This invention relates generally to minimization of reflections from surfaces, and more specifically reflections from objective lenses or other reflective surfaces of wide-angle field of view optical devices.
Reflections from the objective lens or other reflective surfaces of an optical system (glint) have long been a problem, especially in a battlefield environment. These reflections turn out to also be a problem with wide-angle field-of-view (FOV) optics such as night vision goggles. This is especially so when operating in an environment where relatively bright ambient sources such as street lights are present, or in situations where the enemy also has night vision equipment and thus can see reflections of moon or starlight from an objective lens or reflective filter.
An existing method of reducing or eliminating such reflections is to put a honeycomb grid of tubes in front of the objective lens (as is described in U.S. Pat. No. 4,929,055, which is fully incorporated herein by reference). The tubes in these devices have walls that are parallel to the optical axis of the device to which it is fitted.
This technique, however, is not an effective solution with wide angle FOV devices, since if the length-to-width ratio of the tubes which make up the honeycomb of parallel-walled tubes is shallow enough not to vignette the view through the optic, then the tubes are not deep enough to give affective glint protection. This means that in a battlefield situation, wide-angle FOV optical devices are vulnerable to being detected by an envoy, and thus dangerous to use.
Accordingly, it is highly desirable, if not necessary, to devise other techniques for substantially preventing reflections from the reflecting surfaces of wide-angle FOV optical devices.
As can be seen in
An existing method of hiding such reflections is shown in
As shown in
As shown in
The problem has been how to get tubes long enough to provide effective glint protection without vignetting the view through the optic.
It is an objective of the present invention to provide reflection and glint protection while allowing a wide field of view (FOV) for surfaces including optical lenses.
The present invention includes an apparatus for reducing reflection on a surface including a plurality of concentric circular vanes, each of the vanes including a first end proximate the surface. The second end of the plurality of vanes is away from the surface. The first ends of the plurality of vanes are positioned closer together to each other than said second ends of said plurality of vanes.
This surface includes optical lenses, wide FOV lenses, binoculars, telescopes, gun sights and night vision goggles.
In another embodiment, the first ends of the plurality of vanes are positioned further apart from each other than the second ends of the plurality of vanes.
In another embodiment, a plurality of radial vanes are interconnected with the plurality of concentric circular vanes.
The present invention includes a system and method for reducing reflection from a surface of an optical lens comprising vane means for limiting reflections from said surface while maintaining a substantially wide Field of View (FOV) for said optical lens. The vane means is for mounting proximate a surface of the optical lens.
The foregoing and other features and advantages of the present invention will be more fully understood from the following detailed description of illustrative embodiments, taken in conjunction with the accompanying drawings in which:
In the novel technique, shown in one embodiment in
As shown in
As shown in
With this in mind, we describe a technique for protecting wide angle FOV optics from glint as shown in
As shown in
These tubes can be arranged in various manners. For example, in a section through one embodiment of such a shield as shown in
Alternatively, as shown in a section through another embodiment of such a shield in
As shown in
As shown in a front view in
This new technique of using non-parallel tube walls will give critical protection to wide-angle FOV optics on the battlefield.
Note that with this configuration, most points on the surface of the objective lens will have some of their lines of view blocked. This may cause a greater light loss than with the light loss from the earlier method of using a honeycomb of parallel-walled tubes. However, the increased light loss would be acceptable in many battlefield situations if this improved shield keeps the user of the optical device from being detected by the enemy because of reflections.
Further, with respect to the inwardly converging tubular elements as exemplified in
Suitable tubular elements for use in accordance with the present invention are disclosed in U.S. Pat. No. 4,929,055 and PCT/US93/11459, which are both fully incorporated herein by reference.
As various changes could be made in the above constructions without departing from the scope of the invention, it should be understood that all matter contained in the above description or shown in the accompanying drawings shall be interpreted as illustrative and not in a limiting sense.
The present application claims the benefit of U.S. Provisional Application No. 60/048,998 filed Jun. 9, 1997, which is fully incorporated herein by reference.
Number | Name | Date | Kind |
---|---|---|---|
693088 | Wadsworth | Feb 1902 | A |
4323298 | Brennan | Apr 1982 | A |
4365866 | Softly | Dec 1982 | A |
4929055 | Jones | May 1990 | A |
5210645 | Orino et al. | May 1993 | A |
Number | Date | Country |
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2 317 642 | Oct 1974 | DE |
414220 | Aug 1934 | GB |
WO 9533220 | Dec 1995 | WO |
Number | Date | Country | |
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20020039236 A1 | Apr 2002 | US |
Number | Date | Country | |
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60048998 | Jun 1997 | US |