Use of fiber like materials to augment the cycle life of thick thermoprotective seal coatings
Abstract
Some experimental and analytical studies of plasma sprayed ZrO2-Y2O3 thick seal thermoprotective materials over NiCrAlY bond coats with testing to 1040 deg C in a Mach 0.3 burner flame are reviewed. These results indicate the need for material to have both compliance and sufficient strength to function successfully as a thick thermoprotective seal material. Fibrous materials may satisfy many of these requirements. A preliminary analysis simulating the simplified behavior of a 25 mm cylindrical SiO2-fiber material indicated significant radial temperature gradients, a relatively cool interface and generally acceptable stresses over the initial portion of the thermal cycle. Subsequent testing of these fiberlike materials in a Mach 0.3 Jet A/air burner flame confirmed these results.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- August 1982
- Bibcode:
- 1982STIN...8232633H
- Keywords:
-
- Ceramic Coatings;
- Gas Turbines;
- Plasma Spraying;
- Temperature Gradients;
- Thermal Cycling Tests;
- Thermal Protection;
- Engine Parts;
- Inelastic Stress;
- Stress Analysis;
- Substrates;
- Thermodynamic Efficiency;
- Fluid Mechanics and Heat Transfer