FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly to device designed to joint gas turbine engine to aircraft. Proposed device comprise load bearing part to transmit loads, crosspieces and brackets fixed on said parts, including standby parts. All said elements are interconnected with the help of fasteners, including rod-type and hinge-type fasteners, with a spacing relative to load bearing parts transmitting loads. Stand by parts are distributed in engine vertical lengthwise cross section in front and rear attachment rings.
EFFECT: higher reliability of attachment and reduced weight.
3 cl, 9 dwg
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