The invention relates to the technical field of head covers and thermal protection of hypersonic aircrafts, in particular to an aircraft radome connecting structure which comprises a radome, a nut and a heat insulation screw corresponding to the nut, and the radome comprises a connecting end used for being connected with a rear cabin section. At least three nut holes are formed in the inner wall of the connecting end in the circumferential direction at intervals, and bolt holes communicated with the nut holes are further formed in the connecting end. Nuts corresponding to the nut holes are arranged in the nut holes; the heat insulation screws corresponding to the nuts are used for penetrating through the connecting holes in the rear cabin section and the bolt holes in the connecting ends to be connected with the nuts so that the rear cabin section can be connected with the connecting ends. The problem that in the prior art, an adhesive type is adopted or the use temperature of the adhesive is increased by improving the adhesive, but the falling risk still exists can be solved.
本发明涉及高超声速飞行器的头罩及热防护技术领域,具体涉及一种飞行器天线罩连接结构,该飞行器天线罩连接结构,包括:天线罩、螺母和与螺母对应的隔热螺钉,其中,天线罩包括用于与后部舱段连接的连接端,所述连接端的内壁周向间隔设有至少三个螺母孔,所述连接端内还设有与所述螺母孔连通的螺栓孔;与各个所述螺母孔对应的螺母设在所述螺母孔内;与所述螺母对应的隔热螺钉用于穿过所述后部舱段上的连接孔和所述连接端上的螺栓孔与所述螺母连接,以将所述后部舱段和连接端连接。本申请能够解决现有技术中采用粘接剂类型或通过改良粘接剂提高其使用温度,但是依然有脱落风险的问题。
Aircraft radome connecting structure
一种飞行器天线罩连接结构
2022-07-05
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |