Invention Grant
US09176082B2 Measuring the damage to a turbine-blade thermal barrier 有权
测量对涡轮叶片热障的损坏

  • Patent Title: Measuring the damage to a turbine-blade thermal barrier
  • Patent Title (中): 测量对涡轮叶片热障的损坏
  • Application No.: US13700290
    Application Date: 2011-05-27
  • Publication No.: US09176082B2
    Publication Date: 2015-11-03
  • Inventor: Quentin Mistral
  • Applicant: Quentin Mistral
  • Applicant Address: FR Paris
  • Assignee: SNECMA
  • Current Assignee: SNECMA
  • Current Assignee Address: FR Paris
  • Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
  • Priority: FR1054371 20100603
  • International Application: PCT/FR2011/051227 WO 20110527
  • International Announcement: WO2011/151582 WO 20111208
  • Main IPC: G01N25/72
  • IPC: G01N25/72 F01D5/28 G01N17/00
Measuring the damage to a turbine-blade thermal barrier
Abstract:
A method for evaluating damage to a thermal barrier applied to a component made from a metal substrate, the thermal barrier including a sublayer of aluminum and a layer of columnar-structure ceramic material, the sub-layer being positioned between the substrate and the ceramic layer, the method including: a first calibration including selection of a determined number of calibration components that have undergone various degrees of damage, exposing them for a given length of time to radiation, measuring temperature obtained at the surface after the given length of time and establishing a curve connecting an increase in temperature to damage, and a second measuring the damage to the thermal barrier of the component including exposure to the radiation for the length of time, measuring the temperature obtained, and relating the increase in temperature to the calibration curve in order, from the curve, to extract the level of damage.
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