JPS618800U - spoiler device - Google Patents
spoiler deviceInfo
- Publication number
- JPS618800U JPS618800U JP9340984U JP9340984U JPS618800U JP S618800 U JPS618800 U JP S618800U JP 9340984 U JP9340984 U JP 9340984U JP 9340984 U JP9340984 U JP 9340984U JP S618800 U JPS618800 U JP S618800U
- Authority
- JP
- Japan
- Prior art keywords
- spoiler
- flying object
- guided flying
- spoiler device
- guided
- 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
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第１図は誘導飛しよう体のロールモーメントを誘起する
一例を示す図、第２図は後翼に設けられたスポイラー装
置の一例を示す図、第３図、第４図はスポイラーによる
ロールモーメント減少の様子を示す図、第５図は従来の
一般的なスポイラー装置を示す図、第６図、第７図は本
考案の一実施例を示す図であり、図中、１は機体、２は
前翼、３は後翼、４はレートジャイロ、５は気流、１０
はスポイラー、１１はロツド、１２はプレート、１３は
ソレノイド、２１はロツド、２２はベアリング、２３は
油圧発生装置、２４は切換え弁、２５は複動シリンダ、
２６は油圧配管、２７はピン、２８は溝である。
なお図中同一あるいは相当部分には同一符号を付して示
してある。Figure 1 shows an example of inducing roll moment of a guided flying object, Figure 2 shows an example of a spoiler device installed on the rear wing, and Figures 3 and 4 show how the spoiler reduces roll moment. FIG. 5 is a diagram showing a conventional general spoiler device, and FIGS. 6 and 7 are diagrams showing an embodiment of the present invention. Front wing, 3 is rear wing, 4 is rate gyro, 5 is airflow, 10
is a spoiler, 11 is a rod, 12 is a plate, 13 is a solenoid, 21 is a rod, 22 is a bearing, 23 is a hydraulic pressure generator, 24 is a switching valve, 25 is a double-acting cylinder,
26 is a hydraulic pipe, 27 is a pin, and 28 is a groove. Note that the same or corresponding parts in the figures are indicated by the same reference numerals.
Claims (1)
装置において、上記誘導飛しよう体の機軸まわりに回転
するロールモーメントを減少させるためにスポイラーを
設けるとともに、所要の口−ルレートに応じて上記スポ
イラーを移動させる駆動源を上記誘導飛しよう体の機体
内に有し、上記スポイラーを左右もしくは上下を一対と
し、同時に制御七きるようにしたことを特徴とす颯スポ
イラー装置。In a spoiler device for a guided flying object having wings that perform roll motion, a spoiler is provided to reduce the roll moment of the guided flying object rotating around the axis of the guided flying object, and the spoiler is moved according to a required roll rate. A spoiler device characterized in that a driving source for controlling the guided flying object is provided in the body of the guided flying object, and the spoiler is arranged as a pair on the left and right or on the top and bottom, and can be controlled at the same time.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9340984U JPS618800U (en) | 1984-06-22 | 1984-06-22 | spoiler device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9340984U JPS618800U (en) | 1984-06-22 | 1984-06-22 | spoiler device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS618800U true JPS618800U (en) | 1986-01-20 |
Family
ID=30651063
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9340984U Pending JPS618800U (en) | 1984-06-22 | 1984-06-22 | spoiler device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS618800U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH06129799A (en) * | 1992-10-14 | 1994-05-13 | Tech Res & Dev Inst Of Japan Def Agency | Aircraft control device |
-
1984
- 1984-06-22 JP JP9340984U patent/JPS618800U/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH06129799A (en) * | 1992-10-14 | 1994-05-13 | Tech Res & Dev Inst Of Japan Def Agency | Aircraft control device |
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