FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to fuselage structural elements. Antenna cowling installed at aircraft comprises radiolucent front part and rear metallic part and skin reinforced by appropriate structural elements. Said cowling features streamlined torpedo-shape with stiff metal panel at top part extending over the entire length to make the bed for erection of external antennas and having hatches to be closed by covers. Plates strap is fitted atop radiolucent front part. Cowling is fitted at pylon above pilot cockpit canopy, elevated above fuselage and extended forward relative to canopy ledge. Besides, it has cutout made beneath in pylon outline and is secured at load belt with that of the pylon permanently attached to fuselage including rotary antenna attachment beam.
EFFECT: increased field of vision.
9 dwg
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