发明名称 STUD BOLT ASSEMBLY FOR AIRPLANE FUSELAGE CLEARANCE CONTROL
摘要 PURPOSE: A stud bold assembly for adjusting the gap of an aircraft body is provided to uniformly adjust the assembly gap between the body and a radome which is coupled to the body so that an aircraft radar is protected from a strong wind pressure. CONSTITUTION: A stud bold assembly for adjusting the gap of an aircraft body (D) includes a flange (110), a stud bolt (120), a fixing screw (140), and a fixing nut (130). The flange is placed inside a radome (R). One side of the stud bolt is inserted into the coupling hole (111) of the flange, and has a guide hole. The fixing screw penetrates the part of the flange different from the coupling hole, is inserted into the guide hole, and fixes the stud bolt to the flange. The fixing nut is placed at the other side of the stud bolt, and fixes the stud bolt to the body.
申请公布号 KR20130077233(A) 申请公布日期 2013.07.09
申请号 KR20110145829 申请日期 2011.12.29
申请人 KOREA AEROSPACE INDUSTRIES, LTD. 发明人 WOO, SUNG JO
分类号 B64C1/36;B64F5/00;F16B35/00 主分类号 B64C1/36
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