JPS63189898U - - Google Patents

Info

Publication number
JPS63189898U
JPS63189898U JP8080287U JP8080287U JPS63189898U JP S63189898 U JPS63189898 U JP S63189898U JP 8080287 U JP8080287 U JP 8080287U JP 8080287 U JP8080287 U JP 8080287U JP S63189898 U JPS63189898 U JP S63189898U
Authority
JP
Japan
Prior art keywords
control surface
aircraft
bulge
sectional
adjust
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.)
Granted
Application number
JP8080287U
Other languages
Japanese (ja)
Other versions
JPH0521518Y2 (en
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 JP8080287U priority Critical patent/JPH0521518Y2/ja
Publication of JPS63189898U publication Critical patent/JPS63189898U/ja
Application granted granted Critical
Publication of JPH0521518Y2 publication Critical patent/JPH0521518Y2/ja
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Description

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

第1図は本考案の一実施例の断面図、第2図は
本考案の他の実施例の断面図、第3図は従来の舵
翼の断面図、第4図は従来の舵翼の特性に関する
説明図を示す。 1……舵翼、2……舵面、3……固定翼、4…
…配管、5……吸入バルブ、6……排気バルブ、
7……電動モータ、8……ロツド、9……リンク
機構、10……アーム。
Fig. 1 is a sectional view of one embodiment of the present invention, Fig. 2 is a sectional view of another embodiment of the invention, Fig. 3 is a sectional view of a conventional rudder blade, and Fig. 4 is a sectional view of a conventional rudder blade. An explanatory diagram regarding characteristics is shown. 1... Rudder blade, 2... Control surface, 3... Fixed wing, 4...
...Piping, 5...Intake valve, 6...Exhaust valve,
7...Electric motor, 8...Rod, 9...Link mechanism, 10...Arm.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 舵面の形状を変化させるための駆動装置を備え
、航空機の速度に応じて舵面のふくらみ度合を調
整できる航空機用舵面装置。
An aircraft control surface device that is equipped with a drive device to change the shape of the control surface and can adjust the degree of bulge of the control surface according to the speed of the aircraft.
JP8080287U 1987-05-29 1987-05-29 Expired - Lifetime JPH0521518Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8080287U JPH0521518Y2 (en) 1987-05-29 1987-05-29

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8080287U JPH0521518Y2 (en) 1987-05-29 1987-05-29

Publications (2)

Publication Number Publication Date
JPS63189898U true JPS63189898U (en) 1988-12-06
JPH0521518Y2 JPH0521518Y2 (en) 1993-06-02

Family

ID=30931944

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8080287U Expired - Lifetime JPH0521518Y2 (en) 1987-05-29 1987-05-29

Country Status (1)

Country Link
JP (1) JPH0521518Y2 (en)

Also Published As

Publication number Publication date
JPH0521518Y2 (en) 1993-06-02

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