FIELD: protection of flying vehicle engines. SUBSTANCE: protective unit includes swivel protective shield mounted on side wall of air intake in front of main wing of aircraft for deflection from outer side edge of air intake. Besides, that, rational geometric and mass parameters of swivel shield are indicated. EFFECT: reduced intensity of vortex generation in air flow sucked by power plant from surrounding medium when at rest. 2 dwg
Authors
Dates
2001-06-10—Published
1999-01-15—Filed