JPS59137323U - dual fuel engine - Google Patents

dual fuel engine

Info

Publication number
JPS59137323U
JPS59137323U JP3085383U JP3085383U JPS59137323U JP S59137323 U JPS59137323 U JP S59137323U JP 3085383 U JP3085383 U JP 3085383U JP 3085383 U JP3085383 U JP 3085383U JP S59137323 U JPS59137323 U JP S59137323U
Authority
JP
Japan
Prior art keywords
gas
engine
valve
pressure
fuel
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
JP3085383U
Other languages
Japanese (ja)
Other versions
JPS6349540Y2 (en
Inventor
沖田 王駿
南 清和
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Kubota Corp
Original Assignee
Kubota Corp
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 Kubota Corp filed Critical Kubota Corp
Priority to JP3085383U priority Critical patent/JPS59137323U/en
Publication of JPS59137323U publication Critical patent/JPS59137323U/en
Application granted granted Critical
Publication of JPS6349540Y2 publication Critical patent/JPS6349540Y2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Output Control And Ontrol Of Special Type Engine (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]

図面は杢考案に係る二元燃料エンジンの実施例を示し、
第1図は概略断面図、第2図は運転制御構成を示すブロ
ック図であり、そして、第3図イ。 口は実験データを示すグラフであり、さらに、第4図は
別の実施例の概略図である。  。 2・・・シリンダヘッド、3・・・流量調整弁、4・・
・混合器、6・・・流路開閉弁、7・・・圧力調整弁、
16・・・1 ダイヤフラム、111−・・スープリン
グ、20又は23゜24・・・弁機構、GR・・・〃゛
ス流路OR・・・オイル流路、r工・・・空気供給路、
r2・・・ガス燃料供給路、r4・・・バイロフト流路
The drawing shows an example of a dual fuel engine invented by Mokura.
FIG. 1 is a schematic sectional view, FIG. 2 is a block diagram showing the operation control configuration, and FIG. 4 is a graph showing experimental data, and FIG. 4 is a schematic diagram of another example. . 2... Cylinder head, 3... Flow rate adjustment valve, 4...
・Mixer, 6...Flow path opening/closing valve, 7...Pressure adjustment valve,
16...1 diaphragm, 111-... soup ring, 20 or 23゜24... valve mechanism, GR... ゛ flow path OR... oil flow path, r work... air supply path ,
r2...Gas fuel supply path, r4...Biloft flow path.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] シリンダヘッド2に対して、混合器4からの空気とガス
燃料との混合ガスを供給するガス流路GRと、オイル燃
料を供給するオイル流路ORとを連通接続すると共に、
前記ガス流路GRに、流量□    調整弁3を設け、
前記混合器4への空気供給路r□に、エンジン排ガス駆
動型過給機5を接続すると共に、前記混合器4へのガス
燃料供給路r2に、流路開閉弁6及びそれよりも流路下
手側に位置させて圧力調整弁7を夫々設け、前記圧力調
整弁7の操作用ダイヤフラム16を、スプリング18、
及び、前記空気供給路r1カ象のパイロット空気によっ
て増圧側に、且つ、圧力調整後のガス圧によって減圧側
に操作されるように設け、前記開閉弁6を開いてガス燃
料を主体に運転するガス運転モードと、前記開閉弁6を
閉じてオイル燃料によって運転するオイル運転モードと
に、指令信号によって切換えるように構成した二元燃料
エンジンであって、前記ダイヤフラム16に供給するパ
イロット空気圧を減少する二段操作式弁機構20又は2
3.24を、パイロット空気流動用パイロット    
・流路r4に接続すると共に、エンジン負荷が設定負荷
以下の状態でのみパイロット空気圧を減少させるよう、
エンジン負荷に基づいて前記弁機構20  −又は23
.24を自動的に操作する制御装置を設けである二元燃
料エンジン。             ′
A gas passage GR that supplies a mixed gas of air and gas fuel from a mixer 4 and an oil passage OR that supplies oil fuel are connected to the cylinder head 2, and
A flow rate adjustment valve 3 is provided in the gas flow path GR,
An engine exhaust gas-driven supercharger 5 is connected to the air supply path r□ to the mixer 4, and a flow path opening/closing valve 6 and a flow path are connected to the gas fuel supply path r2 to the mixer 4. A pressure regulating valve 7 is provided on the lower side, and a diaphragm 16 for operating the pressure regulating valve 7 is connected to a spring 18,
The air supply path r1 is provided so as to be operated to the pressure increasing side by the pilot air and to the pressure reducing side by the gas pressure after pressure adjustment, and the on-off valve 6 is opened to operate mainly on gas fuel. The dual fuel engine is configured to be switched by a command signal between a gas operation mode and an oil operation mode in which the on-off valve 6 is closed and the engine is operated using oil fuel, and the pilot air pressure supplied to the diaphragm 16 is reduced. Two-stage operated valve mechanism 20 or 2
3.24, pilot air flow pilot
・In addition to connecting to the flow path r4, the pilot air pressure is reduced only when the engine load is below the set load.
The valve mechanism 20 - or 23 based on the engine load
.. A dual fuel engine that is equipped with a control device to automatically operate the engine. ′
JP3085383U 1983-03-02 1983-03-02 dual fuel engine Granted JPS59137323U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3085383U JPS59137323U (en) 1983-03-02 1983-03-02 dual fuel engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3085383U JPS59137323U (en) 1983-03-02 1983-03-02 dual fuel engine

Publications (2)

Publication Number Publication Date
JPS59137323U true JPS59137323U (en) 1984-09-13
JPS6349540Y2 JPS6349540Y2 (en) 1988-12-20

Family

ID=30161726

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3085383U Granted JPS59137323U (en) 1983-03-02 1983-03-02 dual fuel engine

Country Status (1)

Country Link
JP (1) JPS59137323U (en)

Also Published As

Publication number Publication date
JPS6349540Y2 (en) 1988-12-20

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