System for and method of displaying levels of turbulence
First Claim
1. A method of displaying areas of turbulent weather, comprising:
- processing data representative of weather;
displaying weather conditions on a display;
detecting turbulence;
providing at least one first graphical element upon the display, wherein the first graphical element has a first size and a first location representing a size and a location of the turbulence at a first level, the first level being below a threshold; and
providing at least one second graphical element upon the display, wherein the second graphical element has a second size and second location representing a size and a location of the turbulence at a second level, the second level being above the threshold, wherein the second size is determined using an inflation factor, wherein the inflation factor is related to a peak turbulence within a given radius, a filtered peak turbulence within a given radius, a density of turbulence at the second level, or a number of turbulence detections which exceed the threshold within a given radius.
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Abstract
A aircraft hazard warning system or method can be utilized to determine a location of turbulence, hail or other hazard for an aircraft. A processor can process weather radar data representative of weather conditions. An avionic display can display graphical elements representing the weather conditions in response to the processor. The display can provide at least one first graphical element representing a size and a location of the turbulence at a first level. The display can provide at least one second graphical element representing a size and a location of the turbulence at a second level. The size of the second graphical element can have a minimal displayable size or can be determined using an inflation factor.
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Citations
20 Claims
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1. A method of displaying areas of turbulent weather, comprising:
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processing data representative of weather; displaying weather conditions on a display; detecting turbulence; providing at least one first graphical element upon the display, wherein the first graphical element has a first size and a first location representing a size and a location of the turbulence at a first level, the first level being below a threshold; and providing at least one second graphical element upon the display, wherein the second graphical element has a second size and second location representing a size and a location of the turbulence at a second level, the second level being above the threshold, wherein the second size is determined using an inflation factor, wherein the inflation factor is related to a peak turbulence within a given radius, a filtered peak turbulence within a given radius, a density of turbulence at the second level, or a number of turbulence detections which exceed the threshold within a given radius. - View Dependent Claims (2, 3, 4, 5, 6)
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7. An avionics weather display system, comprising:
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a processor for processing weather radar data representative of weather conditions; and an avionic display for displaying graphical elements representing the weather conditions in response to the processor, wherein the processor detects turbulence and causes the display to provide at least one first graphical element, wherein the first graphical element has a first size and a first location representing a size and a location of the turbulence at a first level, the first level being below a threshold, wherein the processor causes the display to provide at least one second graphical element, wherein the second graphical element has a second size and second location representing a size and a location of the turbulence at a second level, the second level being above the threshold, wherein the second size is determined using an inflation factor, wherein the inflation factor is related to a peak turbulence within a given radius, a filtered peak turbulence within a given radius, a density of turbulence at the second level, or a number of turbulence detections which exceed the threshold within a given radius. - View Dependent Claims (8, 9, 10, 11, 12)
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13. A program for an avionics weather display system stored on a non-transitory medium, the program comprising instructions for causing at least one electronic processor to:
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detect turbulence at a first level below a first threshold and at a second level above the first threshold from weather radar data; cause a display to provide at least one first graphical element, wherein the first graphical element has a first size and a first location representing a size and a location of the turbulence at a first level; and cause a display to provide at least one second graphical element, wherein the second graphical element has a second size and second location representing a size and a location of the turbulence at a second level, the second level being above the threshold, wherein the second size is determined using an inflation factor, wherein the inflation factor is a function of a peak turbulence within a given radius or a filtered peak turbulence within a given radius. - View Dependent Claims (14, 17, 18, 19, 20)
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15. A program for an avionics weather display system stored on a non-transitory medium, the program comprising instructions for causing at least one electronic processor to:
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detect turbulence at a first level below a first threshold and at a second level above the first threshold from weather radar data; cause a display to provide at least one first graphical element, wherein the first graphical element has a first size and a first location representing a size and a location of the turbulence at a first level; and cause a display to provide at least one second graphical element, wherein the second graphical element has a second size and second location representing a size and a location of the turbulence at a second level, the second level being above the threshold, wherein the second size is determined using an inflation factor, wherein the inflation factor is a function of a turbulence density at the second level, or a number of turbulence detections which exceed the threshold within a given radius. - View Dependent Claims (16)
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Specification