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公开(公告)号：US06339878B1
公开(公告)日：2002-01-22
申请号：US09536364
申请日：2000-03-27
申请人： William D. Owen , Robert Baumgarten , Eric William Malmborg , Christopher Palazzini , Frank E. Palko
发明人： William D. Owen , Robert Baumgarten , Eric William Malmborg , Christopher Palazzini , Frank E. Palko
IPC分类号： B23P1500
CPC分类号： B23P6/005 , F01D5/005 , Y02T50/673 , Y10T29/49318 , Y10T29/49336
摘要： A method for repairing an airfoil is provided that includes the steps of: (a) determining repair regions of the airfoil that are likely to be damaged during a period of operation; (b) creating a stress profile for the airfoil that considers dynamic, steady-state, and residual stresses; (c) selecting a replacement section patch line using the stress profile and the determination of those regions likely to be damaged during operation; (d) providing an airfoil replacement section with a predetermined shape having a bond surface that substantially mates with the patch line; (e) removing a portion of the airfoil up to the patch line; (f) bonding the airfoil replacement section to the airfoil along the patch line; and (g) shaping the patched airfoil.
摘要翻译： 提供了一种修复翼型的方法，包括以下步骤：（a）确定在操作期间可能损坏的翼型件的修复区域; （b）为考虑动态，稳态和残余应力的翼型产生应力分布; （c）使用应力曲线选择替换部分贴片线，并确定在操作期间可能损坏的那些区域; （d）提供具有预定形状的翼型更换部分，所述预定形状具有与所述贴片线基本配合的粘结表面; （e）将所述翼型件的一部分去除直到所述贴片线; （f）沿翼片将机翼更换部分粘合到翼型件上; 和（g）成形修补翼型。
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公开(公告)号：US06766639B2
公开(公告)日：2004-07-27
申请号：US10261561
申请日：2002-09-30
IPC分类号： F02C600
CPC分类号： F02K3/06 , F02C7/045 , F05D2250/50 , F05D2260/96
摘要： An acoustic-structural LPC splitter assembly which comprises a structural acoustic splitter through which are arranged a plurality of bleed exhaust ports, the acoustic splitter having a first and second end, an inner and outer surface, a front joint for securing the first end, and a slip joint formed at an FEGV interface for securing the second end, wherein the structural acoustic splitter provides support sufficient to maintain concentricity of an LPC inner case.
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