The fabrication, materials characterization, and performance of thin film platinum rhodium thermocouples on gas turbine alloys was investigated. The materials chosen for the study were the turbine blade alloy systems MAR M200+Hf with NiCoCrAlY and FeCrAlY coatings, and vane alloy systems MAR M509 with FeCrAlY. Research was focussed on making improvements in the problem areas of coating substrate stability, adhesion, and insulation reliability and durability. Diffusion profiles between the substrate and coating with and without barrier coatings of Al2O3 are reported. The relationships between fabrication parameters of thermal oxidation and sputtering of the insulator and its characterization and performance are described. The best thin film ...
Operating temperatures in the hot sections of modern gas turbine engines reach as high as 1500°C, ma...
Temperatures of hot section components in today’s gas turbine engines reach as high as 1,500 °C, mak...
Thin film thermocouples have been developed for use on metal parts in jet engines to 1000 C. However...
Thin film surface temperature sensors were developed. The sensors were made of platinum-platinum/10 ...
Temperatures of hot section components in today’s gas turbine engines reach as high as 1,500 °C, mak...
The growth of thrust and improved aeroengine efficiency has been gained by increased temperatures t...
The increasing trend towards high-temperature, fuel efficient jet engines has led to the development...
Thin film thermocouples were developed for use on metal parts in jet engines to 1000 C. However, adv...
The objective is to develop thin film thermocouples (TFTC) for Space Shuttle Main Engine (SSME) comp...
The growth of thrust and improved aeroengine efficiency has been gained byincreased temperatures thr...
The growth of thrust and improved aeroengine efficiency has been gained byincreased temperatures thr...
A technique for fabricating Chromel and Alumel thin film thermocouples was developed. Turbine blade ...
Thin film platinum:palladium thermocouples were fabricated on alumina and mullite surfaces using rad...
The introduction of ceramic thermal barrier coatings, then monolithic ceramic blades and finally bla...
Thin film thermocouples provide a minimally intrusive means of measuring surface temperature in host...
Operating temperatures in the hot sections of modern gas turbine engines reach as high as 1500°C, ma...
Temperatures of hot section components in today’s gas turbine engines reach as high as 1,500 °C, mak...
Thin film thermocouples have been developed for use on metal parts in jet engines to 1000 C. However...
Thin film surface temperature sensors were developed. The sensors were made of platinum-platinum/10 ...
Temperatures of hot section components in today’s gas turbine engines reach as high as 1,500 °C, mak...
The growth of thrust and improved aeroengine efficiency has been gained by increased temperatures t...
The increasing trend towards high-temperature, fuel efficient jet engines has led to the development...
Thin film thermocouples were developed for use on metal parts in jet engines to 1000 C. However, adv...
The objective is to develop thin film thermocouples (TFTC) for Space Shuttle Main Engine (SSME) comp...
The growth of thrust and improved aeroengine efficiency has been gained byincreased temperatures thr...
The growth of thrust and improved aeroengine efficiency has been gained byincreased temperatures thr...
A technique for fabricating Chromel and Alumel thin film thermocouples was developed. Turbine blade ...
Thin film platinum:palladium thermocouples were fabricated on alumina and mullite surfaces using rad...
The introduction of ceramic thermal barrier coatings, then monolithic ceramic blades and finally bla...
Thin film thermocouples provide a minimally intrusive means of measuring surface temperature in host...
Operating temperatures in the hot sections of modern gas turbine engines reach as high as 1500°C, ma...
Temperatures of hot section components in today’s gas turbine engines reach as high as 1,500 °C, mak...
Thin film thermocouples have been developed for use on metal parts in jet engines to 1000 C. However...