Patent · US Active

Simulation experimental test system for turbine blade thermal barrier coating working condition

US12158391B2 · kind B2 · utility

0Cited by
1References
13Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 6, 2019
Grant dateDec 3, 2024
Priority date
Expiry dateMay 22, 2040

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG01M99/002
  • WIPO fieldMeasurement
  • WIPO sectorInstruments

Abstract

Disclosed is a turbine vane thermal barrier coating working condition simulation experiment test system, including: a working state simulation device, a service environment simulation device and a detection device. The working state simulation device is provided on one side of the turbine vane thermal barrier coating to be tested, is connected to the turbine vane thermal barrier coating to be tested, and is configured to simulate a high-speed rotation working state of the turbine vane thermal barrier coating to be tested. The service environment simulation device is provided on the other side of the turbine vane thermal barrier coating to be tested. The detection device is configured to detect damage generated when the turbine vane thermal barrier coating to be tested rotates at a high speed in the service environment.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.