Claims
- 1. A flying spot scanning system comprising:
- means for generating a beam of high intensity light,
- a medium,
- optical means for imaging said beam to a spot at the surface of said medium at a predetermined distance from said optical means,
- a multifaceted polygon located in the path of said imaged beam between said beam generating means and said medium and having reflective facets for reflecting the beam incident to it onto said medium,
- means for rotating said polygon such that the reflected light is scanned in successive traces across said medium, and
- said optical means including a positive cylindrical lens positioned in the optical path of the beam between said polygon and said medium at a location such that runout errors are substantially corrected at said medium, the plane of no power of said cylindrical lens being oriented in the direction of the scan.
- 2. The structure as recited in claim 1:
- said beam generating means being a laser,
- means located between said laser and polygon for modulating the light beam in accordance with information content of electrical signals, and
- said medium being light sensitive.
- 3. The structure as recited in claim 1, wherein said facets are focused in the sagittal plane onto the surface of said medium.
- 4. The structure as recited in claim 3, wherein an intermediate focal point of the beam in the sagittal plane is at a location other than said facets.
- 5. The structure as recited in claim 4, wherein optimum spot size is provided at the surface of said medium.
- 6. The structure as recited in claim 1, wherein said cylindrical lens has a minimum focal number (f/number).sub.2 .congruent. b'/[2 tan.beta. (b' + b)], where b is the object distance of the origin of runout error as seen by said lens, b' is the distance of said lens from said medium surface, and .beta. is the angular measure of runout error.
- 7. The structure as recited in claim 6:
- said beam generating means being a laser,
- means located between said laser and polygon for modulating the light beam in accordance with information content of electrical signals, and said medium being light sensitive.
- 8. The structure as recited in claim 6, wherein said facets are focused in the sagittal plane onto the surface of said medium.
- 9. The structure as recited in claim 8, wherein an intermediate focal point of the beam in the sagittal plane is at a location other than said facets.
- 10. The structure as recited in claim 9, wherein optimum spot size is provided at the surface of said medium.
- 11. A flying spot scanning system comprising:
- means for generating a beam of high intensity light,
- a medium,
- first optical means for expanding said beam,
- second optical means in convolution with said first optical means, said first and second optical means defining a finite conjugate imaging system for imaging said expanded beam to a spot on the surface of said medium at a predetermined distance from said second optical means,
- a multifaceted polygon having reflective facets positioned in the optical path of said expanded beam to reflect said beam toward said medium,
- means for rotating said polygon such that said reflected beam is scanned through a scan angle to provide successive spot scanning traces across said medium,
- said second optical means including a positive cylindrical lens in the optical path of the beam so positioned between said polygon and said medium that runout errors are substantially corrected at said medium, the plane of no power of said cylindrical lens being oriented in the direction of scan.
- 12. The structure as recited in claim 11:
- said beam generating means being a laser,
- means located between said laser and polygon for modulating the light beam in accordance with information content of electrical signals, and
- said medium being light sensitive.
- 13. The structure as recited in claim 11, wherein said facets are focused in the sagittal plane onto the surface of said medium.
- 14. The structure as recited in claim 13, wherein an intermediate focal point of the beam in the sagittal plane is at a location other than said facets.
- 15. The structure as recited in claim 14, wherein optimum spot size is provided at the surface of said medium.
- 16. The structure as defined in claim 11, wherein said cylindrical lens has a minimum focal number (f/number).sub.2 .congruent.b'/[2 tan .beta. (b' + b)], where b is the object distance of the origin of runout error as seen by said lens, b' is the distance of said lens from said medium surface, and .beta. is the angular measure of runout error.
- 17. The structure as recited in claim 11
- said beam generating means being a laser,
- means located between said laser and polygon modulating the light beam in accordance with information content of electrical signals, and
- said medium being light sensitive.
- 18. The structure as recited in claim 16, wherein said facets are focused in the sagittal plane onto the surface of said medium.
- 19. The structure as recited in claim 18, wherein an intermediate focal point of the beam in the sagittal plane is at a location other than said facets.
- 20. The structure as recited in claim 19, wherein optimum spot size is provided at the surface of said medium.
RELATED APPLICATIONS
This application is a continuation-in-part application of application Ser. No. 309,874, filed Nov. 27, 1972, now abandoned.
US Referenced Citations (10)
Foreign Referenced Citations (1)
Number |
Date |
Country |
1,229,309 |
Apr 1971 |
UK |
Non-Patent Literature Citations (1)
Entry |
"Laser Raster Scanner"; by Latta; IBM Tech. Disc. Bulletin; vol. 13, No. 12, May, 1971, pp. 3879-3880. |
Continuation in Parts (1)
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Number |
Date |
Country |
Parent |
309874 |
Nov 1972 |
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