JPH022940Y2 - - Google Patents

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Publication number
JPH022940Y2
JPH022940Y2 JP1983133942U JP13394283U JPH022940Y2 JP H022940 Y2 JPH022940 Y2 JP H022940Y2 JP 1983133942 U JP1983133942 U JP 1983133942U JP 13394283 U JP13394283 U JP 13394283U JP H022940 Y2 JPH022940 Y2 JP H022940Y2
Authority
JP
Japan
Prior art keywords
fuel
tank
pipe
flow path
fuel pump
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
Application number
JP1983133942U
Other languages
Japanese (ja)
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JPS6039765U (en
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
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Priority to JP13394283U priority Critical patent/JPS6039765U/en
Publication of JPS6039765U publication Critical patent/JPS6039765U/en
Application granted granted Critical
Publication of JPH022940Y2 publication Critical patent/JPH022940Y2/ja
Granted legal-status Critical Current

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Description

【考案の詳細な説明】 (産業上の利用分野) この考案は自動車等の車輌に搭載される燃料タ
ンクからガソリン、軽油等の燃料を汲み出す燃料
ポンプの燃料吸込み機構に関し、詳しくはタービ
ン式の燃料ポンプの燃料吸込機構に関する。
[Detailed description of the invention] (Field of industrial application) This invention relates to a fuel suction mechanism for a fuel pump that pumps fuel such as gasoline or diesel oil from a fuel tank mounted on a vehicle such as an automobile. This invention relates to a fuel suction mechanism for a fuel pump.

(従来技術) 一搬に、この種の機構において燃料ポンプに接
続されて燃料タンク内の燃料液中に延出する燃料
吸込パイプは円管により形成されており、このよ
うな燃料吸込パイプの吸込口は燃料タンクの無効
燃料残量を最少とするため、燃料タンクの最下底
面に近接し、かつ例えば坂路走行時のように燃料
タンク底面と燃料液面との並行性が失なわれて燃
料が燃料タンク内で前方もしくは後方に片寄つた
状態となるのを考慮して液位が最も変動しない位
置(以下液位変動最少位置という)で開口させる
のが望ましい。このため通常では、燃料吸込パイ
プを燃料ポンプ接続部から燃料タンク底面近傍に
至り一旦下方へ延出させ、次いでそこから屈曲さ
せて燃料タンク底面とほぼ平行に上記液位変動最
少位置まで至らしめ、吸込口を開口させる構成が
採用されている。
(Prior art) In this type of mechanism, the fuel suction pipe that is connected to the fuel pump and extends into the fuel liquid in the fuel tank is formed of a circular pipe. In order to minimize the amount of inactive fuel remaining in the fuel tank, the opening is located close to the lowest bottom of the fuel tank, and when driving on a slope, for example, the parallelism between the bottom of the fuel tank and the fuel liquid level is lost and the fuel is removed. It is desirable to open at a position where the liquid level changes the least (hereinafter referred to as the position of minimum liquid level fluctuation), considering that the liquid level may be biased towards the front or rear in the fuel tank. For this reason, normally, the fuel suction pipe is extended downward from the fuel pump connection part to near the bottom of the fuel tank, and then bent from there until it reaches the above-mentioned minimum level fluctuation position almost parallel to the bottom of the fuel tank. A configuration in which the suction port is opened is adopted.

(考案が解決しようとする課題) 上記構成において、燃料タンクの無効燃料残量
を少なくする、すなわち有効容量を増大させるに
は燃料タンク底面とほぼ平行な燃料吸込パイプの
延出管部の吸込口を燃料タンクの底面になるべく
近い位置で開口させることが考えられるが、近づ
け過ぎた場合には延出管部が燃料タンク底面に接
触してこれを擦傷し、メツキが剥がれて腐蝕を生
ずる原因となるため延出管部を燃料タンクの底面
に近づけることによる無効燃料残量の減少には限
度が有つた。
(Problem to be solved by the invention) In the above configuration, in order to reduce the remaining amount of inactive fuel in the fuel tank, that is, to increase the effective capacity, the suction port of the extending pipe portion of the fuel suction pipe is approximately parallel to the bottom surface of the fuel tank. It is possible to open the pipe as close to the bottom of the fuel tank as possible, but if it is opened too close, the extending pipe may come into contact with the bottom of the fuel tank and scratch it, causing the plating to peel off and cause corrosion. Therefore, there is a limit to the reduction in the remaining amount of ineffective fuel by bringing the extension pipe closer to the bottom of the fuel tank.

このため、さらに無効燃料残量の減少化を図る
には延出管部の管径を小さくしてその吸込口の位
置を低くすることが考えられるが、この場合には
所要の燃料取出し量が確保できなくなる欠点が有
つた。
Therefore, in order to further reduce the remaining amount of ineffective fuel, it is possible to reduce the diameter of the extension pipe and lower the position of its suction port, but in this case, the required amount of fuel to be taken out is There was a drawback that it could not be secured.

さらに、上記のようなタービン式の燃料ポンプ
ではポンプ内の流路の出口部分の燃料の脈動によ
り第3図に示すようにインペラ羽根枚数×インペ
ラ回転数で決定される周波数(KHz)で縦軸に示
す音圧(dB(A))の音を発生する。この音はイン
ペラ1次の音と称されるもので、このようなイン
ペラ1次の音は燃料ポンプの本体から燃料吸込パ
イプに伝達され、あるいはポンプ内の流路を逆に
辿つて燃料吸込パイプに伝わつて、延出管部内の
反射により振幅を増す、いわゆる“ふえ吹き”現
象により増大することが知られている。なお、自
動車用の燃料ポンプの周波数の範囲は一般に約2
〜6KHzであり、図中の一次周波数P(約3.8KHz)
で音圧が特に高くなり、ふえ吹き現象により増幅
されてキーンという耳障りな音を発生する。
Furthermore, in the above-mentioned turbine-type fuel pump, due to the pulsation of the fuel at the outlet of the flow path inside the pump, the vertical axis changes at a frequency (KHz) determined by the number of impeller blades x impeller rotation speed, as shown in Figure 3. Generates sound with the sound pressure (dB(A)) shown in . This sound is called the first-order sound of the impeller, and the first-order sound of the impeller is transmitted from the main body of the fuel pump to the fuel suction pipe, or reversely follows the flow path inside the pump and enters the fuel suction pipe. It is known that the amplitude increases due to the so-called "blowing" phenomenon, which increases the amplitude due to reflection within the extending pipe section. Furthermore, the frequency range of automobile fuel pumps is generally approximately 2
~6KHz, and the primary frequency P in the figure (approximately 3.8KHz)
The sound pressure becomes particularly high and is amplified by the blow-up phenomenon, producing a harsh, harsh sound.

このようなふえ吹き現象は上記従来技術のもの
のように延出管部の流路の断面形状を円形すなわ
ち縦横比を1/1としたものでは所要とする流路
断面積等との関係でその共鳴周波数が上記インペ
ラ一次の音の周波数とがほぼ等しくなり、特に大
きな騒音を発することとなつていた。
Such a blow-out phenomenon occurs when the cross-sectional shape of the flow path of the extending pipe section is circular, that is, the aspect ratio is set to 1/1, as in the conventional technology described above, due to the relationship with the required cross-sectional area of the flow path, etc. The resonant frequency was almost equal to the frequency of the first-order sound of the impeller, resulting in particularly loud noise.

(課題を解決するための手段) 上記従来技術の欠点に鑑み、本考案の燃料ポン
プの燃料吸込機構は、自動車等の車輌に搭載され
る燃料タンクから先端部を吸込口を備えたほぼ水
平方向の延出管部を有する燃料吸込パイプを介し
て燃料を汲み出すタービン式の燃料ポンプの燃料
吸込機構であつて、前記燃料吸込パイプの前記延
出管部の内部の流路の断面形状をその縦横比が
1/3〜1/6となるように設定して構成され
る。
(Means for Solving the Problems) In view of the drawbacks of the prior art described above, the fuel suction mechanism of the fuel pump of the present invention has a substantially horizontal direction with a suction port extending from the tip of the fuel tank mounted on a vehicle such as an automobile. A fuel suction mechanism for a turbine-type fuel pump that pumps fuel through a fuel suction pipe having an extending pipe portion, wherein the cross-sectional shape of the flow path inside the extending pipe portion of the fuel suction pipe is The aspect ratio is set to be 1/3 to 1/6.

(作用) 本考案の燃料吸込機構は延出管部の内部の流路
の断面形状をその縦横比が1/3〜1/6となる
ように設定したので、流路の断面形状が横長とな
り、延出管部の下面と燃料タンクの底部との間の
距離を相互に接触を生じない適宜距離を保ち、か
つ流路の断面積を燃料ポンプの吐出量に応じた所
定の値に維持した状態で、延出管部の流路の上面
により規定される無効燃料高さを低くすることが
できる。また、縦横比を1/3〜1/6に設定し
たことにより、延出管部の共鳴周波数がインペラ
1自の音の周波数よりずれ、このため延出管部に
伝わるインペラ1次の音のふえ吹き現象による増
大が制御される。
(Function) In the fuel suction mechanism of the present invention, the cross-sectional shape of the flow path inside the extending pipe section is set so that its aspect ratio is 1/3 to 1/6, so the cross-sectional shape of the flow path becomes horizontally long. , the distance between the lower surface of the extending pipe section and the bottom of the fuel tank is maintained at an appropriate distance that does not cause mutual contact, and the cross-sectional area of the flow path is maintained at a predetermined value depending on the discharge amount of the fuel pump. In this state, the height of the dead fuel defined by the upper surface of the flow path of the extending pipe portion can be reduced. In addition, by setting the aspect ratio to 1/3 to 1/6, the resonant frequency of the extending pipe section is shifted from the frequency of the impeller's own sound, which causes the impeller's primary sound to be transmitted to the extending pipe section. Increase due to blow-up phenomenon is controlled.

(実施例) 次にこの考案の一実施例を図面に従つて説明す
る。
(Example) Next, an example of this invention will be described with reference to the drawings.

第1図において、1は略円筒状のタービン式の
燃料ポンプでメインタンクT(図は下底板Taのみ
を示す。)の内部にブラケツト2を介して取り付
けられており、このブラケツト2はメインタンク
Tの図示しない天井壁部に固定されている。ここ
で燃料ポンプ1はその中心軸がメインタンクTの
下底板Taに対しほぼ垂直をなし、またそのほぼ
下半部が、メインタンクTの下底板Ta上に底壁
Saを固定された上部開口状のサブタンクS内に
突出状態とされている。なお、サブタンクSの側
壁SbにはメインタンクTに連通する通路(図示
しない)が設けられており、平地での車輌停止時
における燃料Fの液面LはサブタンクSの底壁
Saとほぼ平行、すなわちメインタンクTの下底
板Taとほぼ平行になつている。3は一端を燃料
ポンプ1の上部の吐出口1aに接続された燃料供
給パイプで、他端は図示しない燃料噴射ノズル等
へ接続されている。4,5は燃料ポンプ1に通電
するための外部配線接続端子である。6は一端を
燃料ポンプ1の下部の吸入口1bに接続されてサ
ブタンクS内すなわちメインタンクT内の燃料F
を吸込むための燃料吸込パイプで、その吸込口6
aには筒状の燃料フイルタ7がこれを覆うように
取り付けられており、以下これらの構成を更に詳
しく説明する。
In Fig. 1, reference numeral 1 denotes a substantially cylindrical turbine-type fuel pump, which is installed inside the main tank T (only the bottom plate Ta is shown in the figure) via a bracket 2. It is fixed to the ceiling wall (not shown) of T. Here, the central axis of the fuel pump 1 is substantially perpendicular to the bottom plate Ta of the main tank T, and the bottom half of the fuel pump 1 is substantially perpendicular to the bottom plate Ta of the main tank T.
The tank Sa projects into a sub-tank S with an opening at the top. Note that the side wall Sb of the sub-tank S is provided with a passage (not shown) that communicates with the main tank T, and the liquid level L of the fuel F when the vehicle is stopped on level ground is equal to the bottom wall of the sub-tank S.
It is almost parallel to Sa, that is, it is almost parallel to the bottom plate Ta of the main tank T. Reference numeral 3 denotes a fuel supply pipe whose one end is connected to the discharge port 1a at the upper part of the fuel pump 1, and the other end is connected to a fuel injection nozzle (not shown) or the like. 4 and 5 are external wiring connection terminals for supplying electricity to the fuel pump 1. 6 has one end connected to the intake port 1b at the lower part of the fuel pump 1, and is connected to the fuel F in the sub tank S, that is, the main tank T.
It is a fuel suction pipe for sucking in fuel, and its suction port 6
A cylindrical fuel filter 7 is attached to cover a, and the structure thereof will be explained in more detail below.

燃料吸込パイプ6は燃料ポンプ1の吸込口1b
との接続部を構成する円筒状の接続管部6Aと、
この接続管部6Aの下端からほぼ直角状に屈曲形
成されてサブタンクSの底壁Saと平行すなわち
メインタンクTの下底板Taと平行に延出する、
断面が横長の長方形状角筒よりなる、延出管部6
Bとを有している。ここで、延出管部6Bの下底
面の高さH1はサブタンクSの底壁Saとの接触
を防止しうる程度の最も小さな寸法に設定されて
おり、また、端部の吸込口6aは液位変動最小一
で開口している。一方、燃料フイルタ7は上記吸
込口6aが内部のほぼ中央下底部に位置するよう
延出管部6Bを覆つて取り付けられており、中心
軸は延出管部6Bと平行をなしている。またここ
で、燃料フイルタ7の燃料ポンプ1に近い側の端
板7aは第2図に示すように延出管部6Bと一体
に形成されている。
The fuel suction pipe 6 is the suction port 1b of the fuel pump 1
A cylindrical connecting pipe portion 6A constituting a connecting portion with the
The connecting pipe portion 6A is bent at a substantially right angle from the lower end thereof and extends parallel to the bottom wall Sa of the sub-tank S, that is, parallel to the lower bottom plate Ta of the main tank T.
Extended pipe section 6 consisting of a rectangular square tube with a horizontally long cross section
It has B. Here, the height H1 of the lower bottom surface of the extension pipe portion 6B is set to the smallest dimension that can prevent contact with the bottom wall Sa of the sub-tank S, and the suction port 6a at the end is It opens with minimum positional fluctuation. On the other hand, the fuel filter 7 is attached so as to cover the extending pipe part 6B so that the suction port 6a is located at the lower bottom in the substantially central part of the fuel filter 7, and the central axis thereof is parallel to the extending pipe part 6B. Further, the end plate 7a of the fuel filter 7 on the side closer to the fuel pump 1 is formed integrally with the extending pipe portion 6B as shown in FIG.

さらに、燃料吸込パイプ6の延出管部6Bの内
部の流路Cの形状について説明すれば、第2図に
おいて、流路Cの高さ寸法eと幅寸法fの比は
1:3〜1:6に設定されており、流路面積は燃
料ポンプ1の所要燃料取出量を確保するに十分な
値に設定される。なお第1図中H2はサブタンク
Sの底壁Saから流路Cの上面までの高さを示し、
この高さ以下の燃料Fが燃料ポンプ1により汲み
出し得ずに残存することとなる。
Furthermore, to explain the shape of the flow path C inside the extending pipe portion 6B of the fuel suction pipe 6, in FIG. :6, and the flow path area is set to a value sufficient to ensure the required amount of fuel taken out by the fuel pump 1. In addition, H2 in FIG. 1 indicates the height from the bottom wall Sa of the sub-tank S to the top surface of the flow path C.
Fuel F below this height cannot be pumped out by the fuel pump 1 and remains.

次に上記実施例の作用効果に関し説明する。外
部配線接続端子4,5を介して燃料ポンプ1に通
電すると、サブタンクS内すなわちメインタンク
T内の燃料Fは燃料フイルタ7により濾過された
後燃料吸込パイプ6を介して燃料ポンプ1内部に
吸い込まれ、さらに燃料供給パイプ3を経て図示
しない燃料噴射ノズル等に供給される。このよう
な燃料Fの給出が行なわれるにつれ、サブタンク
S内の燃料液面Lも徐々に下降するわけであるが
液位が高さH2に達すると、液面Lとメインタン
クTの下底板Taが平行状態の場合、燃料ポンプ
1による燃料Fの吸込が不可能となり、高さH2
以下の燃料Fが無効燃料として残存する。ここで
燃料吸込パイプ6の延出管部6Bは横長の四角形
状とされているので、燃料吸込パイプを通常の円
筒状とした場合に比して同一流量面積で流路Cの
上面位置を低く設定でき、従つて無効燃料残量を
少なくすることができる。
Next, the effects of the above embodiment will be explained. When the fuel pump 1 is energized via the external wiring connection terminals 4 and 5, the fuel F in the sub-tank S, that is, the main tank T, is filtered by the fuel filter 7 and then sucked into the fuel pump 1 via the fuel suction pipe 6. The fuel is further supplied to a fuel injection nozzle (not shown) through the fuel supply pipe 3. As fuel F is supplied in this way, the fuel level L in the sub-tank S also gradually falls, but when the liquid level reaches the height H2, the liquid level L and the bottom plate of the main tank T drop. When Ta is parallel, it becomes impossible for the fuel pump 1 to suck in the fuel F, and the height H2
The following fuel F remains as invalid fuel. Here, since the extending pipe portion 6B of the fuel suction pipe 6 has a horizontally long rectangular shape, the upper surface position of the flow path C is lowered at the same flow area compared to when the fuel suction pipe is made into a normal cylindrical shape. can be set, and therefore the remaining amount of ineffective fuel can be reduced.

さらに、流路Cの高さ寸法eと幅寸法fの比を
1:3〜1:6に設定したことにより同一断面積
の流路であつても騒音の発生を低減できる。この
ような効果を上記「考案が解決しようとする課
題」の欄で説明したインペラ1次の音の延出管部
におけるふえ吹き現象による増大に関連して説明
すると、第4図には第3図中Pで示した周波数の
インペラ1次の音を発生する燃料ポンプ1の延出
管部6における発生音の音圧の変化をe/fの変
化に関連して示してあり、同図中〇は流路Cの断
面積が100mm2の場合、×は流路Cの断面積が200mm2
の場合のプロツトである。図示のようにe/fを
1/3〜1/6の範囲に設定することにより共鳴
周波数がインペラ一次の音の周波数からずれ、こ
のためふえ吹き現象が抑制されて顕著な騒音低減
効果を得ることができる。なおe/f=1は従来
の円管状の延出管部を有する燃料吸込機構の場合
に相当する。また、このような騒音低減効果は図
中では音圧が特に高い周波数P(約3.8KHz)に関
してのみ示したが、e/fを1/3〜1/6の範
囲に設定することによる騒音低減効果は一般の自
動車用の燃料ポンプのインペラ1次の音の周波数
である約2〜6KHzの範囲で得られるものである。
Furthermore, by setting the ratio of the height dimension e to the width dimension f of the channel C to 1:3 to 1:6, noise generation can be reduced even if the channels have the same cross-sectional area. To explain this effect in relation to the increase in the impeller's primary sound due to the blowout phenomenon in the extension pipe section, which was explained in the section "Problems to be solved by the invention," FIG. Changes in the sound pressure of the sound generated in the extension pipe section 6 of the fuel pump 1, which generates the impeller primary sound of the frequency indicated by P in the figure, are shown in relation to changes in e/f. 〇 indicates that the cross-sectional area of channel C is 100 mm 2 , × indicates that the cross-sectional area of channel C is 200 mm 2
This is the plot for the case. As shown in the figure, by setting e/f in the range of 1/3 to 1/6, the resonant frequency deviates from the frequency of the impeller's primary sound, thereby suppressing the blowing phenomenon and achieving a remarkable noise reduction effect. be able to. Note that e/f=1 corresponds to the case of a conventional fuel suction mechanism having a cylindrical extending pipe portion. In addition, although this noise reduction effect is shown only for the frequency P (approximately 3.8 KHz) where the sound pressure is particularly high in the figure, noise reduction by setting e/f in the range of 1/3 to 1/6 The effect is obtained in the range of approximately 2 to 6 kHz, which is the frequency of the primary sound of the impeller of a general automobile fuel pump.

すなわち本実施例の燃料吸込機構では延出管部
6の流路Cの断面形状をe/f=1/3〜1/6
に設定したことにより、インペラ1次のふえ吹き
現象による増大が抑制され、騒音低減を果すこと
ができる。
That is, in the fuel suction mechanism of this embodiment, the cross-sectional shape of the flow path C of the extending pipe portion 6 is set to e/f=1/3 to 1/6.
By setting it to , the increase due to the blowing phenomenon of the primary impeller is suppressed, and noise reduction can be achieved.

なお、以上の実施例において燃料吸込パイプの
延出管部は断面が横長の長方形状角筒としたが、
断面形状は四角形に限らず、例えば長円形のよう
に長軸を有する形状であればいかなる形状であつ
てもよい。
In addition, in the above embodiment, the extension pipe part of the fuel suction pipe was a rectangular square tube with a horizontally long cross section.
The cross-sectional shape is not limited to a square, but may be any shape as long as it has a long axis, such as an oval.

(効果) 以上のように、この考案は、タービン式の燃料
ポンプの燃料吸込機構において、燃料吸込パイプ
の延出管部の内部の流路の断面形状を、その縦横
比が1/3〜1/6としたことにより、延出管部
の下面と燃料タンクの底部との間の距離および流
路の断面積を所定の値に維持した状態で、延出管
部の流路の上面により規定される無効燃料高さを
低くすることができるので、燃料タンクの無効燃
料残量の減少すなわち有効容量の増加を図ること
ができ、さらには上記のような流路の形状設定に
より燃料ポンプ騒音の減少をも図りうるという効
果がある。
(Effects) As described above, in the fuel suction mechanism of a turbine-type fuel pump, the cross-sectional shape of the flow path inside the extending pipe portion of the fuel suction pipe has an aspect ratio of 1/3 to 1. /6, the distance between the lower surface of the extending pipe and the bottom of the fuel tank and the cross-sectional area of the flow path are maintained at predetermined values, and the distance defined by the upper surface of the flow path of the extending pipe is maintained at predetermined values. Since the height of the idle fuel that is generated can be lowered, the remaining amount of idle fuel in the fuel tank can be reduced, that is, the effective capacity can be increased.Furthermore, by setting the shape of the flow path as described above, fuel pump noise can be reduced. This has the effect of reducing the amount of water used.

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

図はこの考案の一実施例を示すもので、第1図
は燃料ポンプの燃料吸込機構を示す部分断面正面
図、第2図は第1図の−線に沿う断面図、第
3図はタービン式燃料ポンプのパワースペクトラ
ム、第4図は燃料吸込パイプの延出管部の流路の
断面の高さと幅の比とインペラ一次の音圧との関
係を示す特性線図である。 1…燃料ポンプ、6…燃料吸込パイプ、6B…
延出管部、7…燃料フイルタ、T…メインタン
ク、S…サブタンク、F…燃料、C…流路。
The figures show one embodiment of this invention. Figure 1 is a partially sectional front view showing the fuel suction mechanism of the fuel pump, Figure 2 is a sectional view taken along the - line in Figure 1, and Figure 3 is a turbine. FIG. 4 is a characteristic diagram showing the relationship between the height and width ratio of the cross section of the extending pipe portion of the fuel suction pipe and the primary sound pressure of the impeller. 1...Fuel pump, 6...Fuel suction pipe, 6B...
Extension pipe section, 7...Fuel filter, T...Main tank, S...Sub tank, F...Fuel, C...Flow path.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 自動車等の車輌に搭載される燃料タンクから先
端部を吸込口を備えたほぼ水平方向の延出管部を
有する燃料吸込パイプを介して燃料を汲み出すタ
ービン式の燃料ポンプの燃料吸込機構であつて、
前記燃料吸込パイプの前記延出管部の内部の流路
の断面形状をその縦横比が1/3〜1/6となる
ように設定したことを特徴とする燃料ポンプの燃
料吸込機構。
A fuel suction mechanism for a turbine-type fuel pump that pumps fuel from a fuel tank mounted on a vehicle such as an automobile through a fuel suction pipe having a substantially horizontally extending pipe section with a suction port at its tip. hand,
A fuel suction mechanism for a fuel pump, characterized in that a cross-sectional shape of a flow path inside the extending pipe portion of the fuel suction pipe is set such that an aspect ratio thereof is 1/3 to 1/6.
JP13394283U 1983-08-29 1983-08-29 Fuel pump fuel suction mechanism Granted JPS6039765U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13394283U JPS6039765U (en) 1983-08-29 1983-08-29 Fuel pump fuel suction mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13394283U JPS6039765U (en) 1983-08-29 1983-08-29 Fuel pump fuel suction mechanism

Publications (2)

Publication Number Publication Date
JPS6039765U JPS6039765U (en) 1985-03-19
JPH022940Y2 true JPH022940Y2 (en) 1990-01-24

Family

ID=30301966

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13394283U Granted JPS6039765U (en) 1983-08-29 1983-08-29 Fuel pump fuel suction mechanism

Country Status (1)

Country Link
JP (1) JPS6039765U (en)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS612292Y2 (en) * 1981-03-11 1986-01-24

Also Published As

Publication number Publication date
JPS6039765U (en) 1985-03-19

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