JPS63108898U - - Google Patents
Info
- Publication number
- JPS63108898U JPS63108898U JP26187U JP26187U JPS63108898U JP S63108898 U JPS63108898 U JP S63108898U JP 26187 U JP26187 U JP 26187U JP 26187 U JP26187 U JP 26187U JP S63108898 U JPS63108898 U JP S63108898U
- Authority
- JP
- Japan
- Prior art keywords
- flap
- output
- speed detector
- aircraft
- computer
- 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
- 238000010586 diagram Methods 0.000 description 4
- 230000000630 rising effect Effects 0.000 description 1
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Description
第１図は本考案におけるフラツプ角度と速度の
関係を示す説明図、第２図は本考案の一実施例の
説明図、第３図はフラツプとフラツプ角度を示す
説明図、第４図はフラツプ角度による滑走距離、
上昇の状態を示す説明図である。
図面中、１は速度検出器、２はコンピユータ、
３はフラツプ操作装置、４は主翼、５はフラツプ
、をそれぞれ示す。
Fig. 1 is an explanatory diagram showing the relationship between the flap angle and speed in the present invention, Fig. 2 is an explanatory diagram of an embodiment of the invention, Fig. 3 is an explanatory diagram showing the flap and flap angle, and Fig. 4 is an explanatory diagram showing the flap angle and the flap angle. Skiing distance by angle,
It is an explanatory view showing a rising state. In the drawing, 1 is a speed detector, 2 is a computer,
Reference numeral 3 indicates a flap operating device, 4 indicates a main wing, and 5 indicates a flap.
Claims (1)
けフラツプ操作指令を出力するコンピユータ、上
記コンピユータの出力によつて制御されるフラツ
プ操作装置よりなることを特徴とする航空機のフ
ラツプ角度可変装置。 1. A flap angle variable device for an aircraft, comprising: an aircraft speed detector; a computer receiving the output of the speed detector and outputting a flap operation command; and a flap operating device controlled by the output of the computer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP26187U JPS63108898U (en) | 1987-01-07 | 1987-01-07 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP26187U JPS63108898U (en) | 1987-01-07 | 1987-01-07 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS63108898U true JPS63108898U (en) | 1988-07-13 |
Family
ID=30777070
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP26187U Pending JPS63108898U (en) | 1987-01-07 | 1987-01-07 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS63108898U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009538779A (en) * | 2006-05-29 | 2009-11-12 | エアバス フランス | Aircraft maneuvering method and apparatus for optimizing auxiliary wing control in high lift configurations |
| JP2009539693A (en) * | 2006-06-13 | 2009-11-19 | エアバス フランス | How to control the aircraft during the approach phase |
-
1987
- 1987-01-07 JP JP26187U patent/JPS63108898U/ja active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009538779A (en) * | 2006-05-29 | 2009-11-12 | エアバス フランス | Aircraft maneuvering method and apparatus for optimizing auxiliary wing control in high lift configurations |
| JP2009539693A (en) * | 2006-06-13 | 2009-11-19 | エアバス フランス | How to control the aircraft during the approach phase |