FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to suspension pylon bearing structure 101 designed to secure turbojet to aircraft wing. This structure comprises first lateral unit 102 and second lateral unit 103 secured to aircraft wing, and fastening element to be attached to turbojet. Note here that said lateral units make female component relative to central plate 104, in fact, elongated along main axis 105 of structure 101. Plate 104 is connected with said fastening element and made from metal or alloy capable of resisting the temperature of, at least, 1000°C for, at least, 15 minutes.
EFFECT: higher load withstandability.
12 cl, 6 dwg
