The invention discloses a connecting structure of a homogeneous ceramic thermal structural part of a high-speed aircraft, and relates to the field of aviation structural material application, and the connecting structure comprises the homogeneous ceramic thermal structural part, a transition adapter frame and a metal connecting end frame; wherein the transition adapter frame is arranged between the homogeneous ceramic thermal structural part and the metal connecting end frame, is used as a connecting part between the homogeneous ceramic thermal structural part and the metal connecting end frame, and is made of a fiber reinforced ceramic matrix composite material or a high-strength and high-modulus resin matrix composite material. The transition adapting frame is additionally arranged between the homogeneous ceramic thermal structural part and the metal connecting end frame, so that the problem of thermal matching of a connecting area of the homogeneous ceramic thermal structural part is solved.
本发明公开了一种高速飞行器均质陶瓷热结构件的连接结构,涉及航空结构材料应用领域,包括:均质陶瓷热结构件、过渡转接框和金属连接端框;其中,过渡转接框介于均质陶瓷热结构件和金属连接端框之间,用于作为均质陶瓷热结构件和金属连接端框之间的连接件,采用纤维增强陶瓷基复合材料或高强高模树脂基复合材料制成。本发明通过在均质陶瓷热结构件与金属连接端框之间增加过渡转接框,以解决均质陶瓷热结构件连接区热匹配的问题。
Connecting structure of homogeneous ceramic thermal structural member
一种均质陶瓷热结构件的连接结构
2023-09-01
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
CONNECTING STRUCTURE OF TRANSPORT BOGIE AND CONNECTING MEMBER
Europäisches Patentamt | 2018
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