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JPS58204938A - Controller of fuel injection timing in diesel engine with supercharger - Google Patents

Controller of fuel injection timing in diesel engine with supercharger

Info

Publication number
JPS58204938A
JPS58204938A JP8650282A JP8650282A JPS58204938A JP S58204938 A JPS58204938 A JP S58204938A JP 8650282 A JP8650282 A JP 8650282A JP 8650282 A JP8650282 A JP 8650282A JP S58204938 A JPS58204938 A JP S58204938A
Authority
JP
Japan
Prior art keywords
pressure
fuel injection
supercharger
injection timing
timing control
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
JP8650282A
Other languages
Japanese (ja)
Inventor
Takaharu Saiki
斉木 敬治
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.)
Toyota Motor Corp
Original Assignee
Toyota Motor 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 Toyota Motor Corp filed Critical Toyota Motor Corp
Priority to JP8650282A priority Critical patent/JPS58204938A/en
Publication of JPS58204938A publication Critical patent/JPS58204938A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D1/00Controlling fuel-injection pumps, e.g. of high pressure injection type
    • F02D1/16Adjustment of injection timing
    • F02D1/18Adjustment of injection timing with non-mechanical means for transmitting control impulse; with amplification of control impulse
    • F02D1/183Adjustment of injection timing with non-mechanical means for transmitting control impulse; with amplification of control impulse hydraulic
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • High-Pressure Fuel Injection Pump Control (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Abstract

PURPOSE:To release advance timing control at supercharge time, by connecting a pressure air chamber in an altitude timing control compensator of fuel injection timing to an intake system in the downstream of a supercharger. CONSTITUTION:A pressure air chamber 74 in an altitude timing control compensator 66 of fuel injection timing is connected to an intake pipe 22 in the downstream of a supercharger 24. The compensator 66 fully opens a valve body 73 on the flatland despite a load and speed of an engine. While on the highland, a decrease of air pressure displaces the valve body 73 downward, and a bleed amount to a pump chamber 38 is decreased to advance timing control earlier than the timing control on the flatland, however at high speed operation of the engine, the valve body 73 is displaced upward by supercharge pressure and fully opened, and the timing control is released.

Description

【発明の詳細な説明】 本発明は過給機付ディーゼル機関における燃料噴射時期
の高地補償装置に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a high altitude compensation device for fuel injection timing in a supercharged diesel engine.

ディーゼル機関での高地走行時、空気密度が低下するこ
とによる圧縮空気温度上昇の不十分のために、着火性が
不良となり、白煙の排出や失火による運転性の不良を起
す。その対策としては燃料噴射時期を進ませることが有
効であり、そこで高度即ち気圧に応じて燃料噴射時期全
補正する装置がすでに提案されている。この装置は絶対
空気圧力に感応する感圧部材に連結し7た弁部材を有し
、その弁部材は、インジェクションポンプのポンプ室内
の燃料を気圧に応じてポンプ吸入側にブリードする。そ
のためポンプ室の圧力は気圧(即ち高度)によって変化
する。かくして、ポンプ室の圧力で開動されるタイマピ
ストンはプランジャと一体となったツーイスカムとロー
シリングとの相対角度位置、即ち燃料噴射時期を高度に
応じて補償することができるのである。
When driving at high altitudes with a diesel engine, the temperature of the compressed air is insufficiently raised due to the decrease in air density, resulting in poor ignition performance and poor drivability due to white smoke emissions and misfires. As a countermeasure against this problem, it is effective to advance the fuel injection timing, and a device has already been proposed that completely corrects the fuel injection timing according to the altitude, that is, the atmospheric pressure. This device has a valve member connected to a pressure sensitive member sensitive to absolute air pressure, which valve member bleeds fuel in the pump chamber of the injection pump to the pump suction side in response to air pressure. Therefore, the pressure in the pump chamber changes depending on the atmospheric pressure (ie, altitude). In this way, the timer piston, which is opened and moved by the pressure in the pump chamber, can compensate the relative angular position between the two-sided cam and the low sill ring, which are integrated with the plunger, depending on the altitude, that is, the fuel injection timing.

しかしながら、上述タイプの燃料噴射時期制御装置全そ
のまま採用すると白煙、失火の心配のない高負荷時の騒
音の面で著しい不利となるというのけ噴射時期を進める
ことはそれ自体騒音を増大させるものである。
However, if the above-mentioned type of fuel injection timing control device is adopted as is, it will be at a significant disadvantage in terms of noise during high loads without the risk of white smoke and misfires, and advancing the injection timing itself will increase noise. It is.

ところで、過給機付のエンジンでは高負荷時及び高回転
には燃料噴射時期全高地であっても進ませる必要はない
のである。即ち、過給によって空気密度、吸入空気温度
が高められていることから白煙、失火のおそれはないか
らである。従って、高地走行時であっても高負荷側及び
高回転側の過給圧が上がった時、噴射時期を遅らせるこ
とにより、白煙、失火が生ずることなく騒音レベルを押
えることができるのである。
By the way, in a supercharged engine, there is no need to advance the fuel injection timing at high loads and high speeds even if the engine is at full altitude. That is, since the air density and intake air temperature are increased by supercharging, there is no risk of white smoke or misfire. Therefore, even when driving at high altitudes, when the supercharging pressure on the high load side and high rotation side increases, by delaying the injection timing, it is possible to suppress the noise level without causing white smoke or misfires.

従〜て、本発明は過給機付のディーゼル機関において、
過給時に燃料噴射時期の進角を解除することができる装
置を提供することを目的とする。
Therefore, the present invention provides a diesel engine with a supercharger,
An object of the present invention is to provide a device that can release the advance of fuel injection timing during supercharging.

この目的を達成するため本発明にあっては、高地進角補
償装置としての感圧部拐の空気圧室を過給□ 機の下流における吸気系に接続している。その結果過給
圧が生ずる筒負荷時及び高回転時に感圧部材はポンプ室
の燃料圧力を進角が解除されるよう制御する。
In order to achieve this object, in the present invention, the air pressure chamber of the pressure sensitive section serving as the high altitude advance compensation device is connected to the intake system downstream of the supercharger. As a result, the pressure sensitive member controls the fuel pressure in the pump chamber so that the advance angle is released during cylinder load and high engine speed when supercharging pressure is generated.

以下図面によって説明すれば第1図において、10はデ
ィーゼル機関のシリンダブロックであり、ピストン12
が設けられる。シリンダブロック10上にシリンダヘッ
ド14が在り、吸気弁16、燃料噴射弁18が設けられ
る。吸気弁16によって開閉される吸気ボート20は吸
気管22によって過給機24の送出口に接続される。
To explain with reference to the drawings below, in FIG. 1, 10 is a cylinder block of a diesel engine, and a piston 12
is provided. A cylinder head 14 is located on the cylinder block 10, and an intake valve 16 and a fuel injection valve 18 are provided. An intake boat 20, which is opened and closed by the intake valve 16, is connected to an outlet of a supercharger 24 through an intake pipe 22.

26は所謂分配型の燃料噴射ポンプであって、ハウジン
グ27内に軸支されかつ図示しないクランク軸によって
回転駆動賂れる入力軸28を備える。入力軸28上にベ
ーン型のフィードポンプ30 (第1図では90°展開
状態で示す。)が取付けられる。フィードポンプ30は
矢印Aの如く回転することにより図示しない燃料タンク
に接続した給油パイプ32より吸入ボート34を介し燃
料を吸入し、吐出ボート36よシボンプ室38内に燃料
を吐出する。プランジャ40はシリンダ42内に設けら
れ、その端部にツーイスカム44が設けられる。ツーイ
ス刀ム44はハウジング27に取付けたローラ46に尚
接し、その結果プランジャ40はフェイスカム44の一
回転中に気筒数に一致した回数だけ図の左右に往復する
。プランジャ40が図の左方に動く吸入ストローク時は
、ポンプ室38内の燃料は矢印Bの如くプランジャ先端
に気筒数だけ形成した凹所50のうち一つを介して加圧
室52に導入される。プランジャ40が図の右方へ動く
圧送ストローク時はその凹所の50はポンプ室38との
連絡を絶たれ、加圧室52内の燃料は中心孔54より、
シリンダ42に気筒数だけ形成したテリベリ孔56のう
ち一つを介し、デリベリ弁58、デリベリパイプ60を
介して燃料噴射弁18に供給される。
Reference numeral 26 denotes a so-called distribution type fuel injection pump, which includes an input shaft 28 that is rotatably supported within a housing 27 and rotationally driven by a crankshaft (not shown). A vane-type feed pump 30 (shown in a 90° expanded state in FIG. 1) is mounted on the input shaft 28. When the feed pump 30 rotates as shown by arrow A, it sucks fuel from a fuel pipe 32 connected to a fuel tank (not shown) through a suction boat 34, and discharges the fuel into a pump chamber 38 through a discharge boat 36. A plunger 40 is provided within a cylinder 42, and a two-sided cam 44 is provided at its end. The two-wheeled blade 44 is still in contact with a roller 46 attached to the housing 27, so that the plunger 40 reciprocates from side to side in the figure a number of times corresponding to the number of cylinders during one rotation of the face cam 44. During the suction stroke in which the plunger 40 moves to the left in the figure, the fuel in the pump chamber 38 is introduced into the pressurizing chamber 52 through one of the recesses 50 formed at the tip of the plunger for the number of cylinders, as shown by arrow B. Ru. During the pumping stroke in which the plunger 40 moves to the right in the figure, the recess 50 is disconnected from the pump chamber 38, and the fuel in the pressurizing chamber 52 flows through the center hole 54.
The fuel is supplied to the fuel injection valve 18 through one of the delivery holes 56 formed in the cylinder 42 for the same number of cylinders, the delivery valve 58, and the delivery pipe 60.

プランジャ40の左右への駆動を行うローラ46はロッ
ド62を介してタイマピストン64(第1図では90°
展開状態で示す。)に連結される。タイマピストン64
0−側は吸入圧が他側はポンプ室38の吐出圧力が作用
する。従って、吐出圧力と吸入圧力との差圧でp−24
6の、7=イスカム44に対する相対角度位置が変化し
、その結果プランジャの圧送ストローク開始時期、換言
すれば燃料噴射時期が制御されろ。
A roller 46 that drives the plunger 40 left and right is connected to a timer piston 64 (90° in FIG. 1) via a rod 62.
Shown in expanded state. ). timer piston 64
The suction pressure acts on the 0- side, and the discharge pressure of the pump chamber 38 acts on the other side. Therefore, the differential pressure between the discharge pressure and the suction pressure is p-24
6, 7=the relative angular position with respect to the iscam 44 changes, and as a result, the pumping stroke start timing of the plunger, in other words, the fuel injection timing is controlled.

66は高度進角補償装置であって、ケース68内にベロ
ーズ70ケ設け、ベローズはポンプ室38をポンプへの
吸入パイプ32につなぐ配管72會開閉する弁体73に
連結される。ベローズ70の内側は真空となっておシ、
外側に空気圧室74が形成される。
Reference numeral 66 denotes an altitude advance compensator, and 70 bellows are provided in a case 68, and the bellows are connected to a valve body 73 that opens and closes a pipe 72 that connects the pump chamber 38 to the suction pipe 32 to the pump. The inside of the bellows 70 becomes a vacuum,
A pneumatic chamber 74 is formed on the outside.

以上の構成は従来技術と同様であるが、この場合空気圧
空間74は大気開放でめった。すると、平地走行時は気
圧(絶対圧)が太きいためベローズ70は収縮し弁体7
3は上方変位する。そのため、ポンプ室38への吸入圧
力のブリード量は大きくなりポンプ室38の内圧は低下
し、ポンプ室内圧を受けるタイマピストン64はローラ
62を噴射時期を遅らせる方向に修正する。このときの
−1797回転数と進角度性との関係は全負荷と部分負
荷とで夫々第2図の(ロノの1点頚線の様に表わされる
。一方、高地走行時は空気圧力室74の圧力は低下−T
ることからベローズ70は伸び弁体73は下方に変位し
て、ポンプ室38への吸入圧力のブリード量を減少させ
る。その結果、ポンプ室38の内圧Qコ2相対的に増大
しタイマピストン64はローラ62の噴射時期を送酸せ
る方向に修正し、このときのエンジン助1転数と進角特
性との関係は第2図の(ロ))の破線で表わされる。
The above configuration is similar to that of the prior art, but in this case, the pneumatic space 74 is rarely opened to the atmosphere. Then, since the atmospheric pressure (absolute pressure) is large when driving on flat ground, the bellows 70 contracts and the valve body 7
3 is displaced upward. Therefore, the amount of suction pressure bleed into the pump chamber 38 increases, the internal pressure of the pump chamber 38 decreases, and the timer piston 64, which receives the pump chamber pressure, corrects the roller 62 to retard the injection timing. The relationship between the -1797 rotation speed and the advance angle at this time is expressed as shown in Figure 2 (one-point neckline of Rono) for full load and partial load, respectively.On the other hand, when driving at high altitude, the air pressure chamber 74 The pressure of -T decreases
Therefore, the bellows 70 expands and the valve body 73 moves downward, reducing the amount of suction pressure bleeding into the pump chamber 38. As a result, the internal pressure Q in the pump chamber 38 increases relatively, and the timer piston 64 corrects the injection timing of the roller 62 in the direction of supplying oxygen. This is represented by the broken line in (b) in FIG.

かかる従来の制御では高負荷時に燃料噴射時期が無用に
進角されるだけでなく騒音を増大させるという始めに述
べた欠点がある。即ち、過給機を備えた機関ではエンジ
ン高負荷時高回転時程吸気圧力は絶対圧力で増大する。
Such conventional control has the drawbacks mentioned above in that it not only unnecessarily advances the fuel injection timing under high loads but also increases noise. That is, in an engine equipped with a supercharger, the intake pressure increases in absolute pressure when the engine is under high load and when the engine speed is high.

一方白煙、失火限界からの要求進角は第3図の通り圧力
の高い程小さい。然るに、従来においては高地と平地と
で第2図の1点鎖線と点線との間で単に進角特性を切替
えるだけであった。従って、高負荷時であって本来は進
角が必要ないのに高地走行時には進角されていたのであ
る。
On the other hand, the required advance angle from the white smoke and misfire limit is smaller as the pressure is higher, as shown in Figure 3. However, in the past, the advance angle characteristics were simply switched between the dashed line and the dotted line in FIG. 2 for highlands and flatlands. Therefore, even though there was no need to advance the engine angle under high load, the engine angle was advanced when driving at high altitudes.

111 本発明では、第1図に示すよ・、うに、高地進角補償装
置の空気圧力室70は配管80を介して過給機24の下
流の吸気管22に接続されている。この本発明の構成の
作動を述べると、吸気管22内の圧力は平地では第2図
(イ)の1点鎖線の如くなり、高地では点線の如くにな
る。平地では、全負荷でも部分負荷でもかつエンジンの
回転数に係わらず、吸気管圧力は尚地補償装置66の弁
体73を全開位置とするレベル(第2図(イフでは75
9 mmHg に対応するtのレベル)ケ必ず超えてい
る。そのためエンジンの回転数に係わらす進角特性、第
2図(ロ)の1点鎖線となる。
111 In the present invention, as shown in FIG. 1, the air pressure chamber 70 of the high altitude advance compensation device is connected to the intake pipe 22 downstream of the supercharger 24 via a pipe 80. To describe the operation of the configuration of the present invention, the pressure inside the intake pipe 22 becomes as shown by the dashed line in FIG. On flat ground, regardless of the engine speed and under full load or partial load, the intake pipe pressure is at the level at which the valve body 73 of the ground compensator 66 is in the fully open position (see Fig. 2 (if
The level of t corresponding to 9 mmHg) is always exceeded. Therefore, the advance angle characteristic is related to the engine speed, as shown by the dashed-dotted line in FIG. 2 (b).

一部尚地では、エンジン回転数がr、 r2より低いと
きは過給圧力が弁体73全全開とする基準レベルtに足
りず弁体73は下降変位し、ポンプ室38へのブリード
業ケ押えポンプ内圧を上げる。
In some areas, when the engine speed is lower than r or r2, the boost pressure is lower than the reference level t for fully opening the valve body 73, and the valve body 73 is displaced downward, causing a bleed to the pump chamber 38. Increase the internal pressure of the presser pump.

そのためこの回転数以下では進角されその回転数以上で
進角されないという第2図(ロ)の実線の如き特性とな
”る。この半うに本発明では高地において進角が必要な
低負衝(低回転)Illにのみ進角全行い高、・1.:
Therefore, the angle is advanced below this number of revolutions, but not advanced above that number of revolutions, as shown by the solid line in Figure 2 (b). (Low rotation) Full advance height only for Ill, ・1.:
.

負荷側で進角解除(、シていることから、白煙、失火の
問題音生ずることなく騒音を低減することかできる。
Since the advance angle is released on the load side, noise can be reduced without producing white smoke or the problematic sounds of misfires.

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

第1図は本発明のシステム全体構成図、第2図はエンジ
ン回転数yc対する吸気管圧力(イ)及び進角特性(ロ
)を夫々示す模式グラフ。 第3図は吸気管圧力に対する白煙及び失火限界における
畳求進角特性を示す模式グラフ。 IO・・・シリンダブロック、12・・・ピストン、1
8・・・燃料噴射弁、22・・・吸気管、24・・・過
給機、26・・・燃料噴射ポンプ、38・・・ポンプ室
、4o・・・プランジャ、44・・・フェイスカム、4
6・・・カムローラ、52・・・加圧室、64・・・タ
イマピストン、66、高地補償装置、70・・・ベロー
ズ、74・・・空気圧力室、80・・・空気圧力室を過
給機下流に接続する配管 特許出願人 トヨタ自動単工業株式会社 特許出願代理人 弁理士 青 木   朗 弁理士 西 舘 和 之 弁理土中山恭介 弁理士山口昭之
FIG. 1 is an overall configuration diagram of the system of the present invention, and FIG. 2 is a schematic graph showing intake pipe pressure (a) and advance angle characteristics (b) with respect to engine speed yc. FIG. 3 is a schematic graph showing the rectification angle characteristics at the white smoke and misfire limit with respect to the intake pipe pressure. IO...Cylinder block, 12...Piston, 1
8... Fuel injection valve, 22... Intake pipe, 24... Supercharger, 26... Fuel injection pump, 38... Pump chamber, 4o... Plunger, 44... Face cam , 4
6... Cam roller, 52... Pressure chamber, 64... Timer piston, 66, High altitude compensation device, 70... Bellows, 74... Air pressure chamber, 80... Air pressure chamber Pipe connecting downstream of the feeder Patent applicant: Toyota Automobile Industry Co., Ltd. Patent application agent: Patent attorney: Akira Aoki, Patent attorney: Kazuyuki Nishidate, Patent attorney: Kyosuke Tsuchinakayama, Patent attorney: Akiyuki Yamaguchi

Claims (1)

【特許請求の範囲】[Claims] 過給機付ディーゼル機関であって、インジークシ、ンポ
ンプが、エンジン回転数に応じた吐出圧の燃料を受ける
ポンプ室と、該ポンプ室内の圧力に応じてカムローラと
プランジャの往復駆動を行うカム手段との相対角度位置
を制御する噴射時期制御機構とを備え、更に前記ポンプ
室は給体空気圧力に感応する感圧部材に連結した弁部材
によって、インジェクションポンプの吸入側に連結ぞn
で、高度に応じた燃料噴射時期制御を行うようになって
いるものにおいて、前記感圧部材の空気圧力を受ける室
は過給機より下流の機関吸気系に連結されていて吸気管
圧力に応じた燃料噴射時期の補正を行うようになってい
る燃料噴射時期制御装置。
A diesel engine with a supercharger, in which an injection pump has a pump chamber that receives fuel at a discharge pressure corresponding to the engine rotation speed, and a cam means that reciprocates a cam roller and a plunger according to the pressure in the pump chamber. and an injection timing control mechanism for controlling the relative angular position of the injection pump, and the pump chamber is connected to the suction side of the injection pump by a valve member connected to a pressure-sensitive member that is sensitive to feed air pressure.
In a device that controls fuel injection timing according to altitude, the chamber that receives the air pressure of the pressure-sensitive member is connected to the engine intake system downstream from the supercharger, and the chamber that receives the air pressure from the pressure-sensitive member is connected to the engine intake system downstream of the supercharger, and the pressure is controlled according to the intake pipe pressure. A fuel injection timing control device that corrects the fuel injection timing.
JP8650282A 1982-05-24 1982-05-24 Controller of fuel injection timing in diesel engine with supercharger Pending JPS58204938A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8650282A JPS58204938A (en) 1982-05-24 1982-05-24 Controller of fuel injection timing in diesel engine with supercharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8650282A JPS58204938A (en) 1982-05-24 1982-05-24 Controller of fuel injection timing in diesel engine with supercharger

Publications (1)

Publication Number Publication Date
JPS58204938A true JPS58204938A (en) 1983-11-29

Family

ID=13888749

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8650282A Pending JPS58204938A (en) 1982-05-24 1982-05-24 Controller of fuel injection timing in diesel engine with supercharger

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JP (1) JPS58204938A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2580334A1 (en) * 1985-04-15 1986-10-17 Ricardo Consulting Eng FUEL SUPPLY SYSTEM FOR INTERNAL COMBUSTION ENGINE WITH TURBOCHARGER

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5584824A (en) * 1978-12-16 1980-06-26 Bosch Gmbh Robert Fuel injector for diesel engine

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5584824A (en) * 1978-12-16 1980-06-26 Bosch Gmbh Robert Fuel injector for diesel engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2580334A1 (en) * 1985-04-15 1986-10-17 Ricardo Consulting Eng FUEL SUPPLY SYSTEM FOR INTERNAL COMBUSTION ENGINE WITH TURBOCHARGER

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