FIELD: aviation; devices for protection of flying vehicle engines against penetration of foreign matter. SUBSTANCE: proposed device has movable triangular lower panel mounted in air intake body. Movable panel performs reciprocating motion in horizontal direction and horizontal oscillatory motion perpendicularly relative to air intake at distance of d = (1.0-1.2) at oscillation period T = 0.5 to 4.0 s; movable panel is located at distance c = 0.005 to 0.01 m from its leading edge. Length llow of panel and height B of midsection of air intake are made at the following relationship: = 0.05 to 1.2. Width blow of panel and width L of midsection of air intake are made at the following relationship: = 0.8 to 0.9. EFFECT: reduced probability of sucking vortex core inside air intake together with foreign matter. 3 dwg
Authors
Dates
2003-05-10—Published
2000-02-21—Filed