FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely, to turbojet aircraft nacelle and turbojet support strut. Strut 9 incorporates part 11 for connection of turbojet blower casing 1 or gas generator casing 5 to aircraft wing and box-like Y-shape part 19 rigidly secured to said connection part 11 and configured to form top part of nacelle fixed inner structure.
EFFECT: possibility to use lighter materials.
19 cl, 22 dwg
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