JPS5992098U - Fluid pressure control device - Google Patents

Fluid pressure control device

Info

Publication number
JPS5992098U
JPS5992098U JP18951182U JP18951182U JPS5992098U JP S5992098 U JPS5992098 U JP S5992098U JP 18951182 U JP18951182 U JP 18951182U JP 18951182 U JP18951182 U JP 18951182U JP S5992098 U JPS5992098 U JP S5992098U
Authority
JP
Japan
Prior art keywords
pressure
valve device
gas pressure
control device
fluid
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
JP18951182U
Other languages
Japanese (ja)
Inventor
湖山 月雄
Original Assignee
富士重工業株式会社
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 by 富士重工業株式会社 filed Critical 富士重工業株式会社
Priority to JP18951182U priority Critical patent/JPS5992098U/en
Publication of JPS5992098U publication Critical patent/JPS5992098U/en
Pending legal-status Critical Current

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  • Loading And Unloading Of Fuel Tanks Or Ships (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

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

第1図は本考案が適用される航空機への燃料供給装置の
従来技術を示す系統図、第2図は本考案の実施例を示す
燃料供給装置の要部のブロック図、第3A図は第2図の
エアタンク20が無い場合の設定エア圧の変動を示すグ
ラフ、第3B図はエアタンクを設けた場合の設定エア圧
の変動を示すグラフである。 なお図面に用いられている符号において、1・・・第1
圧力制御弁装置、2・・・第2圧力制御弁装置、2a・
・・ピストンチェンバー、2b・・・入口、2c・・・
ビ   lストン弁、2d・・・バイアススプリング、
2e・・・出口、3・・・ベノチュリーー管、4,5・
・・ホース端制御弁、6.7・・・ノズル、11・・・
パイロット弁装置、11a・・・ダイヤフラム、11b
・・・サージポペット(X−Y制御弁)、IIC・・・
減圧ポペット(Y−Z制御弁)、11d・・・オリフィ
ス、12・・・Bパイロット弁装置、20・・・エアタ
ンク。
Fig. 1 is a system diagram showing a conventional technology of a fuel supply system for an aircraft to which the present invention is applied, Fig. 2 is a block diagram of main parts of a fuel supply system showing an embodiment of the present invention, and Fig. 3A is a system diagram showing a conventional fuel supply system for an aircraft to which the present invention is applied. FIG. 2 is a graph showing fluctuations in the set air pressure when the air tank 20 is not provided, and FIG. 3B is a graph showing fluctuations in the set air pressure when an air tank is provided. In addition, in the symbols used in the drawings, 1...1st
Pressure control valve device, 2...Second pressure control valve device, 2a.
... Piston chamber, 2b... Inlet, 2c...
Biston valve, 2d...bias spring,
2e...Exit, 3...Venoturi tube, 4,5.
...Hose end control valve, 6.7...Nozzle, 11...
Pilot valve device, 11a... diaphragm, 11b
...Surge poppet (X-Y control valve), IIC...
Decompression poppet (Y-Z control valve), 11d... orifice, 12... B pilot valve device, 20... air tank.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 圧力を制御すべき流体が通過する主弁装置からの出力流
体圧を検出して検出圧と設定圧−との差に応じて上記主
弁装置の開度を調整するようにしたパイロット弁装置を
備える流体制御装置において、上記パイロット弁装置は
、気体圧調整器から与えられる上記設定圧に対応する気
体圧と上記検出圧とが互に逆方向に作用するダイヤフラ
ムと、このダイヤフラムに結合され上記主弁装置を制御
する制御弁とを備え、上記ダイヤフラムの動作による気
体圧供給側の容積変化よりも十分に大きい容積を有する
気体タンクが上記気体圧調整器とパイロット弁装置との
気体圧供給路に介在されていることを特徴とする流体圧
制御装置。
A pilot valve device detects the output fluid pressure from a main valve device through which a fluid whose pressure is to be controlled passes, and adjusts the opening degree of the main valve device according to the difference between the detected pressure and the set pressure. In the fluid control device, the pilot valve device includes a diaphragm on which a gas pressure corresponding to the set pressure applied from a gas pressure regulator and the detected pressure act in opposite directions; A gas tank is provided in the gas pressure supply path between the gas pressure regulator and the pilot valve device, and includes a control valve for controlling the valve device, and has a volume sufficiently larger than the volume change on the gas pressure supply side due to the operation of the diaphragm. A fluid pressure control device characterized in that:
JP18951182U 1982-12-15 1982-12-15 Fluid pressure control device Pending JPS5992098U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18951182U JPS5992098U (en) 1982-12-15 1982-12-15 Fluid pressure control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18951182U JPS5992098U (en) 1982-12-15 1982-12-15 Fluid pressure control device

Publications (1)

Publication Number Publication Date
JPS5992098U true JPS5992098U (en) 1984-06-22

Family

ID=30408568

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18951182U Pending JPS5992098U (en) 1982-12-15 1982-12-15 Fluid pressure control device

Country Status (1)

Country Link
JP (1) JPS5992098U (en)

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