This application is a continuation of U.S. application Ser. No. 15/186,327, filed Jun. 17, 2016, which is a continuation of U.S. application Ser. No. 14/720,042, filed May 22, 2015, now U.S. Pat. No. 9,394,870, which is a continuation of U.S. application Ser. No. 14/303,499, filed Jun. 12, 2014, now U.S. Pat. No. 9,068,541, which claims priority to U.S. patent application Ser. No. 13/024,641, filed Feb. 10, 2011, now U.S. Pat. No. 8,752,528, all of which are hereby incorporated by reference in their entirety.
The present invention relates to a fuel injection device for supplying fuel by injecting it into the intake path of an engine, and specifically relates to a fuel injection device that is provided with a priming pump for loading fuel into the fuel passage leading to the injector during engine start-up, and that is further provided with a fuel return path for returning the gas and excess fuel accumulated in the interior to the fuel tank.
Fuel injection devices that pressurize and supply fuel by injecting it into the intake passage of an engine are well known, as described, for example, in Japanese Patent Publication No. 2001-193610. As shown in
Thus, with this fuel injection device 3B, the fuel return passage 39 extends from the constant-pressure chamber 33B and is connected to the fuel return line 6 that extends to the fuel tank. In addition, a priming pump 34B is provided medially along the fuel return passage 39, so that the air accumulated in the high-pressure fuel passage 37, including the constant-pressure chamber 33B, is discharged manually to the fuel tank at the time of engine start-up, allowing fuel to be introduced all the way up to the solenoid valve 32, and the vapor or excess fuel accumulated in the constant-pressure chamber 33B to be returned to the fuel tank via the fuel return passage 39 at the time of engine operation.
However, with the fuel injection device 3B and other conventional fuel injection devices, the fuel return passage 39 is positioned below the constant-pressure chamber 33B, as shown in the drawing, producing a structure in which the air that has low specific gravity and accumulates at the top is difficult to remove completely. In addition, the vapor that has been generated by the heat of engine operation is also likely to accumulate at the top in a similar manner, which tends to create a situation in which discharge is difficult.
When driving is stopped after engine operation, the fuel tank is heated by the residual heat of the engine, and the fuel inside tends to reach high pressure. To allow the priming pump 34B to operate adequately in response to this high pressure, the spring pressure of a check valve is commonly set high, making it difficult to sufficiently discharge the accumulated vapor with the discharge pressure generated by the fuel pump 31.
The problem thus arises that the air, vapor, or other gas accumulated in the high-pressure fuel passage 37 of the fuel injection device 3B causes pressure fluctuation in the device, impedes the outflow of fuel during discharge, and hence has a variety of adverse effects on engine performance during the period in which the gas is discharged from the solenoid valve 32 to the intake passage 10.
The preset invention is intended to resolve the types of problems described above, and is aimed at providing a fuel injection device for injecting and supplying fuel into the intake passage of an engine, wherein the gas that has accumulated in the device can be smoothly discharged from the device.
The present invention provides a fuel injection device comprising a fuel pump for pressurizing fuel, a solenoid valve for injecting pressurized fuel into the intake passage of an engine, a high-pressure fuel passage that extends from the fuel pump to the solenoid valve and has a medially positioned constant-pressure chamber for adjusting the fuel to a predetermined pressure, and a fuel return passage connected to a fuel return pipe, with the fuel return passage extending from the constant-pressure chamber and having a medially positioned priming pump, wherein the constant-pressure chamber is configured so that the top wall in the upper space thereof is disposed above the opening of the high-pressure fuel passage opposite from the solenoid valve, the fuel return passage opens into the upper space at a position above the opening of the high-pressure fuel passage, and the gas accumulating in the constant-pressure chamber is discharged from the upper space toward the fuel tank via the fuel return passage.
The constant-pressure chamber, which is the area where air or vapor tends to accumulate, is thus configured so that the fuel return passage opens into the upper space at a position above (higher than) the opening of the high-pressure fuel passage opposite from the solenoid valve. A gas that has low specific gravity and accumulates in the upper space of the constant-pressure chamber can flow unassisted into the fuel return passage, and the air or vapor can therefore be efficiently discharged.
According to another aspect of the fuel injection device, the constant-pressure chamber is configured so that the displacement surface of a diaphragm that constitutes pressure adjustment means has a lateral orientation, a vertical space is formed so that the width in a vertical direction is greater than the width in a diaphragm displacement direction perpendicular to the direction of gravity, the high-pressure fuel passage extending from the fuel pump is connected to a lower part of the space, the high-pressure fuel passage opposite from the solenoid valve opens into the space, and the fuel return passage extends from an upper part of the space. As a result, liquid fuel and gas such as air or vapor tend to separate one above the other, and the gas can be efficiently discharged.
According to yet another aspect of the fuel injection device, the priming pump has two laterally connected check valves disposed at a predetermined distance from each other in a medial portion of the fuel return passage, and further has cup-shaped suction/push-out means made of an elastic material for covering the open sides of the two check valves and forming a pump chamber; a bypass channel is formed between the two check valves; a nonreturn valve is provided for restricting passage of a fluid in the bypass channel only in the fuel return direction; the nonreturn valve is closed to block passage of the fluid when the priming pump is used; and the nonreturn valve is opened to allow passage of the fluid during fuel return or gas discharge, thereby producing a device in which discharge of excess fuel or gas is facilitated when the priming pump is not in use, and in which intake of fuel is facilitated when the priming pump is in use.
According to still another aspect of the fuel injection device, an external profile is formed as a substantially rectangular parallelepiped; the fuel pump is disposed inwardly with respect to the bottom surface of the substantially rectangular parallelepiped so that the diaphragm is parallel to the bottom surface; and the constant-pressure chamber is disposed inwardly with respect to one side surface of the substantially rectangular parallelepiped so that the diaphragm is parallel to the side surface. As a result, each of the functional parts is arranged in an efficient manner without being bulky, contributing to overall compactness.
In accordance with the present invention, in which the air inside the constant-pressure chamber is discharged from an upper space that faces the solenoid valve and is disposed above (higher than) the opening of the high-pressure fuel passage, gas that has accumulated in the device can be smoothly discharged.
Embodiments of the invention are described below in reference to the drawings. In the present invention, the upward and downward directions indicate directions corresponding to the direction of gravitational force in the typical state of use of the equipment in which the engine is mounted. In addition, the terms “upper space” and “lower space” denote upper and lower spaces relative to the vertically middle position in a predetermined space under typical conditions of use.
In reference to
In addition, a fuel return passage 38 extends from the constant-pressure chamber 33A and connects to a fuel return pipe 6 so that excess fuel is returned to the fuel tank 2. Two check valves 341, 342 are connected at a designated distance medially on the side of the fuel return passage 38, and a cup-shaped member 343 made of an elastic resin is affixed as suction/push-out means so as to cover the space on the side surface to which the valve openings are exposed to form a priming pump 34A.
In this embodiment, the constant-pressure chamber 33A is formed so that the top wall of the upper space of the chamber is positioned above (higher than) the opening of the high-pressure fuel passage 36 opposite from the solenoid valve 32, and the opening of the fuel return passage 39 is disposed in the upper space at a location that is above (higher than) the opening of the high-pressure fuel passage 36, so that the air, vapor, or other gas accumulated in the constant-pressure chamber 33A is discharged from the upper space towards the fuel tank 2 via the fuel return passage 38.
When, in order to cease high-speed rotation, an accelerator (not illustrated) is released and the throttle lever 7 is returned to the original idle position, the throttle shaft 5 fixed to the throttle lever 7 rotates towards the closed direction due to the urging force of the urging device 6, returning to the original idle position. In this embodiment, a damping member 8 having frictional force is in contact with the throttle shaft 5 in a state of being pressed against the shaft, so that the return to the idle position occurs slowly over time rather than suddenly, as in conventional examples.
In this embodiment, the constant-pressure chamber 33A is configured so that the displacement surface of the pressure-adjusting diaphragm of the chamber faces to the side; a vertical space is formed so that the width of the space in the vertical direction is greater than the width of the space in the displacement direction; and the disk is placed upright so that the top surface faces sideways. In addition, the fuel return passage 38 extends from a location in the vicinity of the top wall in the upper space; the high-pressure fuel passage 36 that extends from the fuel pump 2 is connected at a location in the vicinity of the bottom wall in the lower space; and the high-pressure fuel passage 36 opens towards the solenoid valve 32 slightly above the passage.
With this configuration, the air, vapor, or other gas that has low specific gravity and accumulates in the upper space of the vertically elongated constant-pressure chamber 33A, which extends parallel to the direction of gravity, is readily separated in the vertical direction from the liquid fuel, and is smoothly discharged from the fuel return passage 38 that opens in the vicinity of the top wall of the upper space. On the other hand, the high-pressure fuel passage 36 opposite from the solenoid valve 32 opens into the lower space at a position away from the opening of the fuel return passage 38, allowing optimal engine performance to be maintained because the gas does not readily flow towards the solenoid valve 32.
The fuel return passage 38 is used both to discharge air, vapor, or other gases, and to allow the excess fuel that has been discharged from the fuel pump 31 to be returned to the fuel tank 2. In a conventional fuel injection device, however, the fuel in the fuel tank is pressurized by high temperatures after the engine is stopped. To overcome this shortcoming, the spring pressure of the check valve of the medially disposed priming pump 34A is set high, and considerable resistance is created to the passage of materials through this section, impeding the flow of excess fuel and the discharge of gas.
In this embodiment, two check valves 341, 342 are connected at a designated distance from each other on the side of the fuel return passage 38; a bypass passage is left between the two check valves 341, 342; and a non-return valve 35 is disposed in this portion to prevent passage of fluid only in the fuel return direction. The discharged fuel will thereby be prevented from flowing backwards while being admitted into the pump in an efficient manner, when the priming pump 34A is used during engine start-up. The excess fuel or air will be caused to bypass the priming pump 34A and to flow via the nonreturn valve 35 in a smooth manner during times other than engine startup.
In this embodiment, the fuel injection device 3A has a substantially rectangular parallelepiped external shape, the fuel pump 31 is provided with a diaphragm on the inside of the bottom surface parallel to the bottom surface, and the constant-pressure chamber 33A is provided with a diaphragm parallel to the side surf ace and inward of one side surface thereof. Consequently, the respective required functional parts are arranged in the fuel injection device in an efficient manner without being bulky, and overall compactness is achieved.
As described above, the present invention provides a fuel injection device for injecting and supplying fuel to the intake passage of an engine. Gas that has accumulated in the device can be smoothly discharged, the supplied fuel can be kept at a stable pressure and flow rate during engine operation, and optimal engine performance can be maintained.
1 Engine
2 Fuel tank
3A Fuel injection device
5 Fuel supply pipe
6 Fuel return pipe
10 Intake passage
31 Fuel pump
32 Solenoid valve
33A Constant-pressure chamber
34A Primping pump
35 Non-return valve
36 High-pressure fuel passage
38 Fuel return passage
341, 342 Check valves
Number | Date | Country | Kind |
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2010-031583 | Feb 2010 | JP | national |
Number | Date | Country | |
---|---|---|---|
Parent | 15186327 | Jun 2016 | US |
Child | 15811257 | US | |
Parent | 14720042 | May 2015 | US |
Child | 15186327 | US | |
Parent | 14303499 | Jun 2014 | US |
Child | 14720042 | US | |
Parent | 13024641 | Feb 2011 | US |
Child | 14303499 | US |