IP Library › Patent Application 16272411
Patent Application
App. No. 16/272,411

METHOD OF FORMING HIGH THERMAL CONDUCTIVITY COMPOSITE DIELECTRIC MATERIALS

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Patent No.
US None
App. No.
16/272,411
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 (28)

1 . 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.