US4012713A
Expired / Lapsed
US
⏱️ 0.0 years remaining
System for providing an indication of wind shear
Assignee: Safe Flight Instrument LLC
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Filing: 1975-11-05
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Granted: 1977-03-15
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Expires: 1995-11-05
Abstract
Abstract The output of a transducer providing a signal in accordance with the instantaneous air speed of an aircraft is differentiated and fed to a summing device which subtracts therefrom a signal in accordance with the horizontal acceleration of the aircraft, this signal being derived from the output of an inertial instrument such as an accelerometer. The output of the summing device represents the magnitude of the wind shear condition (rate of change of wind velocity with changes in altitude). This signal is fed to appropriate indicator means which may comprise an appropriate display, a peak magnitude storage device, a warning device indicating a dangerous wind shear condition, or a telemetering device providing a wind shear reading to a ground station for use in advising other aircraft.
Inventors
- 👤 Leonard M. Greene
- 👤 Ramon Bloch
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-03 12:20
CPC Classifications
G; G01; G01W; G01W1/00; G01P; G01P5/00; G05; G05D; G05D1/00; G05D1/04; G05D1/06; G05D1/0607; G05D1/0615; G06; G06G; G06G7/00; G06G7/48; G06G7/78
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
85 words
A system for generating a windshear signal representing the windshear condition encountered by an aircraft comprising: means for generating a signal representing the rate of change of the instantaneous airspeed of the aircraft, means for generating a signal representing the horizontal inertial acceleration of the aircraft, means for subtracting the horizontal inertial acceleration signal from the rate of change of instantaneous airspeed signal to provide a windshear signal representing windshear, and means for processing said windshear signal to provide an indication representing the magnitude thereof.
Claim 2
Independent Claim
85 words
A system for generating a windshear signal representing the windshear condition encountered by an aircraft comprising: means for generating a signal representing the rate of change of the instantaneous airspeed of the aircraft, means for generating a signal representing the horizontal inertial acceleration of the aircraft, means for subtracting the horizontal inertial acceleration signal from the rate of change of instantaneous airspeed signal to provide a windshear signal representing windshear, and means for processing said windshear signal to provide an indication representing the magnitude thereof.
Claim 3
Dependent Claim
22 words
The device of claim 1 wherein said processing means comprises a display for directly displaying the magnitude of the wind shear signal.
Claim 4
Dependent Claim
41 words
The system of claim 1 wherein said processing means comprising a warning device for generating a warning signal and detector means responsive to the wind shear signal for actuating said warning device when the wind shear signal exceeds a predetermined value.
Claim 5
Dependent Claim
57 words
The device of claim 1 wherein said processing means comprises peak detector means for providing an output in accordance with the peak value of said wind shear signal, storage means for storing the peak output of said detector means and display means for providing a display in accordance with the peak signal stored in said storage means.
Claim 6
Dependent Claim
26 words
The system of claim 1 wherein said processing means comprises a telemetering transmitter for transmitting said signal in accordance with wind shear to a ground station.
Claim 7
Dependent Claim
46 words
The system of claim 1 wherein said means for generating a signal in accordance with the rate of change of airspeed comprises an instantaneous airspeed transducer for providing an output signal in accordance with instantaneous airspeed and differentiator means for differentiating the output of said transducer.
Claim 8
Dependent Claim
67 words
The system of claim 1 wherein said means for generating a signal in accordance with aircraft horizontal acceleration comprises an accelerometer mounted along the fuselage reference line of said aircraft for sensing accelerations along said reference line, means for generating a signal in accordance with the pitch of said aircraft and means for subtracting said signal in accordance with aircraft pitch from the output of said accelerometer.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1980-03-14 | 1980-09-13 | 1981-03-15 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1984-03-14 | 1984-09-13 | 1985-03-15 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1988-03-14 | 1988-09-13 | 1989-03-15 | $7700.00 | Window Closed / Lapsed |