JPS6027300U

JPS6027300U - Shell attachment mechanism of flying object

Info

Publication number: JPS6027300U
Application number: JP11805983U
Authority: JP
Inventors: 森山　宏
Original assignee: 三菱電機株式会社
Priority date: 1983-07-29
Filing date: 1983-07-29
Publication date: 1985-02-23

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Abstract] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

[Brief explanation of the drawing]

第１図は従来の結合機構の実施例を示す図、第２図は第
１図に示す結合機構の要部断面図、第３図はこの考案の
結合機構を示した図、第４図及び第５図は第３図に示す
結合機構の要部詳細図、第６図はこの考案の結合機構の
実施例を示した図であり、１は第１の外殻、２は第２の
外殻、４は雌部嵌合部、５は取付ネジ、７は雄部嵌合部
、１０は接合部分、１１はすき間、１４は貫通穴、１５
は円錐部、１６はネジ穴、１７は結合ブロック、１８は
傾斜部分である。なお、図中同一符号は同−又は相当部
分を示す。第２図第４図第３図−Ｃ９，３ ′　　ゾ＼＼冷澄※葵英３縛ぐｒ５６７１　　□６１１Ｄ　’Fig. 1 is a diagram showing an embodiment of a conventional coupling mechanism, Fig. 2 is a sectional view of a main part of the coupling mechanism shown in Fig. 1, Fig. 3 is a diagram showing a coupling mechanism of this invention, Fig. 4, and FIG. 5 is a detailed view of the main part of the coupling mechanism shown in FIG. 3, and FIG. 6 is a diagram showing an embodiment of the coupling mechanism of this invention, where 1 is the first outer shell, and 2 is the second outer shell. Shell, 4 is a female fitting part, 5 is a mounting screw, 7 is a male fitting part, 10 is a joint part, 11 is a gap, 14 is a through hole, 15
16 is a conical portion, 16 is a screw hole, 17 is a coupling block, and 18 is an inclined portion. Note that the same reference numerals in the figures indicate the same or equivalent parts. Figure 2 Figure 4 Figure 3-C9, 3' ＼＼ Cold Clear * Aoi Ei 3 Bind r 5 67 1 □611D '

Claims

[Scope of utility model registration request]

A cylindrical female fitting part is formed at the first outer shell (SHELL) end, and a cylindrical male fitting part is formed at the second outer shell end, and assembled by fitting them together. In the outer shell coupling mechanism for a flying object that allows coupling, a through hole is provided in the training center around the female fitting portion of the first outer shell, and a through hole is provided in the male fitting portion of the second outer shell. A conical part is formed around the entire circumference where the through hole is located when the female part fitting part is fitted, and a screw hole into which a mounting screw for assembly can be screwed is provided. A second outer shell is fitted into the second outer shell, which has a shape that fits into the through hole and has an inclined part that matches the inclination of the conical part provided in the male part fitting part, and further has a threaded part of the mounting screw passed through the second outer shell. Insert the coupling block, which has a hole that can be accessed eccentrically from the center of the external shape, into the female fitting part, pass the mounting screw through the hole in the coupling block suspension, and tighten it into the screw hole in the male fitting part. As a result, the inclined part of the coupling block comes into contact with the conical part of the male fitting part, and the outer periphery of the coupling block presses the inner wall of the through hole of the female fitting part, so that the first and second outer shells can be coupled. A mechanism for connecting the outer shell of a flying object.