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US3581099A Expired / Lapsed US ⏱️ 0.0 years remaining

Toric imaging lens for slot censors for satellites

Assignee: Ernst Leitz Wetzlar GmbH
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Filing: 1968-03-07
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Granted: 1971-05-25
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Expires: 1988-03-07
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Abstract

Abstract Five embodiments of slot sensors for stabilizing the position of a satellite in space are disclosed. All embodiments comprise a glass body having a refractive circumferential surface of 180* angular aperture. In the image plane of the refractive surface is disposed a slot diaphragm, the slot of which is arranged to coincide with the center plane of said glass body. Behind the slot diaphragm there is provided a photoelectric receiver which is sensitive to the electromagnetic rays which are incident on the sensor. In the different embodiments the slot diaphragms are shown to be positioned either in front of or behind the center of rotation of the toric glass body (in the direction of light travel) depending on the radius of the toric shape and on the refractive index of the glass.

Inventors

  • 👤 Georg G F Franke

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 17:34
CPC Classifications
B; B64; B64G; B64G1/00; B64G1/22; B64G1/24; B64G1/36; B64G1/365; G; G01; G01J; G01J1/00; G01J1/02; G01J1/04; G01J1/0407; G01J1/0411; G01J1/0425; G01J1/0437; G01J1/06; G02; G02B; G02B3/00; G01J1/0204; G01J1/0209

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 79 words
A toric imaging lens with a center plane for slot sensors for satellites, comprising in combination: a plane toric lens with boundary surfaces parallel and symmetric with said center plane and having a radius of rotation extending through an angle of 180*, said plane toric lens having a cylindrical recess concentric therewith, said recess having a slot diaphragm on said center plane; and a photoelectric receiver positioned in said center plane at the center of said radius of rotation.
Claim 2
Dependent Claim 79 words
A toric imaging lens with a center plane for slot sensors for satellites, comprising in combination: a plane toric lens with boundary surfaces parallel and symmetric with said center plane and having a radius of rotation extending through an angle of 180*, said plane toric lens having a cylindrical recess concentric therewith, said recess having a slot diaphragm on said center plane; and a photoelectric receiver positioned in said center plane at the center of said radius of rotation.
Claim 3
Dependent Claim 20 words
The lens of claim 1, wherein said diaphragm is a transparent opening on an opaque wall on said cylindrical recess.
Claim 4
Dependent Claim 31 words
The lens of claim 1, wherein said toric lens comprises two toric semiring lenses having cylindrical inner surfaces and said slot diaphragm is a slit in a solid, semicircular support material.
Claim 5
Dependent Claim 21 words
A slot sensor according to claim 3, wherein said ring lenses are substantially of the following radii and spacings: n 1.5

References Cited (Backward Citations)

US3040661A Cited
US2561508A Cited
US3062964A Cited
US3411011A Cited
US3361512A Cited
US3423593A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1974-05-24 1974-11-23 1975-05-25 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1978-05-24 1978-11-23 1979-05-25 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1982-05-24 1982-11-23 1983-05-25 $7700.00 Window Closed / Lapsed

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