System and method of determining increased turbulence susceptibility with elapsed flight time

• US 8,742,973 B1
• Filed: 09/22/2011
• Issued: 06/03/2014
• Est. Priority Date: 09/22/2011
• Status: Active Grant

• Current Assignee: Rockwell Collins, Inc. (Rtx Corporation)
• Original Assignee: Rockwell Collins, Inc. (Rtx Corporation)
• Inventors: Fersdahl, Mark C.
• Primary Examiner(s): BYTHROW, PETER M
• Application Number:
  US13/240,555
• Time in Patent Office: 985 Days
• Field of Search: 342/26.R, 342/26.A, 342/26.B, 342/26.C, 342/26.D, 701 3- 18
• US Class Current: 342/26.B
• CPC Class Codes: G01S 13/953 mounted on aircraft
• CPC Class Codes: G01S 7/411 Identification of targets based on measurements of radar reflectivity G01S7/415 takes precedence
• 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 aircraft based radar system is provided. The radar system includes processing electronics configured to estimate a vertical loading on the aircraft using radar return data and a time value.

Claims

1. An aircraft based radar system, comprising:

processing electronics configured to estimate a vertical loading on the aircraft using radar return data and a time parameter defined by a plurality of time sub-parameters,

wherein at least two time sub-parameters include an elapsed time from takeoff and an elapsed time from completion of an initial climb, the completion of the initial climb being based on throttle position.

2. The system of claim 1, wherein the processing electronics are further configured to estimate the vertical loading on the aircraft using at least one of airspeed and throttle position.

3. The system of claim 1, wherein the processing electronics are further configured to estimate the vertical loading on the aircraft using at least one of altitude and air pressure.

4. The system of claim 1, wherein the processing electronics are further configured to estimate the vertical loading on the aircraft using a spectral width parameter of the radar return data.

5. The system of claim 1, wherein takeoff is based on throttle position.

6. The system of claim 1, wherein the elapsed time from takeoff is based on sensing of takeoff.

7. The system of claim 1 further comprising a memory configured to store vertical loading estimates based on at least one of airspeed and altitude.

8. A method for indicating susceptibility of an aircraft to turbulence, comprising:

calculating a spectral width parameter from radar return data; and

estimating, with a processing electronics, a vertical loading on the aircraft using the spectral width parameter and a T factor, the T factor being a function of an elapsed time from completion of an initial climb, wherein completion of the initial climb is based on throttle position.

9. The method of claim 8, wherein the T factor is further a function of the elapsed time from takeoff;

and wherein takeoff is based on a throttle position.

10. The method of claim 8 further comprising modifying the function of the T factor in response to in-situ determinations of turbulence.

11. The method of claim 8, wherein estimating the vertical loading on the aircraft further comprises using at least one of airspeed and throttle position.

12. The method of claim 8, wherein estimating the vertical loading on the aircraft further comprises using at least one of altitude and air pressure.

13. The method of claim 8 further comprising causing an indication of estimated vertical loading on the aircraft.

14. The method of claim 13 further comprising causing the estimated vertical loading to be displayed as turbulence on a flight deck display.

15. The method of claim 13 further comprising causing a warning to be annunciated in response to the estimated vertical loading on the aircraft exceeding a threshold value.

16. A turbulence detection and display system, comprising:

a means for a receiving a time signal, radar data, an altitude signal, and an airspeed signal; and

a means for determining a signal representative of the presence of a turbulence threat based on the radar data and the time signal, the altitude signal, and the airspeed signal,

wherein the time signal is an elapsed time from completion of an initial climb, the completion of the initial climb being based on throttle position.

17. The system of claim 16, wherein the time signal comprises a UTC label received by a radar.

18. The system of claim 16, wherein the time signal is received from a timer.

19. The system of claim 16, wherein the time signal further comprises an elapsed time from takeoff, and takeoff is based on throttle position.

20. The system of claim 16, wherein completion of an initial climb is based on sensing completion of an initial climb.