JPH0474558B2 - - Google Patents
Info
- Publication number
- JPH0474558B2 JPH0474558B2 JP26568686A JP26568686A JPH0474558B2 JP H0474558 B2 JPH0474558 B2 JP H0474558B2 JP 26568686 A JP26568686 A JP 26568686A JP 26568686 A JP26568686 A JP 26568686A JP H0474558 B2 JPH0474558 B2 JP H0474558B2
- Authority
- JP
- Japan
- Prior art keywords
- vapor
- hole
- fuel
- pump
- holes
- 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.)
- Expired
Links
- 239000000446 fuel Substances 0.000 claims description 24
- 238000000605 extraction Methods 0.000 description 17
- 230000000694 effects Effects 0.000 description 10
- 238000002485 combustion reaction Methods 0.000 description 2
- 230000001771 impaired effect Effects 0.000 description 2
- 230000006866 deterioration Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Description
【発明の詳細な説明】
<産業上の利用分野>
本発明は、自動車用内燃機関に使用されるター
ビン型燃料ポンプに関し、殊にそのベーパ抜き構
造に関する。DETAILED DESCRIPTION OF THE INVENTION <Industrial Application Field> The present invention relates to a turbine-type fuel pump used in an internal combustion engine for an automobile, and particularly to its vapor removal structure.
<従来の技術>
近年、自動車用内燃機関においては、燃料タン
ク内の燃料を機関への燃料供給部である燃料噴射
弁等に供給するための燃料ポンプとして、タービ
ン型燃料ポンプ(非容積型の円周流ポンプ)が使
用される傾向にある(実願昭60−141392号等参
照)。<Prior art> In recent years, in internal combustion engines for automobiles, turbine-type fuel pumps (non-positive displacement Circumferential flow pumps) tend to be used (see Utility Model Application No. 141392-1980, etc.).
かかるタービン型燃料ポンプは、第3図及び第
4図に示すように、ポンプハウジング1内を固定
シヤフト2回りに図示しない電動モータによりジ
ヨイント3を介して図示矢印A方向に回転駆動さ
れるインペラ4によつて、このインペラ4外周に
凹設した溝4aの作用で、吸込口5から燃料を吸
込み、燃料流路6を経て、吐出口7より燃料を吐
出するものである。 As shown in FIGS. 3 and 4, this turbine-type fuel pump includes an impeller 4 which is rotated in the direction of arrow A in the drawing by an electric motor (not shown) inside the pump housing 1 around a fixed shaft 2 via a joint 3. Accordingly, by the action of the groove 4a formed in the outer periphery of the impeller 4, fuel is sucked in from the suction port 5, and is discharged from the discharge port 7 via the fuel flow path 6.
また、燃料温度が高温の状況下で再始動する場
合に、ポンプ内部にベーパが発生し、このベーパ
発生量が多いと吐出流量を低下させるので、燃料
流路6の別途には小径のベーパ抜き孔8を設け、
ポンプ内で発生したベーパを、このベーパ抜き孔
8から燃料タンク内へ逃がすようにしている。 In addition, when restarting under high fuel temperature conditions, vapor is generated inside the pump, and if the amount of vapor generated is large, the discharge flow rate will be reduced. A hole 8 is provided,
The vapor generated within the pump is allowed to escape into the fuel tank through this vapor vent hole 8.
<発明が解決しようとする問題点>
ところで、前記ベーパ抜き孔によるベーパ抜き
作用としては、ベーパ抜き孔を燃圧の高い吐出口
寄りに配置した方が良いが、この場合には、ベー
パの発生の少ない低温時にベーパ抜き孔からの燃
料排出量が多くなり低温時のポンプ効率が悪くな
る。このため、従来では低温時の特性悪化を防ぐ
ために小径(例えば直径0.7〜1.4mm程度)のベー
パ抜き孔を燃圧の低い吸込口寄りに設けるように
しており、従つて、ベーパ抜きの効果が充分とは
言えなかつた。<Problems to be Solved by the Invention> Incidentally, for the vapor removal effect of the vapor removal hole, it is better to arrange the vapor removal hole near the discharge port where the fuel pressure is high, but in this case, the vapor generation can be prevented. When the temperature is low, the amount of fuel discharged from the vapor vent hole increases, and the pump efficiency at low temperatures deteriorates. For this reason, conventionally, in order to prevent deterioration of characteristics at low temperatures, a small diameter (for example, about 0.7 to 1.4 mm in diameter) vapor removal hole is provided near the suction port where the fuel pressure is low, so that the vapor removal effect is sufficient. I couldn't say that.
本発明は上記の実情に鑑みてなされたもので、
低温時のポンプ効率を維持し、しかも高温時に充
分なベーパ抜き作用の得られるタービン型燃料ポ
ンプを提供することを目的とする。 The present invention was made in view of the above circumstances, and
It is an object of the present invention to provide a turbine-type fuel pump that maintains pump efficiency at low temperatures and provides sufficient vapor removal action at high temperatures.
<問題点を解決するための手段>
このため本発明は、ベーパ抜き孔を燃料流路に
沿つて近接配置する複数の孔の集合体で構成し
た。<Means for Solving the Problems> For this reason, in the present invention, the vapor extraction hole is constituted by an aggregate of a plurality of holes arranged close to each other along the fuel flow path.
<作用>
上記の構成によれば、ベーパ抜き孔を複数の孔
の集合体、即ち従来の孔より小径(ベーパ核より
は大)の孔を燃料流路に沿つて互いに近接させて
複数設け、各孔の開口断面積の総和が従来の1つ
のベーパ抜き孔の開口断面積と略同じとなるよう
に形成してあり、従つて、従来のような1ケ所に
設けるものに比べてベーパ間の干渉が少なくなり
ベーパ抜き作用が良好となる。また、各孔を近接
して配置してあり、各孔における燃圧が略等しい
ので、燃料の洩れ量も従来と略同量に抑えること
ができ低温時のポンプ効率が損なわれることはな
い。<Function> According to the above configuration, the vapor extraction hole is an aggregate of a plurality of holes, that is, a plurality of holes having a smaller diameter than the conventional hole (larger than the vapor core) are provided close to each other along the fuel flow path, The total opening cross-sectional area of each hole is formed to be approximately the same as the opening cross-sectional area of one conventional vapor extraction hole. Interference is reduced and the vapor removal effect is improved. Further, since the holes are arranged close to each other and the fuel pressure in each hole is approximately equal, the amount of fuel leakage can be suppressed to approximately the same amount as in the past, and pump efficiency at low temperatures is not impaired.
<実施例>
以下、本発明の一実施例を図面に基づいて詳細
に説明する。尚、従来と同一部分には同一符号を
付して説明を省略する。<Example> Hereinafter, an example of the present invention will be described in detail based on the drawings. Incidentally, the same parts as in the prior art are given the same reference numerals, and the description thereof will be omitted.
本実施例を示す第1図において、本実施例のベ
ーパ抜き孔は、燃料流路6に沿つて近接配置する
複数、例えば2つのベーパ抜き孔11A,11B
の集合体で構成されている。 In FIG. 1 showing this embodiment, the vapor vent holes of this embodiment include a plurality of vapor vent holes 11A and 11B, for example, two vapor vent holes 11A and 11B arranged close to each other along the fuel flow path 6.
It is made up of a collection of.
更に詳述すれば、吸込口5寄りの従来と略同様
の位置に、燃料流路6に沿つて互いに近接する2
ケ所に分散させて従来のベーパ抜き孔8よりも小
径(ベーパ核よりは大)のベーパ抜き孔11A,
11Bを設けて構成する。 To be more specific, two parts are placed close to each other along the fuel flow path 6 at substantially the same position as the conventional one near the suction port 5.
Vapor extraction holes 11A are dispersed in multiple locations and have a smaller diameter than the conventional vapor extraction holes 8 (larger than the vapor core).
11B.
各ベーパ抜き孔11A,11Bの孔径は、各ベ
ーパ孔き孔11A,11Bの開口断面積の総和が
従来の1つのベーパ抜き孔8の開口断面積と略等
しくなるように形成する。例えば、従来のベーパ
抜き孔8の孔径が1.4mmである場合、各ベーパ抜
き孔11A,11Bの孔径をそれぞれ1.0mmとす
る。また、ベーパ抜き孔11A,11Bは中心角
(図中θで示す)で20゜以内の範囲に設けるように
する。 The diameter of each vapor extraction hole 11A, 11B is formed so that the sum of the opening cross-sectional areas of each vapor extraction hole 11A, 11B is approximately equal to the opening cross-sectional area of one conventional vapor extraction hole 8. For example, when the diameter of the conventional vapor extraction hole 8 is 1.4 mm, the diameter of each vapor extraction hole 11A, 11B is set to 1.0 mm. Further, the vapor extraction holes 11A and 11B are provided within a range of 20 degrees in terms of center angle (indicated by θ in the figure).
かかる構成によれば、従来よりも小径のベーパ
抜き孔11A,11Bを2ケ所に設けることによ
つて、ベーパ同士の干渉が従来よりも少なくな
り、また上流側のベーパ抜き孔11Aで排出でき
なかつたベーパを下流側のベーパ抜き孔11Bか
ら排出できるようになるため、ベーパ抜き効果を
向上できる。更に、2つのベーパ抜き孔11A,
11Bを従来と略同様の位置において近接させて
あるため、各ベーパ抜き孔11A,11Bにおけ
る燃圧が略同じで、しかも、両者の開口断面積の
和が従来と同じにしてあるので、低温時での燃料
の洩れ量を従来と略同量に抑えることができ、低
温時のポンプ効率は損なわれない。 According to this configuration, by providing the vapor extraction holes 11A and 11B with smaller diameters than in the past, interference between the vapors is reduced compared to the conventional one, and the vapor cannot be discharged through the vapor extraction hole 11A on the upstream side. Since the vapor can be discharged from the vapor extraction hole 11B on the downstream side, the vapor extraction effect can be improved. Furthermore, two vapor extraction holes 11A,
11B are placed close to each other in substantially the same position as in the past, the fuel pressure in each vapor vent hole 11A and 11B is substantially the same, and the sum of the cross-sectional areas of both openings is the same as in the past. The amount of fuel leaked can be suppressed to approximately the same amount as before, and pump efficiency at low temperatures is not impaired.
第2図に本実施例と従来例とのベーパ抜きの効
果の比較を示し、図中の各直線より上方がベーパ
抜きが良好に行われる領域を示す。 FIG. 2 shows a comparison of the vapor removal effects of this embodiment and the conventional example, and the area above each straight line in the figure shows the region where vapor removal is performed well.
これによれば、同一のポンプ内圧では本実施例
(鎖線で示す)の方が従来例(実線で示す)に比
べてベーパ抜き効果の良好な領域がより高温側に
ずれていることから、ベーパ抜き効果が向上して
いることが明らかである。 According to this, at the same pump internal pressure, the region where the vapor removal effect is better in this embodiment (indicated by the chain line) is shifted to the higher temperature side compared to the conventional example (indicated by the solid line), so the vapor removal effect is shifted to the higher temperature side. It is clear that the punching effect is improved.
<発明の効果>
以上述べたように本発明によれば、低温時のポ
ンプ効率を損なうことなく、高温時のベーパ抜き
作用を向上でき、高温時の吐出流量特性を向上で
きる。<Effects of the Invention> As described above, according to the present invention, the vapor removal action at high temperatures can be improved without impairing the pump efficiency at low temperatures, and the discharge flow rate characteristics at high temperatures can be improved.
第1図は本発明の一実施例の要部断面図、第2
図は同上実施例と従来例とのベーパ抜きの効果を
比較する図、第3図は従来例を示すタービン型燃
料ポンプの断面図(第4図の−断面図)、第
4図は第3図の−断面図を示す。
1……ポンプハウジング、4……インペラ、5
……吸込口、6……燃料流路、7……吐出口、1
1A,11B……ベーパ抜き孔。
Fig. 1 is a sectional view of a main part of an embodiment of the present invention, Fig.
The figure is a diagram comparing the effect of vapor removal between the above embodiment and the conventional example, Fig. 3 is a cross-sectional view of a turbine-type fuel pump showing the conventional example (-cross-sectional view of Fig. 4), A cross-sectional view of the figure is shown. 1... Pump housing, 4... Impeller, 5
...Suction port, 6...Fuel flow path, 7...Discharge port, 1
1A, 11B...Vapor extraction hole.
Claims (1)
き孔を有するタービン型燃料ポンプにおいて、前
記ベーパ抜き孔を、前記燃料流路に沿つて近接配
置する複数の孔の集合体で構成したことを特徴と
するタービン型燃料ポンプ。1. In a turbine-type fuel pump having a vapor vent hole in the fuel flow path from the suction port to the discharge port, the vapor vent hole is configured as an aggregate of a plurality of holes arranged close to each other along the fuel flow path. Features a turbine-type fuel pump.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP26568686A JPS63120889A (en) | 1986-11-10 | 1986-11-10 | Turbine type fuel pump |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP26568686A JPS63120889A (en) | 1986-11-10 | 1986-11-10 | Turbine type fuel pump |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS63120889A JPS63120889A (en) | 1988-05-25 |
JPH0474558B2 true JPH0474558B2 (en) | 1992-11-26 |
Family
ID=17420593
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP26568686A Granted JPS63120889A (en) | 1986-11-10 | 1986-11-10 | Turbine type fuel pump |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS63120889A (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS63160387U (en) * | 1987-04-08 | 1988-10-20 | ||
JPS63160388U (en) * | 1987-04-08 | 1988-10-20 | ||
JPH0734226Y2 (en) * | 1989-02-10 | 1995-08-02 | 愛三工業株式会社 | Cascade type fuel supply pump |
-
1986
- 1986-11-10 JP JP26568686A patent/JPS63120889A/en active Granted
Also Published As
Publication number | Publication date |
---|---|
JPS63120889A (en) | 1988-05-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0605184B1 (en) | Turbocharger having reduced noise emissions | |
US4508492A (en) | Motor driven fuel pump | |
US5680700A (en) | Regenerative fuel pump | |
JPH0151910B2 (en) | ||
JP7099625B2 (en) | Turbine housing and turbocharger | |
US4478550A (en) | Pump apparatus | |
US11359642B2 (en) | Electric compressor | |
JPS63105296A (en) | Turbine type fuel pump | |
JPH0474558B2 (en) | ||
US6942447B2 (en) | Impeller pumps | |
US6283704B1 (en) | Circumferential flow type liquid pump | |
JPH064034Y2 (en) | Tarbooger | |
JPH05180189A (en) | Scroll pump | |
JPH0874791A (en) | Centrifugal compressor | |
CN210660222U (en) | Nozzle ring positioning and sealing structure of mixed flow turbocharger | |
JP2626303B2 (en) | Circular flow liquid pump | |
JP3542477B2 (en) | Fuel pump | |
JPS585429A (en) | Exhaust turbine supercharger | |
JPS6021504Y2 (en) | Power distribution cap for engine ignition | |
JPH09112270A (en) | Engine cooling device | |
JPH0431660A (en) | Circumferential flow type liquid pump | |
JPS6012892Y2 (en) | exhaust turbo supercharger | |
JPH061736U (en) | Turbocharger structure | |
JPH075270Y2 (en) | Vane air pump | |
JPH053755Y2 (en) |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
LAPS | Cancellation because of no payment of annual fees |