JPH01147198U - - Google Patents

Info

Publication number
JPH01147198U
JPH01147198U JP3544488U JP3544488U JPH01147198U JP H01147198 U JPH01147198 U JP H01147198U JP 3544488 U JP3544488 U JP 3544488U JP 3544488 U JP3544488 U JP 3544488U JP H01147198 U JPH01147198 U JP H01147198U
Authority
JP
Japan
Prior art keywords
control system
actuator
control
pilot
serves
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
JP3544488U
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 JP3544488U priority Critical patent/JPH01147198U/ja
Publication of JPH01147198U publication Critical patent/JPH01147198U/ja
Pending legal-status Critical Current

Links

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に係わる航空機の操
縦操作装置を示す構成図、第2図A及びBはそれ
ぞれ本考案の他の実施例を示す図、第3図は航空
機の従来の操縦操作系統を示す構成図である。 1……操縦桿(又はペダル)、2……操縦リン
ク、3……舵面アクチユエータ、4……舵面、5
……操縦コンピユータ、11……信号アクチユエ
ータ、12,12a,12b,13……モータ、
14……減速歯車。
FIG. 1 is a configuration diagram showing an aircraft control device according to an embodiment of the present invention, FIGS. 2A and B are diagrams each showing other embodiments of the present invention, and FIG. 3 is a diagram showing a conventional aircraft control system. FIG. 3 is a configuration diagram showing an operation system. 1... Control stick (or pedal), 2... Control link, 3... Control surface actuator, 4... Control surface, 5
...Control computer, 11...Signal actuator, 12, 12a, 12b, 13...Motor,
14...Reduction gear.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] パイロツトによる直接操縦手段から操舵手段に
対しその操作力を伝達する操縦系と、この操縦系
に連結され自動操縦コンピユータからの操縦信号
に応じて該操縦系を駆動操作するアクチユエータ
と、このアクチユエータの出力軸を駆動する動力
源となる低回転大トルク型のモータとを具備し、
上記アクチユエータの操縦系に対する減速比を小
さくしたことを特徴とする航空機の操縦操作装置
A control system that transmits the operating force from the direct control means of the pilot to the steering means, an actuator connected to this control system that drives and operates the control system in response to a control signal from an autopilot computer, and an output of this actuator. Equipped with a low-rotation, high-torque motor that serves as the power source for driving the shaft.
An aircraft control device characterized in that the actuator has a small reduction ratio with respect to a control system.
JP3544488U 1988-03-17 1988-03-17 Pending JPH01147198U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3544488U JPH01147198U (en) 1988-03-17 1988-03-17

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3544488U JPH01147198U (en) 1988-03-17 1988-03-17

Publications (1)

Publication Number Publication Date
JPH01147198U true JPH01147198U (en) 1989-10-11

Family

ID=31262091

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3544488U Pending JPH01147198U (en) 1988-03-17 1988-03-17

Country Status (1)

Country Link
JP (1) JPH01147198U (en)

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