JPH03112697U - - Google Patents
Info
- Publication number
- JPH03112697U JPH03112697U JP2225390U JP2225390U JPH03112697U JP H03112697 U JPH03112697 U JP H03112697U JP 2225390 U JP2225390 U JP 2225390U JP 2225390 U JP2225390 U JP 2225390U JP H03112697 U JPH03112697 U JP H03112697U
- Authority
- JP
- Japan
- Prior art keywords
- deployable
- medicine
- fuselage
- deployment
- wing
- 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 4
- 239000003381 stabilizer Substances 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 2
- 239000007789 gas Substances 0.000 description 1
Landscapes
- Transmission Devices (AREA)
- 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
この考案の機体内部構成図、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。な
お、図中同一符号は同一、又は相当部分を示す。
Figures 1 and 2 are general configuration diagrams of an embodiment of the guided flying object of this invention, Figures 3 and 4 are internal configuration diagrams of the aircraft of this invention, and Figure 5 is a conventional guided flying object. It is a figure showing one example of this. 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 equivalent parts.
Claims (1)
置に取り付けられた操舵翼と、機体の後半部所定
位置に収納された展開安定翼と、前記展開安定翼
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
動するピストンによつて構成され、かつ前記展開
安定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
は前記展開安定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展開安定翼を
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 steering wing attached to a predetermined position in the front half of the fuselage, a deployable stabilizing wing stored in a predetermined position in the rear half of the fuselage, and a deployment mechanism for deploying the deployable stabilizer wing, A deployment actuator is constructed of a time delay medicine, a power medicine ignited by the time delay medicine, and a piston actuated by the power medicine, and a deployment actuator that generates energy for deploying the deployment stabilizing wings. Before launch, the deployable stabilizing wings are stored in the aircraft body, and after launch, the piston is actuated by the pressure of the combustion gas of the output charge, and after a predetermined delay time, the deployable stabilizing wings are operated by the pressure of the combustion gas of the output charge. A guided flying object characterized by being configured to be deployed using energy.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2225390U JPH03112697U (en) | 1990-03-06 | 1990-03-06 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2225390U JPH03112697U (en) | 1990-03-06 | 1990-03-06 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH03112697U true JPH03112697U (en) | 1991-11-18 |
Family
ID=31525268
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2225390U Pending JPH03112697U (en) | 1990-03-06 | 1990-03-06 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH03112697U (en) |
-
1990
- 1990-03-06 JP JP2225390U patent/JPH03112697U/ja active Pending
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