JPH0225400U - - Google Patents
Info
- Publication number
- JPH0225400U JPH0225400U JP10399588U JP10399588U JPH0225400U JP H0225400 U JPH0225400 U JP H0225400U JP 10399588 U JP10399588 U JP 10399588U JP 10399588 U JP10399588 U JP 10399588U JP H0225400 U JPH0225400 U JP H0225400U
- Authority
- JP
- Japan
- Prior art keywords
- band
- launcher
- flying object
- launching hook
- separated
- 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
- 238000000926 separation method Methods 0.000 claims description 5
- 238000010586 diagram Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
Landscapes
- Toys (AREA)
Description
第１図は本考案の一実施例を示す機体の正面説
明図、第２図は第１図の右側面説明図、第３図は
第１図のスプリングボツクスの拡大断面図、第４
図は第１図の分離離脱機構の拡大断面図、第５図
は上記分離離脱機構の作動後の説明図、第６図は
発射姿勢に支持されたロケツトの側面図、第７図
は従来のランチングフツクの構造を示す図で、第
６図のロケツトを正面から見た拡大説明図、第８
図は従来の他のランチングフツクの構造を示す説
明図、第９図は第８図のランチングフツクの作動
後の状態を示す説明図である。
４……ランチヤ、５，６……ランチヤレール、
１１……機体、１２，１３……ランチングフツク
、１４……バンド、１４ａ，１４ｂ……ハーフバ
ンド、１７……セパレーシヨンナツト、１８……
分離離脱機構、Ｒ……飛しよう体としてのロケツ
ト。
Fig. 1 is an explanatory front view of the fuselage showing one embodiment of the present invention, Fig. 2 is an explanatory right side view of Fig. 1, Fig. 3 is an enlarged sectional view of the spring box shown in Fig. 1, and Fig. 4
The figures are an enlarged sectional view of the separation and release mechanism shown in Fig. 1, Fig. 5 is an explanatory view of the separation and release mechanism after operation, Fig. 6 is a side view of the rocket supported in the firing attitude, and Fig. 7 is a conventional This is a diagram showing the structure of the launching hook, an enlarged explanatory view of the rocket in Figure 6 viewed from the front, and Figure 8.
9 is an explanatory view showing the structure of another conventional launching hook, and FIG. 9 is an explanatory view showing the state of the launching hook of FIG. 8 after it is operated. 4...Lancia, 5,6...Lancia rail,
11... Airframe, 12, 13... Launching hook, 14... Band, 14a, 14b... Half band, 17... Separation nut, 18...
Separation/detachment mechanism, R...Rocket as a flying body.
Claims (1)
しよう体の機体に取り付けられるとともに、ラン
チヤに係合して飛しよう体を発射姿勢に支持する
ランチングフツクの取付構造において、飛しよう
体の機体に分離離脱式のバンドを巻き付けるとと
もに、このバンドにランチングフツクを固定し、
前記バンドには、機体がランチヤから離脱したの
ちにバンドを複数に分離して機体から離脱させる
分離離脱機構を設けたことを特徴とするランチン
グフツクの取付構造。 In the mounting structure of the launching hook, which is attached to the body of a flying object to be launched while being suspended from the launcher, and also engages with the launcher and supports the flying object in the launch posture, it is separated into the body of the flying object. At the same time as wrapping a removable band, fixing the launching hook to this band,
A launching hook mounting structure characterized in that the band is provided with a separation/detachment mechanism that separates the band into a plurality of parts and detaches the band from the aircraft body after the aircraft body is separated from the launcher.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10399588U JPH0225400U (en) | 1988-08-05 | 1988-08-05 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10399588U JPH0225400U (en) | 1988-08-05 | 1988-08-05 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0225400U true JPH0225400U (en) | 1990-02-20 |
Family
ID=31335321
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP10399588U Pending JPH0225400U (en) | 1988-08-05 | 1988-08-05 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0225400U (en) |
-
1988
- 1988-08-05 JP JP10399588U patent/JPH0225400U/ja active Pending
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