← Back to Patent Explorer
US4712108A Expired / Lapsed US ⏱️ 0.0 years remaining

Method and apparatus for detecting microbursts

Assignee: Cardion Newco Inc
•
Filing: 1985-10-21
•
Granted: 1987-12-08
•
Expires: 2005-10-21
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract The invention provides a method and apparatus for detecting specialized meteorological conditions, in particular a microburst. The detector is localized so as to process radar return signals from regions in which aircraft are particularly vulnerable to microbursts. The detector includes a Doppler radar and an intelligent processor. Doppler radar returns are stored in an array wherein the contents of each cell identify the wind velocity parallel to propagation path. A pattern matching process identifies the existence of a microburst, maximum wind velocity associated with the microburst, and the location of the center. By tracking the microburst center as a function of time, the microburst velocity and direction can be determined, allowing prediction for microburst location in the future. Based on observed microburst lifetimes, the expected duration of the microburst can also be predicted. Although the apparatus of the invention can be configured as a stand alone or dedicated unit, it can also be configured as an add-on to an existing ASDE-3.

Inventors

  • 👤 Carl Schwab

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-23 03:28
CPC Classifications
G; G01; G01S; G01S13/00; G01S13/88; G01S13/95; G01S13/951; Y; Y02; Y02A; Y02A90/00; Y02A90/10

Claims Analysis

Total Claims: 19
Claim 1
Independent Claim 161 words
A microburst detector comprising a doppler radar detector propagating electromagnetic energy along a propagation path sweeping in range and azimuth across a region in space including at least one end of an airport runway, and an intelligent processor responsive to signals from said doppler radar, said intelligent processor including storage means for storing a representation of an array of cells located in rows and columns storing data representative of wind velocity components parallel to said propagation path, said intelligent processor performing a pattern matching function for searching for a specific pattern of data within said cells of the array for locating a center of a particular circle wherein data of equal and opposite signs are stored in a pair of cells located along one diameter of the particular circle and null or near null data are stored at another pair of cells along a perpendicular diameter of said particular circle, and means for signalling a microburst on detection of said pattern.
Claim 2
Dependent Claim 161 words
A microburst detector comprising a doppler radar detector propagating electromagnetic energy along a propagation path sweeping in range and azimuth across a region in space including at least one end of an airport runway, and an intelligent processor responsive to signals from said doppler radar, said intelligent processor including storage means for storing a representation of an array of cells located in rows and columns storing data representative of wind velocity components parallel to said propagation path, said intelligent processor performing a pattern matching function for searching for a specific pattern of data within said cells of the array for locating a center of a particular circle wherein data of equal and opposite signs are stored in a pair of cells located along one diameter of the particular circle and null or near null data are stored at another pair of cells along a perpendicular diameter of said particular circle, and means for signalling a microburst on detection of said pattern.
Claim 3
Dependent Claim 49 words
The microburst detector of claim 1 which includes gating means for gating range and azimuth signals from said doppler radar, said gating means connected between said doppler radar and said intelligent processor so that signals passed to said intelligent processor define a region of vulnerability for aircraft to microbursts.
Claim 4
Dependent Claim 48 words
The microburst detector of claim 2 in which said gating means includes limiting means for controlling said gating means to gate signals to said intelligent processor selected from a region along an aircraft flight path to or from said runaway for a distance less than approximately four miles.
Claim 5
Dependent Claim 48 words
The microburst detector of claim 2 in which said gating means includes limiting means for controlling said gating means to gate signals to said intelligent processor selected from a region along an aircraft flight path to or from said runaway for a distance less that approximately one mile.
Claim 6
Dependent Claim 44 words
The microburst detector of claim 2 in which said gating means includes limiting means for controlling said gating means to gate signals to said intelligent processor selected from a region along an aircraft flight path which is less than approximately 1200 feet in altitude.
Claim 7
Dependent Claim 44 words
The microburst detector of claim 2 in which said gating means includes limiting means for controlling said gating means to gate signals to said intelligent processor selected from a region along an aircraft flight path which is less than approximately 300 feet in altitude.
Claim 8
Dependent Claim 48 words
The microburst detector of claim 1 in which said intelligent processor comprises means for performing performs a timing function to initiate execution of said pattern matching on a timed basis in which each execution of said pattern matching is initiated no more often than about once per minute.
Claim 9
Dependent Claim 90 words
The microburst detector of claim 1 in which said doppler radar detector includes: a rotating reflector, a first horn for transmitting pulsed RF energy to be reflected by said reflector for sweeping in range and azimuth, a second horn for transmitting pulsed RF energy to be reflected by said reflector for sweeping in range and azimtuh, and means for mounting said first and second horns to propagate energy from said first horn at an angle to horizontal and to propagate energy from said second horn in a generally horizontal direction.
Claim 10
Dependent Claim 26 words
The microburst detector of claim 1 in which said doppler radar detector includes a rotating reflector, and an ASDE radar detector associated with said rotating reflector.
Claim 11
Independent Claim 127 words
A method of microburst detection comprising the steps of: (a) selecting a region in space for monitoring within which aircraft are vulnerable to abrupt changes in wind velocity vectors, (b) providing a doppler radar and employing said doppler radar for detecting wind speed vectors, or at least components of wind speed vectors parallel to a propagation path defined by said doppler radar, (c) storing said sensed wind speed vectors in a read/write memory using a plurality of memory locations so that there is a one-to-one correspondence between different memory locations and different portions of said monitored region, and (d) comparing said stored, sensed wind speed vectors with a predetermined pattern so as to detect any correspondence between said predetermined pattern and said stored, sensed wind speed vectors.
Claim 12
Independent Claim 127 words
A method of microburst detection comprising the steps of: (a) selecting a region in space for monitoring within which aircraft are vulnerable to abrupt changes in wind velocity vectors, (b) providing a doppler radar and employing said doppler radar for detecting wind speed vectors, or at least components of wind speed vectors parallel to a propagation path defined by said doppler radar, (c) storing said sensed wind speed vectors in a read/write memory using a plurality of memory locations so that there is a one-to-one correspondence between different memory locations and different portions of said monitored region, and (d) comparing said stored, sensed wind speed vectors with a predetermined pattern so as to detect any correspondence between said predetermined pattern and said stored, sensed wind speed vectors.
Claim 13
Dependent Claim 54 words
The method of claim 10 which includes the further steps executed in the event that said method determines a correspondence between said predetermined pattern and said stored, sensed wind velocity vectors, of: (i) deriving a geogrpahical coordinate determined in part by said predetermined pattern and in part by said stored, sensed wind velocity vectors.
Claim 14
Dependent Claim 40 words
The method of claim 10 in which said selecting step comprises selecting a region which is located relative to an airport runway and which extends for about five miles from a nominal take off or landing point on said runway.
Claim 15
Dependent Claim 40 words
The method of claim 10 in which said selecting step comprises selecting a region which is located relative to an airport runway and which extends for about one mile from a nominal take off or landing point on said runway.
Claim 16
Dependent Claim 31 words
The method of claim 10 in which said selecting step comprises selecting a region which is located relative to an airport runway and extends in altitude up to about 1200 feet.
Claim 17
Dependent Claim 31 words
The method of claim 10 in which said selecting step comprises selecting a region which is located relative to an airport runway and extends in altitude up to about 300 feet.
Claim 18
Dependent Claim 40 words
The method of claim 10 in which said storing step includes the step of ordering said sensed wind speed vectors in a multi-cell array with plural rows and columns wherein there are about 150 or less cells in each column.
Claim 19
Dependent Claim 48 words
The method of claim 10 in which said storing step includes the step of ordering said wind speed vectors in a multi-cell array with plural rows and columns wherein each cell represents a portion of said monitored region, each cell representing less than about 200 feet in range.

References Cited (Backward Citations)

US3573824A Cited
US4015257A Cited
US3984685A Cited
US4043194A Cited
US4223309A Cited
US4336606A Cited
US4351188A Cited
US4370652A Cited
US4516125A Cited
US4589070A Cited
US4649388A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1990-12-07 1991-06-08 1991-12-08 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1994-12-07 1995-06-08 1995-12-08 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1998-12-07 1999-06-08 1999-12-08 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag