JPS6454698U - - Google Patents
Info
- Publication number
- JPS6454698U JPS6454698U JP14555687U JP14555687U JPS6454698U JP S6454698 U JPS6454698 U JP S6454698U JP 14555687 U JP14555687 U JP 14555687U JP 14555687 U JP14555687 U JP 14555687U JP S6454698 U JPS6454698 U JP S6454698U
- Authority
- JP
- Japan
- Prior art keywords
- medicine
- fuselage
- deployable
- wing
- deploying
- 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 description 5
- 239000003381 stabilizer Substances 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、２は操舵翼、３は展開安定翼、７
はロツク装置、８は引つ張り、１０はアーム、１
１は軸、１２と１３は歯車、１４はシリンダ、１
５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。なお、図中同一
符号は同一、又は相当部分を示す。
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, 2 is a steering wing, 3 is a deployment stabilizing wing, and 7 is a steering wing.
is the locking device, 8 is the tension, 10 is the arm, 1
1 is the shaft, 12 and 13 are gears, 14 is the cylinder, 1
5 is a piston, 16 is a hole, 17 is a shaft, 18 is a spark plug, 19 is a time delay medicine, 20 is an output medicine, 21 is O
The ring 22 is a combustion gas. Note that the same reference numerals in the figures indicate the same or equivalent parts.
Claims (1)
置に収納された展開安定翼と、機体の後半部所定
位置に取り付けられた操舵翼と、前記展開安定翼
を展開するための展開機構と、前記展開安定翼を
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
開安定翼を展開するための弾性エネルギを蓄える
ための引張バネーとから成り、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展開安定翼
を引張バネー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 fuselage of a flying body, a deployable stabilizing wing stored in a predetermined position in the front half of the fuselage, a steering wing attached to a predetermined position in the rear half of the fuselage, and a deployment mechanism for deploying the deployable stabilizer wing, A lock device is provided in the fuselage for storing the deployable stabilizing wing, 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 stabilizing wings. A guided flying object characterized in that a gas cylinder is actuated by the pressure of the gas of the output medicine, and after a predetermined delay time, the deployable stabilizing wings are deployed by elastic energy stored in a tension spring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14555687U JPS6454698U (en) | 1987-09-24 | 1987-09-24 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14555687U JPS6454698U (en) | 1987-09-24 | 1987-09-24 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6454698U true JPS6454698U (en) | 1989-04-04 |
Family
ID=31414249
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP14555687U Pending JPS6454698U (en) | 1987-09-24 | 1987-09-24 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6454698U (en) |
-
1987
- 1987-09-24 JP JP14555687U patent/JPS6454698U/ja active Pending