FIELD: engine building.
SUBSTANCE: invention relates to the protection of aircraft engines from the ingress of foreign objects. Onboard engine protection device against the ingress of foreign objects contains movable lower panel (1) located in housing (7) of the air intake, and has two panels (12, 13) of the lower panel on two transverse axes in the lower part. Panels (12, 13) simultaneously make oscillatory movements upwards in the transverse plane of the bottom panel at the corners αn = 25–30° with periods of oscillation T = 1.0–4.0 s. Rear panel (12) is located from the edge of bottom panel (1) at a relative length of
EFFECT: invention increases the efficiency of the engine protection device in all operating modes on the ground.
1 cl, 3 dwg
Authors
Dates
2019-02-13—Published
2017-12-29—Filed