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SYSTEM AND METHOD FOR COVERING BLADE MOUNTING REGION OF TURBINE BLADE

机译:涡轮叶片的叶片安装区域的覆盖系统和方法

摘要

PROBLEM TO BE SOLVED: To provide a system and method for covering a blade mounting region of turbine blades.SOLUTION: A system 10 includes a turbine 18 having a turbine rotor 38, a plurality of blades 48, and a segmented cover assembly 40. The turbine rotor includes a blade mounting region 58 having a plurality blade mounts and first and second grooves 64, 66 extending circumferentially along the blade mounting region. The plurality of blades are disposed in the blade mounts 50. A segmented cover assembly includes a plurality of cover segments 74 configured to mount in the first and second grooves extending in a circumferential direction. A cover body 54 includes first and second lips extending along first and second circumferential portions of the cover body. The first lip is configured to mount in the circumferential direction along the first groove, and the second lip is configured to mount in the circumferential direction along the second groove.
机译:解决的问题:提供一种用于覆盖涡轮叶片的叶片安装区域的系统和方法。解决方案:系统10包括具有涡轮转子38,多个叶片48和分段式盖组件40的涡轮18。涡轮转子包括具有多个叶片安装座的叶片安装区域58以及沿着叶片安装区域周向延伸的第一和第二凹槽64、66。多个叶片布置在叶片安装座50中。分段的盖组件包括多个盖段74,所述多个盖段74构造成安装在沿圆周方向延伸的第一和第二凹槽中。盖体54包括沿着盖体的第一和第二圆周部分延伸的第一和第二唇。第一唇缘构造成沿着第一凹槽在圆周方向上安装,第二唇缘构造成沿着第二凹槽在圆周方向上安装。

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