JPS63145799U - - Google Patents

Info

Publication number
JPS63145799U
JPS63145799U JP3840087U JP3840087U JPS63145799U JP S63145799 U JPS63145799 U JP S63145799U JP 3840087 U JP3840087 U JP 3840087U JP 3840087 U JP3840087 U JP 3840087U JP S63145799 U JPS63145799 U JP S63145799U
Authority
JP
Japan
Prior art keywords
circuit
gust
drive motor
control surface
dummy load
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
JP3840087U
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 JP3840087U priority Critical patent/JPS63145799U/ja
Publication of JPS63145799U publication Critical patent/JPS63145799U/ja
Pending legal-status Critical Current

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  • Control Of Electric Motors In General (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概要図である。 図面中、1は駆動モータ、2は減速歯車装置、
3は制御装置、4はダミー負荷抵抗、5は切換装
置、6は航空機地上安全スイツチ、7はガストダ
ンパースイツチ、8は機体電源、9は脚、10は
舵面をそれぞれ示す。
FIG. 1 is a schematic diagram of an embodiment of the present invention. In the drawing, 1 is a drive motor, 2 is a reduction gear device,
3 is a control device, 4 is a dummy load resistor, 5 is a switching device, 6 is an aircraft ground safety switch, 7 is a gust damper switch, 8 is an aircraft power source, 9 is a landing gear, and 10 is a control surface.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 機内電源によつて作動され舵面を操作する駆動
モータと減速歯車装置を有し可逆特性を有する電
気制御式アクチユエータ、上記駆動モータの作動
回路に並列に接続された回路中に設けられたダミ
ー負荷抵抗、及び上記ダミー負荷抵抗の回路に設
けられガストダンパースイツチによつて制御され
る切換装置からなることを特徴とする航空機舵面
の突風破損防止装置。
An electrically controlled actuator that has a reversible characteristic and includes a drive motor that is operated by an on-board power source to operate a control surface and a reduction gear device, and a dummy load that is installed in a circuit that is connected in parallel to the operating circuit of the drive motor. A gust damage prevention device for an aircraft control surface, comprising a resistor and a switching device provided in the circuit of the dummy load resistor and controlled by a gust damper switch.
JP3840087U 1987-03-18 1987-03-18 Pending JPS63145799U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3840087U JPS63145799U (en) 1987-03-18 1987-03-18

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3840087U JPS63145799U (en) 1987-03-18 1987-03-18

Publications (1)

Publication Number Publication Date
JPS63145799U true JPS63145799U (en) 1988-09-26

Family

ID=30850608

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3840087U Pending JPS63145799U (en) 1987-03-18 1987-03-18

Country Status (1)

Country Link
JP (1) JPS63145799U (en)

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