Claims
- 1. A method for fabricating high-precision, thermally stable electromagnetic coil vanes, comprising the steps of:forming first and second coil pattern elements of substantially the same size and shape; and aligning and bonding the first and second coil pattern elements to respective first and second surfaces, of a substrate having a low coefficient of thermal expansion using a bonding composition contacting the substrate and a surface of each of said first and second coil pattern elements facing said substrate wherein the first and second coil pattern elements are positioned at substantially corresponding locations with respect to each other on the first and second surfaces of the substrate.
- 2. The method as recited in claim 1, wherein the first and second coil pattern elements have a ratio of wire width to gap of at least 2.5:1.
- 3. The method as recited in claim 1, wherein the substrate has the coefficient of thermal expansion of approximately 0.56×10−6/° C.
- 4. The method as recited in claim 1, wherein the substrate is quartz.
- 5. The method as recited in claim 1, wherein the bonding composition is thermagon, a heat curable bonding composition that cures without thermal deformation.
- 6. The method for fabricating high precision, thermally stable electromagnetic coil vanes, according to claim 1, further comprising the steps of:forming third, fourth, fifth and sixth complementary coil pattern elements; aligning and bonding the third, fourth, fifth and sixth complementary coil pattern elements to the substrate, wherein the third and fourth, and fifth and sixth coil pattern elements are positioned at substantially the same locations with respect to each other on the one the one surface and the other surface of the substrate, respectively; and curing the bonding composition on the opposing surfaces of the substrate to each coil pattern element.
- 7. The method as recited in claim 1, wherein the steps of aligning and bonding the first and second coil pattern elements comprises the steps of:extending a material into gaps of the first and second coil pattern elements to maintain a substantially uniform spacing of wires of the first and second coil pattern elements; placing a tape upon the first and second coil pattern elements to enable the spacing of the first and second coil pattern elements to be adhesively maintained; adhering the first coil pattern element to the first surface of the substrate, wherein the tape is affixed to the first coil pattern element; adhering the second coil pattern element relative to the second surface of the substrate, wherein the tape is affixed to the second coil pattern element, and wherein the first and second coil pattern elements are positioned at substantially the same locations with respect to each other on the first and second surfaces of the substrate, respectively; and clamping the first and second coil pattern elements and the substrate.
- 8. The method as recited in claim 7, further comprising the step of heating the first and second coil pattern elements and the substrate to enable the bonding composition to cure and bond the first and second coil pattern elements to the substrate.
- 9. The method as recited in claim 7, wherein the material is sheet metal.
- 10. The method as recited in claim 7, wherein the at least one of the aligning steps comprises the step of aligning a clamp plate with respect to a coil taping fixture.
- 11. The method as recited in claim 1, further comprising the step of removing the tape from the first and second coil pattern elements subsequent to said clamping step.
- 12. The method as recited in claim 5, wherein the tape is copper tape.
- 13. The method as recited in claim 12, wherein at least one of the aligning steps comprises the step of aligning the clamp plate to a clamp base.
- 14. The method as recited in claim 13, wherein at least one of the aligning steps further comprises the step of securing the clamp plate to the clamp base by a plurality of shoulder screws.
- 15. The method as recited in claim 14, wherein at least one of the aligning and bonding steps further comprises the step of positioning a spring between the shoulder screws and the clamp plate.
- 16. The method as recited in claim 15, herein the end spaces of each spring contact a spacer.
CROSS-REFERENCE TO RELATED APPLICATION
This application is related to U.S. patent application Ser. No. 09/324,899, filed Jun. 3, 1999, now U.S. Pat. No. 6,153,885 issued Nov. 28, 2000 by Rodney, Kendall for“Torroidal Charged particle Deflector With High Mechanical Stability and Accuracy” and assigned to a common assignee herewith. U.S. Pat. No. 6,153,885 is incorporated herein by reference.
US Referenced Citations (21)
Foreign Referenced Citations (3)
Number |
Date |
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403211804 |
Sep 1991 |
JP |
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Aug 1993 |
JP |
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Jun 1996 |
JP |