Patent References 3761691 3814912 Apparatus for computing the acceleration of an aircraft along its flight path Wind shear warning system System for providing an indication of wind shear Apparatus for computing the rate of change of energy of an aircraft Wind shear warning system for aircraft Aircraft instrument Ground proximity warning system with time and altitude based mode switching Aircraft liftmeter InventorsAssigneeApplicationNo. 06/834374 filed on 02/28/1986US Classes:340/968, Wind shear244/191, Acceleration control340/963, Flight alarm340/967, Attitude (including yaw, angle of attack, roll, pitch, glide slope)701/15, With indication or control of take-off701/16, With indication or control of landing73/178TTake-off and landing monitorsExaminersPrimary: Orsino, Joseph A.Assistant: Swarthout, Brent A. Attorney, Agent or FirmInternational ClassesG05D 1/00 (20060101)G05D 1/06 (20060101) AbstractAn improved windshear warning apparatus for aircraft, responsive to both the magnitude of the wind shear and the allowable time the windshear can be tolerated at a given magnitude. The sensed magnitude is used to compute the allowable time before providing a windshear alarm. For large windshear rates, the allowable time is short; conversely for small windshear rates which exceed a threshold level, a longer time period is computed before an alarm occurs. Since a windshear rate must persist for the computed allowable time before activating the alarm, windshear rates that are above the threshold level for elapsed time less than the computed allowable time will not result in an enunciation, while high magnitude windshear rates of short duration will not cause false alarms since they do not exceed the computed allowable time. | |