FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely, to engine mount. Proposed mount comprises beam 2 with attachments and tie-rod 4 with one end hinged to rod 6 linked to said beam and opposite hinged to gas turbine engine. Rod 6 is arranged at beam via elastic linkage 7 composed of two layered cylinders 71, 72, elastomer and metal to retain rod 6 by its ends.
EFFECT: decreased vibration transmitted by gas turbine engine.
9 cl, 3 dwg
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