| 摘要 |
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 |
