METHOD FOR PROVISION OF AIRCRAFT FLIGHT VORTEX SAFETY Russian patent published in 2013 - IPC G08G5/02 

FIELD: aircraft engineering.

SUBSTANCE: proposed method comprises transmitting date on generated vortex trace, flight speed, tine of "board-board" radio transmission in broadcast mode and/or "point-point" mode, and receiving said data by aircraft subscriber or aircraft subscribers. Note here that appropriate aircraft subscriber calculates magnitudes of bank perturbation effects corresponding to current parameters of vortex trace from aircraft generating said vortex trace and measures vertex situation in front of aircraft subscriber. Besides, it calculates bank perturbation moment to compare bank perturbation moment magnitudes calculated using aforesaid results with bank perturbation moment magnitudes calculated using the data received from aircraft generating said vortex trace. Note here that data required for defining vortex situation in front of aircraft subscriber are obtained by static pressure transducers mounted at front "critical" points of aircraft wings. Note also that maximum calculated magnitudes of bank perturbation moment is selected as expected effect of vortex trace on aircraft subscriber to load selected magnitude as correcting magnitude into aircraft subscriber control system.

EFFECT: higher safety.

3 dwg