Multi-material mirror system

Patent metadata

Field	Value
Publication number	US-10877237-B2
Application number	US-201715828223-A
Country	US
Kind code	B2
Filing date	Nov 30, 2017
Priority date	Nov 30, 2017
Publication date	Dec 29, 2020
Grant date	Dec 29, 2020

Abstract

A mirror system is disclosed. The mirror system can include a primary mirror, and a secondary mirror supported relative to the primary mirror. The primary mirror and the secondary mirror can have different coefficients of thermal expansion (CTE). A negative CTE strut is also disclosed. The negative CTE strut can include a main body portion. The negative CTE strut can also include a first coupling portion and a second coupling portion disposed opposite one another about the main body portion and defining a strut length. The first and second coupling portions can each be configured to interface with an external structure. In addition, the negative CTE strut can include an offsetting extension member having a first end coupled to the main body portion and a second end coupled to the first coupling portion by an intermediate extension member. The first end can be between the first coupling portion and the second end. The first and second ends can define an offset length parallel to the strut length. When the negative CTE strut increases in temperature, the offset length can be configured to increase due to thermal expansion of the offsetting extension member sufficient to cause the strut length to decrease.

First claim

What is claimed is:

1. A mirror system, comprising:
a base having a near-zero CTE;
a primary mirror strut having a negative CTE;
a primary mirror coupled to, and supported by, the base via the primary mirror strut, the primary mirror having a non-zero CTE; and
a secondary mirror supported relative to the primary mirror, wherein the primary mirror and the secondary mirror have different coefficients of thermal expansion (CTE).

2. The mirror system of claim 1 , wherein the secondary mirror has a near-zero CTE.

3. The mirror system of claim 1 , further comprising a thermal strap thermally coupling the primary mirror and the primary mirror strut.

4. The mirror system of claim 1 , further comprising a secondary mirror strut extending from the base and coupled to the secondary mirror.

5. The mirror system of claim 4 , wherein the secondary mirror strut has a near-zero CTE.

6. The mirror system of claim 1 , wherein the base comprises at least one of a composite material or a nickel-iron alloy.

7. The mirror system of claim 6 , wherein the composite material comprises carbon fiber.

8. The mirror system of claim 6 , wherein the nickel-iron alloy comprises 64FeNi.

9. The mirror system of claim 1 , wherein the primary mirror comprises at least one of SiC or aluminum.

10. The mirror system of claim 1 , wherein the secondary mirror comprises at least one of a lithium-aluminosilicate glass-ceramic material or a titania-silicate glass material.

11. The mirror system of claim 1 , wherein the primary mirror and the secondary mirror form a Cassegrain reflector.

12. A mirror system, comprising:
a support structure having a base with a near-zero CTE, and primary and secondary mirror struts extending from the base, the primary mirror strut comprising a negative CTE;
a primary mirror coupled to the base by the primary mirror strut, the primary mirror being supported by the base and having a non-zero coefficient of thermal expansion (CTE); and
a secondary mirror coupled to the base by the secondary mirror strut and having a near-zero CTE.

13. The mirror system of claim 12 , further comprising a thermal strap thermally coupling the primary mirror and the primary mirror strut.

14. The mirror system of claim 12 , wherein the support structure comprises at least one of a composite material or a nickel-iron alloy.

15. The mirror system of claim 14 , wherein the composite material comprises carbon fiber.

16. The mirror system of claim 14 , wherein the nickel-iron alloy comprises 64FeNi.

17. The mirror system of claim 12 , wherein the secondary mirror strut has a near-zero CTE.

18. The mirror system of claim 12 , wherein the primary mirror comprises at least one of SiC or aluminum.

19. The mirror system of claim 12 , wherein the secondary mirror comprises at least one of a lithium-aluminosilicate glass-ceramic material or a titania-silicate glass material.

20. The mirror system of claim 12 , wherein the primary mirror and the secondary mirror form a Cassegrain reflector.

Assignees

• Raytheon Co

Inventors

• Carrigan Keith
• Silny John F

Classifications

• G02B17/061

  on-axis systems with at least one of the mirrors having a central aperture · CPC title

• G02B7/183

  specially adapted for very large mirrors, e.g. for astronomy, {or solar concentrators} · CPC title

• G02B7/008

  with means for compensating for changes in temperature or for controlling the temperature; thermal stabilisation · CPC title

• G02B7/181 Primary

  with means for compensating for changes in temperature or for controlling the temperature; thermal stabilisation · CPC title

• G02B23/16

  Housings; Caps; Mountings; Supports, e.g. with counterweight · CPC title