Weather radar system and method for estimating vertically integrated liquid content

• US 9,612,328 B1
• Filed: 10/06/2016
• Issued: 04/04/2017
• Est. Priority Date: 03/07/2008
• 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: Breiholz, Arlen E., Kronfeld, Kevin M.
• Primary Examiner(s): BYTHROW, PETER M
• Application Number:
  US15/287,673
• Time in Patent Office: 180 Days
• Field of Search: 342 26 R, 342 26 A, 342 26 B, 342 26 C, 342 26 D, 342179
• CPC Class Codes: B64D 43/00 Arrangements or adaptations of instruments arrangements of cameras B64D47/08; aeronautical measuring instruments per se G01C
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• CPC Class Codes: G01S 13/86 Combinations of radar systems with non-radar systems, e.g. sonar, direction finder
• CPC Class Codes: G01S 13/95 for meteorological use
• CPC Class Codes: G01S 13/953 mounted on aircraft
• CPC Class Codes: G01S 7/02 of systems according to group G01S13/00
• CPC Class Codes: G01S 7/04 Display arrangements
• CPC Class Codes: G01S 7/062 in which different colours are used
• CPC Class Codes: G01S 7/22 Producing cursor lines and indicia by electronic means
• CPC Class Codes: Y02A 90/10 Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation

Abstract

A hazard warning system includes a processing system. The processing system determines a vertically integrated liquid (VIL) parameter. The processing system receives radar reflectivity data associated with an aircraft radar antenna and determines the VIL parameter by determining a first reflectivity value at a first altitude and a second reflectivity value at a second altitude using the radar reflectivity data. The processing system determines the VIL parameter using a base storm altitude and a top storm altitude.

Claims

1. An aircraft hazard warning system, comprising:

a processing system configured to determine a vertically integrated liquid (VIL) parameter, the processing system configured to receive radar reflectivity data associated with an aircraft radar antenna and determine the VIL parameter by determining a first reflectivity value at a first altitude and a second reflectivity value at a second altitude in response to the radar reflectivity data, the processing system being configured to determine if the VIL parameter is above a threshold and cause a display to provide a VIL region indicative of the VIL parameter being above the threshold, wherein the VIL region allows at least one weather region indicative of rainfall rates associated with the same location as the VIL region to be viewable.

2. The aircraft hazard warning system of claim 1, wherein a VIL warning is provided on an electronic display if the VIL parameter is above the threshold.

3. The aircraft hazard warning system of claim 1, wherein the VIL region is provided as a speckled region, a striped region, a bright region, a region with outlined contours, or a region with varying color saturation or brightness.

4. The aircraft hazard warning system of claim 1, wherein the first altitude is a freezing altitude.

5. The aircraft hazard warning system of claim 1, wherein the first and second reflectivity values are determined from a weather model based upon at least one reflectivity sample from the radar reflectivity data.

6. The aircraft hazard warning system of claim 1, wherein the processing system determines a predictive VIL parameter based upon historical VIL parameter data.

7. The aircraft hazard warning system of claim 1, wherein the VIL parameter is compared to a received VIL value from an off-aircraft source.

8. The aircraft hazard warning system of claim 1, wherein the VIL parameter is provided to a ground station or other aircraft.

9. The aircraft hazard warning system of claim 1, wherein the processing system is configured to determine the VIL parameter by using the first and second reflectivity values at two elevation angles.

10. An aircraft hazard warning system, comprising:

a processing system for determining a vertically integrated liquid (VIL) parameter, the processing system configured to determine an altitude value based on received temperature data, wherein the processing system is configured to determine the VIL parameter based on the determined altitude value, wherein the processing system is configured to use the VIL parameter to detect lightning, a convective cell, turbulence, hail, or ice.

11. The aircraft hazard warning system of claim 10, wherein the processing system uses a different equation for the VIL parameter for tropical/continental, and tropical/oceanic, and mid-continent environments.

12. The aircraft hazard warning system of claim 10, wherein the VIL parameter is used in inferential weather detection.

13. The aircraft hazard warning system of claim 10, wherein the altitude value includes values indicative of:

a base storm altitude, a top storm altitude, a freezing level altitude, and a predefined temperature level altitude.

14. The aircraft hazard warning system of claim 13, wherein the predefined temperature level altitude is −

40°

Celsius.

15. The aircraft hazard warning system of claim 10, wherein the temperature data includes at least one of a local atmospheric temperature value, a local temperature variation with time value, a local temperature variation with altitude value, and a remotely determined temperature value.

16. A method of determining a vertically integrated liquid (VIL) parameter on an aircraft using an electronic processor, the method comprising:

receiving radar reflectivity data and determining a first reflectivity value at a first altitude and a second reflectivity value at a second altitude using the electronic processor;

providing the VIL parameter in response to the first reflectivity value and the second reflectivity value; and

storing a rate of change over time of the VIL parameter.

17. The method of claim 16, wherein the first altitude is a freezing level altitude and the second altitude is a predefined temperature altitude.

18. The method of claim 17, wherein the rate of change is used to predict a predicted VIL parameter.

19. The method of claim 16, further comprising performing additional vertical sweeps to obtain more accurate VIL parameters in a limited region or performing additional horizontal sweeps to improve interpolation.

20. The method of claim 16, further comprising determining the VIL parameter by using the first and second reflectivity values at two elevation angles.