Aviation display depiction of weather threats
US-9978168-B1 · May 22, 2018 · US
US11442164B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11442164-B2 |
| Application number | US-201916434863-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 7, 2019 |
| Priority date | Jun 7, 2019 |
| Publication date | Sep 13, 2022 |
| Grant date | Sep 13, 2022 |
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A method for determining convective cell growth from weather radar reflectivity data includes receiving first weather reflectivity values and receiving second weather reflectivity values at a point in time subsequent to receiving the first weather reflectivity values, storing the first and second weather reflectivity values in cells of a three-dimensional buffer, for each of the first and second weather reflectivity values, calculating a vertically-integrated reflectivity (VIR) value for a column of cells in the three-dimensional buffer, the column of cells being associated with a latitude/longitude position, and comparing the VIR value for the second weather reflectivity values against the VIR for the first weather reflectivity values to determine a difference in the VIR values. Furthermore, the method includes displaying a cell growth hazard indication at a weather display in an area of the weather display that corresponds to the latitude/longitude position.
Opening claim text (preview).
What is claimed is: 1. A system for determining convective cell growth from weather radar reflectivity data comprising: a display device couple to receive display commands and configured, in response to the display commands, to display one or more images; and a processing device coupled to the display device and configured to: a) receive first weather reflectivity values and receiving second weather reflectivity values at a point in time subsequent to receiving the first weather reflectivity values; b) store the first and second weather reflectivity values in cells of a three- dimensional buffer; c) for each of the first and second weather reflectivity values, calculate a vertically-integrated reflectivity (VIR) value for a column of cells in the three- dimensional buffer, the column of cells being associated with a latitude/longitude position; d) compare the VIR value for the second weather reflectivity values against the VIR for the first weather reflectivity values to determine a difference in the VIR values; and e) when the difference in the VIR values is greater than a threshold value, supply display commands to the display device that cause the display device to display a convective cell growth hazard indication on the display device in an area of the display device that corresponds to the latitude/longitude position. 2. The system of claim 1 , further comprising a weather radar system, wherein the first and second weather reflectivity values are generated by the weather radar system. 3. The system of claim 2 , wherein the point in time subsequent is indicative of a scanning rate of the weather radar system. 4. The system of claim 2 , wherein the three-dimensional buffer is representative of a volume of airspace in front of the weather radar system. 5. The system of claim 2 , wherein the column of cells comprises reflectivity values for all altitudes scanned by the weather radar system at the latitude/longitude position. 6. The system of claim 2 , wherein the display device comprises a cockpit weather radar display of an aircraft. 7. The system of claim 6 , wherein the display device is further configured, in response to display commands from the processing device, to display reflectivity imagery along with the convective cell growth hazard indication, wherein the convective cell growth hazard indication is overlaid on the reflectivity imagery. 8. The system of claim 6 , wherein the display device is further configured, in response to display commands from the processing device, to display hail or lightning hazard indications overlaid on the reflectivity imagery. 9. The system of claim 8 , wherein the convective cell growth hazard indication and the hail or lightning hazard indications comprise a display hierarchy wherein only one indication is displayed at a location based on the hierarchy. 10. An aircraft comprising the system of claim 1 .
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