JPS63119200U - - Google Patents

Info

Publication number
JPS63119200U
JPS63119200U JP991687U JP991687U JPS63119200U JP S63119200 U JPS63119200 U JP S63119200U JP 991687 U JP991687 U JP 991687U JP 991687 U JP991687 U JP 991687U JP S63119200 U JPS63119200 U JP S63119200U
Authority
JP
Japan
Prior art keywords
divided
drive source
snake
aircraft
operated
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
JP991687U
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 JP991687U priority Critical patent/JPS63119200U/ja
Publication of JPS63119200U publication Critical patent/JPS63119200U/ja
Pending legal-status Critical Current

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  • Transmission Devices (AREA)

Description

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

第1図は本考案の一実施例の平面図、第2図は
上記実施例の作動時の状態の一例を示す説明図、
第3図は従来の前縁フラツプの平面図である。 図面中、1は前縁フラツプ、2は主翼、3はギ
ヤード・ロータリー・アクチユエータ、4はパワ
ー・ドライブ・ユニツト、5はトルク・チユーブ
、6は変速ギア・ボツクス、をそれぞれ示す。
Fig. 1 is a plan view of an embodiment of the present invention, Fig. 2 is an explanatory diagram showing an example of the state of the above embodiment during operation,
FIG. 3 is a plan view of a conventional leading edge flap. In the drawings, 1 is a leading edge flap, 2 is a main wing, 3 is a geared rotary actuator, 4 is a power drive unit, 5 is a torque tube, and 6 is a transmission gear box.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 複数に分割された蛇面、上記分割された蛇面に
共通する駆動源、同駆動源によつて作動され分割
された舵面の作動角を各々異るように動かす作動
機構から成ることを特徴とする航空機における舵
の作動装置。
It is characterized by comprising a snake surface divided into a plurality of parts, a drive source common to the divided snake surfaces, and an operating mechanism that is operated by the same drive source and moves the operating angles of the divided control surfaces differently. A rudder actuation device for an aircraft.
JP991687U 1987-01-28 1987-01-28 Pending JPS63119200U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP991687U JPS63119200U (en) 1987-01-28 1987-01-28

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP991687U JPS63119200U (en) 1987-01-28 1987-01-28

Publications (1)

Publication Number Publication Date
JPS63119200U true JPS63119200U (en) 1988-08-02

Family

ID=30795685

Family Applications (1)

Application Number Title Priority Date Filing Date
JP991687U Pending JPS63119200U (en) 1987-01-28 1987-01-28

Country Status (1)

Country Link
JP (1) JPS63119200U (en)

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