Title :
Embedded temperature and heat flux sensors for advanced health monitoring of turbine engine components
Author :
Gutleber, Jonathan ; Brogan, Jeffrey ; Gambino, Richard J. ; Gouldstone, Christopher ; Greenlaw, Robert ; Sampath, Sanjay ; Longtin, Jon ; Zhu, Dongming
Author_Institution :
MesoScribe Technol., Inc., Stony Brook, NY
Abstract :
MesoScribe Technologies has developed a process for producing embedded, conformal, thick film sensors based on direct write technology. Thermocouple and heat flux sensors can be fabricated directly onto engineering components and embedded into functional coatings. This provides for a variety of vital advantages: reliability, robustness and survivability in extremely harsh environments, cost effective implementation, and fabrication onto surfaces that are large, conformal (non-flat) and flexible. Embedded thermocouples and heat flux sensors were deposited onto superalloy substrates and subjected to a number of high temperature tests including isothermal furnace heating, cyclic burner rig testing, and continuous flame impingement. Initial testing yields Seebeck coefficients within 3% of commercial thermocouples. Results also demonstrate that embedded Type K thermocouples survive over 200 thirty minute burner rig cycles with surface temperatures exceeding 1150degC. Embedding thermocouples at different depths within the TBC allows for simultaneous temperature measurements within the temperature gradient. In addition, over 20 hours of continuous flame impingement have been recorded with stable output. Embedded thermocouples were also tested at NASA GRC using a 3.5 kW CO 2 high heat flux laser which also allows extraction of thermal conductivity. The test comprised of 75 thirty minute cycles with a surface temperature of 1150degC and metal interface temperature of 930degC for a total duration of 41 hours. This very first test showed the capability of the embedded TC in terms of performance and durability. This paper summarizes the harsh environment test results as well as provides an overview of the capabilities of direct write technology to instrument propulsion and space structures
Keywords :
Seebeck effect; aerospace engines; aircraft maintenance; aircraft testing; gas turbines; thermocouples; thick film devices; 1150 C; 20 hours; 3.5 kW; 30 min; 30 ms; 41 hours; 930 C; Seebeck coefficients; advanced health monitoring; continuous flame impingement; direct write technology; embedded temperature sensor; embedded thermocouples; harsh environment test; heat flux sensors; instrument propulsion; isothermal furnace heating; rig testing; space structures; superalloy substrates; thick film sensors; turbine engine components; Fires; Heat engines; Monitoring; Space technology; Temperature measurement; Temperature sensors; Testing; Thermal conductivity; Thermal sensors; Turbines;
Conference_Titel :
Aerospace Conference, 2006 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
0-7803-9545-X
DOI :
10.1109/AERO.2006.1656117