INTEGRATED AIRCRAFT VORTEX SAFETY SYSTEM Russian patent published in 2008 - IPC G01S13/93 G01C23/00 G01F17/00 

Abstract RU 2324953 C2

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

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RU 2 324 953 C2

Authors

Baranov Nikolaj Alekseevich

Belotserkovskij Andrej Sergeevich

Kanevskij Mikhail Igorevich

Pasekunov Igor' Vladimirovich

Dates

2008-05-20Published

2003-07-25Filed