JPS6160508U - - Google Patents
Info
- Publication number
- JPS6160508U JPS6160508U JP14518984U JP14518984U JPS6160508U JP S6160508 U JPS6160508 U JP S6160508U JP 14518984 U JP14518984 U JP 14518984U JP 14518984 U JP14518984 U JP 14518984U JP S6160508 U JPS6160508 U JP S6160508U
- Authority
- JP
- Japan
- Prior art keywords
- antenna
- fitting
- metal fitting
- screw
- hole
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 239000002184 metal Substances 0.000 claims description 8
- 238000010586 diagram Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
Landscapes
- Details Of Aerials (AREA)
- Support Of Aerials (AREA)
Description
第1図は飛しよう体用アンテナの取付部位図、
第2図は従来の飛しよう体用アンテナ取付機構を
示す断面図、第3図は第2図に示すもののA−A
断面図、第4図は第2図に示すもののB−B断面
図、第5図は第2図に示すもののC−C断面図、
第6図はこの考案による飛しよう体用アンテナ取
付機構のアンテナ後部からの図、第7図は第6図
に示すもののD−D断面図、第8図は解放状態を
示す図、第9図は、第7図における後端部部分図
である。
図中、1は飛しよう体用アンテナ、2はシエル
A、3はシエルB、4はアンテナ開口部、5はア
ンテナフランジ部、6は導波管部品、7は導波管
フランジ部、8は導波管開口部、12はガイドピ
ン、13はガイドピン穴、21は後端部壁面、2
2は丸穴、24は固定金具、25はスプリングピ
ン、26は傾斜底面をもつた角穴、27は傾斜面
、28はネジ部、29は底部接触面、30は締付
金具、35は平面部、36は保持穴A、37は保
持穴B、38は取付金具、39は壁面穴、41は
抜止リングである。尚、各図中同一符号は同一又
は相当部分を示すものとする。
Figure 1 is a diagram of the installation part of the flying body antenna.
Figure 2 is a sectional view showing a conventional flying body antenna mounting mechanism, and Figure 3 is an A-A of the one shown in Figure 2.
4 is a BB sectional view of the thing shown in FIG. 2, FIG. 5 is a C-C sectional view of the thing shown in FIG. 2,
Fig. 6 is a view from the rear of the antenna of the antenna mounting mechanism for a flying object according to this invention, Fig. 7 is a sectional view taken along line DD of the antenna shown in Fig. 6, Fig. 8 is a view showing the released state, Fig. 9 7 is a partial view of the rear end in FIG. 7. FIG. In the figure, 1 is a flying body antenna, 2 is a shell A, 3 is a shell B, 4 is an antenna opening, 5 is an antenna flange, 6 is a waveguide component, 7 is a waveguide flange, and 8 is a A waveguide opening, 12 a guide pin, 13 a guide pin hole, 21 a rear end wall surface, 2
2 is a round hole, 24 is a fixing metal fitting, 25 is a spring pin, 26 is a square hole with an inclined bottom surface, 27 is an inclined surface, 28 is a threaded part, 29 is a bottom contact surface, 30 is a tightening metal fitting, 35 is a flat surface 36 is a holding hole A, 37 is a holding hole B, 38 is a mounting bracket, 39 is a wall hole, and 41 is a retaining ring. Note that the same reference numerals in each figure indicate the same or corresponding parts.
Claims (1)
号の送受信を行うアンテナ取付機構において、ア
ンテナの前端部及び中間部はボルト締めにより固
定し、一方アンテナの後端部壁面には、機体の前
方から後方にかけて外表面側に勾配をもつ傾斜底
面を有した穴部を形成し、さらにアンテナの上記
傾斜底面穴に係合する傾斜面と機軸方向に移動す
るためのネジ部と、機軸方向に滑動するための底
部接触面を形成した締付金具を、上記締付金具の
ネジ部に嵌合し、上記締付金具を軸方向に移動す
るためのネジ金具を介して、上記締付金具の底部
接触面に接触する平面部と上記ネジ金具を保持す
る保持穴を形成し機体壁面上に固定される取付金
具に取り付け、上記ネジ金具に対向して設けたア
ンテナの後端部壁面穴を通して上記ネジ金具を回
転させることにより、上記締付金具を軸方向に移
動させて上記両傾斜面を係合させることにより両
傾斜面に発生する摩擦斜面分力によつてアンテナ
後端部を機体に押し付けるように固定したことを
特徴とする、アンテナ取付機構。 In the antenna mounting mechanism that is attached to the outer wall of the flying body and transmits and receives various electrical signals, the front end and middle part of the antenna are fixed with bolts, while the rear end wall of the antenna is attached to the front and rear parts of the aircraft. a hole portion having a sloped bottom surface with a slope toward the outer surface side, and a screw portion for sliding in the direction of the axis and a slope surface that engages with the hole in the sloped bottom surface of the antenna, and a screw portion for sliding in the direction of the axis. The bottom contact surface of the tightening fitting is fitted into the threaded part of the tightening fitting, and the bottom contact surface of the tightening fitting is fitted through the threaded fitting for moving the tightening fitting in the axial direction. A holding hole for holding the screw metal fitting is formed in the flat part that comes into contact with the screw metal fitting, and the screw metal fitting is attached to a mounting metal fitting fixed on the wall surface of the aircraft body, and the screw metal fitting is passed through a wall hole at the rear end of the antenna provided opposite to the screw metal fitting. By rotating, the above-mentioned fastening fitting is moved in the axial direction and both the above-mentioned inclined surfaces are engaged, and the rear end of the antenna is fixed so as to be pressed against the aircraft body by the frictional slope component force generated on both inclined surfaces. The antenna mounting mechanism is characterized by:
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP14518984U JPS6160508U (en) | 1984-09-26 | 1984-09-26 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP14518984U JPS6160508U (en) | 1984-09-26 | 1984-09-26 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6160508U true JPS6160508U (en) | 1986-04-23 |
Family
ID=30703445
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP14518984U Pending JPS6160508U (en) | 1984-09-26 | 1984-09-26 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6160508U (en) |
-
1984
- 1984-09-26 JP JP14518984U patent/JPS6160508U/ja active Pending
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