FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to engine nacelle and engine nacelle component mounting system. Said mounting system for nacelle component (2a, 2b, 3a, 3b) comprises mounting zone formed by said component to interact with jointing zone formed by engine pylon. Besides, system comprises attachment appliances 10 to allow rigid and split joint between said component and pylon. Mounting appliances and additional attachment appliances may turn both about one another and relevant nacelle.
EFFECT: simplified design and higher strength.
11 cl, 16 dwg
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