JPH0387096U - - Google Patents
Info
- Publication number
- JPH0387096U JPH0387096U JP14885589U JP14885589U JPH0387096U JP H0387096 U JPH0387096 U JP H0387096U JP 14885589 U JP14885589 U JP 14885589U JP 14885589 U JP14885589 U JP 14885589U JP H0387096 U JPH0387096 U JP H0387096U
- Authority
- JP
- Japan
- Prior art keywords
- deployable
- wings
- types
- medicine
- fuselage
- 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
- 239000003814 drug Substances 0.000 claims description 6
- 239000000567 combustion gas Substances 0.000 claims description 3
- 230000000087 stabilizing effect Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 2
- 239000007789 gas Substances 0.000 description 1
Landscapes
- Toys (AREA)
Description
第１図及び第２図はこの考案による誘導飛しよ
う体の一実施例の全体構成図、第３図、第４図は
機体内部構成図、第５図は従来の誘導飛しよう体
の一実施例を示す図である。
図において、８……展開アクチユエータ、９…
…アーム、１０……軸、１１，１２……歯車、１
３……軸、１６……ガスシリンダ、１７……ピス
トン、１８……軸、１９……シアピン、２０……
点火プラグ、２１……延時薬、２２……出力薬、
２３……Ｏリング、２４……燃焼ガスである。尚
、図中同一符号は同一または相当部分を示す。
Figures 1 and 2 are overall configuration diagrams of an embodiment of a guided flying object based on this invention, Figures 3 and 4 are internal configuration diagrams of the aircraft, and Figure 5 is an implementation of a conventional guided flying object. It is a figure which shows an example. In the figure, 8...deployment actuator, 9...
...Arm, 10...Axle, 11,12...Gear, 1
3... shaft, 16... gas cylinder, 17... piston, 18... shaft, 19... shear pin, 20...
Spark plug, 21... Time delay medicine, 22... Output medicine,
23... O ring, 24... Combustion gas. Note that the same reference numerals in the figures indicate the same or corresponding parts.
Claims (1)
置に収納された展開安定翼と、機体の後半部所定
位置に収納された展開操舵翼と、前記二種の展開
翼を展開するための展開機構と、延時薬と前記延
時薬により点火される出力薬と前記出力薬により
作動するピストンとによつて構成され、かつ前記
二種の展開翼を展開するためのエネルギを発生す
る展開アクチユエータとから成り、飛しよう体の
発射前は前記二種の展開翼を機体内に収納してお
き、発射後、前記ピストンを前記出力薬の燃焼ガ
スの圧力で作動させ所定の遅れ時間後に前記二種
の展開翼を前記出力薬の燃焼ガスのエネルギにて
展開させるように構成したことを特徴とする誘導
飛しよう体。 A fuselage of a flying body, a deployable stabilizing wing stored in a predetermined position in the front half of the fuselage, a deployable steering wing stored in a predetermined position in the rear half of the fuselage, and a deployable wing for deploying the two types of deployable wings. a mechanism, and a deployment actuator configured with a time delay medicine, an output medicine ignited by the time delay medicine, and a piston operated by the output medicine, and which generates energy for deploying the two types of deployment wings. Before launching the flying object, the two types of deployable wings are stored inside the aircraft body, and after the launch, the piston is actuated by the pressure of the combustion gas of the output charge, and after a predetermined delay time, the two types of deployable wings are A guided flying object, characterized in that the deployable wings are configured to be deployed by the energy of the combustion gas of the power charge.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14885589U JPH0387096U (en) | 1989-12-25 | 1989-12-25 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14885589U JPH0387096U (en) | 1989-12-25 | 1989-12-25 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0387096U true JPH0387096U (en) | 1991-09-04 |
Family
ID=31695286
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP14885589U Pending JPH0387096U (en) | 1989-12-25 | 1989-12-25 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0387096U (en) |
-
1989
- 1989-12-25 JP JP14885589U patent/JPH0387096U/ja active Pending
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