Claims
- 1. A device (50) for steering an incident electromagnetic beam (L) from its original path to produce a deviated beam (T) transmitted at an angle (δ) from its original path, comprising:
an optical element (52) that is dynamically balanced but optically unbalanced, the optical element being comprised of at least two identically formed sections (52A, 52B) each of which are made of different materials, the materials forming the respective sections being substantially equal in density, but having significantly different indices (n1, n2) of refraction, so to produce deviation of the beam when the optical element is rotated or oscillated about an axis (S) of movement; and, means (M1) for rotating or oscillating the optical element about its axis.
- 2. The device of claim 1 further including a coupling lens (56) interposed between the incident beam and the optical element, and a coupling lens (58) interposed between the optical element and an output of the device.
- 3. The device of claim 2 in which at least one coupling lens comprises a plano-concave lens.
- 4. The device of claim 3 in which a curvature of a concave surface of at least one lens corresponds to that of an outer surface of the optical element (52).
- 5. The device of claim 2 in which the index of refraction of each coupling lens corresponds to that of the section of the optical element to which it is adjacent, so to minimize any deviation of the beam at the curved surfaces of the lenses and the optical element.
- 6. The device of claim 2 in which a diameter of the coupling lens (58) interposed between the optical element and an output of the device, is larger than the diameter of the coupling lens (56) interposed between the incident beam and the optical element, so to prevent vignetting.
- 7. The device of claim 5 in which one of the coupling lenses is made of a material which achromatizes the device so to minimize deviation in a beam due to color or wavelength
- 8. The device of claim 1 in which the optical element comprises a right circular cylinder with each section comprising one-half of the cylinder.
- 9. The device of claim 1 in which the optical element comprises a sphere with each section comprising a hemisphere.
- 10. The device of claim 1 in which each section forming the optical element comprises an optical wedge and the axis (S) of movement is parallel to the incident light beam (L).
- 11. The device of claim 1 in which the materials from which the sections are formed have substantially equal coefficients of thermal expansion
- 12. The device of claim 2 further including means (M2, M3) for moving at least one of the coupling lenses.
- 13. The device of claim 12 in which the coupling lenses are separately movable by their respective moving means.
- 14. The device of claim 2 in which an outer surface (58s) of the coupling lens (58) interposed between the optical element and the output of the device is a convex lens surface, which reduces the range of deviation attainable by the device.
- 15. The device of claim 2 in which an outer surface (58s) of the coupling lens (58) interposed between the optical element and the output of the device is a concave lens surface which increases the range of deviation attainable by the device.
- 16. The device of claim 2 in which an outer surface (58s) of the coupling lens (58) interposed between the optical element and the output of the device is an acylindrical surface which effects linearity of a scanned beam (T).
- 17. The device of claim 1 further including a second optical element (152) operating with the first said optical element so to provide a two-dimensional scanning device (150).
- 18. The device of claim 2 in which additional concave components with curvature nominally matching the curvature of the optical element are placed in close proximity to the optical element to stabilize its rotational movement.
CROSS REFERENCE TO RELATED APPLICATIONS
[0001] Provisional patent application No. 60/364,574 filed Mar. 18, 2002.
STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT
[0002] A portion of the research and development work involved in this invention was funded by the United States Army Space & Missile Defense Command.
Provisional Applications (1)
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Number |
Date |
Country |
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60364574 |
Mar 2002 |
US |