Optical assemblies for aircraft displays
A light emitting diode display panel may comprise a substrate, a plurality of light emitting diodes located over the substrate, and an optical assembly located over the plurality of light emitting diodes. The optical assembly may include a lens array and a diffuser. An inner surface of the lens array may define a plurality of inner curves.
1. A method of making of light emitting diode display panel, comprising:
locating a plurality of light emitting diodes over a substrate;
forming an optical assembly including a lens array and a diffuser, wherein the lens array defines at least one of a plurality of inner curves or a plurality of outer curves, wherein forming the optical assembly comprises:
forming a first region of the diffuser comprising a least one of a first surface pattern, a first material, a first thickness, or a first surface coating, and forming a second region of the diffuser comprising at least one of a second surface pattern, a second material, a second thickness, or a second surface coating, the first surface pattern being different from the second surface pattern, the second material being different from the first material, the second thickness being different from the first thickness, the second surface coating being different from the first surface coating, wherein the first region of the diffuser is located over the first light emitting diode of the plurality of light emitting diodes, and wherein the second region of the diffuser is located over the second light emitting diode of the plurality of light emitting diodes; and
coupling the optical assembly over the plurality of light emitting diodes.
2. The method of claim 1 , wherein forming the optical assembly comprises determining a design of the lens array and the diffuser based on an image quality assessment.
3. The method of claim 1 , wherein forming the optical assembly comprises forming the diffuser integrally with the lens array using at least one of injection molding or additive manufacturing.
4. The method of claim 1 , wherein coupling the optical assembly over the plurality of light emitting diodes comprises locating a plurality of standoffs between the lens array and the substrate.
5. The method of claim 4 , wherein forming the optical assembly further comprises at least one of:
forming a first inner curve of the plurality of inner curves having a first geometry and a second inner curve of the plurality of inner curves having a second geometry, the second geometry being different from the first geometry, wherein the first inner curve is located over a first light emitting diode of the plurality of light emitting diodes, and wherein the second inner curve is located over a second light emitting diode of the plurality of light emitting diodes; or
forming a first outer curve of the plurality of inner curves having a third geometry and a second outer curve of the plurality of inner curves having a fourth geometry, the third geometry being different from the fourth geometry, wherein the first outer curve is located over the first light emitting diode of the plurality of light emitting diodes, and wherein the second outer curve is located over the second light emitting diode of the plurality of light emitting diodes.
6. An aircraft cabin structure, comprising:
a surface; and
a light emitting diode display panel mounted to the surface, the light emitting diode display panel including:
a substrate;
a plurality of light emitting diodes located over the substrate; and
an optical assembly located over the plurality of light emitting diodes, the optical assembly including a lens array and a diffuser, wherein at least one of a first surface pattern of a first region of the diffuser, a first thickness of the first region of the diffuser, a first surface coating of the first region of the diffuser, or a first material of the first region of the diffuser is different from at least one of a second surface pattern of a second region of the diffuser, a second thickness of the second region of the diffuser, a second surface coating of the second region of the diffuser, or a second material of the second region of the diffuser.
7. The aircraft cabin structure of claim 6 , wherein an inner surface of the lens array defines a plurality of inner curves, and wherein an outer surface of the lens array defines a plurality of outer curves.
8. The aircraft cabin structure of claim 7 , further comprising a plurality of standoffs coupled between the substrate and the lens array.
9. A light emitting diode display panel, comprising:
a substrate;
a plurality of light emitting diodes located over the substrate; and
an optical assembly located over the plurality of light emitting diodes, the optical assembly including a lens array and a diffuser, wherein at least one of a first surface pattern of a first region of the diffuser, a first thickness of the first region of the diffuser, a first surface coating of the first region of the diffuser, or a first material of the first region of the diffuser is different from at least one of a second surface pattern of a second region of the diffuser, a second thickness of the second region of the diffuser, a second surface coating of the second region of the diffuser, or a second material of the second region of the diffuser.
10. The light emitting diode display panel of claim 9 , wherein an inner surface of the lens array defines a plurality of inner curves.
11. The light emitting diode display panel of claim 10 , wherein a geometry of a first inner curve of the plurality of inner curves is different from a geometry of a second inner curve of the plurality of inner curves, and wherein the first inner curve is located over a first light emitting diode of the plurality of light emitting diodes and the second inner curve is located over a second light emitting diode of the plurality of light emitting diodes.
12. The light emitting diode display panel of claim 10 , wherein each inner curve of the plurality of inner curves includes a dedicated inner curve of the plurality of inner curves.
13. The light emitting diode display panel of claim 12 , wherein an outer surface of the lens array defines a plurality of outer curves.
14. The light emitting diode display panel of claim 13 , wherein each light emitting diode of the plurality of light emitting diodes includes a dedicated outer curve of the plurality of outer curves.
15. The light emitting diode display panel of claim 10 , further comprising a plurality of standoffs coupled between the substrate and the lens array.
16. The light emitting diode display panel of claim 9 , wherein the diffuser is integral to the lens array.
17. The light emitting diode display panel of claim 9 , wherein the first region of the diffuser is located over a first light emitting diode of the plurality of light emitting diodes and the second region of the diffuser is located over a second light emitting diode of the plurality of light emitting diodes, and wherein the first light emitting diode emits light having a first wavelength and the second light emitting diode emits light having a second wavelength different from the first wavelength.
18. The light emitting diode display panel of claim 9 , further comprising a controller operably coupled to the plurality of light emitting diodes, the controller being configured to perform an image quality assessment for a displayed image.
19. The light emitting diode display panel of claim 18 , wherein the controller is configured to compare the displayed image to a target image, and adjust at least one of a sharpness, a contrast, or a brightness of the of the light emitting diode display panel based on the comparison of the displayed image to the target image.