This application claims priority of Korean Application No. 10-2003-0019344, filed on Mar. 28, 2003.
The present invention relates to a fuel drain structure in a fuel line, and more particularly to a drain structure for draining fuel from the line when the engine stops running.
In general, when an engine stops running and fuel provided from a fuel pump remains in a fuel line, the fuel tends to flow into the engine via an injector due to pressure increased by high temperature around the engine, which contributes to air pollution by excessive incomplete combustion when the engine gets re-started.
Embodiments of the present invention provide a fuel drain structure in a fuel line for effectively draining the fuel leftover in the fuel line when the engine ceases moving, thereby preventing the fuel from leaking into a combustion chamber via an injector and thus reducing incomplete combustion of the fuel when the engine is re-started.
In one embodiment of the present invention, a fuel drain structure in a fuel line comprises a regulator adjusting pressure of fuel pumped out from a fuel pump to a fuel line, wherein the regulator includes a housing forming a chamber by coupling with a valve seat. A fuel inlet is at one side of the chamber while a fuel outlet is formed at the valve seat. A valve is resiliently supported via a spring at an upper side of the valve seat. A bypass channel connects a fuel influx passage and a fuel efflux passage of the regulator, such that the fuel leftover inside the fuel line is forced to flow into the fuel tank through the bypass channel while the engine stops running.
For a better understanding of the nature and objects of the present invention, reference should be made to the following detailed description with the accompanying drawings, in which:
A preferred embodiment of the present invention will now be described in detail with reference to the accompanying drawings.
As shown in
With reference to
The valve 36 resiliently supported by a spring 37 is secured at an upper side of the valve seat 33. When pressure of the fuel applied to the fuel inlet 34 is higher than the resilient force of the spring 37, the valve 36 ascends, and the fuel starts to pass through the fuel outlet 35.
A bypass channel 40 traverses the influx and efflux passages of the regulator 30. The bypass channel 40 may be an independent pipe or integrally formed with the housing 31. By way of reference, the bypass channel is preferably about b 0.3 mm in diameter.
The cross-sectional view of the inlet side of the bypass channel 40 is funnel-shaped, and the inlet of the bypass channel 40 has a larger diameter than the outlet. A rotary valve 50 having a sectoral-spool shape in its cross-sectional view is mounted at the inlet side of the bypass channel 40. The rotary valve 50 operates in response to an actuator 62 activated by an electronic control unit (ECU) 60. The ECU may comprise a processor and other associated hardware and software or firmware as may be selected and programmed by a person of ordinary skill in the art based on the teachings set forth herein.
The rotary valve 50 is activated by the actuator 62 in the embodiment of the present invention, however, the operational means may be an actuator, a rotational force of a motor or the like. The ECU 60 renders the rotary valve 50 to be closed when the engine is started, and be opened when the engine is stopped in motion.
The operation of the present invention will now be described.
Once the engine starts to move, the fuel pumped out from the fuel pump is delivered into the feed line 21 through the opened fuel-stopping solenoid valve 14, and is injected via the injector 16 into the engine at a preset pressure. Fuel not injected through the injector returns to the fuel tank 11.
When the engine stops its motion, some of the fuel still remains in the fuel line without being injected through the injector 16.
The ECU 60, therefore, detects whether the engine ceases running, and if so, stops the activation of the fuel pump 12, and closes the fuel-stopping solenoid valve 14. The ECU 60 further rotates the rotary valve 50 to an open side for leading the fuel rested between the fuel-stopping solenoid valve 14 and the regulator 30 of the fuel line to be discharged through the bypass channel 40.
The fuel remaining in the fuel line returns to the fuel tank 11 through the bypass channel 40, such that the fuel is not injected into the engine 10 via the injector 16 due to the temperature and pressure being increased by heat around the engine.
As apparent from the foregoing, there is an advantage in the fuel drain structure in a fuel line in that the fuel inlet side and fuel outlet side of the regulator is connected by the bypass channel being opened and closed via the rotary valve, resulting to prevent the fuel remaining in the fuel line from entering the engine through the injector when the engine stops its operation, thus reducing pollution in the course of re-starting the engine.
Number | Date | Country | Kind |
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10-2003-0019344 | Mar 2003 | KR | national |
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60-222550 | Nov 1985 | JP |
Number | Date | Country | |
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20040187849 A1 | Sep 2004 | US |