FIELD: aircraft engineering.
SUBSTANCE: stalling warning system comprises an angle of attack sensor, warning means, two sensors for local angles of attack, set apart from each other at a distance of not less than 60 % of the full span of the wing, sensors for ailerons position or control position sensor in a transverse channel, control unit. Means of notification are made in the form of a combined needle indicator, which contains a housing with two opposite sectorial scales, left and right arrows.
EFFECT: flight safety and acceleration of piloting training are ensured.
13 cl, 14 dwg
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