A fairing assembly (114A) for an aerial vehicle (100) having a tank (202) that forms a body (110) of the vehicle and a wing (112) coupled to the tank is provided. The fairing assembly includes a substructure (164) configured to couple with a tank skin (378) of the tank, a thermal protection system (190) coupled to the substructure, and a seal assembly (192) coupled to the substructure, the seal assembly being configured to overlap at least a portion of an edge (118) of the wing.
ОБТЕКАТЕЛЬНЫЙ УЗЕЛ И СПОСОБ ДЛЯ НЕГО
25.11.2019
Patent
Elektronische Ressource
Russisch
IPC: | B64C AEROPLANES , Flugzeuge |
УЗЕЛ ПОДУШКИ БЕЗОПАСНОСТИ, УЗЕЛ И СПОСОБ НАДУВАНИЯ ПОДУШКИ БЕЗОПАСНОСТИ
Europäisches Patentamt | 2019