JPH03120295U - - Google Patents

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Publication number
JPH03120295U
JPH03120295U JP2822490U JP2822490U JPH03120295U JP H03120295 U JPH03120295 U JP H03120295U JP 2822490 U JP2822490 U JP 2822490U JP 2822490 U JP2822490 U JP 2822490U JP H03120295 U JPH03120295 U JP H03120295U
Authority
JP
Japan
Prior art keywords
right main
main wings
circulation
utility
lower surfaces
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
Application number
JP2822490U
Other languages
Japanese (ja)
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed filed Critical
Priority to JP2822490U priority Critical patent/JPH03120295U/ja
Publication of JPH03120295U publication Critical patent/JPH03120295U/ja
Pending legal-status Critical Current

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Description

【図面の簡単な説明】[Brief explanation of drawings]

第1図a,bは本考案の一実施例の全体図、第
2図a〜fは同実施例の要部の説明図、第3図は
エルロンをもつた従来のロール制御技術の説明図
、第4図は、スポイラをもつた従来のロール制御
技術の説明図、第5図a〜dはエルロンによるロ
ール制御技術の問題点の説明図である。 1…気流吹き出し溝、2…流量調節装置、3…
エルロン、4…スポイラ、5…フラツプ、7…カ
バー、8…高圧空気導入路、10…航空機、11
…主翼、12…操縦桿。
Figures 1 a and b are general views of an embodiment of the present invention, Figures 2 a to f are explanatory diagrams of essential parts of the same embodiment, and Figure 3 is an explanatory diagram of a conventional roll control technology with ailerons. , FIG. 4 is an explanatory diagram of a conventional roll control technique using a spoiler, and FIGS. 5 a to 5 d are explanatory diagrams of problems in the roll control technique using ailerons. 1... Air flow outlet groove, 2... Flow rate adjustment device, 3...
Aileron, 4... Spoiler, 5... Flap, 7... Cover, 8... High pressure air introduction path, 10... Aircraft, 11
...Main wing, 12...Control stick.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 左右の主翼の各々の上面及び下面の翼面に沿つ
て気流を吹き出す吹き出し口を設け、左右主翼ま
わりの空気の循環を制御するようにしたことを特
徴とする航空機の機体制御装置。
An aircraft body control device characterized in that an air outlet is provided along the upper and lower surfaces of each of the left and right main wings to control the circulation of air around the left and right main wings.
JP2822490U 1990-03-22 1990-03-22 Pending JPH03120295U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2822490U JPH03120295U (en) 1990-03-22 1990-03-22

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2822490U JPH03120295U (en) 1990-03-22 1990-03-22

Publications (1)

Publication Number Publication Date
JPH03120295U true JPH03120295U (en) 1991-12-10

Family

ID=31531037

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2822490U Pending JPH03120295U (en) 1990-03-22 1990-03-22

Country Status (1)

Country Link
JP (1) JPH03120295U (en)

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