JPH03112691U - - Google Patents
Info
- Publication number
- JPH03112691U JPH03112691U JP1632290U JP1632290U JPH03112691U JP H03112691 U JPH03112691 U JP H03112691U JP 1632290 U JP1632290 U JP 1632290U JP 1632290 U JP1632290 U JP 1632290U JP H03112691 U JPH03112691 U JP H03112691U
- Authority
- JP
- Japan
- Prior art keywords
- stabilizing
- wing
- section
- attached
- blade
- 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
- 230000000087 stabilizing effect Effects 0.000 claims description 15
- 238000000926 separation method Methods 0.000 claims description 2
- 230000008878 coupling Effects 0.000 claims 2
- 238000010168 coupling process Methods 0.000 claims 2
- 238000005859 coupling reaction Methods 0.000 claims 2
- 230000006641 stabilisation Effects 0.000 claims 1
- 238000011105 stabilization Methods 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 3
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Description
第１図は、この考案の一実施例を示す図であり
、第２図はこの考案の一実施例の動作図、第３図
は従来の誘導飛しよう体の構成図である。図にお
いて１……誘導制御部、２……弾頭部、３……推
進部、４……操舵翼、５……安定翼部、６……シ
リンダ状安定翼、７……ピストン状安定翼、８…
…誘導飛しよう体、９……信号ケーブル、１０…
…制御装置、１１……電源装置、１２……分離機
構、１３……板ばね、１４……安定翼を示す。な
お、各図中同一符号は同一又は相当部分を示す。
FIG. 1 is a diagram showing an embodiment of this invention, FIG. 2 is an operational diagram of an embodiment of this invention, and FIG. 3 is a diagram showing the configuration of a conventional guided flying object. In the figure, 1... Guidance control unit, 2... Warhead, 3... Propulsion unit, 4... Steering wing, 5... Stabilizing wing section, 6... Cylindrical stabilizing wing, 7... Piston-shaped stabilizing wing, 8...
...Guided flying object, 9...Signal cable, 10...
...control device, 11...power supply device, 12...separation mechanism, 13...leaf spring, 14...stabilizing blade. Note that the same reference numerals in each figure indicate the same or corresponding parts.
Claims (1)
れた安定翼部と、前記安定翼部の後方に取付けら
れた推進部と、前記推進部に取付けられた操舵翼
とを備えている後翼操舵の誘導飛しよう体におい
て、前記安定翼部に取付けられ、内部が空洞のシ
リンダ状安定翼と、前記シリンダ状安定翼の内部
に前記シリンダ状安定翼の外部方向へ伸展可能に
取付けられたピストン状安定翼と、前記ピストン
状安定翼を前記シリンダ状安定翼の外に押し出す
ための板ばねと、前記ピストン状安定翼が前記シ
リンダ状安定翼内に位置するように前記ピストン
状安定翼とシリンダ状安定翼との間を結合し、そ
の結合をロツクオン信号により制御装置から発生
する制御信号により解放し、前記ピストン状安定
翼を板ばねの作用により進展させるための分離機
構とを具備したことを特徴とする誘導飛しよう体
。 A rear wing steering system comprising a guidance control section, a stabilizing wing section attached to the rear of the guidance control section, a propulsion section attached to the rear of the stabilization wing section, and a steering wing attached to the propulsion section. In the guided flying object, a cylindrical stabilizing wing is attached to the stabilizing wing section and has a hollow interior; a stabilizing blade; a leaf spring for pushing the piston-shaped stabilizing blade out of the cylindrical stabilizing blade; and a plate spring for pushing the piston-shaped stabilizing blade out of the cylindrical stabilizing blade; It is characterized by comprising a separation mechanism for coupling the stabilizing wing with the stabilizing wing, releasing the coupling by a control signal generated from a control device in response to a lock-on signal, and advancing the piston-shaped stabilizing wing by the action of a leaf spring. A guided flying body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1632290U JPH03112691U (en) | 1990-02-21 | 1990-02-21 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1632290U JPH03112691U (en) | 1990-02-21 | 1990-02-21 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH03112691U true JPH03112691U (en) | 1991-11-18 |
Family
ID=31519591
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1632290U Pending JPH03112691U (en) | 1990-02-21 | 1990-02-21 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH03112691U (en) |
-
1990
- 1990-02-21 JP JP1632290U patent/JPH03112691U/ja active Pending
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JPH03112691U (en) | ||
| IT1145447B (en) | CONTROL SYSTEM FOR THE AXLE WITH REAR STEERING BARREL OF LOAD VEHICLES | |
| JPS6281142U (en) | ||
| JPH03112692U (en) | ||
| JPH03112693U (en) | ||
| JPS6323599U (en) | ||
| JPH0314598U (en) | ||
| JPS6169700U (en) | ||
| JPS6438500U (en) | ||
| JPS6169699U (en) | ||
| JPH0346796U (en) | ||
| JPH0237316U (en) | ||
| JPS6446699U (en) | ||
| JPH01179766U (en) | ||
| JPH0254099U (en) | ||
| JPH0232498U (en) | ||
| JPH01178498U (en) | ||
| JPH0225397U (en) | ||
| JPH0285296U (en) | ||
| JPS6049898U (en) | radio controlled glider | |
| JPS63115899U (en) | ||
| JPS61191253U (en) | ||
| JPS63111197U (en) | ||
| JPS6163109U (en) | ||
| JPS6361699U (en) |