FIELD: aviation.
SUBSTANCE: invention relates to a fairing node of an aircraft. The fairing node for an air vehicle includes fairing (114), primary structure (164), heat protection system (190) and sealing node (192). Fairing (114) is connected to a tank near edge (118) of wing (112). Heat protection system (190) and sealing node (192) are connected to primary structure (164). The sealing node is made with the possibility of overlapping at least part of edge (118) of wing (112).
EFFECT: invention simplifies the fairing structure.
25 cl, 19 dwg
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Authors
Dates
2021-11-09—Published
2018-05-24—Filed