JPH03128296U - - Google Patents
Info
- Publication number
- JPH03128296U JPH03128296U JP1990037186U JP3718690U JPH03128296U JP H03128296 U JPH03128296 U JP H03128296U JP 1990037186 U JP1990037186 U JP 1990037186U JP 3718690 U JP3718690 U JP 3718690U JP H03128296 U JPH03128296 U JP H03128296U
- Authority
- JP
- Japan
- Prior art keywords
- lid
- flying object
- fuselage
- hole
- 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
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/38—Range-increasing arrangements
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Description
第１図は、この考案による飛しよう体の一実施
例の発射前の縦断面図、第２図はこの考案による
飛しよう体の発射後の縦断面図、第３図、第４図
はこの考案の飛しよう体を示す横断面図、第５図
、第６図は、従来の展開翼付飛しよう体のそれぞ
れ、発射前、発射後の縦断面図である。
図において１……ランチヤー、２……飛しよう
体、３……展開翼、４……蓋、５……コイルバネ
、６……ローラーである。なお、図中同一または
相当部分には同一符号を付して示してある。
Fig. 1 is a vertical sectional view of an embodiment of the flying object according to this invention before launch, Fig. 2 is a longitudinal sectional view of the flying object according to this invention after launching, and Figs. 5 and 6, which are cross-sectional views showing the proposed flying object, are longitudinal sectional views of a conventional flying object with deployable wings before and after launch, respectively. In the figure, 1... launcher, 2... flying body, 3... deployable wings, 4... lid, 5... coil spring, 6... roller. It should be noted that the same or equivalent parts in the drawings are designated by the same reference numerals.
Claims (1)
た展開翼を飛しよう体発射後に展開させる機構を
有する飛しよう体において、上記展開翼の展開後
に形成される機体側面の翼出口の穴を、塞ぐため
の蓋と、一端が機体側面に設けられかつ他端が上
記蓋に設けられ、上記展開翼の展開に伴ない上記
蓋を上記穴方向に可動させるコイルばねとを具備
した飛しよう体。 In a flying object having a mechanism for deploying a deployable wing stored in a hole formed in a hole formed in the fuselage body of the flying object after the flying object is launched, a wing exit hole on the side of the fuselage formed after the deployable wing is deployed. , a flying body comprising a lid for closing, and a coil spring having one end provided on a side surface of the fuselage and the other end provided on the lid, for moving the lid in the direction of the hole as the deployable wings are deployed. .
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1990037186U JPH03128296U (en) | 1990-04-06 | 1990-04-06 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1990037186U JPH03128296U (en) | 1990-04-06 | 1990-04-06 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH03128296U true JPH03128296U (en) | 1991-12-24 |
Family
ID=31544072
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1990037186U Pending JPH03128296U (en) | 1990-04-06 | 1990-04-06 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH03128296U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3010798A4 (en) * | 2013-06-16 | 2017-03-08 | Rafael Advanced Defense Systems Ltd. | Shutter mechanism for covering a wing deployment opening |
-
1990
- 1990-04-06 JP JP1990037186U patent/JPH03128296U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3010798A4 (en) * | 2013-06-16 | 2017-03-08 | Rafael Advanced Defense Systems Ltd. | Shutter mechanism for covering a wing deployment opening |
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