The invention relates to a
rare earth oxide high-temperature
thermistor material suitable for
temperature measurement and control of an aero-engine and a preparation method thereof, the
thermistor takes
holmium oxide,
erbium trioxide,
thulium trioxide,
ytterbium trioxide,
lutetium trioxide and
tantalum pentoxide as raw materials, the
chemical composition is RETaO4, Ln = Ho, Er, Tm, Yb, Rm = 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 16, 17, 17, 17, 17, 17, 17, 17, 17, 17, 17, 17, 17, 17, 17, 17, 17, 17, 17, 17 The material constant B value range is 10565-15673 K, the resistivity is 2.20 * 10 < 5 >-1.295 * 10 < 6 >
omega.cm at the temperature of 500 DEG C, the linear determination coefficient R2 of ln rho and 1000 / T is greater than 99%, the
resistance drift rate is between 3.01% and 60%, and the absolute value of the
resistance drift rate of (HoErTmYbLu) 1 / 5TaO4 after aging for 50 hours at the temperature of 1500 DEG C is less than 3.01%. The high-temperature
thermistor prepared by the preparation method is stable in resistance performance and good in consistency, has an excellent
negative temperature coefficient thermosensitive characteristic in a wide temperature range of 400-1500 DEG C, and is suitable for manufacturing a high-performance high-temperature thermistor suitable for
temperature measurement and control of an aero-engine.