Invention Grant
US08622016B2 Wear indication system for compressor diaphragms of gas turbine engines 失效
燃气轮机发动机压缩机隔膜的磨损指示系统

  • Patent Title: Wear indication system for compressor diaphragms of gas turbine engines
  • Patent Title (中): 燃气轮机发动机压缩机隔膜的磨损指示系统
  • Application No.: US13252429
    Application Date: 2011-10-04
  • Publication No.: US08622016B2
    Publication Date: 2014-01-07
  • Inventor: David J. Wiebe
  • Applicant: David J. Wiebe
  • Applicant Address: US FL Orlando
  • Assignee: Siemens Energy, Inc.
  • Current Assignee: Siemens Energy, Inc.
  • Current Assignee Address: US FL Orlando
  • Main IPC: G01D21/00
  • IPC: G01D21/00 F16D66/02
Wear indication system for compressor diaphragms of gas turbine engines
Abstract:
A wear indication system for use in turbine engines to measure gap closure that indicates the amount of wear found on a compressor diaphragm outer hook to prevent contact between a compressor vane attached to the compressor diaphragm outer hook and an upstream compressor blade. The wear indication system enables the wear to be serviced before failure occurs. The wear indication system may be formed from a base mounting plate having one or more wearable material layers attached thereto. In one embodiment, the wear indication system may have multiple wearable material layers. The outermost wearable layer may have a cross-sectional area less than a wearable layer to which it is attached to enable visual determination of the amount of wear that has occurred. The wearable layers may be formed from a honeycomb shaped material enabling wear to occur without threatening downstream components with damage.
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