FIELD: protective devices.
SUBSTANCE: invention relates to ground-based means of protecting aircraft gas turbine engines. Method for controlling vortex formation on the surface of an aerodrome under aircraft air intakes consists in locating the general-purpose ground service facility on the gas field. Ground maintenance vehicle (3) with the shield (5) is located at a distance Rz = 15–20DLEQ from the longitudinal axis of the aircraft at the corners δ = ±45° and δ = ±135° in four possible positions, where
EFFECT: invention makes it possible to reduce the intensity of the vortex formation in front of the air intakes of the aircraft in the counter-lateral and posterolateral direction of the wind at the surface of the aerodrome.
1 cl, 2 dwg
Authors
Dates
2018-10-01—Published
2016-12-08—Filed