JPS643052U - - Google Patents
Info
- Publication number
- JPS643052U JPS643052U JP9782587U JP9782587U JPS643052U JP S643052 U JPS643052 U JP S643052U JP 9782587 U JP9782587 U JP 9782587U JP 9782587 U JP9782587 U JP 9782587U JP S643052 U JPS643052 U JP S643052U
- Authority
- JP
- Japan
- Prior art keywords
- pump
- injection
- fuel injection
- 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.)
- Pending
Links
- 238000002347 injection Methods 0.000 claims description 21
- 239000007924 injection Substances 0.000 claims description 21
- 239000000446 fuel Substances 0.000 claims description 6
- 238000010586 diagram Methods 0.000 description 5
- 238000001514 detection method Methods 0.000 description 2
Landscapes
- Fuel-Injection Apparatus (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Description
第1図は本考案のクレーム対応図、第2図は本
考案の一実施例を示すブロツク図、第3図はこの
実施例の制御内容を示す流れ図である。第4図A
と第4図Bは機関回転数を一定とした場合におい
て機関負荷を相違させた実験結果で、それぞれ低
負荷域と中高負荷域での騒音レベルとHC及びN
Ox排出量に対する噴射期間比の影響を示す特性
図である。第5図は従来例のポンプ断面図、第6
図Aと第6図Bはそれぞれ通常噴射とパイロツト
噴射時の燃料噴射特性を示す説明図、第7図はフ
エイスカムのカム速度特性図である。
1…ポンプハウジング、3…プランジヤポンプ
、5…ポンプ室、7…プランジヤ、9…フエイス
カム、11…ローラ、12…プランジヤ室、13
…熱料戻し通路、14…電磁弁、16…電磁弁駆
動回路、22…機関回転数検出手段、23…機関
負荷検出手段、24…負荷時の全噴射期間算出手
段、25…無負荷時の全噴射期間算出手段、26
…領域判定手段、27…パイロツト噴射の噴射期
間算出手段、28…主噴射の噴射期間算出手段、
29…駆動パルス発生手段、41…回転数センサ
、42…上死点センサ、43…アクセル開度セン
サ、44…コントロールユニツト、46…メモリ
、47…開閉時期センサ。
FIG. 1 is a diagram corresponding to the claims of the present invention, FIG. 2 is a block diagram showing an embodiment of the present invention, and FIG. 3 is a flowchart showing the control contents of this embodiment. Figure 4A
Figure 4B shows the results of experiments with different engine loads when the engine speed is constant, and the noise level and HC and N in the low load range and medium-high load range, respectively.
FIG. 3 is a characteristic diagram showing the influence of the injection period ratio on the amount of Ox discharged. Figure 5 is a sectional view of a conventional pump;
Figures A and 6B are explanatory diagrams showing fuel injection characteristics during normal injection and pilot injection, respectively, and Figure 7 is a cam speed characteristic diagram of the face cam. DESCRIPTION OF SYMBOLS 1... Pump housing, 3... Plunger pump, 5... Pump chamber, 7... Plunger, 9... Face cam, 11... Roller, 12... Plunger chamber, 13
...heat return passage, 14...electromagnetic valve, 16...electromagnetic valve drive circuit, 22...engine rotation speed detection means, 23...engine load detection means, 24...total injection period calculation means at load, 25...at no load Total injection period calculation means, 26
...Area determination means, 27.. Injection period calculation means for pilot injection, 28.. Injection period calculation means for main injection,
29... Drive pulse generating means, 41... Rotation speed sensor, 42... Top dead center sensor, 43... Accelerator opening sensor, 44... Control unit, 46... Memory, 47... Opening/closing timing sensor.
Claims (1)
プと高圧プランジヤポンプを設け、ポンプハウジ
ングに形成したフイードポンプの低圧ポンプ室と
プランジヤポンプの高圧プランジヤ室とを連通す
る燃料戻し通路に駆動パルスにて開閉される電磁
弁を介装し、この電磁弁の開閉により燃料の噴射
開始時期と噴射期間とが可変制御される燃料噴射
ポンプを備える一方で、燃料の噴射を2回に分け
、主噴射に先立つてパイロツト噴射を行うように
したデイーゼル機関の燃料噴射制御装置において
、前記パイロツト噴射の噴射期間を無負荷時の全
噴射期間の1/2としたことを特徴とするデイー
ゼル機関の燃料噴射制御装置。 A low-pressure feed pump and a high-pressure plunger pump that rotate in synchronization with engine rotation are provided, and an electromagnetic pump that opens and closes using a drive pulse is installed in the fuel return passage that communicates the low-pressure pump chamber of the feed pump formed in the pump housing with the high-pressure plunger chamber of the plunger pump. The fuel injection pump is equipped with a valve, and the fuel injection start timing and injection period are variably controlled by the opening and closing of this solenoid valve.The fuel injection pump is divided into two injections, and the pilot injection is performed prior to the main injection. What is claimed is: 1. A fuel injection control device for a diesel engine, characterized in that the injection period of the pilot injection is set to 1/2 of the total injection period under no-load conditions.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9782587U JPS643052U (en) | 1987-06-25 | 1987-06-25 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9782587U JPS643052U (en) | 1987-06-25 | 1987-06-25 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS643052U true JPS643052U (en) | 1989-01-10 |
Family
ID=31323559
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9782587U Pending JPS643052U (en) | 1987-06-25 | 1987-06-25 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS643052U (en) |
-
1987
- 1987-06-25 JP JP9782587U patent/JPS643052U/ja active Pending