JPH01106797U - - Google Patents
Info
- Publication number
- JPH01106797U JPH01106797U JP19896287U JP19896287U JPH01106797U JP H01106797 U JPH01106797 U JP H01106797U JP 19896287 U JP19896287 U JP 19896287U JP 19896287 U JP19896287 U JP 19896287U JP H01106797 U JPH01106797 U JP H01106797U
- 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実施例を示す
図である。
図において、７はロツク装置、８は引張バネ、
１０はアーム、１１は軸、１２，１３は歯車、１
４はシリンダ、１５はピストン、１６は穴、１７
は軸、１８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 embodiment of a conventional guided flying object. In the figure, 7 is a locking device, 8 is a tension spring,
10 is an arm, 11 is a shaft, 12 and 13 are gears, 1
4 is a cylinder, 15 is a piston, 16 is a hole, 17
18 is a shaft, 18 is a spark plug, 19 is a time delay medicine, 20 is an 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
舵翼とを展開するための弾性エネルギを蓄えるた
めの引張バネとから成り、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
を引張バネに蓄えられた弾性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 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 tension spring for storing elastic 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 elastic energy stored in a tension spring. body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19896287U JPH01106797U (en) | 1987-12-29 | 1987-12-29 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19896287U JPH01106797U (en) | 1987-12-29 | 1987-12-29 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH01106797U true JPH01106797U (en) | 1989-07-18 |
Family
ID=31489439
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP19896287U Pending JPH01106797U (en) | 1987-12-29 | 1987-12-29 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH01106797U (en) |
-
1987
- 1987-12-29 JP JP19896287U patent/JPH01106797U/ja active Pending