Icing hazard detection for aircraft

• US 5,028,929 A
• Filed: 04/30/1990
• Issued: 07/02/1991
• Est. Priority Date: 04/30/1990
• Status: Expired due to Term

• Current Assignee: University Corporation For Atmospheric Research
• Original Assignee: University Corporation For Atmospheric Research
• Inventors: Kropfli, Robert A., Sand, Wayne R.
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): Sotomayor, John B.
• Application Number:
  US07/515,487
• Time in Patent Office: 428 Days
• Field of Search: 342/26, 342/460, 342/22
• US Class Current: 342/26.00B
• CPC Class Codes: G01S 13/106 using transmission of pulses having some particular characteristics G01S13/12, G01S13/22, G01S13/24, G01S13/26, G01S13/28 and G01S13/30 take precedence
• CPC Class Codes: G01S 13/953 mounted on aircraft
• 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

An airborne Icing Hazard Detector for aircraft uses dual frequency radar beams which are transmitted into a cloud ahead of the aircraft. The reflected signals at each of the two frequencies are compared and processed to determine the presence, amount and location of regions of liquid water in the cloud. The presence of liquid water is determined as a result of liquid water attenuating the power of one of the signals a greater amount than the other signal, due to different attenuation characteristics of the two signals at the two frequencies. A temperature sensor provides ambient temperature information to determine if the detected liquid water is super-cooled. Upon detection of a predetermined amount of liquid water and the determination that it is super-cooled, an advance warning indication is provided to allow the pilot to avoid flying through the volumetric region of supercooled liquid water and risking ice formation on the aircraft.

Claims

1. Apparatus for detecting the presence of a region containing super-cooled liquid water or SLW in a cloud in a flight path ahead of an aircraft, comprising:

means for transmitting a first radar beam signal at a first predetermined frequency into the cloud in front of the aircraft;

means for transmitting a second radar beam signal at a first predetermined frequency into the cloud in front of the aircraft;

one of the radar beam signals at the first or second predetermined frequencies exhibiting significantly different attenuation from propagation of that signal through the region of liquid water than the other one of the radar beam signals;

the first and second transmitted radar beam signals reflecting from the cloud and creating first and second reflected signals which are received at the aircraft and which have the first and second predetermined frequencies, respectively;

means for determining the power of the first and second reflected signals received at the aircraft and for supplying first and second received signals having magnitudes related to the power of the reflected signals received at the aircraft;

means for sensing the temperature ambient of the aircraft and supplying a temperature signal representative of the ambient temperature;

processor means responsive to the transmission of the first and second radar beam signals, the reception and magnitude of the first and second received signals, and the temperature signal, for;

calculating the difference in power of the first and second received signals;

detecting a region of liquid water from the difference of power of the first and second received signals;

determining if the difference in power of the first and second received signals exceeds a predetermined threshold level representative of a quantity of liquid water which could result in an icing hazard; and

utilizing the temperature signal to determine whether the detected region of liquid water is at a temperature in a range of 0°

Celsius and less; and

signalling an icing hazard condition if the difference in the magnitudes of the first and second received signals exceeds the predetermined threshold and if the determined temperature of the detected region of liquid water is 0°

Celsius or less.

2. Apparatus as defined in claim 1 wherein said processor means further determines the amount of liquid water.

3. Apparatus as defined in claim 2 wherein said processor means determines the amount of liquid water over the range of the detected liquid water region.

4. Apparatus as defined in claim 2 wherein said processor means calculates the range differential of the difference in the power of the first and second received signals to determine the amount of liquid water over the length interval of the detected liquid water region.

5. Apparatus as defined in claim 2 wherein said processor means interpolates the difference in power of the first and second received signals over the length interval of the detected liquid water region to determine the amount of liquid water over the length interval of the detected liquid water region.

6. apparatus as defined in claims 4 or 5 further comprising:

indicator means responsive to the processor means signalling an icing hazard and for indicating the icing hazard to a pilot of the aircraft.

7. Apparatus as defined in claim 6 wherein said indicator means further signals the location of the region presenting the icing hazard.

8. Apparatus as defined in claim 6 wherein the indicator means further signals the size of the region presenting the icing hazard.

9. Apparatus as defined in claim 6 wherein the indicator means further signals the size and location of the region presenting the icing hazard by presenting plan position indicator and range height indicator displays.

10. A method of detecting the presence of a region containing super-cooled liquid water or SLW in a cloud in a flight path ahead of an aircraft, comprising:

transmitting a first radar beam signal at a first predetermined frequency into the cloud in front of the aircraft;

transmitting a second radar beam signal at a first predetermined frequency into the cloud in front of the aircraft;

selecting the predetermined frequencies of the radar beam signals so the first radar beam signal exhibits a significantly different attenuation from propagation of that signal through the region of liquid water than the other one of the radar beam signals;

reflecting the first and second transmitted radar beam signals from the cloud to create first and second reflected signals which are received at the aircraft and which have the first and second predetermined frequencies, respectively;

determining the power of the first and second reflected signals received at the aircraft and supplying first and second received signals having magnitudes related to the power of the reflected signals received at the aircraft;

sensing the temperature ambient of the aircraft and supplying a temperature signal representative of the ambient temperature;

calculating the difference in power of the first and second received signals;

detecting a region of liquid water from the difference of power of the first and second received signals;

determining if the difference in power of the first and second received signals exceeds a predetermined threshold level representative of a quantity of liquid water which could result in an icing hazard;

utilizing the temperature signal to determine whether the detected region of liquid water is at a temperature in a range of 0°

Celsius and less; and

signalling an icing hazard condition if the difference in the magnitudes of the first and second received signals exceeds the predetermined threshold and if the determined temperature of the detected region of liquid water is 0°

Celsius or less.

11. A method as defined in claim 10 further comprising:

determining the amount of liquid water.

12. A method as defined in claim 11 further comprising:

determining the amount of liquid water over the range of the detected liquid water region.

13. A method as defined in claim 12 further comprising:

calculating the range differential of the difference in the power of the first and second received signals to determine the amount of liquid water over the length interval of the detected liquid water region.

14. A method as defined in claim 11 further comprising:

interpolating the difference in power of the first and second received signals over the length interval of the detected liquid water region to determine the amount of liquid water over the length interval of the detected liquid water region.

15. A method as defined in claims 13 or 14 further comprising:

indicating the icing hazard to a pilot of the aircraft.

16. A method as defined in claim 15 further comprising:

signalling the location of the region presenting the icing hazard.

17. A method as defined in claim 15 further comprising:

signalling the size of the region presenting the icing hazard.

18. A method as defined in claim 15 further comprising:

signalling the size and location of the region presenting the icing hazard by presenting plan position indicator and range height indicator displays.