IP Library › Granted Patent US 10,488,646
Granted Patent B2
US 10,488,646 · App. 16/075,191 · Granted Nov 26, 2019

Realtime aiming zeroing reconnaissance sight

Inventors: Scott A Derushia (Amherst, NH); Michael J Choiniere (Merrimack, NH); John H Koltookian (Medford, MA)
Assignee: BAE Systems Information and Electronic Systems Integration Inc.
G02B23/145F41G1/14G02B23/105G03H1/22G03H2001/2284
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Quick Facts
Patent No.
US 10,488,646
App. No.
16/075,191
Granted
Nov 26, 2019
Kind
B2
Abstract

A holographic, single-unit, augmented sight has a housing containing a see-through holographic eyepiece; at least one of a visible light digital camera and an LWIR digital camera; a display to display an image from the camera(s); a shutter presenting the display; a red dot fiber-coupled LED reticle assembly using a spherical ball configuration sandwiched between two matching seats which are compressed together to contain the spherical ball configuration optical position; and a lever attached to the spherical ball configuration to rotate the ball by moving the lever up/down, left/right to adjust windage and elevation; a lower coupling prism presenting the reticle of the reticle assembly.

Claims (50)

1. A holographic, single-unit, augmented sight device comprising:

a single housing containing

a holographic eyepiece;

at least two internal digital cameras in said housing;

a display to display an image from either of said two internal digital cameras;

a shutter switching to said display;

a red dot fiber-coupled LED reticle assembly;

a lower coupling prism presenting a reticle of said reticle assembly;

wherein said at least two internal digital cameras include a visible wavelength digital color camera and a Long Wave Infrared (LWIR) digital camera;

wherein said red dot fiber-coupled LED reticle assembly comprises:

a spherical ball configuration;

said spherical ball configuration sandwiched between two matching seats, said seats compressed together to contain said ball configuration optical position; and

a lever attached to said spherical ball configuration, said lever configured to rotate said spherical ball by moving said lever up/down and left/right thereby providing a slight translation necessary to adjust windage and elevation, whereby only minor translation is needed for red dot adjustment.

2. The device of claim 1 , wherein said display is an OLED/LCD display.

3. The device of claim 1 , wherein said shutter is an electro-optical shutter.

4. The device of claim 1 , wherein said red dot fiber-coupled LED reticle assembly comprises:

two compression plates;

a collimator;

optics; and

two drive screws for lever adjustment;

whereby two sliding translation stages move said collimator position up/down or left/right, and a part count is significantly reduced, reducing cost and increasing reliability of aim point position.

5. The device of claim 1 , further comprising molded glass optics.

6. The device of claim 1 , wherein said device includes only one prism.

7. The device of claim 6 , wherein said device is a Realtime Aiming Zeroing Reconnaissance system.

8. The device of claim 1 , wherein said device is a pocket scope/viewer.

9. The device of claim 1 , further comprising a zoom capability.

10. The device of claim 1 , further comprising a red dot aim point generated by the red dot fiber-coupled LED reticle assembly for the at least two internal digital cameras.

11. A method for using a holographic, single-unit, augmented sight device comprising:

providing a single housing containing a holographic eyepiece; at least two internal digital cameras; a display to display an image from either of said two internal digital cameras; a shutter presenting said display; a red dot fiber-coupled LED reticle assembly; and a lower coupling prism presenting reticle of said reticle assembly; and

aiming, through said holographic, single-unit, augmented sight at a target in at least one of visible and Long Wave Infrared (LWIR) wavelengths;

wherein said at least two internal digital cameras comprise a visible wavelength digital color camera and a LWIR digital camera; and

wherein windage and elevation adjustment is accomplished by rotating a spherical ball of said red dot fiber-coupled LED reticle assembly by moving a lever up/down, left/right, whereby only minor translation is needed for red dot adjustment.

12. The method of claim 11 , wherein said at least two internal digital cameras each comprise:

about a 40 degree field of view at about a 1 power zoom;

about a 20 degree field of view at about a 2 power zoom;

about a 10 degree field of view at about a 4 power zoom; and

about a 5 degree field of view at about an 8 power zoom, wherein said about 5 degree, about 8 power zoom is full native resolution.

13. The method of claim 11 , wherein said aiming includes both color visible and LWIR wavelengths.

14. The method of claim 11 , wherein a cover is flipped down to sight optics that serves to turn on a visible camera subsystem and block light coming into said sight, allowing clear viewing of said display which provides a magnified scene to a user.

15. A holographic, single-unit, augmented sight system comprising:

a single housing containing

a holographic eyepiece;

a visible wavelength digital camera;

an Long Wave Infrared (LWIR) wavelength digital camera;

a display to display an image from said cameras;

an LCD shutter presenting said display;

a red dot fiber-coupled LED reticle assembly comprising a spherical ball configuration;

said spherical ball configuration sandwiched between two matching compression plate seats, said seats compressed together to contain said ball configuration optical position; a collimator; optics; and two drive screws; a lever attached to said spherical ball configuration, said lever providing a means to rotate said ball by moving said lever up/down, left/right thereby providing a slight translation necessary to adjust windage and elevation, whereby only minor translation is needed for red dot adjustment and a part count is significantly reduced, reducing cost and increasing reliability of aim point position; and

a lower coupling prism presenting reticle of said reticle assembly;

said sight providing about a 40 degree field of view at about a 1 power zoom; about a 20 degree field of view at about a 2 power zoom; about a 10 degree field of view at about a 4 power zoom; and about a 5 degree field of view at about an 8 power zoom.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 3, 2018
From: DERUSHIA, SCOTT A.; CHOINIERE, MICHAEL J.; KOLTOOKIAN, JOHN H.
To: BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC.
Reel/Frame 046547/0150 →
Continuity (1)
Related Publication 20190041626A1 · Feb 7, 2019
Cited By (1)
US 12,723,842