An airplane transition beam butt joint structure comprises a transition beam and a wing, an external store is hung on the transition beam, the transition beam and the wing are in butt joint at a front point and a rear point, a front butt joint intersection point structure and a rear butt joint intersection point structure exist between the transition beam and the wing, and the front butt joint intersection point structure and the rear butt joint intersection point structure are both designed to be force transmission structures. The gravity center of an external hanging object hung on the transition beam can be flexibly arranged within the range between the front butt joint intersection point structure and the rear butt joint intersection point structure.
一种飞机过渡梁对接结构,含有过渡梁和机翼,在过渡梁上挂载有外挂物,所述的过渡梁与机翼采用前后两点对接,过渡梁与机翼之间存在前对接交点结构和后对接交点结构,前对接交点结构和后对接交点结构均设计为传力结构,外挂在过渡梁上的外挂物重心可以在前对接交点结构和后对接交点结构之间的范围内灵活布置。
Aircraft transition beam butt joint structure
一种飞机过渡梁对接结构
2023-05-02
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Aircraft cabin cableless butt joint device and butt joint method thereof
Europäisches Patentamt | 2020
|Shore crane bearing rail beam joint butt joint structure
Europäisches Patentamt | 2022
|Europäisches Patentamt | 2021
|Amphibious aircraft wing butt joint posture adjusting method
Europäisches Patentamt | 2023
|