JPS59157549U - fuel injection pump - Google Patents

fuel injection pump

Info

Publication number
JPS59157549U
JPS59157549U JP3939983U JP3939983U JPS59157549U JP S59157549 U JPS59157549 U JP S59157549U JP 3939983 U JP3939983 U JP 3939983U JP 3939983 U JP3939983 U JP 3939983U JP S59157549 U JPS59157549 U JP S59157549U
Authority
JP
Japan
Prior art keywords
injection timing
fuel
altitude
detection device
fuel injection
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
JP3939983U
Other languages
Japanese (ja)
Other versions
JPH0244036Y2 (en
Inventor
清則 長門
Original Assignee
マツダ株式会社
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 マツダ株式会社 filed Critical マツダ株式会社
Priority to JP3939983U priority Critical patent/JPS59157549U/en
Publication of JPS59157549U publication Critical patent/JPS59157549U/en
Application granted granted Critical
Publication of JPH0244036Y2 publication Critical patent/JPH0244036Y2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • High-Pressure Fuel Injection Pump Control (AREA)
  • Fuel-Injection Apparatus (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 the drawing]

図面は本考案の実施態様を例示し、第1図ないし第6図
は実施例1を示し、第1図は燃料噴射ポンプの全体断面
図、第2図は要部断面図、第3図は゛アクチュエータの
平面図、第4図A−Dはそれぞれ作動状態を説明する要
部断面図、第5図および第6図は噴射時期の進角特性を
示す説明図、第7図ないし第9図は実施例2を示し、第
7図は概略構成図、第8図は制御回路の変形例を示すブ
ロック図、第9図は第7図における制御回路のフローチ
ャート図、第10図は実施例3を示す概略構成図である
。 ′1・・・・・・フィードポンプ、3・・・・・・入力
軸、4・・曲燃料供給通路、5・・・・・・ポンプ室、
6・・・・・・レギュレータバルブ、8・・・・・・カ
ム、9・・・・・・プランジャ、10・・・・・・スピ
ードタイマ機構、11・・・・・・タイマピストン、1
2・・・・・・ガバナシャフト、15・・・・・・フラ
イウェイト、17・・・・・・ガバナスリーブ、24・
・・・・・コントロールスリーブ、25a・・・・・・
低地用燃料逃し通路、25b・・・・・・高地用燃料逃
し通路、26a・・・・・・低地用ポート、26b・・
・・・・高地用ポート、27・・・・・・タイミングコ
ントロールスリーブ、28・・・・・・アクチュエータ
、29・・・・・・制御回路、30・・・・・・気圧セ
ンサー、31・・曲ソレノイド、33・・・・・・アク
チュエータ、36・・・・・・タイマピストン、43・
・・・・・圧力制御弁、44・・・・・・制御回路、5
8・・・・・・アクチュエータ、61・・・・・・制御
回路。
The drawings illustrate embodiments of the present invention, and FIGS. 1 to 6 show Embodiment 1. FIG. 1 is an overall sectional view of the fuel injection pump, FIG. A plan view of the actuator, FIGS. 4A to 4D are cross-sectional views of main parts explaining the operating state, FIGS. 5 and 6 are explanatory diagrams showing the advance characteristics of the injection timing, and FIGS. 7 to 9 are Embodiment 2 is shown, FIG. 7 is a schematic configuration diagram, FIG. 8 is a block diagram showing a modification of the control circuit, FIG. 9 is a flowchart of the control circuit in FIG. 7, and FIG. 10 is a diagram showing the third embodiment. FIG. '1...Feed pump, 3...Input shaft, 4...Curved fuel supply passage, 5...Pump chamber,
6...Regulator valve, 8...Cam, 9...Plunger, 10...Speed timer mechanism, 11...Timer piston, 1
2...Governor shaft, 15...Fly weight, 17...Governor sleeve, 24...
...Control sleeve, 25a...
Low-altitude fuel relief passage, 25b... High-altitude fuel relief passage, 26a... Low-altitude port, 26b...
...High altitude port, 27...Timing control sleeve, 28...Actuator, 29...Control circuit, 30...Barometric pressure sensor, 31... - Curved solenoid, 33... Actuator, 36... Timer piston, 43...
...Pressure control valve, 44...Control circuit, 5
8... Actuator, 61... Control circuit.

Claims (3)

【実用新案登録請求の範囲】[Scope of utility model registration request] (1)燃料の噴射時期を変更する噴射時期可変装置と、
大気圧を検出する大気圧検出装置と、エンジンの負荷状
態を検出する負荷検出装置と、上記雨検出装置の出力に
応じ、大気圧低下状態にあって低負荷時には噴射時期を
進角方向へ高負荷時には噴射時期を遅角方向に噴射時期
可変装置を駆動させる噴射時期制御装置とを備えたこと
を特徴とする燃料噴射ポシプ。
(1) An injection timing variable device that changes the fuel injection timing;
An atmospheric pressure detection device detects atmospheric pressure, a load detection device detects the engine load state, and the injection timing is advanced in the advance direction when the atmospheric pressure is low and the load is low according to the output of the rain detection device. 1. A fuel injection system comprising: an injection timing control device that drives an injection timing variable device to retard the injection timing when under load.
(2)噴射時期可変装置がエンジン回転数に応じた、燃
料圧力により噴射時期を制御するスピードタイマ機構で
構成され、噴射時期制御装置がガバナシャフトに形成さ
れた低地用および高地用燃料逃し通路と、ガバナシャフ
トに嵌装され燃料噴射量に対応してガバナシャフトを摺
動するガバナスリーブと、該ガバナスリーブに開設され
た低地用および高地用ポートと、ガバナスリーブに嵌装
され該ガバナスリーブの低地用および高地用ポートを開
閉するタイミングコントロールスリーブとを備え、大気
圧検出装置の出力に応じて上記タイミングコントロール
スリーブを駆動する構成とした実用新案登録請求の範囲
第1項記載の燃料噴射ポンプ。
(2) The injection timing variable device is composed of a speed timer mechanism that controls the injection timing by fuel pressure according to the engine rotation speed, and the injection timing control device is configured with a low-altitude and high-altitude fuel relief passage formed in the governor shaft. , a governor sleeve that is fitted to the governor shaft and slides on the governor shaft in accordance with the fuel injection amount; a low-altitude port and a high-altitude port that are fitted to the governor sleeve; 2. The fuel injection pump according to claim 1, wherein the fuel injection pump is provided with a timing control sleeve that opens and closes ports for high altitude and high altitude use, and is configured to drive the timing control sleeve in accordance with the output of an atmospheric pressure detection device.
(3)  噴射時期可変装置が燃料噴射ポンプの入力軸
とプランジャを駆動するカムとの位相を変更することに
よって噴射時期を可変とするアクチュエータと、該アク
チュエータに作用する作動圧力を制御する圧力制御弁と
により構成され噴射時期制御装置は少なくとも大気圧検
出装置および負荷検出装置の信号に応じて上記圧力制御
弁を駆動する出力信号を発生する構成とした実用新案登
録請求の範囲第1項記載の燃料噴射ポンプ。
(3) An actuator in which the injection timing variable device varies the injection timing by changing the phase between the input shaft of the fuel injection pump and a cam that drives the plunger, and a pressure control valve that controls the operating pressure acting on the actuator. The fuel according to claim 1, wherein the injection timing control device is configured to generate an output signal for driving the pressure control valve in response to signals from at least an atmospheric pressure detection device and a load detection device. injection pump.
JP3939983U 1983-03-17 1983-03-17 fuel injection pump Granted JPS59157549U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3939983U JPS59157549U (en) 1983-03-17 1983-03-17 fuel injection pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3939983U JPS59157549U (en) 1983-03-17 1983-03-17 fuel injection pump

Publications (2)

Publication Number Publication Date
JPS59157549U true JPS59157549U (en) 1984-10-23
JPH0244036Y2 JPH0244036Y2 (en) 1990-11-22

Family

ID=30170051

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3939983U Granted JPS59157549U (en) 1983-03-17 1983-03-17 fuel injection pump

Country Status (1)

Country Link
JP (1) JPS59157549U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS623948U (en) * 1985-06-24 1987-01-10
JP2011174411A (en) * 2010-02-24 2011-09-08 Yanmar Co Ltd Engine
JP2014013043A (en) * 2013-10-22 2014-01-23 Yanmar Co Ltd Engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS623948U (en) * 1985-06-24 1987-01-10
JP2011174411A (en) * 2010-02-24 2011-09-08 Yanmar Co Ltd Engine
JP2014013043A (en) * 2013-10-22 2014-01-23 Yanmar Co Ltd Engine

Also Published As

Publication number Publication date
JPH0244036Y2 (en) 1990-11-22

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