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公开(公告)号：US20160333849A1
公开(公告)日：2016-11-17
申请号：US15151806
申请日：2016-05-11
IPC分类号： F03D1/06
CPC分类号： F03D1/0675 , F05B2240/311 , Y02E10/721
摘要： A wind turbine blade which is at least 45m long. The blade has a main axis in the lengthwise direction from root to tip and an aerodynamic shell surrounding a spar which extends in a lengthwise direction along a substantial proportion of the blade at least a portion of the half of the shell closest to the tip. The blade is reinforced by high stiffness fibres having a Young's modulus to density ratio of greater than 50 GPa/(g·cm−3), and an electrical resistivity of greater than 1010 Ω·cm. The fibres are biaxial with a first axis angled with respect to the main axis at an acute angle and a second axis angled with respect to the main axis at an acute angle in the opposite sense to the first angle.
摘要翻译： 至少45米长的风力涡轮机叶片。 叶片具有从根部到尖端的长度方向上的主轴线，以及围绕翼梁的空气动力学外壳，所述翼梁围绕所述叶片的大部分沿所述叶片的大部分沿所述叶片的至少一部分最靠近所述尖端延伸。 叶片由杨氏模量密度比大于50GPa /（g·cm-3）的高刚度纤维和大于1010Ω·cm的电阻率增强。 纤维是双轴的，第一轴线以相对于主轴线成锐角的第一轴线和相对于主轴线成角度的第二轴线以与第一角度相反的方式成锐角。
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公开(公告)号：US20230175476A1
公开(公告)日：2023-06-08
申请号：US17923719
申请日：2020-05-08
CPC分类号： F03D1/0675 , B29C70/48 , B29C70/865 , F05B2280/6003 , F05B2230/90 , B29L2031/085
摘要： A method of manufacturing a wind turbine blade, comprising the steps of:
placing one or more shell fibre layers on a mould surface of a blade mould,
placing a plurality of separately provided preforms directly on the one or more shell fibre layers in a stacked arrangement,
infusing and curing the stacked preform arrangement, the one or more shell fibre layers together via a resin in mould cavity of the blade mould to form a wind turbine blade part with a spar cap integrated in a shell part providing part of the aerodynamic shape of the wind turbine blade.-
公开(公告)号：US20160348644A1
公开(公告)日：2016-12-01
申请号：US15166849
申请日：2016-05-27
发明人： Paul Trevor HAYDEN , Harald BEHMER
CPC分类号： F03D1/0683 , B29C65/48 , B29C65/483 , B29C65/5014 , B29C65/5064 , B29C66/1162 , B29C66/12261 , B29C66/12822 , B29C66/12842 , B29C66/43 , B29C66/721 , B29C66/7212 , B29C66/73751 , B29C66/73753 , B29C70/06 , B29C70/30 , B29L2031/085 , B32B3/02 , B32B5/26 , B32B2250/20 , B32B2260/023 , B32B2260/046 , B32B2603/00 , F03D13/10 , F05B2230/23 , F05B2280/6003 , Y02E10/721 , Y02P70/523 , B29K2307/04 , B29K2309/08 , B29K2309/14 , B29K2077/00
摘要： A composite member comprises first and second elongate composite elements. Each has a wedge shaped end with a complimentary tapered end surface. At least one of the components is formed of a stack of fibre layers impregnated in resin, with the tapered end surface being formed by each fibre layer extending longitudinally progressively further than the adjacent layer towards the thin end of the wedge at which the fibre layers have the greatest longitudinal extent. The components are joined at their tapered ends by an adhesive, and the properties of the cured composite material of the at least one component and/or the properties of the adhesive are different in the vicinity of the thin end of the wedge as compared to the rest of the tapered surface in order to reduce the stress concentrations in this region.
摘要翻译： 复合构件包括第一和第二细长复合元件。 每个具有楔形端部，具有互补的锥形端面。 至少一个部件由浸渍在树脂中的一叠纤维层形成，其中锥形端表面由每个纤维层形成，每个纤维层相对于相邻的层向纵向逐渐向楔形物的薄端延伸，纤维层具有 最大的纵向范围。 这些部件在其锥形端部通过粘合剂连接，并且与楔形件的薄端部相比，至少一个部件的固化的复合材料的性质和/或粘合剂的性质在楔形薄端附近是不同的 其余的锥形表面，以减少该区域的应力集中。
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公开(公告)号：US20210372373A1
公开(公告)日：2021-12-02
申请号：US17290947
申请日：2019-11-05
摘要： A sparcap for a spar structure inside a wind turbine blade is provided. A down conductor element is integrated on a side of the sparcap such that after assembly of the sparcap into the spar structure, the down conductor element extends along an outer corner of the spar structure.
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公开(公告)号：US20210340948A1
公开(公告)日：2021-11-04
申请号：US17283379
申请日：2019-10-29
摘要： A rotor blade assembly includes a rotor blade defining a pressure side and a suction side extending between a leading edge and a trailing edge. Further, the rotor blade assembly includes at least one structural feature secured within the rotor blade and spaced apart from the trailing edge to define a void between the pressure side, the suction side, and the trailing edge. Moreover, the rotor blade assembly includes an adhesive filling the void between the pressure side, the suction side, and the trailing edge to provide an adhesive connection between the pressure side, the suction side, the trailing edge, and the structural feature(s). In addition, the adhesive contacts the structural feature(s) at an interface and defines a fillet profile.
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公开(公告)号：US20170021578A1
公开(公告)日：2017-01-26
申请号：US15207738
申请日：2016-07-12
CPC分类号： B29C70/548 , B29C70/446 , B29C70/48 , B29C2033/422
摘要： The present invention relates to a method of moulding a composite article using a mould. The mould includes first and second rigid mould parts between them defining a mould cavity. A reservoir of resin is connected to an inlet into the mould cavity. A suction pump is connected to a port on the opposite side of the mould cavity from the inlet. At least one of the mould parts has an arrangement of grooves on the surface facing the mould cavity to distribute resin across the mould cavity. The method includes laying up fibres in the mould cavity, injecting resin from the reservoir by running the suction pump to fill the mould cavity with resin, curing the resin article to form a moulded article and opening the mould and removing the article.
摘要翻译： 本发明涉及使用模具成型复合制品的方法。 模具包括在它们之间的第一和第二刚性模具部件，其限定模腔。 树脂储存器连接到模腔中的入口。 抽吸泵与入口相对的模腔相反侧的端口连接。 至少一个模具部件在面向模具腔的表面上具有凹槽的布置，以将树脂分布在模具腔体上。 该方法包括在模腔中放置纤维，通过运行抽吸泵将树脂从储存器中注入，用树脂填充模具腔，固化树脂制品以形成模塑制品并打开模具并移除制品。
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公开(公告)号：US20230167806A1
公开(公告)日：2023-06-01
申请号：US17910623
申请日：2021-04-21
CPC分类号： F03D80/30 , F03D1/0675 , F05B2240/302 , F05B2240/307 , F05B2280/105 , F05B2280/1072
摘要： Disclosed is a tip section for a wind turbine blade. The tip section comprises an intermediary blade section comprising a first shell part forming a first side of the intermediary blade section and a second shell part forming a second side of the intermediary blade section, the intermediary blade section having a leading edge and a trailing edge and extending from an intermediary blade section first end to an intermediary blade section second end; a tip part forming an end of the tip section and having been rigidly attached to the intermediary blade section first end, the tip part having an outer surface comprising a metal area; and a number of one or more superficial metal strips extending along an outer surface of the intermediary blade section. A wind turbine blade with such a tip section and the manufacturing of such a wind turbine blade is also disclosed.
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8.发明申请WIND TURBINE BLADE AND A METHOD OF MOULDING A WIND TURBINE BLADE TIP SECTION 审中-公开风力涡轮机叶片和风力涡轮机叶片部分的成型方法公开(公告)号：US20160348642A1
公开(公告)日：2016-12-01
申请号：US15166484
申请日：2016-05-27
发明人： Paul Trevor HAYDEN , Harald BEHMER
摘要： A wind turbine blade and a method of moulding a wind turbine blade tip section. The overall wind turbine blade has an elongate structure extending in a radial sense in a finished wind turbine. The blade comprises a fairing that one is supported along its length by a spar extended along the full length of the fairing from the root end to the tip. The fairing is in two parts with a main part extending from the root for most the of the longitudinal length of the blade and the tip section forming the remainder of the blade.
摘要翻译： 风力涡轮机叶片和模制风力涡轮机叶片尖端部分的方法。 整个风力涡轮机叶片具有在成品风力涡轮机中以径向方向延伸的细长结构。 叶片包括整流罩，其沿着其长度由沿整流罩的整个长度从根端延伸到尖端的翼梁支撑。 整流罩分为两部分，其中主要部分从叶片的纵向长度的大部分延伸出来并且叶片部分形成叶片的其余部分。
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公开(公告)号：US20160346965A1
公开(公告)日：2016-12-01
申请号：US15162674
申请日：2016-05-24
CPC分类号： B29C43/12 , B29C33/02 , B29C33/10 , B29C43/3642 , B29C65/02 , B29C65/48 , B29C65/483 , B29C65/4835 , B29C65/7802 , B29C66/1162 , B29C66/1282 , B29C66/12841 , B29C66/14 , B29C66/342 , B29C66/5261 , B29C66/5268 , B29C66/721 , B29C66/73751 , B29C66/73752 , B29C66/73753 , B29C66/73754 , B29C66/73755 , B29C66/73941 , B29C66/81455 , B29C66/9292 , B29L2031/08 , B29L2031/085 , F03D1/0675 , Y02E10/721 , Y02P70/523
摘要： A method of forming a scarf joint between first and second elongate composite components, each having a complimentary tapered end surface is disclosed. At least one of the components is formed of a stack of fibre layers impregnated in resin, with the tapered end surface being formed by each fibre layer extending longitudinally progressively further than the adjacent layer. The method comprises applying adhesive to at least one of the tapered end surfaces, attaching a moulding tool around the first and second elongate components with their tapered end surfaces being adjacent to one another, applying a positive pressure increase to urge the tapered surfaces towards one another without locally reducing the pressure below the vapour pressure of the resin or adhesive throughout the curing process, and curing the resin and adhesive in the moulding tool with the pressure applied.
摘要翻译： 公开了一种在第一和第二细长复合部件之间形成切割接头的方法，每个具有互补的锥形端面。 至少一个部件由浸渍在树脂中的一叠纤维层形成，锥形端面由每个纤维层形成，每个纤维层比相邻层纵向逐渐延伸。 该方法包括将粘合剂施加到至少一个锥形端表面，将模制工具围绕第一和第二细长部件附接，其锥形端表面彼此相邻，施加正压力以增加锥形表面朝向彼此 而不会在整个固化过程中局部地将压力降低到树脂或粘合剂的蒸汽压力以下，并且在施加压力下固化模制工具中的树脂和粘合剂。
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公开(公告)号：US20160215757A1
公开(公告)日：2016-07-28
申请号：US14909193
申请日：2014-07-30
CPC分类号： F03D1/0675 , B29C70/086 , B29K2063/00 , B29K2105/089 , B29K2309/08 , B29K2675/00 , B29L2031/085 , F05B2260/95 , F05B2280/702 , Y02E10/721 , Y02P70/523
摘要： An erosion resistant aerodynamic fairing for a rotor blade. A fairing body is formed from at least one reinforcing fibre layer set in a cured resin. An erosion resistant pre-form is fixed to an outer surface of the fairing body. The erosion resistant pre-form comprises a thermoplastic film outer layer fused to a fibre substrate. The fibre substrate of the erosion resistant pre-form is impregnated with the cured resin of the fairing body which fixes at the preform to the fairing body.
摘要翻译： 用于转子叶片的抗侵蚀气动整流罩。 整流罩主体由固化树脂中的至少一个增强纤维层形成。 防侵蚀预制件固定到整流罩本体的外表面。 抗侵蚀预成型件包括与纤维基材熔合的热塑性薄膜外层。 防腐蚀预成型件的纤维基材用整流罩本体的固化树脂浸渍在预成型件上固定在整流罩上。
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