US2019256423A1PendingUtilityA1
Method of forming high thermal conductivity composite dielectric materials
Est. expiryMar 30, 2036(~9.7 yrs left)· nominal 20-yr term from priority
Inventors:Michael David Hill
C04B 2235/3222C04B 2235/3234C04B 2235/3224C04B 2235/3206C04B 2235/3236C04B 35/465C04B 2235/3225C04B 35/117C04B 2235/9607C04B 2235/3208C04B 2235/3227C04B 2235/3255C04B 35/46C04B 2235/3232
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Claims
Abstract
Disclosed herein are embodiments of materials having high thermal conductivity along with a high dielectric constants. In some embodiments, a two phase composite ceramic material can be formed having a contiguous aluminum oxide phase with a secondary phase embedded within the continuous phase. Example secondary phases include calcium titanate, strontium titanate, or titanium dioxide.
Claims
exact text as granted — not AI-modified1 . A method of forming a composite ceramic material, the method comprising:
mixing together materials that will form out a primary phase of aluminum oxide, a first secondary phase of CaTiO 3 located within the primary phase, and a second secondary phase of LaAlO 3 located within the primary phase, the materials forming the primary phase being generally non-reactive with materials forming the first and second secondary phases; and sintering the materials to form a composite ceramic having the primary phase and the first and second secondary phases, the composite ceramic having a dielectric constant of greater than 20 and a thermal conductivity of greater than 20 W·m −1 ·K −1 .
2 . (canceled)
3 . The method of claim 1 wherein the composite ceramic has a thermal conductivity of greater than 30 W·m −1 ·K −1 .
4 . (canceled)
5 . The method of claim 1 wherein the primary phase is generally contiguous.
6 . The method of claim 1 wherein the composite ceramic has a dielectric constant of greater than 25.
7 . The method of claim 1 wherein the composite ceramic has a dielectric constant of greater than 35.
8 . The method of claim 1 wherein the composite ceramic has a temperature drift of resonant frequency lower than 1000 ppm/Degree C.
9 . The method of claim 1 further comprising machining the composite ceramic.
10 . The method of claim 9 further comprising forming a radiofrequency component from the composite ceramic.
11 . A method of forming a composite ceramic material, the method comprising:
mixing together materials that will form out a primary phase of aluminum oxide, a first secondary phase of CaTiO 3 located within the primary phase, and a second secondary phase of La 2 MgTiO 6 located within the primary phase, the materials forming the primary phase being generally non-reactive with materials forming the first and second secondary phases; and sintering the materials to form a composite ceramic having the primary phase and the first and second secondary phases, the composite ceramic having a dielectric constant of greater than 20 and a thermal conductivity of greater than 20 W·m −1 ·K −1 .
12 . The method of claim 11 wherein the composite ceramic has a thermal conductivity of greater than 30 W·m −1 ·K −1 .
13 . The method of claim 11 wherein the primary phase is generally contiguous.
14 . The method of claim 11 wherein the composite ceramic has a dielectric constant of greater than 25.
15 . The method of claim 11 wherein the composite ceramic has a dielectric constant of greater than 35.
16 . The method of claim 11 wherein the composite ceramic has a temperature drift of resonant frequency lower than 1000 ppm/Degree C.
17 . A method of forming a composite ceramic material, the method comprising:
mixing together materials that will form out a primary phase of aluminum oxide, and a plurality of secondary phases, a first of the plurality of secondary phases being CaTiO 3 and a second of the plurality of secondary phases being selected from the group consisting of LaAlO 3 , La 2 MgTiO 6 , YALO 3 , SmAlO 3 , Mg 4 Nb 2 O 9 , and La 4 Ti 3 O 12 ; and sintering the materials to form a composite ceramic having the primary phase and the plurality of secondary phases, the composite ceramic having a dielectric constant of greater than 20.
18 . The method of claim 17 wherein the composite ceramic has a thermal conductivity of greater than 20 W·m −1 ·K −1 .
19 . The method of claim 17 wherein the composite ceramic has a thermal conductivity of greater than 30 W·m −1 ·K −1 .
20 . The method of claim 17 wherein the composite ceramic has a dielectric constant of greater than 25.
21 . The method of claim 17 wherein the composite ceramic has a dielectric constant of greater than 35.
22 . The method of claim 17 wherein the composite ceramic has a temperature drift of resonant frequency lower than 1000 ppm/Degree C.Join the waitlist — get patent alerts
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