Air turbulence detection

• US 4,937,447 A
• Filed: 02/24/1989
• Issued: 06/26/1990
• Est. Priority Date: 02/24/1989
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Original Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Inventors: Barrett, Joseph J.
• Primary Examiner(s): Hannaher, Constantine
• Assistant Examiner(s): Eisenberg, J.
• Application Number:
  US07/316,371
• Time in Patent Office: 487 Days
• Field of Search: 250/338.1, 250/338.5, 250/339
• US Class Current: 250/339.04
• CPC Class Codes: G01J 5/0014 for sensing the radiation from gases, flames
• CPC Class Codes: G01J 5/601 using spectral scanning
• CPC Class Codes: G01J 5/602 using selective, monochromatic or bandpass filtering
• CPC Class Codes: G01W 2001/003 Clear air turbulence detection or forecasting, e.g. for aircrafts

Abstract

Air turbulence (windshear as well as clear air turbulence) in navigable airspace is detected by remotely sensing changes in the spatial temperature profile of an air column ahead of an aircraft by repeatedly sensing the intensity of the thermal radiation from the column of atmospheric air in at least two spectral peaks in the 4.17 to 4.2 μm region of the CO₂ spectral emission band, and comparing the relative intensity of the spectral peaks over time. Apparatus which includes a tunable Fabry-Perot etalon is provided for the practice of the method.

Claims

1. Apparatus for remotely sensing changes in the spatial temperature profile of a column of atmospheric air comprising, in combination:

(a) collecting means for receiving the thermal radiation from a column of atmospheric air, and for directing it to intensity sensing means;

(b) intensity sensing means comprising means for sequentially sensing the intensity in said column of atmospheric air of at least two spectral peaks in the 4.17 to 4.2 μ

m region of the CO₂ spectral emission band; and

(c) means for detecting temporal changes in the relative intensity of said spectral peaks.

2. The apparatus of claim 1 wherein said intensity sensing means includes a frequency tunable Fabry-Perot etalon.

3. The apparatus of claim 2 wherein said intensity sensing means further comprises a blocking filter in combination with said tunable Fabry-Perot etalon for selectively passing infrared radiation including the carbon dioxide band in the 4.17 to 4.2 μ

m region.

4. The apparatus of claim 3 further comprising scanner control means associated with said Fabry-Perot etalon for sequentially scanning selected peaks within the 4.17 to 4.2 μ

m region of the CO₂ spectral emission band.

5. The apparatus of claim 4 wherein said means for detecting temporal changes in the relative intensity of said spectral peaks further comprises signal processing and display means to provide an indication of sensed changes in the temperature profile of the column of atmospheric air.

6. The apparatus of claim 1 wherein said intensity sensing means comprises, in combination, a blocking filter for selectively passing infrared radiation including the carbon dioxide band in the 4.17 to 4.2 μ

m region;

a frequency tunable Fabry-Perot etalon with associated scanner control means for sequentially scanning selected peaks within the 4.17 to 4.2 μ

m region of the CO₂ spectral emission band transmitted through said blocking filter;

infrared radiation detector means for sensing the intensity of the infrared radiation passing through said Fabry-Perot etalon; and

focusing means for directing said passing infrared radiation onto said radiation detector.

7. The apparatus of claim 6 wherein said means for detecting temporal changes in the relative intensity of said spectral peaks further comprises signal processing and display means to provide an indication of sensed changes in the temperature profile of the column of atmospheric air.

8. The method for remotely sensing changes in the spatial temperature profile of a column of atmospheric air comprising, in combination:

(a) repeatedly sensing the intensity of the thermal radiation from said column of atmospheric air in at least two spectral peaks in the 4.17 to 4.2 μ

m region of the CO₂ spectral emission band; and

(b) comparing the relative intensity of said spectral peaks over time.

9. The method of claim 8 wherein said spectral peaks are located at opposite ends of the 4.17 to 4.2 μ

m region for the CO₂ spectral emission band.

10. The method of claim 8 further comprising the step of displaying changes over time of the sensed differences in the relative intensity of said spectral peaks.