INTEGRATED AIRCRAFT VORTEX SAFETY SYSTEM

FIELD: aircraft operation. ^ SUBSTANCE: system contains information subsystems providing recording and saving of the information about assumed relative positions of the aircraft and dangerous aerodynamic forces and moments acting at the aircraft, induced by vortex trails of vortex generators; vortex...

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Bibliographische Detailangaben
Hauptverfasser:	PASEKUNOV IGOR' VLADIMIROVICH, BELOTSERKOVSKIJ ANDREJ SERGEEVICH, KANEVSKIJ MIKHAIL IGOREVICH, BARANOV NIKOLAJ ALEKSEEVICH
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	ANALOGOUS ARRANGEMENTS USING OTHER WAVES DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES GYROSCOPIC INSTRUMENTS LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUIDLEVEL METERING BY VOLUME NAVIGATION PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS RADIO DIRECTION-FINDING RADIO NAVIGATION SURVEYING TESTING
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Beschreibung
Zusammenfassung:	FIELD: aircraft operation. ^ SUBSTANCE: system contains information subsystems providing recording and saving of the information about assumed relative positions of the aircraft and dangerous aerodynamic forces and moments acting at the aircraft, induced by vortex trails of vortex generators; vortex trail areas at a predictable point of time, at a predicted distance from the aircraft; and presentation of this information to the user. The user setting the danger criteria may be the aircraft crew and/or air traffic control services. The information may be visualised in a form that is easy for perception, in an amount sufficient for the generation of a signal prescribing an avoidance manoeuvre for the aircraft to avoid the dangerous vortex trail area. ^ EFFECT: flight safety increase. ^ 15 cl, 5 dwg