Waveguide combiner system and method with less susceptibility to glare

• US 9,599,813 B1
• Filed: 05/10/2013
• Issued: 03/21/2017
• Est. Priority Date: 09/30/2011
• Status: Active Grant

• Current Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Buchholz, Chris M., Wilson, Brandon E., Stratton, Eric P., Keith, Christopher A., Stahl, Kurt A.
• Primary Examiner(s): Pham, Thomas K
• Assistant Examiner(s): Pichler, Marin
• Application Number:
  US13/892,057
• Time in Patent Office: 1,411 Days
• Field of Search: 359/566, 359/569, 359/572, 359/575, 359/576, 359/13, 359/630, 359/632, 359/633, 349/7, 349/8, 349/9, 348/115
• US Class Current: 1/1
• CPC Class Codes: B64D 43/00 Arrangements or adaptations of instruments arrangements of cameras B64D47/08; aeronautical measuring instruments per se G01C
• CPC Class Codes: G02B 2027/0118 comprising devices for improving the contrast of the display / brillance control visibility
• CPC Class Codes: G02B 2027/0125 Field-of-view increase by wavefront division
• CPC Class Codes: G02B 2027/0145 creating an intermediate image
• CPC Class Codes: G02B 2027/0194 with combiner of laminated type, for optical or mechanical aspects
• CPC Class Codes: G02B 27/0081 with means for altering, e.g. enlarging, the entrance or exit pupil
• CPC Class Codes: G02B 27/0101 characterised by optical features G02B27/0172 takes precedence
• CPC Class Codes: G02B 27/0103 comprising holographic elements
• CPC Class Codes: G02B 27/0149 characterised by mechanical features G02B27/0176 takes precedence
• CPC Class Codes: G02B 27/4205 having a diffractive optical element [DOE] contributing to image formation, e.g. whereby modulation transfer function MTF or optical aberrations are relevant
• CPC Class Codes: G02B 5/18 Diffraction gratings holographic optical elements G02B5/32, G03H; integrally combined with optical fibres G02B6/02057; for coupling light guides G02B6/34; integrally combined with optical integrated light guides G02B6/12; grating systems G02B27/44
• CPC Class Codes: G02B 6/0016 Grooves, prisms, gratings, scattering particles or rough surfaces
• CPC Class Codes: G02B 6/0035 provided on the surface of the light guide or in the bulk of it
• CPC Class Codes: G02F 1/163 Operation of electrochromic cells, e.g. electrodeposition cells; Circuit arrangements therefor

Abstract

A system and method for a head up display (HUD) can mitigate glare. The head up display can include a waveguide combiner including an input grating and an output grating and a glare mitigator disposed to prevent glare through the output grating from reaching an eye box. The glare mitigator can be a shade, a diffuser, a dimming element, or other device for mitigating glare. The glare mitigator can be an active or passive glare mitigator.

Claims

1. A head up display for use in a cockpit and for providing light from an image source, the head up display comprising:

a waveguide comprising a first waveguide portion physically coupled with a second waveguide portion, the first waveguide portion having a first end and disposed under and parallel to a top surface of a glare shield, the second waveguide portion having a second end and disposed at an angle with respect to the top surface of the glare shield, the waveguide having a first coupler at the first end and a second coupler at the second end, the waveguide positioned as a combiner and allowing viewing of an outside scene and information from the image source, the waveguide configured to cause light associated with the information to travel by total internal reflection from the first end to the second end, the waveguide having a glare reducer attached to the second waveguide portion and disposed between a surface of the waveguide and a windshield of the cockpit or between the surface of the waveguide and a ceiling of the cockpit, wherein the glare reducer is a directional diffuser configured to diffuse ambient light that enters the cockpit through the windshield before the ambient light enters the waveguide so that the ambient light enters the waveguide and travels through the waveguide towards the second coupler at an incident angle that causes the ambient light to diffract away from an eye motion box of a pilot upon exiting the waveguide, thereby reducing sunspot imaging via diffraction through the second coupler.

2. The head up display of claim 1, wherein the glare reducer is a diffuser spaced apart from the surface of the waveguide.

3. The head up display of claim 2, wherein the diffuser is attached to a top end of the waveguide and extends approximately parallel to the line of sight from a pilot towards a front of the cockpit.

4. The head up display of claim 1, wherein the first and second couplers are diffractive elements.

5. The head up display of claim 1, wherein the second coupler is disposed entirely above the top surface.

6. The head up display of claim 1, wherein the waveguide has substantially the same width as an exit pupil of collimating optics.

7. The head up display of claim 1, wherein light from the image source enters and leaves the waveguide on a same side.

8. The head up display of claim 1, wherein light from the image source enters and leaves on opposing sides.

9. The head up display of claim 1, further comprising a lens disposed between the waveguide and the image source.

10. The head up display of claim 1, wherein the first coupler has a greater efficiency than the second coupler.

11. A head up display, comprising:

a waveguide combiner including a first waveguide portion physically coupled with a second waveguide portion, the first waveguide portion having an input grating and disposed under and parallel to a top surface of a glare shield, the second waveguide portion having an output grating and disposed at an angle with respect to the top surface of the glare shield, wherein light travels from the input grating to the output grating by total internal reflection; and

a glare mitigator disposed to prevent glare through the output grating from reaching an eye box, the glare mitigator configured to diffuse ambient light before the ambient light enters the waveguide combiner so that the ambient light enters the waveguide combiner and travels through the waveguide combiner towards the output grating at an incident angle that causes the ambient light to diffract away from an eye motion box of a pilot upon exiting the waveguide combiner, thereby reducing sunspot imaging via diffraction through the output grating.

12. The head up display of claim 11, wherein the glare mitigator is a diffusive layer disposed above the output grating.

13. The head up display of claim 11, wherein the glare mitigator is a shade or a diffuser disposed above a glare shield and not parallel to the waveguide combiner.

14. The head up display of claim 11, wherein the glare mitigator includes an ambient sensor and an active element for diffusing sunlight in response to the ambient sensor.