System and method for ice detection

• US 9,846,230 B1
• Filed: 12/21/2015
• Issued: 12/19/2017
• Est. Priority Date: 03/15/2013
• Status: Active Grant

• Current Assignee: Rockwell Collins, Inc. (Rtx Corporation)
• Original Assignee: Rockwell Collins, Inc. (Rtx Corporation)
• Inventors: Finley, Jeffery A., Kronfeld, Kevin M., Koenigs, Gregory J., Robertson, Roy E.
• Primary Examiner(s): Windrich, Marcus E
• Application Number:
  US14/977,084
• Time in Patent Office: 729 Days
• Field of Search: 342 26 R- 26 D
• CPC Class Codes: G01S 13/953 mounted on aircraft
• CPC Class Codes: G01S 7/003 Transmission of data between radar, sonar or lidar systems and remote stations
• CPC Class Codes: G01S 7/025 involving the transmission of linearly polarised waves
• CPC Class Codes: G01S 7/062 in which different colours are used
• 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 or weather radar system or method can be utilized to determine a location of ice. The system and method can be used in an aircraft. The aircraft weather radar system can include a radar antenna and an electronic processor. The radar antenna receives radar returns. The processor determines levels of icing conditions and causes the levels to be displayed on an electronic display.

Claims

1. An aircraft hazard warning system, comprising:

an electronic processing system configured to determine an icing condition at least in part in response to radar reflectivity data sensed onboard an aircraft, the electronic processing system being configured to cause an electronic display to provide an indication of the icing condition, wherein the electronic processing system is configured to determine a presence of a stratiform rain region and determine a number of old convective core cells in the stratiform rain region, wherein the presence of the stratiform rain region and the number of old convective core cells in the stratiform rain region is used to determine a presence of the icing condition.

2. The aircraft hazard warning system of claim 1, wherein a first level of an icing condition level is provided as a speckled yellow region on the electronic display.

3. The aircraft warning system of claim 2, wherein a second level of the icing condition level is provided as a speckled red region on the electronic display.

4. The aircraft warning system of claim 1, wherein icing condition levels are determined in response to a size of the stratiform rain region determined from the radar reflectivity data and temperature data and the number of old convective core cells in the stratiform rain region.

5. The aircraft warning system of claim 1, wherein icing condition levels are determined in response to a number of embedded convective core cells in the stratiform rain region determined in response to the radar reflectivity data and temperature data.

6. The aircraft warning system of claim 1, wherein a blow off region is detected in response to a wind direction, the blow off region being an indication of the icing condition.

7. The aircraft warning system of claim 1, wherein an icing condition level is determined by determining a presence of a blow off region in response to a size of a convective cell and a wind direction.

8. The aircraft hazard warning system of claim 7, wherein the wind direction is provided by a flight management system.

9. The aircraft hazard warning system of claim 1, wherein the electronic processing system is part of an avionic weather radar system.

10. The aircraft hazard warning system of claim 4, wherein the radar reflectivity data comprises reflectivity data corresponding to at least two frequencies from a multi-frequency radar system, and wherein the electronic processing system is configured to determine an icing condition level based at least in part on a comparison of the reflectivity data corresponding to the at least two frequencies from the multi-frequency radar system.

11. The aircraft hazard warning system of claim 1, wherein the electronic processing system receives radar reflectivity data comprises at least two polarization diverse radar signals received from a polarization diversity radar system, and wherein the electronic processing system is configured to determine an icing condition level based at least in part on a comparison of the at least two polarization diverse radar signals.

12. The aircraft hazard warning system of claim 1, wherein the electronic processing system is configured to receive data from one or more off-aircraft sources, and wherein the processing system is configured to determine an icing condition level based at least in part on the data received from the one or more off-aircraft sources.

13. The aircraft hazard warning system of claim 1, wherein the processing system is configured to transmit an icing condition level to an off-aircraft source.

14. The aircraft hazard warning system of claim 1, wherein the electronic processing system is configured to determine an icing condition level based at least in portion on a convective level of a convective cell based on at least one of an area and a volume of reflectivity.

15. A method of displaying an indication of an icing condition on an aircraft display in an avionics system, the method comprising:

receiving radar reflectivity data and temperature data and determining a presence of a stratiform rain region;

determining whether the stratiform rain region included old convective cells within a time period; and

providing the indication of the icing condition in response to a presence of the old convective cells in the stratiform rain region.

16. The method of claim 15, wherein a level of the icing condition is determined in response to wind parameter and a size of a convective cell, wherein the wind parameter is a high altitude parameter.

17. The method of claim 16, wherein the presence of the convective cells is determined using atmospheric temperature data comprising one or more of:

local temperature, local temperature variations with time, local variations with altitude, remotely determined temperature, and remotely determined temperature gradients in either range or altitude.

18. The method of claim 16, wherein vertical structure analysis data is used to determine the presence of the convective cells and comprises one or more of:

vertical height, vertical growth rate, vertical history assessment, assessment of whether an aircraft path will intersect a portion of a weather cell, and cell maturity.

19. The method of claim 15, wherein lightning data is used to determine the presence of the convective cells.

20. An aircraft weather radar system, comprising:

a radar antenna for receiving radar returns; and

a processor configured to identify an icing condition and cause an electronic display to display a region of the icing condition, wherein the processor is configured to determine a size of a stratiform rain region and determine a number of old embedded convective core cells in the stratiform rain region within a time period, wherein the icing condition is detected in response to the number of the old embedded convective core cells in the stratiform rain region.