Systems and methods for a mobile flight simulator of an electric aircraft
US-2023154350-A1 · May 18, 2023 · US
US9916768B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9916768-B2 |
| Application number | US-201614997055-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 15, 2016 |
| Priority date | Jan 15, 2016 |
| Publication date | Mar 13, 2018 |
| Grant date | Mar 13, 2018 |
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Systems and methods for providing sunlight simulation in a vehicle simulator include a vehicle simulator. The vehicle simulator includes a visual projector configured to generate visual scene images and a bright forward field of view projector mounted with the visual projector, wherein the bright forward field of view projector includes plural light emitting diode (LED) light sources configured to generate a bright forward field of view. The vehicle simulator also includes a projection screen configured to project the visual scene images generated by the visual projector or the bright forward field of view generated by the bright forward field of view projector.
Opening claim text (preview).
What is claimed is: 1. A system comprising: a display screen configured to display a projected image; a first projector configured to project a visual image on the display screen; and a second projector fixedly coupled to the first projector, the second projector including a plurality of light emitting diode light sources configured to project simulated ambient solar lighting on the display screen. 2. The system of claim 1 , further comprising a back projection screen configured to generate the projected image based on the visual image, the simulated ambient solar lighting, or both. 3. The system of claim 1 , wherein the plurality of light emitting diode light sources are arranged in a curved configuration. 4. The system of claim 3 , wherein the curved configuration has a radius of curvature of 150 centimeters. 5. The system of claim 1 , wherein each light emitting diode of the plurality of light emitting diode light sources has a maximum luminance contribution of 1,900 foot Lamberts. 6. The system of claim 1 , wherein the the plurality of light emitting diode light sources have a total combined luminance of 10,000 foot Lamberts to 14,000 foot Lamberts. 7. The system of claim 1 , further comprising a controller configured to control operation of the first projector and the second projector. 8. The system of claim 1 , wherein the display screen includes a collimating mirror. 9. The system of claim 1 , further comprising a cabin shell, wherein the display screen is viewable from within the cabin shell. 10. The system of claim 1 , wherein the first projector is configured to project a cross-cockpit out-the-window image as the visual image, and wherein the simulated ambient solar lighting simulates the sun above a forward horizon and above a cloud deck. 11. A system comprising: a cabin configured to receive therein a person, the cabin including at least one window; and a visual display system including: a display screen configured to display a projected image; a first projector configured to project a visual image on the display screen; and a second projector fixedly coupled to the first projector, the second projector including a plurality of light emitting diode light sources configured to project simulated ambient solar lighting on the display screen. 12. The system of claim 11 , wherein the visual display system is configured to project the simulated ambient solar lighting without using high pressure discharge lamps. 13. The system of claim 11 , wherein the cabin is a portion of an aircraft cockpit shell. 14. The system of claim 11 , wherein the visual image includes an out-the-window image. 15. The system of claim 14 , further comprising a back projection screen configured to generate the projected image based on the out-the-window image, the simulated ambient solar lighting, or both, wherein the display screen includes a collimating mirror configured to display the projected image towards the cabin. 16. A method comprising: projecting a visual image from a first projector; displaying the visual image at a display screen; projecting simulated ambient solar lighting from a second projector fixedly coupled to the first projector, wherein the simulated ambient solar lighting is generated by a plurality of light emitting diode light sources of the second projector; and displaying the simulated ambient solar lighting at the display screen. 17. The method of claim 16 , further comprising positioning the first projector and the second projector such that the visual image and the simulated ambient solar lighting are displayed at the display screen relative to an expected pilot's eye point. 18. The method of claim 16 , further comprising: projecting the visual image from a back projection screen to the display screen, wherein the first projector projects the visual image to the back projection screen; and projecting the simulated ambient solar lighting from the back projection screen to the display screen, wherein the second projector projects the simulated ambient solar lighting to the back projection screen. 19. The method of claim 16 , wherein the simulated ambient solar lighting is projected without using high pressure discharge lamps. 20. The method of claim 16 , wherein the simulated ambient solar lighting is projected using only the plurality of light emitting diode light sources.
for teaching control of aircraft, e.g. Link trainer · CPC title
Projectors with built-in or built-on screen · CPC title
Multi-projection systems (video walls G06F3/1446) · CPC title
for controlling the light source (light source control per se H05B35/00 – H05B47/00; control of an illumination source for displays in general G09G3/3406) · CPC title
using multiple light sources · CPC title
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