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    • 1. 发明授权
    • Method and apparatus for replacing a vane assembly in a turbine engine
    • 用于更换涡轮发动机中的叶片组件的方法和装置
    • US5690469A
    • 1997-11-25
    • US660050
    • 1996-06-06
    • James L. DealFoster P. LammGustavo Moreno
    • James L. DealFoster P. LammGustavo Moreno
    • F01D25/00F01D5/00F01D5/30F01D9/04F04D29/32
    • F01D9/042F01D5/005F01D5/3023F04D29/322Y02T50/673Y10T29/49318Y10T29/49323
    • A repair kit for replacing an unserviceable vane assembly in a turbine engine includes a serviceable vane subassembly 120 having a serviceable airfoil 124 with a base 134 attached to the root end thereof and an opposing base 156 which is unattached to but slidably engagable with the serviceable airfoil. The opposing base is slipped over the tip end of the airfoil and slid toward the opposing base. The vane subassembly and opposing base are pivoted into position between inner and outer engine cases in place of an unserviceable vane assembly so that receptor sockets 148, 150 in the attached base engage support pins 72 extending from the inner case. An adhesive 182 is applied to the tip end of the serviceable airfoil and the opposing base is translated into its installed position near the tip end of the airfoil. Upon curing of the adhesive, the opposing base becomes attached to the airfoil. The base is secured to the outer case by studs 196 and nuts 198.
    • 用于更换涡轮发动机中的不可使用的叶片组件的修理工具包括可维修的叶片子组件120,其具有可使用的翼型件124,其具有附接到其根端的基部134和相对的底座156,其相对于底座156可滑动地与可用的翼型接合 。 相对的底座滑过翼型的末端并滑向相对的底座。 叶片子组件和相对的底座可以代替不可使用的叶片组件枢转到内外发动机壳体之间的位置,使得附接的底座中的接收器插座148,150接合从内壳延伸的支撑销72。 粘合剂182被施加到可使用的翼型件的末端,并且相对的底座被平移到靠近翼型的末端的安装位置。 在粘合剂固化时,相对的底部附着到翼型件上。 基座通过螺栓196和螺母198固定到外壳。