Compact head up display (HUD) for cockpits with constrained space envelopes

• US 8,749,890 B1
• Filed: 09/30/2011
• Issued: 06/10/2014
• 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: Wood, Robert B., Brown, Robert D., Theriault, Ricky J., Pond, Duane P. M., Burns, Lincoln J.
• Primary Examiner(s): Jones, James
• Application Number:
  US13/250,994
• Time in Patent Office: 984 Days
• Field of Search: 359/630
• US Class Current: 359/632
• CPC Class Codes: G02B 2027/015 involving arrangement aiming to get less bulky devices
• CPC Class Codes: G02B 27/0101 characterised by optical features G02B27/0172 takes precedence
• CPC Class Codes: G02B 27/0149 characterised by mechanical features G02B27/0176 takes precedence
• 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 5/30 Polarising elements light-modulating devices with active elements G02F1/00
• CPC Class Codes: G02B 6/34 utilising prism or grating G02B6/293 takes precedence

Abstract

A head up display includes an image source, collimating optics, and a combiner. The collimating optics are disposed between the combiner and the image source. The combiner receives collimated light from the collimating optics at an input and provides the collimated light to an output. The collimating light travels from the input to the output within the combiner by total internal refraction. An input diffraction grating is disposed in a first area and an output diffraction grating is disposed in a second area. The first area is smaller than the second area.

Claims

1. A head up display, comprising:

a micro display image source;

collimating optics capable of providing a field of view of at least 30 degrees horizontally by 18 degrees vertically; and

a combiner, the collimating optics being disposed between the combiner and the image source, the collimating optics providing collimated light associated with the micro display image source, the collimating optics having a compact folded beam path, the combiner receiving the collimated light from the collimating optics at an input and providing the collimated light to an output, the collimating light traveling from the input to the output within the combiner by total internal reflection, wherein an input diffraction grating is disposed in a first area at the input and an output diffraction grating is disposed in a second area at the output, wherein the first area is smaller than the second area by a factor of greater than or equal to 3, wherein the combiner provides pupil expansion in the vertical direction.

2. The head up display of claim 1, wherein the collimating optics are a catadioptric system.

3. The head up display of claim 2, wherein an exit pupil of the combiner is approximately 4 by 4 units and an exit pupil of the collimator is approximately 4 by 1 units.

4. The head up display of claim 1, further comprising:

a stow mechanism for moving the combiner in at least two degrees freedom when the combiner is moved from a stow position to an operational position.

5. The head up display of claim 1, further comprising:

display electronics for providing real-time graphics for display on the micro display image source, wherein the real-time graphics comprise a flight vector symbol positioned to overlay the real world scene as viewed by a pilot through the combiner.

6. The head up display of claim 5, wherein the collimating optics are a folded catadioptric system.

7. The head up display of claim 1, wherein the micro display image source is a micro liquid crystal display.

8. The head up display of claim 3, wherein the input diffraction grating and the output diffraction grating are surface relief gratings.

9. The head up display of claim 2, wherein the input diffraction grating receives the collimated light from a corrective lens in the collimating optics.

10. The head up display of claim 1, wherein the combiner is a single piece of transparent glass.

11. A method of displaying information on a head up display, the method comprising:

collimating light from an image source using collimating optics, the collimating optics being a folded catadioptric system capable of providing a field of view of at least 30 degrees horizontally by 18 degrees vertically;

diffracting the collimated light into a transparent substrate waveguide at an input;

propagating the collimated light through the substrate waveguide to an output;

diffracting the collimated light from the substrate waveguide at the output, wherein a pupil is expanded in at least one direction by the substrate waveguide.

12. The method of claim 11, wherein the substrate waveguide operates as a combiner.

13. The method of claim 11, wherein the collimating step is performed by collimating optics having a lens in close proximity to the input.

14. The method of claim 13, wherein the collimating optics include a polarizing beam splitter.

15. The method of claim 11, wherein diffracting steps use surface relief gratings.

16. A head up display for providing an image from an image source, the display comprising:

collimating optics having a first exit aperture of a first size;

a combiner receiving collimated light from the collimating optics at an input and providing the collimated light to an output, the collimating light traveling from the input to the output within the combiner by total internal refraction, wherein the combiner has a second exit aperture of a second size, the second size being larger than the first size; and

a stow mechanism for moving the combiner out of a head path in a crash event and for aligning the combiner to the collimating optics when in an operational position and for moving the combiner out of a pilot'"'"'s view in a stowed position, wherein when moving from the operational position to the stowed position, the combiner rotates in a clockwise or counter clockwise direction when viewed from a position of a pilot.

17. The display of claim 16, wherein the first size has a same width as the second size.

18. The system of claim 17, wherein the second size has a height approximately four times a height of the first size.

19. The system of claim 17, wherein the combiner moves in at least two degrees of freedom as the combiner rotates in the clockwise or counterclockwise direction across a stow path from the operational position to the stowed position.

20. The system of claim 17, wherein the combiner is a substrate waveguide including surface relief diffraction gratings.