JPH01111999U - - Google Patents
Info
- Publication number
- JPH01111999U JPH01111999U JP670288U JP670288U JPH01111999U JP H01111999 U JPH01111999 U JP H01111999U JP 670288 U JP670288 U JP 670288U JP 670288 U JP670288 U JP 670288U JP H01111999 U JPH01111999 U JP H01111999U
- Authority
- JP
- Japan
- Prior art keywords
- medicine
- fuselage
- deployable steering
- wing
- deployable
- 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 7
- 230000000087 stabilizing effect Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 3
- 239000000567 combustion gas Substances 0.000 description 1
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (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図は機体内部
構成図、第４図、第５図はロツク装置の断面図、
第６図は従来の誘導飛しよう体の一例を示す図で
ある。
図において、７はロツク装置、１０はうず巻き
ばね、１１は軸、１２と１３は歯車、１４はシリ
ンダ、１５はピストン、１６は穴、１７は軸、１
８は点火プラグ、１９は延時薬、２０は出力薬、
２１はＯリング、２２は燃焼ガスである。尚、図
中同一符号は同一または相当部分を示す。
1 and 2 are general configuration diagrams of an embodiment of the guided flying object according to this invention, FIG. 3 is an internal configuration diagram of the aircraft, and FIGS. 4 and 5 are sectional views of the locking device.
FIG. 6 is a diagram showing an example of a conventional guided flying object. In the figure, 7 is a locking device, 10 is a spiral spring, 11 is a shaft, 12 and 13 are gears, 14 is a cylinder, 15 is a piston, 16 is a hole, 17 is a shaft, 1
8 is the spark plug, 19 is the delay medicine, 20 is the output medicine,
21 is an O-ring, and 22 is a 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操舵翼と、機体の後半部所定
位置に固定された安定翼と、前記展開操舵翼を展
開するための展開機構と、前記展開操舵翼を収納
しておくために機体に設けられ、かつ延時薬と前
記延時薬により点火される出力薬と前記出力薬に
より作動するガスシリンダとによつて構成したロ
ツク装置と、機体内に装着され、かつ前記展開操
舵翼を展開するためのねじりトルクエネルギを蓄
えるためのうず巻きばねとから成り、飛しよう体
の発射前は前記の展開操舵翼を機体内に収納して
おき、発射後、前記ガスシリンダを前記出力薬の
ガスの圧力で作動させ所定の遅れ時間後に前記の
展開操舵翼をうず巻きばねに蓄えられたねじりト
ルク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 flying body, a deployable steering wing stored in a predetermined position in the front half of the fuselage, a stabilizing wing fixed in a predetermined position in the rear half of the fuselage, and a deployment mechanism for deploying the deployable steering wing; A lock device is provided in the fuselage for storing the deployable steering blade, and is constituted by a time delay medicine, a power medicine ignited by the time delay medicine, and a gas cylinder operated by the power medicine; and a spiral spring for storing torsional torque energy for deploying the deployable steering wing. , wherein the gas cylinder is actuated by the pressure of the gas of the output medicine, and after a predetermined delay time, the deployable steering blade is deployed by torsional torque stored in a spiral spring. body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP670288U JPH01111999U (en) | 1988-01-22 | 1988-01-22 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP670288U JPH01111999U (en) | 1988-01-22 | 1988-01-22 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH01111999U true JPH01111999U (en) | 1989-07-27 |
Family
ID=31211089
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP670288U Pending JPH01111999U (en) | 1988-01-22 | 1988-01-22 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH01111999U (en) |
-
1988
- 1988-01-22 JP JP670288U patent/JPH01111999U/ja active Pending
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