JPH02100099U - - Google Patents
Info
- Publication number
- JPH02100099U JPH02100099U JP866489U JP866489U JPH02100099U JP H02100099 U JPH02100099 U JP H02100099U JP 866489 U JP866489 U JP 866489U JP 866489 U JP866489 U JP 866489U JP H02100099 U JPH02100099 U JP H02100099U
- Authority
- JP
- Japan
- Prior art keywords
- fuselage
- canard
- deployable
- predetermined position
- deployment
- 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
- 241000272517 Anseriformes Species 0.000 claims description 4
- 238000010586 diagram Methods 0.000 description 4
Landscapes
- Toys (AREA)
Description
第１図〜第３図はこの考案の一実施例を示す図
、第４図はマツハ数に対するフラツタ速度の関係
を示す図、第５図〜第７図は他の実施例を示す図
、第８図は従来の飛しよう体の地上ランチヤ搭載
時を示す図である。
図において、１は地上ランチヤ、２は機体、３
は展開カナード、４は展開操舵翼、５は慣性装置
、６はロツク装置、７は展開中心軸、８は歯車、
９は歯車、１０は軸、１１はうず巻きバネ、１２
はトーシヨンバー、１３はカサ歯車、１４はカサ
歯車、１５は引張バネ、１６はアーム、１７はカ
ナード、１８は操舵翼、イはある翼構造に対する
フラツタ速度、ロはある高度における速度一定の
直線、ハはフラツタマージン、ニはＴｒａｎｓｏ
ｎｉｃ Ｄｉｐである。なお図中同一符号は同一
または相等部分を示す。
Figures 1 to 3 are diagrams showing one embodiment of this invention, Figure 4 is a diagram showing the relationship between the flutter speed and the Matsuha number, and Figures 5 to 7 are diagrams showing other embodiments. FIG. 8 is a diagram showing a conventional flying vehicle mounted on a ground launcher. In the figure, 1 is the ground launcher, 2 is the aircraft, and 3
is a deployment canard, 4 is a deployment steering blade, 5 is an inertial device, 6 is a locking device, 7 is a deployment center axis, 8 is a gear,
9 is a gear, 10 is a shaft, 11 is a spiral spring, 12
is a torsion bar, 13 is a bevel gear, 14 is a bevel gear, 15 is a tension spring, 16 is an arm, 17 is a canard, 18 is a steering blade, A is a flutter speed for a certain wing structure, B is a straight line with constant speed at a certain altitude, H is Flat Margin, D is Transo
It's nic dip. 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カナードと、機体の後半部所
定位置に収納された展開操舵翼と、機体の飛しよ
う速度を検知するための慣性装置と、ロツク装置
及び展開動力源から構成され、前記慣性装置から
の出力信号を受けて前記カナード及び前記操舵翼
を展開するための展開機構とを備えたことを特徴
とする誘導飛しよう体。 A flying body, a deployable canard stored in a predetermined position in the front half of the fuselage, a deployable steering wing stored in a predetermined position in the rear half of the fuselage, and an inertial device for detecting the flight speed of the fuselage. , a locking device and a deployment power source, and a deployment mechanism for deploying the canard and the steering wing in response to an output signal from the inertial device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP866489U JPH02100099U (en) | 1989-01-27 | 1989-01-27 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP866489U JPH02100099U (en) | 1989-01-27 | 1989-01-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH02100099U true JPH02100099U (en) | 1990-08-09 |
Family
ID=31214743
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP866489U Pending JPH02100099U (en) | 1989-01-27 | 1989-01-27 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH02100099U (en) |
-
1989
- 1989-01-27 JP JP866489U patent/JPH02100099U/ja active Pending
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4246721A (en) | Aerial toy | |
| US10967967B2 (en) | Systems and methods for winged drone platform | |
| JP2755492B2 (en) | Missile with deployable steering wings | |
| US4588146A (en) | Biaxial folding lever wing | |
| US3997136A (en) | Toy-kite airplane | |
| CA2013180A1 (en) | Winged kite | |
| US4377052A (en) | Folded paper airplane | |
| JPH02100099U (en) | ||
| Burk Jr et al. | Radio-controlled model design and testing techniques for stall/spin evaluation of general-aviation aircraft | |
| JP3076798B1 (en) | Guided flying object | |
| JPS62166500U (en) | ||
| JPH0228998U (en) | ||
| JPS62799A (en) | Guided missile | |
| RU93003032A (en) | CORRECTABLE AIRCRAFT, STABILIZED BY A ROLL WITH A LASER SELF-EVENT HEAD | |
| JPS628599U (en) | ||
| Turner | A roll-balance free-flight test vehicle for the measurement of aileron rolling power and roll damping at M= 0.8 to 2.5 | |
| JPS59148999U (en) | Guided flying vehicle control device | |
| JPS62206398A (en) | Guided missile | |
| WOLOWICZ | Free wing assembly for an aircraft[Patent] | |
| JPH01157998U (en) | ||
| Lee et al. | Spin-Tunnel Investigation of a 1/28-Scale Model of a Subsonic Attack Airplane | |
| JPS6239200U (en) | ||
| JPH0442000U (en) | ||
| FINK et al. | Airframe noise component interaction studies[Final Report] | |
| JPH05694A (en) | Rotor blade of helicopter |