US4303862A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Clear air turbulence detector
Assignee: Individual
•
Filing: 1979-07-18
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Granted: 1981-12-01
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Expires: 1999-07-18
Abstract
Abstract A clear air turbulence detector includes an ultraviolet laser for generating a coherent beam which scans an area on an aircraft's flight path. A photodetector monitors optical radiation backscattered from the area, providing an intensity-controlling electrical signal for a CRT display. Updrafts contain greater-than-normal amounts of ultraviolet-absorbing water vapor and result in a blank spot on the display while downdrafts contain less-than-normal amounts of water vapor and result in a bright spot on the display.
Inventors
- 👤 Allen R. Geiger
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-23 09:54
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: 13
Claim 1
Independent Claim
136 words
A system for use in an aircraft in flight for detecting clear air turbulence in a predetermined area along the aircraft's flight path comprising: a laser device for providing a coherent beam of optical radiation having a wavelength in the ultraviolet region; horizontal and vertical scan generator means for directing the coherent beam through a predetermined area in the aircraft's flight path which clear air turbulence is to be detected; a photodetector for detecting optical radiation backscattered from the predetermined area to produce electrical signals proportional to the intensity of the backscattered radiation; and display means connected to said photodetector and operating in synchronism with said horizontal and vertical scan generator means for providing a visual display of the intensity of backscattered radiation over the predetermined area, turbulence being indicated by nonuniformities in the visual display.
Claim 2
Independent Claim
136 words
A system for use in an aircraft in flight for detecting clear air turbulence in a predetermined area along the aircraft's flight path comprising: a laser device for providing a coherent beam of optical radiation having a wavelength in the ultraviolet region; horizontal and vertical scan generator means for directing the coherent beam through a predetermined area in the aircraft's flight path which clear air turbulence is to be detected; a photodetector for detecting optical radiation backscattered from the predetermined area to produce electrical signals proportional to the intensity of the backscattered radiation; and display means connected to said photodetector and operating in synchronism with said horizontal and vertical scan generator means for providing a visual display of the intensity of backscattered radiation over the predetermined area, turbulence being indicated by nonuniformities in the visual display.
Claim 3
Dependent Claim
16 words
A system as defined in claim 1 wherein the display means comprises a cathode ray tube.
Claim 4
Dependent Claim
33 words
A system as defined in claim 2 wherein an updraft is indicated by a region of reduced intensity on the visual display while a downdraft is indicated by a region of increased intensity.
Claim 5
Dependent Claim
83 words
A system as defined in claim 3 wherein the scan generator means includes a first rotating drum having faceted reflecting surfaces, said first drum rotating about an axis perpendicular to the axis of the coherent beam; and a second rotating drum having faceted reflecting surfaces, said second drum rotating about an axis parallel to the axis of the coherent beam; said first drum providing a horizontal component of movement of the coherent beam while said second drum provides a vertical component of movement.
Claim 6
Dependent Claim
34 words
A system as defined in claim 4 wherein the horizontal and vertical sweep of the electron beam in said cathode ray tube is synchronized with the rotary positions of said first and second drums.
Claim 7
Dependent Claim
48 words
A system as defined in claim 1 and wherein the scan generator means comprises a horizontal scan generator which causes the beam to travel along a horizontal path and a vertical scan generator which imparts a vertical component of movement to the beam during or between horizontal sweeps.
Claim 8
Dependent Claim
31 words
A system as defined in claim 1 and further including means for cancelling out any variations in the intensity of the coherent beam of optical radiation emitted by the laser device.
Claim 9
Dependent Claim
18 words
A system as defined in claim 1 and wherein the laser device is a continuous wave laser device.
Claim 10
Independent Claim
82 words
A method of detecting clear air turbulence along the flight path of a flying aircraft comprising the steps of: directing a coherent beam of ultraviolet radiation in a rectilinear manner through a predetermined area to be monitored in the flightpath of the flying aircraft; and providing a visual display of the intensity of backscattered optical radiation over the predetermined area with updrafts being identifiable as regions of relatively lesser backscattered radiation and downdrafts being identifiable as regions of relatively greater backscattered radiation.
Claim 11
Independent Claim
82 words
A method of detecting clear air turbulence along the flight path of a flying aircraft comprising the steps of: directing a coherent beam of ultraviolet radiation in a rectilinear manner through a predetermined area to be monitored in the flightpath of the flying aircraft; and providing a visual display of the intensity of backscattered optical radiation over the predetermined area with updrafts being identifiable as regions of relatively lesser backscattered radiation and downdrafts being identifiable as regions of relatively greater backscattered radiation.
Claim 12
Dependent Claim
26 words
A method as defined in claim 9 wherein the coherent beam undergoes both horizontal and vertical deflection as it is directed through the area being monitored.
Claim 13
Dependent Claim
15 words
A method of claim 9 and wherein the coherent beam of ultraviolet radiation is continuous.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1984-11-30 | 1985-06-01 | 1985-12-01 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1988-11-30 | 1989-06-01 | 1989-12-01 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1992-11-30 | 1993-06-01 | 1993-12-01 | $7700.00 | Window Closed / Lapsed |