发明名称 Turbine blade and method of fabricating the same
摘要 <p>A turbine blade 12 includes at least two blade segments 16,18. Each blade segment includes first and second shells 21,23 joined together, a base region 22, at least one joint region 24 including a mating face 28. Each of the first and second shells includes an outer skin 26,27, a base spar cap 46 attached to an inner surface of the outer skin in the base region, a joint spar cap attached to the inner surface of the outer skin in the joint region and adjacent to at least a portion of the base spar cap. The joint spar cap 34 includes holes in the mating face of the joint region. The turbine blade 12 further includes fasteners 64,66 within the holes for securing the at least two blade segments together.</p>
申请公布号 EP2208885(A2) 申请公布日期 2010.07.21
申请号 EP20090177435 申请日期 2009.11.30
申请人 GENERAL ELECTRIC COMPANY 发明人 CHEN, XIANGLEI;BAEHMANN, PEGGY LYNN;LIN, WENDY WEN-LING;ZHOU, YOUDONG;QUEK, SHU CHING;PRAVEEN, GRAMA NARASIMHAPRASAD;KIRKPATRICK, BOWDEN;ZIIRIN, ROBERT MICHAEL;QIAN, GANG
分类号 F03D1/06 主分类号 F03D1/06
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