体段与叶片叶尖段,通过叶片连接件将叶片主体段和叶片叶尖段两段进行连接,形成完整的叶片结构。The invention also discloses a blade tip serialized segmented blade. The blade is designed by the above-mentioned method. The blade is divided into two sections: the main body section of the blade and the tip section of the blade. The main section of the blade and the tip section of the blade are connected by the blade connector The two sections are connected to form a complete blade structure.

叶片主体段的长度范围占叶片整体的90%~98%,叶片主体段包含叶片的主要承力构件主梁、腹板和尾缘梁。The length range of the main section of the blade accounts for 90%~98% of the whole blade, and the main section of the blade includes the main beam, web and trailing edge beam of the main load-bearing components of the blade.

至少有三款不同长度叶片叶尖段与一个叶片主体段匹配,与叶片主体段组装后形成至少三款整体长度不同的叶片。At least three types of blade tip segments with different lengths are matched with one blade body segment, and at least three types of blades with different overall lengths are formed after being assembled with the blade body segment.

本发明对叶片进行气动外形设计,通过多目标优化设计出一款基础叶片,并在其基础上,通过载荷计算,结构校核,选取载荷影响低的位置对叶片进行分段。将叶片分成两段,分别是叶片主体段和叶片叶尖段。在确定分段位置的基础上,对叶片气动外形进一步优化,保证叶片主体段外形不变,改变叶尖段的外形及长度,至少优化三款。叶片主体段与叶片叶尖段通过便于安装拆卸的连接件进行连接。依据风场风况不同,可更换适合的叶尖段,匹配最有利于风场风况的风力机叶片。本发明相比传统风机叶片,降低了模具制造成本,叶尖系列化使得一套叶片可选多种长度,降低叶片生产成本的同时,提升了发电量。The invention designs the aerodynamic shape of the blade, designs a basic blade through multi-objective optimization, and on the basis of the blade, calculates the load and checks the structure, and selects a position with low load influence to segment the blade. Divide the blade into two sections, the main section of the blade and the tip section of the blade. On the basis of determining the segment position, the aerodynamic shape of the blade is further optimized to ensure that the shape of the main section of the blade remains unchanged, and the shape and length of the tip section are changed, and at least three models are optimized. The main section of the blade is connected with the tip section of the blade through a connecting piece that is convenient for installation and disassembly. According to the different wind conditions of the wind field, the appropriate blade tip section can be replaced to match the wind turbine blades that are most conducive to the wind conditions of the wind field. Compared with traditional fan blades, the invention reduces mold manufacturing costs, and the serialization of blade tips enables a set of blades to be selected in various lengths, thereby reducing blade production costs and increasing power generation.

本发明具有如下有益效果:The present invention has following beneficial effect:

1、进行叶片叶尖系列化设计,实现了一款叶片多种长度,使得该叶片适用于各类型风场。1. Carry out serial design of the blade tips, and realize a blade with multiple lengths, making the blade suitable for various types of wind farms.

2、可以最大限度的挖掘利用风能,提升发电量。2. It can maximize the utilization of wind energy and increase the power generation.

3、降低了叶片的设计成本,生产成本,制造成本。3. The design cost, production cost and manufacturing cost of the blade are reduced.

附图说明Description of drawings

图1:叶尖系列化分段叶片整体效果图。Figure 1: The overall rendering of the blade tip series segmented blade.

具体实施方式detailed description

下面结合具体实施例对本发明作进一步说明。The present invention will be further described below in conjunction with specific examples.

一种叶尖系列化分段叶片设计方法,包括如下步骤:A blade tip serialization segmented blade design method, comprising the following steps:

步骤1:首先进行风机叶片气动外形设计,通过选用高效低阻的翼型,进行合理的翼型排布。采用CFD软件并对风力机流场高精度性能进行数值模拟,包括二维翼型数值模拟和三维叶片数值模拟,生成一款基础叶片,规格:发电功率1.5MW及其以上,叶片长度大于40m,叶片气动效率cp值大于0.48;Step 1: First, carry out the aerodynamic shape design of the fan blade, and carry out a reasonable airfoil arrangement by selecting an airfoil with high efficiency and low resistance. CFD software is used to simulate the high-precision performance of the wind turbine flow field, including two-dimensional airfoil numerical simulation and three-dimensional blade numerical simulation, and a basic blade is generated. Specifications: power generation 1.5MW and above, blade length greater than 40m, The cp value of blade aerodynamic efficiency is greater than 0.48;

步骤2:对该基础款叶片进行结构铺层设计,结构属性计算,建立BLADED模型,通过与对应功率整机参数匹配,获取叶片载荷;Step 2: Design the structural layer of the basic blade, calculate the structural properties, establish the BLADED model, and obtain the blade load by matching the parameters of the corresponding power machine;

步骤3:通过气动-结构-载荷的相互迭代修改,依据气动外形进行初步结构设计,依据结构设计结果计算载荷,载荷反馈结构设计,对结构安全系数低的位置进行铺层加强设计或者是气动外形修改,再反馈计算载荷,如此反复迭代,确定基础叶片最终结构。Step 3: Carry out preliminary structural design based on the aerodynamic shape through mutual iterative modification of aerodynamic-structure-load, calculate the load based on the structural design results, load feedback structural design, and carry out ply reinforcement design or aerodynamic shape for positions with low structural safety factors Modify, then feed back the calculated load, and iterate repeatedly to determine the final structure of the basic blade.

步骤4:依据结构校核最终结果,生成叶片各截面各部件安全系数。以叶片尖部为起点,在叶尖点至叶片总长度10%截面的范围内选取安全系数大于1.5且距离叶尖最远处作为叶尖分段截面大小判断载荷对叶片结构影响较小的位置进行分段,将叶片分为叶片主体段和叶尖段。Step 4: According to the final result of the structure check, generate the safety factor of each section and each part of the blade. Taking the tip of the blade as the starting point, within the range from the tip point to the 10% section of the total length of the blade, select the position with a safety factor greater than 1.5 and the furthest distance from the tip as the segmental section size of the tip to determine the position where the load has less influence on the blade structure For segmentation, the blade is divided into a blade body segment and a blade tip segment.

步骤5:依据不同风场风况,对叶尖段进行进一步的气动结构优化,生成三款以上不同长度叶尖段。对叶尖段结构进行设计,满足强度要求的同时,满足叶片防雷要求。Step 5: According to the wind conditions of different wind fields, further optimize the aerodynamic structure of the tip section, and generate more than three types of tip sections with different lengths. The structure of the tip section is designed to meet the strength requirements and at the same time meet the lightning protection requirements of the blades.

一种叶尖系列化分段叶片,采用上述的方法设计叶片,叶片分为两段:叶片主体段与叶片叶尖段,通过叶片连接件将叶片主体段和叶片叶尖段两段进行连接,形成完整的叶片结构。叶片主体段的长度范围占叶片整体的90%~98%,叶片主体段包含叶片的主要承力构件主梁、腹板和尾缘梁。至少有三款不同长度叶片叶尖段与一个叶片主体段匹配,与叶片主体段组装后形成至少三款整体长度不同的叶片。A blade tip series segmented blade, the blade is designed by the above method, the blade is divided into two sections: the main section of the blade and the tip section of the blade, and the main section of the blade and the tip section of the blade are connected by the blade connector, Form a complete leaf structure. The length range of the main section of the blade accounts for 90%~98% of the whole blade, and the main section of the blade includes the main beam, web and trailing edge beam of the main load-bearing components of the blade. At least three types of blade tip segments with different lengths are matched with one blade body segment, and at least three types of blades with different overall lengths are formed after being assembled with the blade body segment.

以上所述,仅是本发明的较佳实施例,并非对本发明作任何形式上的限制,任何熟悉本专业的技术人员,在不脱离本发明技术方案范围内,依据本发明的技术实质,对以上实施例所作的任何简单的修改、等同替换与改进等,均仍属于本发明技术方案的保护范围之内。The above are only preferred embodiments of the present invention, and are not intended to limit the present invention in any form. Any skilled person who is familiar with the profession, without departing from the scope of the technical solutions of the present invention, according to the technical essence of the present invention, Any simple modifications, equivalent replacements and improvements made in the above embodiments still fall within the protection scope of the technical solution of the present invention.

Claims (6)

1. a blade tip seriation subsection blade method for designing, it is characterised in that: comprise the steps:
Step 1: first carry out fan blade pneumatic design, by selecting the aerofoil profile of efficient low-resistance, uses CFD software to wind energy conversion system Flow field high precision performance carries out numerical simulation, including dimensional airfoil numerical simulation and three dimendional blade numerical simulation, generates a base Plinth blade, specification: generated output 1.5MW and more than, length of blade is more than 40m, and blade aerodynamic efficiency cp value is more than 0.48;
Step 2: this basis money blade carries out structure Lay up design, structure attribute calculates, and sets up BLADED model, obtains leaf Sheet load;
Step 3: by the mutual iteration of Aerodynamic-structure-load, carry out preliminary structure design according to aerodynamic configuration, according to structure Design result assumed (specified) load, load feedback arrangement designs, the position that design margin evaluation is low is carried out laying amendment or gas Dynamic profile amendment, then feed back assumed (specified) load, so iterate, determine basis blade final structure;
Step 4: check final result according to structure, generates each cross section of blade each piece safety coefficient.
2., with blade tip as starting point, in the range of blade tip point to vane overall length degree 10% cross section, choose safety coefficient more than 1.5 And distance blade tip farthest is as blade tip segmentation cross section, and blade is divided into blade body section and blade tip section.
3. blade tip seriation subsection blade as claimed in claim 1, it is characterised in that: according to different wind fields after step 4 Wind regime, carries out further pneumatic structure optimization to blade tip section, and optimization need to consider chord length distribution function, torsional angle distribution letter Number, relative thickness distribution function, it is ensured that blade profile smoothes out, and seamlessly transits, generate more than three sections different lengths at blade section Blade tip section.
4. a blade tip seriation subsection blade, it is characterised in that: use the method design blade described in claim 1, blade It is divided into two sections: blade body section and blade and blade apical segment, by blade connection, blade body section and blade and blade apical segment two sections is entered Row connects, and forms complete blade construction.
5. the blade tip seriation subsection blade stated such as claim 3, it is characterised in that: the length range of blade body section accounts for blade Overall 90% ~ 98%, blade body section comprises main load-carrying member girder, web and the trailing edge beam of blade.
6. the blade tip seriation subsection blade stated such as claim 3, it is characterised in that: at least three sections of different length blade tips Duan Yuyi blade body section coupling, forms, after assembling from blade body section, the blade that at least three money entire length are different.
CN201610221174.XA 2016-04-12 2016-04-12 Blade tip serialization segmentation blade and design method thereof Pending CN105822510A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112065652A (en) * 2020-09-10 2020-12-11 中材科技风电叶片股份有限公司 Wind turbine generator, wind turbine blade and active mass distribution control device of blade
CN112780485A (en) * 2021-03-02 2021-05-11 三一重能股份有限公司 Wind power blade design method and device

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101458735A (en) * 2008-12-31 2009-06-17 重庆大学 Aerofoil with high lift-drag ratio
EP2321105A2 (en) * 2008-06-27 2011-05-18 REpower Systems AG Method and manufacturing mold for the production of a rotor blade for a wind turbine
CN103277245A (en) * 2013-06-14 2013-09-04 中国科学院工程热物理研究所 Large-thickness blunt-trailing-edge wind-power airfoil profiles and a design method thereof
CN104033331A (en) * 2014-06-06 2014-09-10 株洲时代新材料科技股份有限公司 Method for designing wind power generation blade family
CN104405596A (en) * 2014-12-12 2015-03-11 华北电力大学 Wind turbine generator system low-wind-speed airfoil section family

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2321105A2 (en) * 2008-06-27 2011-05-18 REpower Systems AG Method and manufacturing mold for the production of a rotor blade for a wind turbine
CN101458735A (en) * 2008-12-31 2009-06-17 重庆大学 Aerofoil with high lift-drag ratio
CN103277245A (en) * 2013-06-14 2013-09-04 中国科学院工程热物理研究所 Large-thickness blunt-trailing-edge wind-power airfoil profiles and a design method thereof
CN104033331A (en) * 2014-06-06 2014-09-10 株洲时代新材料科技股份有限公司 Method for designing wind power generation blade family
CN104405596A (en) * 2014-12-12 2015-03-11 华北电力大学 Wind turbine generator system low-wind-speed airfoil section family

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
刘克刚: "风力机叶片设计与流场仿真", 《中国优秀硕士学位论文全文数据库 工程科技II辑》 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112065652A (en) * 2020-09-10 2020-12-11 中材科技风电叶片股份有限公司 Wind turbine generator, wind turbine blade and active mass distribution control device of blade
CN112780485A (en) * 2021-03-02 2021-05-11 三一重能股份有限公司 Wind power blade design method and device

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