FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed device comprises annular box and detachable elastic elements. Front ends of said elements are brought under nacelle wall inner edge while annular box inner surface is jointed with jet nozzle by con-rods. Said con-rods are arranged at an angle to engine lengthwise axis. Every elastic element is secured to annular box by, at least, two threaded joints with self-locking nuts. The latter are arranged in said box to displace along and across engine lengthwise axis. Elastic element rear end is brought into annular groove made in the box.
EFFECT: higher reliability of joint.
6 dwg
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