AIRCRAFT WAKE VORTEX PREDICTOR AND VISUALIZER
A method to predict a location, intensity and movement of wake vortexes, and to detect wake vortexes, comprises collecting one or more ground-based measurements related to predicting the location, intensity and movement of wake vortexes; collecting one or more airborne-based measurements related to...
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Main Authors | , , , |
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Format | Patent |
Language | English French |
Published |
07.08.2008
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Subjects | |
Online Access | Get full text |
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Summary: | A method to predict a location, intensity and movement of wake vortexes, and to detect wake vortexes, comprises collecting one or more ground-based measurements related to predicting the location, intensity and movement of wake vortexes; collecting one or more airborne-based measurements related to predicting the location, intensity and movement of wake vortexes; integrating the ground-based and the airborne-based measurements to predict the location, intensity and movement of wake vortexes using a wake vortex prediction model selected from a plurality of wake vortex prediction models based on a group of inputs or parameters including the ground-based and the airborne-based measurements; and detecting wake vortexes by use of tracer material or substance emitted by an aircraft generating the wake vortexes. The step of detecting the wake vortexes comprises directing a tracer from a first aircraft into a vortical flow generated by the first aircraft, the tracer being visually indistinguishable from its surroundings to an unaided observer on the ground or in a following aircraft whilst the tracer is in the vortical flow; detecting a characteristic corresponding to the presence of the visually indistinguishable tracer directed into the vortical flow; and based at least in part on the detected characteristic, directing the flight of the first aircraft, or a second aircraft following the first aircraft, or both. |
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Bibliography: | Application Number: CA20072944681 |