High intensity light source blocking system and method

• US 9,415,745 B1
• Filed: 06/08/2012
• Issued: 08/16/2016
• Est. Priority Date: 06/08/2012
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Clemen, Mark Joseph Jr., Stewart, Alan F., Davis, Keith John, Wilenski, Mark Stewart
• Primary Examiner(s): Olszewski, John R
• Assistant Examiner(s): Cass, Jean-Paul
• Application Number:
  US13/491,691
• Time in Patent Office: 1,530 Days
• US Class Current: 1/1
• CPC Class Codes: B60J 3/04 adjustable in transparency
• CPC Class Codes: B60R 22/00 Safety belts or body harnesses in vehicles safety belts or body harnesses in general A62B35/00
• CPC Class Codes: B64C 1/1476 Canopies; Windscreens or similar transparent elements
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00

Abstract

A high intensity light source blocking system for a vehicle operated by a crew member within a cockpit includes an crew member position or eye-position detection system, a transparent dynamic-darkening display covering a window in the crew member cockpit, and a scene imager configured to detect a presence of a high intensity light source and an emanation direction relative to the crew member cockpit. A computing device is connected to the position or eye-position detection system, the transparent dynamic-darkening display and the scene imager, and controls the darkening of a portion of the dynamic-darkening display upon the occurrence of either the high intensity light source having an intensity value equal to or greater than a predetermined threshold, or the crew member position or eye-position being subject to either a direct portion of the high intensity light source or a substantial reflection thereof off a surface within the crew member cockpit.

Claims

1. A laser light blocking system for a vehicle operated by at least one crew member within a crew member cockpit, the system including:

an eye-position detection system that outputs a crew member eye-position relative to the crew member cockpit;

a transparent dynamic-darkening display covering at least one window in the crew member cockpit;

a scene imager system configured to detect a presence of a laser light from a laser device and an emanation direction of the laser light relative to the crew member cockpit, the scene imager system comprising a plurality of one of photo-detectors and spectral intensity detectors on a portion of the vehicle exterior to the crew member cockpit and within the interior of the crew member cockpit;

a computing device connected to the eye-position detection system, the transparent dynamic-darkening display and the scene imager system, the computing device controlling the darkening of at least a portion of the dynamic-darkening display upon the occurrence of;

the laser light having an intensity value equal to or greater than a predetermined threshold; and

the crew member eye-position being subject to at least one of at least a direct portion of the laser light, or a substantial reflection of at least a portion of the laser light reflected from a surface within the crew member cockpit, a laser light direction calculated relative to the crew member cockpit based on a difference in received light intensity signals in at least two of the plurality of one of photo-detectors and spectral intensity detectors based upon low-level scattering in one of

the air surrounding aircraft crew member cockpit, and

the crew member cockpit.

2. The laser light blocking system according to claim 1, the eye-position detection system including one of:

an eye-position detecting sensor integral with a crew member helmet;

or

a crew member cockpit mounted eye-position detecting sensor.

3. The laser light blocking system according to claim 1, the transparent dynamic-darkening display comprising at least one of a Liquid Crystal Display (LCD) element and an electrochromic element.

4. The laser light blocking system according to claim 3, the transparent dynamic-darkening display comprising a plurality of addressable dynamic-darkening elements that substantively covers the at least one window in the crew member cockpit.

5. The laser light blocking system according to claim 1, the at least one window in the crew member cockpit comprising a plurality of windows, where each of the plurality of windows is covered by the transparent dynamic-darkening display.

6. The laser light blocking system according to claim 1, the at least one window in the crew member cockpit comprising a canopy that covers a substantial portion of the crew member cockpit.

7. The laser light blocking system according to claim 1, the at least one scene imager comprising a broad frequency range one of a photo-detector and a spectral intensity detector configured to detect at least one frequency of the laser light and the intensity value of the laser light.

8. The laser light blocking system according to claim 7, the at least one scene imager further comprising an imager array configured to determine the emanation direction of the laser light relative to the crew member cockpit.

9. The laser light blocking system according to claim 1, the at least a portion of the dynamic-darkening display:

configured to applied to at least two windows in the crew member cockpit;

configured to applied to all windows in the crew member cockpit;

or

comprises two different portions of the dynamic-darkening display based on at least two crew members'"'"' eye-position relative to the crew member cockpit.

10. A laser light blocking system for an aircraft operated by at least one crew member within a crew member cockpit, the system including:

an eye-position detection system that outputs a crew member eye-position relative to the crew member cockpit;

a transparent dynamic-darkening display canopy covering the crew member cockpit;

a scene imager system configured to detect a presence of a laser light from a laser device and an emanation direction of the laser light relative to the crew member cockpit, the scene imager system comprising a plurality of one of photo-detectors and spectral intensity detectors on a portion of the vehicle exterior to the crew member cockpit and within the interior of the crew member cockpit;

a computing device connected to the eye-position detection system, the transparent dynamic-darkening display canopy and the scene imager system, the computing device controlling the darkening of at least a portion of the dynamic-darkening display canopy upon the occurrence of;

the laser light having an intensity value equal to or greater than a predetermined threshold; and

the crew member eye-position being subject to at least one of at least a direct portion of the laser light, or a substantial reflection of at least a portion of the laser light reflected from a surface within the crew member cockpit, a laser light direction calculated relative to the crew member cockpit based on a difference in received light intensity signals in at least two of the plurality of one of photo-detectors and spectral intensity detectors based upon low-level scattering in one of

the air surrounding aircraft crew member cockpit, and

the crew member cockpit.

11. The laser light blocking system according to claim 10, the eye-position detection system comprising one of:

a sensor integral with a crew member helmet; and

crew member cockpit sensors.

12. The laser light blocking system according to claim 10, the transparent dynamic-darkening display canopy comprising:

a plurality of addressable dynamic-darkening elements that substantively cover the transparent dynamic-darkening display canopy; and

at least one of a Liquid Crystal Display (LCD) element and an electrochromic element.

13. The laser light blocking system according to claim 10, the at least one scene imager comprising an imager array of one of broad frequency range photo-detectors and spectral intensity detectors configured to:

detect at least one frequency of the laser light and the intensity value of the laser light; and

determine the emanation direction of the laser light relative to the crew member cockpit.

14. The laser light blocking system according to claim 10, the at least a portion of the dynamic-darkening display canopy that is darkened further comprises darkening a gradient portion configured to transition between substantially transparent light transmission around a peripheral portion, to substantially opaque light transmission at a central portion.

15. A method that dynamically darkens an active window canopy of a crew member cockpit of an aircraft, the method comprising:

detecting a laser light from a laser device impinging on an active window canopy of a crew member cockpit;

darkening the entire active window canopy based on detecting the laser light and determining whether the laser light is above an intensity threshold;

configuring a plurality of one of photo-detectors and spectral intensity detectors on a portion of the aircraft exterior to the crew member cockpit and within the interior of the crew member cockpit;

calculating a laser light direction relative to the crew member cockpit based on a difference in received light intensity signals in at least two of the plurality of one of photo-detectors and spectral intensity detectors based upon low-level scattering in one of

the air surrounding aircraft crew member cockpit, and

the crew member cockpit; and

making the active window canopy transparent while darkening only a portion of the active window canopy at a first location on the active window canopy based upon determining the direction of the laser light and determining a relative position of at least one crew member in the crew member cockpit.

16. The method that dynamically darkens an active window canopy according to claim 15, where the darkening only the portion of the active window canopy at the first location further includes:

addressing a first series of addressable elements in a plurality of addressable dynamic-darkening elements that comprise the active window canopy, the first series of addressable elements corresponding to a first relative position of a first crew member in the crew member cockpit.

17. The method that dynamically darkens an active window canopy according to claim 16, where the darkening only the portion of the active window canopy at the first location further includes:

addressing a second series of addressable elements in the plurality of addressable dynamic-darkening elements that comprise the active window canopy, the second series of addressable elements corresponding to one of;

a second relative position of a second crew member in the crew member cockpit; and

the substantial reflection of the direction portion of the laser light reflected from the surface within the crew member cockpit with respect to a first relative position of a first crew member in the crew member cockpit.

18. The method that dynamically darkens an active window canopy according to claim 15, further comprising calculating a geo-location position of the laser light based on the plurality of one of photo-detectors and spectral intensity detectors calculating the laser light direction and a geospatial location system on the aircraft configured to compute an aircraft geospatial location.

19. The method that dynamically darkens an active window canopy according to claim 15, the darkening at least the portion of the active window canopy further comprises darkening a gradient portion of the active window canopy configured to transition between substantially transparent light transmission around a peripheral portion, to substantially opaque light transmission at a central portion.

20. The method that dynamically darkens an active window canopy according to claim 15, wherein the determining the relative position of that at least one crew member in the crew member cockpit further comprises:

determining a crew member eye-position for the at least one crew member in the crew member cockpit.

21. The method that dynamically darkens an active window canopy according to claim 20, wherein making the active window canopy transparent while darkening only a portion of the active window canopy at a first location on the active window canopy further comprises:

determining the direction of the laser light when the crew member eye-position for the at least one crew member is in one of

a direct portion of the high intensity light source; and

a substantial reflection of the direct portion of the laser light reflected from the surface within the crew member cockpit.