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US4359640A Expired / Lapsed US ⏱️ 0.0 years remaining

Clear air turbulence detection

Assignee: AERO-GEOPHYSICAL Inc
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Filing: 1981-02-27
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Granted: 1982-11-16
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Expires: 2001-02-27
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Abstract

Abstract Apparatus is disclosed for use on an aircraft for detecting clear air turbulence (CAT) and/or wake vortex (WV). In one embodiment of the invention, a beam of light from a continuous wave UV laser scans an area on the aircraft's flight path. A photodetector monitors optical radiation backscattered from the area, providing an intensity-controlling signal for a CRT display. Clear air turbulence is indicated by non-uniformities on the display. In another embodiment of the invention, a pair of beams of light from a pair nitrogen gas pulse UV lasers are arranged to converge at a region in front of the aircraft. The backscattered radiation from the region is monitored for turbulent areas by a receiver which includes a photodetector and which is connected to an oscilloscope where the return pulse amplitude is analyzed. Velocity determinations of the air parcel monitored are made by causing the two beams to scan either horizontally or vertically. In still another embodiment of the invention, a pair of beams of light, one from a nitrogen gas UV pulse laser and the other from a blue dye laser are arranged to converge at a region in front of the aircraft. The backscattered radiation is monitored for turbulent regions by a receiver and oscilloscope combination. Velocity determinations of the air parcel monitored are made by causing the two beams to scan vertically. In a further embodiment of the invention which is used to detect and monitor wake vortex (WV) as well as clear air turbulence (CAT), either a nitrogen gas pulse UV laser of or a multispectral helium cadmium laser is used to generate a light beam which scans an area in front of the aircraft. Backscattered radiation or the presence of wake vortex is detected by a receiver which includes a slaved image orthicon. Also disclosed is a UV laser television system.

Inventors

  • 👤 Allen R. Geiger

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-23 12:48
CPC Classifications
G; G01; G01S; G01S17/00; G01S17/88; G01S17/95; G01W; G01W1/00; G01W2001/003; Y; Y02; Y02A; Y02A90/00; Y02A90/10

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 73 words
A system for use in an aircraft for detecting clear air turbulance along the aircraft's flight path comprising: a. a pair of pulse lasers for generating a pair of coherent beams arranged to converge at a point in front of the aircraft's flight path, b. receiver means for detecting backscattered radiation produced at said point by said beams and for producing electrical signals related thereto, and c. display means for displaying said signals.
Claim 2
Independent Claim 73 words
A system for use in an aircraft for detecting clear air turbulance along the aircraft's flight path comprising: a. a pair of pulse lasers for generating a pair of coherent beams arranged to converge at a point in front of the aircraft's flight path, b. receiver means for detecting backscattered radiation produced at said point by said beams and for producing electrical signals related thereto, and c. display means for displaying said signals.
Claim 3
Dependent Claim 14 words
The system of claim 1 and wherein the two lasers are nitrogen gas lasers.
Claim 4
Dependent Claim 24 words
The system of claim 1 and wherein one of the lasers is a nitrogen gas laser and the other laser is a dye laser.
Claim 5
Dependent Claim 26 words
The system of claim 1 and further including means for causing said pair of beams to scan at their point of convergence in a horizontal direction.
Claim 6
Dependent Claim 27 words
The system of claim 1 or 4 further including means for causing said pair of beams to scan at their point of convergence in a vertical direction.

References Cited (Backward Citations)

US3415984A Cited
US3856402A Cited
US3931462A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1985-11-15 1986-05-17 1986-11-16 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1989-11-15 1990-05-17 1990-11-16 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1993-11-15 1994-05-17 1994-11-16 $7700.00 Window Closed / Lapsed

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