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CN201771696U - Integral blade of large scaled wind generating set - Google Patents

Integral blade of large scaled wind generating set Download PDF

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Publication number
CN201771696U
CN201771696U CN201020254251XU CN201020254251U CN201771696U CN 201771696 U CN201771696 U CN 201771696U CN 201020254251X U CN201020254251X U CN 201020254251XU CN 201020254251 U CN201020254251 U CN 201020254251U CN 201771696 U CN201771696 U CN 201771696U
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blade
fiber
trailing edge
integral
shell
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任伟华
李海龙
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INNER MONGOLIA SPACEFILGHT YIJIU TECHNOLOGY DEVELOPMENT Co Ltd
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INNER MONGOLIA SPACEFILGHT YIJIU TECHNOLOGY DEVELOPMENT Co Ltd
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    • 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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Abstract

本实用新型提供一种风力发电机组整体叶片,其内外纤维增强材料层是连续的,无任何胶结部位。在该整体叶片的内部有抗剪腹板及预制的梁帽,抗剪腹板和梁帽通过纤维增强基体材料固定,可以提高叶片的承载能力,缩短叶片的制造周期;因为叶片的后缘相对较窄,放置芯模有困难,所以整体叶片的后缘位置放置提前加工好的后缘粘结角,同时,因为整体叶片没有使用有毒的结构胶粘接材料,减少了对环境的污染和对操作人员的危害,也降低了成本。

Figure 201020254251

The utility model provides an integral blade of a wind power generating set, the inner and outer fiber reinforced material layers of which are continuous without any cemented parts. There are shear webs and prefabricated spar caps inside the integral blade, and the shear webs and spar caps are fixed by fiber-reinforced matrix materials, which can improve the bearing capacity of the blade and shorten the manufacturing cycle of the blade; because the trailing edge of the blade is relatively It is narrow, and it is difficult to place the mandrel, so the trailing edge of the overall blade is placed at the trailing edge bonding angle that has been processed in advance. At the same time, because the overall blade does not use toxic structural adhesive bonding materials, environmental pollution and damage to the environment are reduced. Operator hazards are also reduced.

Figure 201020254251

Description

一种大型风力发电机组整体叶片 A large-scale wind turbine integral blade

技术领域technical field

本实用新型属于风力发电领域,尤其涉及一种大型复合材料风力发电机组整体叶片。 The utility model belongs to the field of wind power generation, in particular to an integral blade of a large composite material wind power generating set. the

背景技术Background technique

目前,公知的大型复合材料风力发电机组叶片是采用真空辅助成型(VARI)工艺,分别制造叶片的迎风面壳体和背风面壳体两部分,在壳体前缘和后缘部位涂覆结构胶粘接成一个整体。两个壳体的中间,通常有抗剪腹板,抗剪腹板的数量根据结构设计来确定,抗剪腹板与壳体之间的连接也是通过胶接实现。采用该方法制造出来的叶片存在如下问题:粘接材料与纤维材料在材料特性上有差别,粘接部位容易开裂,在大载荷作用下叶片容易失效;抗剪腹板与上下壳体之间的粘接尺寸不好控制,增加制造难度;叶片的质量相对较重,原材料使用成本较高,没有充分发挥复合材料的特性;上下壳体胶接的过程中,操作人员暴露在有毒的结构胶挥发的气体中,对操作人员的健康造成威胁。 At present, the known large-scale composite material wind turbine blades adopt the vacuum-assisted forming (VARI) process to manufacture the windward side shell and the leeward side shell of the blade respectively, and apply structural glue on the leading edge and trailing edge of the shell. Bonded into a whole. In the middle of the two shells, there is usually a shear web. The number of shear webs is determined according to the structural design, and the connection between the shear web and the shell is also realized by bonding. The blades produced by this method have the following problems: there are differences in material properties between the bonding material and the fiber material, the bonding parts are prone to cracking, and the blades are prone to failure under heavy loads; The size of the bonding is not easy to control, which increases the difficulty of manufacturing; the quality of the blade is relatively heavy, the cost of raw materials is high, and the characteristics of the composite material are not fully utilized; during the bonding process of the upper and lower shells, the operator is exposed to the volatilization of toxic structural adhesives In the gas, it poses a threat to the health of the operator. the

实用新型内容Utility model content

为了克服现有叶片强度不足,制作周期长,制作成本高和对操作人员健康造成威胁的不足,本实用新型提供一种整体叶片,叶片在模具中一次成型,叶片承载能力提高,不使用粘接材料,不仅避免有害气体对人和环境的影响,同时缩短了叶片的加工周期,而且降低了叶片的制造成本。 In order to overcome the insufficient strength of existing blades, long production cycle, high production cost and threats to the health of operators, the utility model provides an integral blade, which is formed in a mold at one time, and the bearing capacity of the blade is improved without using bonding. The material not only avoids the impact of harmful gas on people and the environment, but also shortens the processing cycle of the blade and reduces the manufacturing cost of the blade. the

本实用新型解决上述技术问题所采用的技术方案是:一种风力发电用整体叶片,包括叶片壳体和位于叶片壳体中部的抗剪腹板。叶片壳体包括外部纤维铺层、夹芯、梁帽和内部纤维铺层。内外纤维铺层是连续的增强纤维,没有胶结部位,提高了叶片的强度。梁帽与夹芯同层置于内外纤维铺层之间。此外,梁帽经由纤维铺层搭接在抗剪腹板两端。 The technical solution adopted by the utility model to solve the above-mentioned technical problems is: an integral blade for wind power generation, including a blade shell and a shear web located in the middle of the blade shell. The blade shell consists of outer fiber layup, core, spar cap and inner fiber layup. The inner and outer fiber layers are continuous reinforcing fibers without cemented parts, which improves the strength of the blade. The beam cap and the sandwich core are placed between the inner and outer fiber layers in the same layer. In addition, the spar caps are lapped at both ends of the shear web via fiber layups. the

梁帽的长度延伸出抗剪腹板两端横向长度。此外,上述风力发电用整体叶片还包括至少一个所述抗剪腹板,用于承载所述叶片壳体,并且抗剪腹板通过纤维铺层与叶片壳体贴合,注胶后抗剪腹板和纤维铺层通过浸渍树脂材料固化而连接,使得抗剪腹板与叶片壳体成为整体,进一步提高了叶片的承载能力。此外,抗剪腹板可以是一个、两个、三个或更多,可根据叶片结构设计要求确定抗剪腹板的数量。 The length of the spar cap extends beyond the transverse length of the ends of the shear web. In addition, the above-mentioned integral blade for wind power generation also includes at least one said shear web, which is used to carry the blade shell, and the shear web is bonded to the blade shell through fiber layup, and the shear web is And the fiber layup is connected by impregnating the resin material to solidify, so that the shear web and the blade shell are integrated, and the bearing capacity of the blade is further improved. In addition, there can be one, two, three or more shear webs, and the number of shear webs can be determined according to the design requirements of the blade structure. the

内外纤维铺层采用玻璃纤维或碳纤维织物。叶片壳体用浸渍树脂材料采用不饱和聚酯树脂、乙烯基树脂或环氧树脂材料。 Fiberglass or carbon fiber fabrics are used for inner and outer fiber layups. The impregnated resin material for the blade shell adopts unsaturated polyester resin, vinyl resin or epoxy resin material. the

在叶片壳体后缘部位预埋置后缘粘结角,确保叶片后缘位置的几何形状,同时降低芯模的制作难度,并方便固化后取出芯模,整体提高了叶片的制造效率。 The trailing edge bonding angle is pre-embedded at the trailing edge of the blade shell to ensure the geometry of the trailing edge of the blade, while reducing the difficulty of making the mandrel and making it easy to take out the mandrel after curing, which improves the manufacturing efficiency of the blade as a whole. the

后缘粘结角采用轻木或PVC泡沫材料制成,其形状由叶片后缘处的几何形状所确定,可以是三角形结构。 The trailing edge bonding angle is made of balsa wood or PVC foam material, and its shape is determined by the geometry of the blade trailing edge, which can be a triangular structure. the

同时本实用新型采用真空辅助成型工艺提前预制抗剪腹板和梁帽,达到缩短叶片制造过程中注胶的时间,减少占模时间,提高生产效率的目的。 At the same time, the utility model adopts the vacuum-assisted forming process to prefabricate the shear web and the beam cap in advance, so as to shorten the time of glue injection in the blade manufacturing process, reduce the time occupied by the mold, and improve the production efficiency. the

本实用新型的有益效果是,叶片在模具中一次成型,保证叶片强度、刚度的同时,不使用粘接材料,缩短叶片制造时间,降低制造成本。 The beneficial effect of the utility model is that the blade is molded in a mold at one time, while ensuring the strength and rigidity of the blade, no bonding material is used, the manufacturing time of the blade is shortened, and the manufacturing cost is reduced. the

附图说明Description of drawings

下面结合附图对本实用新型进一步说明。 Below in conjunction with accompanying drawing, the utility model is further described. the

图1是现阶段叶片结构的截面示意图。 Fig. 1 is a schematic cross-sectional view of the blade structure at the present stage. the

图2是本实用新型整体叶片的结构示意图。 Fig. 2 is a structural schematic view of the whole blade of the utility model. the

图3是本实用新型整体叶片迎风面纤维铺层的制作示意图。 Fig. 3 is a schematic diagram of making the fiber layup on the windward side of the overall blade of the present invention. the

图4是本实用新型整体叶片芯模安放示意图。 Fig. 4 is a schematic diagram of placement of the integral blade mandrel of the present invention. the

图5是本实用新型整体叶片气囊和芯模间纤维铺层示意图。 Fig. 5 is a schematic diagram of the fiber layup between the integral blade airbag and the mandrel of the present invention. the

图6是本实用新型整体叶片背风面铺层的制作示意图。 Fig. 6 is a schematic diagram of making the leeward layer of the overall blade of the utility model. the

图7是本实用新型整体叶片注胶示意图。 Fig. 7 is a schematic diagram of glue injection for the whole blade of the present invention. the

图中:1.迎风面壳体,2.背风面壳体,3、4.抗剪腹板,5.前缘结构胶,6.腹板结构胶,7.后缘结构胶,8.整体叶片迎风面壳体,9.整体叶片迎风面梁帽,10.整体叶片背风面壳体,11.整体叶片背风面梁帽,12、13.抗剪腹板,14.后缘粘结角,15、16、17.腹板纤维铺层,18.模具加热系统,19.迎风面模具,20.外部纤维铺层,21.夹芯,22.内部纤维铺层,23.模具前缘吸胶用凹槽,24.模具后缘出胶用凹槽,25、26、27.芯模,28.背风面模具,29.注胶设备,30.吸胶设备。 In the figure: 1. Shell on the windward side, 2. Shell on the leeward side, 3, 4. Shear web, 5. Structural glue on the leading edge, 6. Structural glue on the web, 7. Structural glue on the trailing edge, 8. Overall Shell on the windward side of the blade, 9. Spar cap on the windward side of the integral blade, 10. Shell on the leeward side of the integral blade, 11. Spar cap on the leeward side of the integral blade, 12, 13. Shear web, 14. Bonding angle of the trailing edge, 15, 16, 17. Web fiber layup, 18. Mold heating system, 19. Windward side mold, 20. External fiber layup, 21. Sandwich, 22. Internal fiber layup, 23. Adhesive suction at the front edge of the mold Groove, 24. Groove for glue outlet at the trailing edge of the mold, 25, 26, 27. Mandrel, 28. Leeward mold, 29. Glue injection equipment, 30. Glue suction equipment. the

具体实施方式Detailed ways

在图1中,现阶段公知的叶片主要由迎风面壳体1和背风面壳体2,抗剪腹板3和4构成,迎风面壳体1和背风面壳体2分别在前缘位置使用前缘结构胶5胶接,在后缘位置使用后缘结构胶7胶接,同时上下两壳体与抗剪腹板3和4之间也是通过腹板结构胶6胶接固定。 In Fig. 1, the known blades at this stage are mainly composed of the windward side shell 1 and the leeward side shell 2, and the shear webs 3 and 4, and the windward side shell 1 and the leeward side shell 2 are respectively used at the leading edge position The leading edge structural glue 5 is glued, and the trailing edge structural glue 7 is glued at the trailing edge position. At the same time, the upper and lower shells and the shear webs 3 and 4 are also glued and fixed by the web structural glue 6 . the

在图2所示整体叶片的结构示意图中,整体叶片迎风面壳体8中有包含整体叶片迎风面梁帽9,整体叶片背风面壳体10中包含整体叶片背风面梁帽11,抗剪腹板12,13通过纤维 铺层15,16,17与整体叶片迎风面壳体8、整体叶片背风面壳体10贴合,经树脂材料浸渍后与纤维铺层15、16、17固化连接,进而与整体叶片迎风面壳体和背风面壳体8、10成为整体。整体叶片后缘部位有预制的后缘粘结角14,前后缘部位纤维铺层连续铺放。根据结构设计要求确定抗剪腹板的数量,抗剪腹板可以是一个,二个,也可以是三个或者更多。如图1所示,整体叶片迎风面梁帽9和整体叶片背风面梁帽11长度大于抗剪腹板12、13两端横向长度。 In the structural diagram of the integral blade shown in Figure 2, the shell 8 on the windward side of the integral blade contains a beam cap 9 on the windward side of the integral blade, and the shell 10 on the leeward side of the integral blade contains a spar cap 11 on the leeward side of the integral blade. The boards 12, 13 are laminated with the windward shell 8 of the integral blade and the leeward shell 10 of the integral blade through the fiber lay-ups 15, 16, 17, and are solidified and connected with the fiber lay-ups 15, 16, 17 after being impregnated with a resin material, and then It is integral with the windward side shell and the leeward side shell 8, 10 of the integral blade. There is a prefabricated trailing edge bonding angle 14 at the trailing edge of the overall blade, and the fiber layups at the trailing and trailing edges are laid continuously. The number of shear webs is determined according to the structural design requirements, and the number of shear webs can be one, two, or three or more. As shown in FIG. 1 , the lengths of the spar cap 9 on the windward side of the integral blade and the spar cap 11 on the leeward side of the integral blade are greater than the transverse lengths at both ends of the shear webs 12 and 13 . the

图3所示为整体叶片迎风面纤维铺层的制作示意图,这是整体叶片制造的第一步,将外部纤维铺层20放于整体叶片迎风面模具19上,在该迎风面模具19上安装模具加热系统18,其中纤维铺层可以是玻璃纤维也可以是碳纤维织物;接着,在外部纤维铺层20上铺放夹芯21和迎风面梁帽9,再铺放内部纤维铺层22,在迎风面模具19的右侧纤维铺层上安放后缘粘结角14,后缘粘结角14采用轻木或PVC泡沫材料提前加工而成,保证叶片在后缘部位的强度。如图3所示,后缘粘结角14的形状由叶片后缘部位的几何设计形状所确定,如三角形结构。迎风面模具19的前缘位置挖有模具前缘吸胶用凹槽23,用于后期叶片注胶插入注胶管,最后将多余的纤维铺层搭放在迎风面模具19的两侧。 Fig. 3 shows the schematic diagram of making the fiber layup on the windward side of the integral blade. This is the first step in the manufacture of the integral blade. The outer fiber layup 20 is placed on the windward side mold 19 of the integral blade, and installed Mold heating system 18, wherein the fiber layup can be glass fiber or carbon fiber fabric; then, on the outer fiber layup 20, the sandwich core 21 and the windward side spar cap 9 are laid, and then the inner fiber layup 22 is laid. The trailing edge bonding angle 14 is placed on the right fiber layer of the windward side mold 19, and the trailing edge bonding angle 14 is processed in advance by using balsa wood or PVC foam material to ensure the strength of the blade at the trailing edge. As shown in FIG. 3 , the shape of the trailing edge bonding angle 14 is determined by the geometric design shape of the trailing edge of the blade, such as a triangular structure. The front edge of the mold 19 on the windward side is dug with a groove 23 for sucking glue at the front edge of the mold, which is used for inserting the glue into the injection pipe for the later blades, and finally the redundant fiber layup is placed on both sides of the mold 19 on the windward side. the

在图4的整体叶片芯模安放示意图中,迎风面纤维铺层的制作完毕后,将通过真空辅助成型工艺提前预制好的抗剪腹板12、13放置于内部纤维铺层22上,抗剪腹板12、13的定位通过芯模25、26、27实现,芯模25、26、27采用软体材料,能够承受一定的压力,因为芯模的外形面用来保证叶片内腔的几何尺寸,要保证背风面铺层之后不会产生过大的变形,同时芯模25、26、27是可以压缩的,叶片注胶固化以后以便保证芯模25、26、27能够顺利取出。 In the schematic diagram of the overall blade mandrel placement in Figure 4, after the fiber layup on the windward side is fabricated, the shear webs 12 and 13 prefabricated by the vacuum-assisted forming process are placed on the inner fiber layup 22 to resist shearing. The positioning of the webs 12, 13 is realized by mandrels 25, 26, 27. The mandrels 25, 26, 27 are made of soft materials and can withstand a certain pressure, because the outer surface of the mandrel is used to ensure the geometric dimensions of the inner cavity of the blade. It is necessary to ensure that excessive deformation will not occur after the leeward side is laid, and the mandrel 25, 26, 27 can be compressed simultaneously, so as to ensure that the mandrel 25, 26, 27 can be taken out smoothly after the blade glue is injected and solidified. the

图5所示为整体叶片气囊和芯模之间的纤维铺层示意图,腹板纤维铺层15、16和17贴合抗剪腹板12、13,并在上下两端留有多余部分,多余部分搭在芯模25、26、27上。 Figure 5 is a schematic view of the fiber layup between the integral blade airbag and the mandrel. The web fiber layup 15, 16 and 17 fit the shear webs 12 and 13, and there are redundant parts at the upper and lower ends. Part rides on the mandrel 25,26,27. the

在图6的整体叶片背风面铺层的制作示意图中,将迎风面模具19两侧原有多余纤维铺层铺放到芯模25、27上,首先将内部纤维铺层22折回到芯模25、27上,接着铺放夹芯21,放置整体叶片背风面梁帽11,最后折回外部纤维铺层20。 In the schematic diagram of the production of the overall blade leeward side layup in Figure 6, the original excess fiber layup on both sides of the windward side mold 19 is placed on the mandrel 25, 27, and the inner fiber layup 22 is first folded back to the mandrel 25 , 27, then lay the sandwich core 21, place the overall blade leeward spar cap 11, and finally fold back the outer fiber layup 20. the

图7所示为整体叶片注胶示意图,背风面铺层的制作完毕后,将背风面模具28扣到迎风面模具19上,整体将模具逆时针翻转90°,在模具前缘吸胶用凹槽23上插入注胶管并与注胶设备29联通,模具后缘出胶用凹槽24与吸胶设备30联通。将背风面和迎风面模具28和19抽真空,向迎风面和背风面铺层注入树脂与固化剂的混合液体,树脂材料可以是不饱和聚酯树脂、乙烯基树脂或环氧树脂。在内外压强差的作用下,液体自下而上渗透整个铺层;混合液体流入吸胶设备30以后,停止注胶;通过模具加热系统18加热混合液体,等待固化成 型。最后,开启模具,脱模后取出叶片和内腔中的芯模25、26、27,形成整体叶片。 Figure 7 is a schematic diagram of glue injection for the overall blade. After the leeward side layup is finished, the leeward side mold 28 is fastened to the windward side mold 19, and the mold is turned 90° counterclockwise as a whole. The groove 23 is inserted with a glue injection pipe and communicated with the glue injection equipment 29, and the groove 24 for glue outlet at the trailing edge of the mold is communicated with the glue suction equipment 30. Vacuumize the molds 28 and 19 on the leeward side and the windward side, inject the mixed liquid of resin and curing agent into the windward side and the leeward side layup, and the resin material can be unsaturated polyester resin, vinyl resin or epoxy resin. Under the effect of internal and external pressure difference, the liquid permeates the entire layer from bottom to top; after the mixed liquid flows into the glue suction device 30, the injection of glue is stopped; the mixed liquid is heated by the mold heating system 18, and waits for curing and forming. Finally, the mold is opened, and the core molds 25, 26, 27 in the blade and the inner cavity are taken out after demoulding to form a whole blade. the

本文仅仅对本实用新型的优选实施方式进行了描述,然而对于本领域的技术人员而言,在不脱离本实用新型的精神的前提下是可以对本实用新型做出各种改进。因此,本实用新型并不限于上述优选实施方式,其保护范围由所附的权利要求书予以限定。 This article only describes the preferred implementation of the utility model, but for those skilled in the art, various improvements can be made to the utility model without departing from the spirit of the utility model. Therefore, the utility model is not limited to the preferred embodiments described above, and its protection scope is defined by the appended claims. the

Claims (9)

1.一种风力发电机用整体叶片,包括叶片壳体和位于叶片壳体中部的抗剪腹板,其特征在于,所述叶片壳体包括外部纤维铺层、夹芯、梁帽和内部纤维铺层,所述内外纤维铺层是连续的增强纤维,无胶接部位,所述梁帽经由纤维铺层搭接在所述抗剪腹板两端,并且与所述夹层同层位于内外纤维铺层之间。1. An integral blade for a wind power generator, comprising a blade shell and a shear web positioned at the middle of the blade shell, characterized in that the blade shell includes an outer fiber layup, a sandwich core, a spar cap and an inner fiber layup, the inner and outer fiber layups are continuous reinforcing fibers without glue joints, the spar caps are lapped at both ends of the shear web through the fiber layups, and are located on the same layer as the interlayer between the inner and outer fiber between layers. 2.根据权利要求1所述的整体叶片,其特征在于,所述梁帽延伸出所述抗剪腹板。2. The integral blade of claim 1, wherein the spar cap extends beyond the shear web. 3.根据权利要求1所述的整体叶片,其特征在于,包括至少一个所述抗剪腹板,用于承载所述叶片壳体,所述抗剪腹板通过纤维铺层与所述叶片壳体贴合。3. The integral blade according to claim 1, characterized in that it comprises at least one said shear web for carrying said blade shell, said shear web is bonded to said blade shell through fiber layup Considerate fit. 4.根据权利要求3所述的整体叶片,所述抗剪腹板与所述纤维铺层通过浸渍树脂材料并固化而连接。4. A monolithic blade according to claim 3, the shear web and the fiber layup being joined by impregnation with a resin material and curing. 5.根据权利要求1所述的整体叶片,其特征在于,所述内外纤维铺层采用玻璃纤维或碳纤维织物。5. The integral blade according to claim 1, wherein the inner and outer fiber layers are made of glass fiber or carbon fiber fabric. 6.根据权利要求1所述的整体叶片,其特征在于,所述叶片壳体的浸渍用树脂材料采用不饱和聚酯树脂、乙烯基树脂或环氧树脂材料。6 . The integral blade according to claim 1 , wherein the resin material for impregnation of the blade shell is made of unsaturated polyester resin, vinyl resin or epoxy resin material. 7.根据权利要求1所述的整体叶片,其特征在于,所述叶片壳体后缘位置埋有后缘粘结角。7. The integral blade according to claim 1, characterized in that, a trailing edge bonding angle is buried at the trailing edge of the blade shell. 8.根据权利要求7所述的整体叶片,其特征在于,所述后缘粘结角是采用轻木或PVC泡沫材料制成。8. The integral blade according to claim 7, wherein the trailing edge bonding angle is made of balsa wood or PVC foam material. 9.根据权利要求7所述的整体叶片,其特征在于,所述后缘粘结角是三角形结构的。 9. The integral blade according to claim 7, wherein the trailing edge bonding corner is triangular in structure. the
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Cited By (12)

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CN102518567A (en) * 2011-12-26 2012-06-27 无锡韦伯风能技术有限公司 Lightweight high-strength blade and manufacturing technology thereof
CN102672978A (en) * 2012-05-22 2012-09-19 昆山华风风电科技有限公司 Technique for manufacturing blade of wind-driven generator
CN103057126A (en) * 2012-12-14 2013-04-24 内蒙古金岗重工有限公司 Large-scale composite material integral molding blade and molding process thereof
CN105003393A (en) * 2015-06-29 2015-10-28 天津东汽风电叶片工程有限公司 Protective layer with ice removing and ice preventing functions for blade leading edge of wind driven generator
CN106378942A (en) * 2016-11-16 2017-02-08 连云港中复连众复合材料集团有限公司 Manufacturing and installation method of megawatt-stage wind turbine blade girder cap
CN107618192A (en) * 2017-09-28 2018-01-23 国电联合动力技术有限公司 A kind of wind power generation unit blade bonding angle and preparation method thereof
CN108044957A (en) * 2017-11-06 2018-05-18 中材科技(酒泉)风电叶片有限公司 Bonding angle is prefabricated and integral pouring and forming process
CN109397722A (en) * 2018-11-30 2019-03-01 深圳寰球乐飞技术有限公司 A kind of connection method and connection structure of the prefabricated web and blade shell of wind electricity blade
CN113830287A (en) * 2021-10-11 2021-12-24 贵州贵飞飞机设计研究院有限公司 Control surface with separated beam body edge strip and web plate surface and manufacturing method thereof
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Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102518567A (en) * 2011-12-26 2012-06-27 无锡韦伯风能技术有限公司 Lightweight high-strength blade and manufacturing technology thereof
CN102672978A (en) * 2012-05-22 2012-09-19 昆山华风风电科技有限公司 Technique for manufacturing blade of wind-driven generator
CN102672978B (en) * 2012-05-22 2015-01-28 昆山华风风电科技有限公司 Technique for manufacturing blade of wind-driven generator
CN103057126A (en) * 2012-12-14 2013-04-24 内蒙古金岗重工有限公司 Large-scale composite material integral molding blade and molding process thereof
CN105003393A (en) * 2015-06-29 2015-10-28 天津东汽风电叶片工程有限公司 Protective layer with ice removing and ice preventing functions for blade leading edge of wind driven generator
CN105003393B (en) * 2015-06-29 2017-12-12 东方电气(天津)风电叶片工程有限公司 A kind of wind driven generator vane front edge protective layer with ice-removing and ice-preventing function
CN106378942A (en) * 2016-11-16 2017-02-08 连云港中复连众复合材料集团有限公司 Manufacturing and installation method of megawatt-stage wind turbine blade girder cap
CN106378942B (en) * 2016-11-16 2018-10-09 连云港中复连众复合材料集团有限公司 A kind of preparation of blade of MW class wind turbine girder spar cap and its installation method
CN107618192B (en) * 2017-09-28 2024-05-24 国电联合动力技术有限公司 Wind turbine generator blade bonding angle and preparation method thereof
CN107618192A (en) * 2017-09-28 2018-01-23 国电联合动力技术有限公司 A kind of wind power generation unit blade bonding angle and preparation method thereof
CN108044957A (en) * 2017-11-06 2018-05-18 中材科技(酒泉)风电叶片有限公司 Bonding angle is prefabricated and integral pouring and forming process
CN108044957B (en) * 2017-11-06 2020-06-09 中材科技(酒泉)风电叶片有限公司 Prefabricated and integrated pouring forming process for bonding angle
CN109397722B (en) * 2018-11-30 2024-02-09 深圳寰球乐飞技术有限公司 Connection method and connection structure of prefabricated web plate and blade shell of wind power blade
CN109397722A (en) * 2018-11-30 2019-03-01 深圳寰球乐飞技术有限公司 A kind of connection method and connection structure of the prefabricated web and blade shell of wind electricity blade
WO2022247654A1 (en) * 2021-05-24 2022-12-01 中联重科股份有限公司 Fiber composite beam structure and manufacturing method therefor, boom section, boom, and mechanical device
CN113830287A (en) * 2021-10-11 2021-12-24 贵州贵飞飞机设计研究院有限公司 Control surface with separated beam body edge strip and web plate surface and manufacturing method thereof
CN113830287B (en) * 2021-10-11 2024-07-12 中航贵州飞机有限责任公司 Manufacturing method of control surface with separated beam body edge strip and web surface
CN115822867A (en) * 2023-02-01 2023-03-21 新创碳谷集团有限公司 Modularized wind power blade structure and manufacturing method thereof
CN115992791A (en) * 2023-02-08 2023-04-21 振石集团华智研究院(浙江)有限公司 Wind blade web structure, manufacturing method and wind blade

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