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US4040096A Expired / Lapsed US ⏱️ 0.0 years remaining

Flying spot scanner with runout correction

Assignee: Xerox Corp
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Filing: 1975-10-28
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Granted: 1977-08-02
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Expires: 1995-10-28
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Abstract

Abstract A flying spot scanning system is provided by utilizing reflected light from a multifaceted rotating polygon which is then directed to the scanned medium. A light source illuminates a portion of the mirrored sides of the polygon during each scanning cycle, to provide a desired sequence of spot scanning. In each scanning cycle, information is transmitted to the scanned medium by modulating the light from the light source in accordance with a video signal. An optical convolution of elements is selected in combination with the light source to assure a uniform spot size throughout the scan width on the scanned medium. One of these elements is a cylindrical lens placed in the optical path between the polygon and the scanned medium for allowing a wide variance in runout tolerance of the scanning system.

Inventors

  • 👤 Gary K. Starkweather

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-27 14:57
CPC Classifications
H; H04; H04N; H04N1/00; H04N1/04; H04N1/113; H04N1/1135; G; G02; G02B; G02B26/00; G02B26/08; G02B26/10; G02B26/12; G02B26/127; G02B27/00; G02B27/0025; G02B27/0031; G06; G06K; G06K15/00; G06K15/02; G06K15/12; G06K15/1204; G06K15/1219; H04N3/00; H04N3/02; H04N3/08

Claims Analysis

Total Claims: 22
Claim 1
Independent Claim 144 words
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.
Claim 2
Dependent Claim 144 words
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.
Claim 3
Dependent Claim 40 words
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.
Claim 4
Dependent Claim 22 words
The structure as recited in claim 1, wherein said facets are focused in the sagittal plane onto the surface of said medium.
Claim 5
Dependent Claim 27 words
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.
Claim 6
Dependent Claim 19 words
The structure as recited in claim 4, wherein optimum spot size is provided at the surface of said medium.
Claim 7
Dependent Claim 61 words
The structure as recited in claim 1, wherein said cylindrical lens has a minimum focal number (f/number) 2 ≅ b'/[2 tanβ (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 β is the angular measure of runout error.
Claim 8
Dependent Claim 40 words
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.
Claim 9
Dependent Claim 22 words
The structure as recited in claim 6, wherein said facets are focused in the sagittal plane onto the surface of said medium.
Claim 10
Dependent Claim 27 words
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.
Claim 11
Dependent Claim 19 words
The structure as recited in claim 9, wherein optimum spot size is provided at the surface of said medium.
Claim 12
Dependent Claim 165 words
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.
Claim 13
Dependent Claim 165 words
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.
Claim 14
Dependent Claim 40 words
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.
Claim 15
Dependent Claim 22 words
The structure as recited in claim 11, wherein said facets are focused in the sagittal plane onto the surface of said medium.
Claim 16
Dependent Claim 27 words
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.
Claim 17
Dependent Claim 19 words
The structure as recited in claim 14, wherein optimum spot size is provided at the surface of said medium.
Claim 18
Dependent Claim 61 words
The structure as defined in claim 11, wherein said cylindrical lens has a minimum focal number (f/number) 2 ≅b'/[2 tan β (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 β is the angular measure of runout error.
Claim 19
Dependent Claim 39 words
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.
Claim 20
Dependent Claim 22 words
The structure as recited in claim 16, wherein said facets are focused in the sagittal plane onto the surface of said medium.
Claim 21
Dependent Claim 27 words
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.
Claim 22
Dependent Claim 19 words
The structure as recited in claim 19, wherein optimum spot size is provided at the surface of said medium.

References Cited (Backward Citations)

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USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1980-08-01 1981-01-31 1981-08-02 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1984-08-01 1985-01-31 1985-08-02 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1988-08-01 1989-01-31 1989-08-02 $7700.00 Window Closed / Lapsed

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