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    • 1. 发明申请
    • WIND TURBINE BLADE TUBULAR SPAR FABRICATING METHOD
    • 风力涡轮叶片管状制造方法
    • WO2012042506A8
    • 2013-01-31
    • PCT/IB2011054314
    • 2011-09-30
    • WILIC SARLCASAZZA MATTEOVERDESCA MATTEOSABBADIN AMEDEOBABY PHILIP
    • CASAZZA MATTEOVERDESCA MATTEOSABBADIN AMEDEOBABY PHILIP
    • F03D1/06
    • B29D99/0025B29C70/443B29L2031/085F03D1/0675F05B2280/6003Y02E10/721Y02P70/523
    • A method of fabricating a wind turbine blade tubular spar, wherein the tubular spar (22) extends along a given axis (A), is made of reinforced polymer material having fibres arranged in at least two directions, and a polymer matrix incorporating the fibres, and has two caps (23) and two webs (24); the method including the steps of : molding and cross-linking at least part of a cap (23) or web (24) in composite material; molding and cross-linking an L-shaped structure (25), which has two opposite parallel flanges (30, 37), and at least partly incorporates the previously molded, cross-linked cap (23) or web (24) of composite material; repeating the above steps to mold and cross-link a further L-shaped structure (25); and joining the two cross-linked, L- shaped structures (25), with the flanges (30, 37) positioned facing in pairs.
    • 一种制造风力涡轮机叶片管状翼梁的方法,其中所述管状翼梁(22)沿着给定的轴线(A)延伸,由具有至少两个方向布置的纤维的增强聚合物材料和包含纤维的聚合物基体制成, 并具有两个盖(23)和两个腹板(24); 该方法包括以下步骤:将复合材料中的帽(23)或纤维网(24)的至少一部分成型和交联; 模制和交联具有两个相对的平行凸缘(30,37)的L形结构(25),并且至少部分地并入先前模制的复合材料的交联盖(23)或网(24) ; 重复上述步骤以模制和交联另外的L形结构(25); 并连接两个交联的L形结构(25),其中所述凸缘(30,37)成对地定位。
    • 3. 发明申请
    • WIND TURBINE BLADE TUBULAR SPAR FABRICATING METHOD
    • 风力涡轮叶片管状制造方法
    • WO2012042506A3
    • 2012-09-13
    • PCT/IB2011054314
    • 2011-09-30
    • WILIC SARLCASAZZA MATTEOVERDESCA MATTEOSABBADIN AMEDEOBABY PHILIP
    • CASAZZA MATTEOVERDESCA MATTEOSABBADIN AMEDEOBABY PHILIP
    • F03D1/06
    • B29D99/0025B29C70/443B29L2031/085F03D1/0675F05B2280/6003Y02E10/721Y02P70/523
    • A method of fabricating a wind turbine blade tubular spar, wherein the tubular spar (22) extends along a given axis (A), is made of reinforced polymer material having fibres arranged in at least two directions, and a polymer matrix incorporating the fibres, and has two caps (23) and two webs (24); the method including the steps of : molding and cross-linking at least part of a cap (23) or web (24) in composite material; molding and cross-linking an L-shaped structure (25), which has two opposite parallel flanges (30, 37), and at least partly incorporates the previously molded, cross-linked cap (23) or web (24) of composite material; repeating the above steps to mold and cross-link a further L-shaped structure (25); and joining the two cross-linked, L- shaped structures (25), with the flanges (30, 37) positioned facing in pairs.
    • 一种制造风力涡轮机叶片管状翼梁的方法,其中所述管状翼梁(22)沿着给定的轴线(A)延伸,由具有至少两个方向布置的纤维的增强聚合物材料和包含纤维的聚合物基体制成, 并具有两个盖(23)和两个腹板(24); 该方法包括以下步骤:将复合材料中的帽(23)或纤维网(24)的至少一部分成型和交联; 模制和交联具有两个相对的平行凸缘(30,37)的L形结构(25),并且至少部分地并入先前模制的复合材料的交联盖(23)或网(24) ; 重复上述步骤以模制和交联另外的L形结构(25); 并连接两个交联的L形结构(25),其中所述凸缘(30,37)成对地定位。