US4118622A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Cone optical system
Assignee: Organisation Europeenne de Recherches Spatiales
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Filing: 1976-11-18
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Granted: 1978-10-03
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Expires: 1996-11-18
Abstract
Abstract A cone optical system comprising: (a) a convex conical mirror having a symmetry axis, (b) a refracting element having at least one conical surface, with a common symmetry axis with said convex conical mirror, said mirror and refracting element having apex angles selected such that a first paraxial light beam impinging said convex mirror in a direction substantially perpendicular to said symmetry axis is reflected toward said refracting element, traverses same and emerges therefrom as a second paraxial light beam, and (c) a collecting lens on the side of said refracting element opposite said mirror and adapted to focus said second light beam onto an image point located on said symmetry axis.
Inventors
- 👤 Karl-Heinz David
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-27 05:34
CPC Classifications
G; G02; G02B; G02B5/00; G02B5/001; G02B19/00; G02B19/0004; G02B19/0028; G02B19/0033; G02B19/0076; G02B19/008
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
128 words
A cone optical system, comprising: (a) a convex conical mirror (1) having a symmetry axis (Z), (b) a refracting element (2) having at least one conical surface with a common symmetry axis with said convex conical mirror, said mirror and refracting element having apex angles (α, β 1 , β 2 ) selected such that a first paraxial light beam (I) impinging said convex mirror (1) along a direction substantially perpendicular to said symmetry axis is reflected toward said refracting element (2), traverses same and emerges therefrom as a second paraxial light beam (II), and (c) a collecting lens (3) on the side of said refracting element opposite said mirror and adapted to focus said second light beam onto an image point (C) located on said symmetry axis.
Claim 2
Dependent Claim
128 words
A cone optical system, comprising: (a) a convex conical mirror (1) having a symmetry axis (Z), (b) a refracting element (2) having at least one conical surface with a common symmetry axis with said convex conical mirror, said mirror and refracting element having apex angles (α, β 1 , β 2 ) selected such that a first paraxial light beam (I) impinging said convex mirror (1) along a direction substantially perpendicular to said symmetry axis is reflected toward said refracting element (2), traverses same and emerges therefrom as a second paraxial light beam (II), and (c) a collecting lens (3) on the side of said refracting element opposite said mirror and adapted to focus said second light beam onto an image point (C) located on said symmetry axis.
Claim 3
Dependent Claim
30 words
A cone optical system as claimed in claim 1, wherein the apex angle (β 2 ) of one of the conical surfaces of said refracting element is equal to 180°.
Claim 4
Dependent Claim
21 words
A cone optical system as claimed in claim 1, wherein said convex mirror (1) and refracting element (2) have frusto-conical surfaces.
Claim 5
Dependent Claim
24 words
A cone optical system as claimed in claim 1, wherein said refracting element has its base so shaped as to form said collecting lens.
Claim 6
Dependent Claim
152 words
In an artificial spinning satellite having a spin axis, an apparatus comprising a cone optical system having its symmetry axis perpendicular to said spin axis, said optical system including (a) a convex conical mirror (1) having a symmetry axis (Z), (b) a refracting element (2) having at least one conical surface, with a common symmetry axis with said convex conical mirror, said mirror and refracting element having apex angles (α, β 1 , β 2 ) selected such that a first paraxial light beam (I) impinging said convex mirror (I) along a direction substantially perpendicular to said symmetry axis is reflected toward said refracting element (2), traverses same and emerges therefrom as a second paraxial light beam (II), and (c) a collecting lens (3) on the side of said refracting element opposite said mirror and adapted to focus said second light beam onto an image point (C) located on said symmetry axis.
Claim 7
Dependent Claim
152 words
In an artificial spinning satellite having a spin axis, an apparatus comprising a cone optical system having its symmetry axis perpendicular to said spin axis, said optical system including (a) a convex conical mirror (1) having a symmetry axis (Z), (b) a refracting element (2) having at least one conical surface, with a common symmetry axis with said convex conical mirror, said mirror and refracting element having apex angles (α, β 1 , β 2 ) selected such that a first paraxial light beam (I) impinging said convex mirror (I) along a direction substantially perpendicular to said symmetry axis is reflected toward said refracting element (2), traverses same and emerges therefrom as a second paraxial light beam (II), and (c) a collecting lens (3) on the side of said refracting element opposite said mirror and adapted to focus said second light beam onto an image point (C) located on said symmetry axis.
Claim 8
Dependent Claim
151 words
In an artificial spinning satellite having a spin axis, an apparatus comprising a cone optical system having its symmetry axis parallel with said spin axis, said system including (a) a convex conical mirror (1) having a symmetry axis (Z), (b) a refracting element (2) having at least one conical surface with a common symmetry axis with said convex conical mirror, said mirror and refracting element having apex angles (α, β 1 , β 2 ) selected such that a first paraxial light beam (I) impinging said convex mirror (1) along a direction substantially perpendicular to said symmetry axis is reflected toward said refracting element (2) traverses same and emerges therefrom as a second paraxial light beam (II), and (c) a collecting lens (3) on the side of said refracting element opposite said mirror and adapted to focus said second light beam onto an image point (C) located on said symmetry axis.
Claim 9
Dependent Claim
151 words
In an artificial spinning satellite having a spin axis, an apparatus comprising a cone optical system having its symmetry axis parallel with said spin axis, said system including (a) a convex conical mirror (1) having a symmetry axis (Z), (b) a refracting element (2) having at least one conical surface with a common symmetry axis with said convex conical mirror, said mirror and refracting element having apex angles (α, β 1 , β 2 ) selected such that a first paraxial light beam (I) impinging said convex mirror (1) along a direction substantially perpendicular to said symmetry axis is reflected toward said refracting element (2) traverses same and emerges therefrom as a second paraxial light beam (II), and (c) a collecting lens (3) on the side of said refracting element opposite said mirror and adapted to focus said second light beam onto an image point (C) located on said symmetry axis.
Claim 10
Dependent Claim
36 words
A cone optical system as claimed in claim 1, and photoelectric detecting means (4) located at said image point and having a sensitive element that is located in a plane (X-Y) perpendicular to said symmetry axis.
References Cited (Backward Citations)
US3383511A
Cited
US3838277A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1981-10-02 | 1982-04-03 | 1982-10-03 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-10-02 | 1986-04-03 | 1986-10-03 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-10-02 | 1990-04-03 | 1990-10-03 | $7700.00 | Window Closed / Lapsed |