1. Field of the Invention
The present invention relates to the field of fuel injectors and fuel injection systems.
2. Prior Art
Fuel injector performance, particularly in diesel engines, has a substantial influence in overall engine performance, especially with respect to emissions. Of particular importance is the speed at which fuel injection can be terminated. In particular, if fuel injection is terminated merely by the reduction in injection pressure it is difficult to rapidly terminate injection because of the compressability of the fuel and actuation fluid in an intensifier type fuel injector, resulting in a trail off in atomization resulting in unacceptable levels of unburned fuel in the exhaust. Accordingly various types of direct needle control have been proposed to provide injection control other than by controlling injection pressure.
Also fuel injectors, particularly diesel fuel injectors, are using ever increasing injection pressures, now going as high as 3000 bar (45,000 psi). Diesel fuel has a compressibility of approximately 1% per 67 bar (1000 psi), so that at the injection pressure, the fuel has been substantially compressed. In intensifier type fuel injectors, injection occurs directly as a result of intensification, so that injection begins on intensification and terminates on termination of intensification. Consequently the volume of fuel intensified is set equal to the maximum injection volume needed, plus of course some overhead volume for the needle chamber, passageways to the needle chamber, etc. At a partial power setting for the engine, much less than the maximum injection volume is needed, yet the full amount is compressed and then depressurized, losing the energy required for the compression of the fuel not injected, which at low power settings and at idle, can be most of the substantial amount of energy used for intensification. In fuel injectors having direct needle control, the operation is a bit different, in that intensification occurs, then injection by the direct needle control, then termination of injection, again by direct needle control, and then depressurization to refill the intensification chamber for the next cycle. While this cycle is a bit different, the losses of intensification energy are not different.
Injectors using direct needle control to control injection of fuel supplied to the injector at injection pressure are also known. These injection systems are more efficient because fuel, once compressed, is sooner or later all injected regardless of the engine power setting. They also have the advantage of not cycling the fuel pressure in the needle chamber on each injection event, helping reduce, but not eliminate, the possibility of eventual injector tip breakage. However such systems have serious drawbacks. Aside from the safety issues of having a rail at injection pressures and the associated plumbing problems, there is a serious risk to the engine, in that if an injection tip breaks off, a direct and continuous flow path from the high pressure rail to the combustion chamber is provided, which could result in a hydraulic lock of the engine with catastrophic results.
In the description to follow, the phrase injection event refers to a complete injection event, which may comprise sub-events, such as, by way of one example, a pre-injection, followed by a main injection, either as a single main injection, or a series of smaller injections. An injection event may begin at any time after the end of a combustion cycle (power stroke) and will end before the end of the next combustion cycle (power stroke). Thus successive injection events in an engine operating in a two stroke or two cycle mode will occur each engine crankshaft rotation (each 360 degrees of crankshaft rotation), while successive injection events in an engine operating in a four stroke or four cycle mode will occur each pair of engine crankshaft rotations (each 720 degrees of crankshaft rotation).
First referring to
A second smaller spool valve generally indicated by the numeral 40 is coupled to the side of the injector for direct needle control. In a preferred embodiment, spool valve 40 is a three-way magnetically latching spool valve, magnetically latching on actuation, and releasing for spring return on receipt of a small reverse current, though other types of valves, including other spool valves may be used if desired. In the embodiment disclosed, the valve either couples actuation fluid pressure in line 42 to line 44 when actuated, or alternatively, blocks the flow of actuation fluid in line 42 and couples line 44 to a low pressure vent 46 when the spool is released. Through the three-way valve 40, pressure in line 44 controllably pressurizes the region under piston 48, which in turn controls actuator pin 24. The area above piston 48 is permanently coupled to the source of actuation fluid under pressure, and accordingly is always pressurized when the engine is running. For piston 48 and the intensifier, the actuation fluid is preferably engine oil, though some other actuation fluid may be used, such as fuel.
In operation, with the area under piston 48 vented, spring 22 and actuation fluid pressure above piston 48 will hold the needle closed, even against intensified fuel pressure in the needle chamber. When injection is to occur, needle control valve 40 is actuated to couple actuation fluid pressure to the region below piston 48, which pressure balances the piston, allowing intensified fuel pressure in the needle chamber to force the needle open against spring 22. Of course at the end of injection, the needle control valve 40 is released, to again vent the area under piston 48 to allow actuation fluid pressure over piston 48 to force the needle closed. Of course the needle control valve 40 may be operated more than once, first to provide a pre-injection, followed by a second injection, or even to provide pulsed injections.
Of particular importance to the present invention are the large storage volumes 50, also shown in the cross section of
Alternatively, a sensor such as a Hall effect sensor may be used to sense when the intensifier reaches or approaches the limit of its travel to trigger intensifier recycling, regardless of whether injection is occurring or not, or between injection events. As a further alternative, the intensifier may have a displacement less than the volume of fuel injected during an injection event at maximum engine power, and be operated multiple times between and during an injection event at maximum power.
The present invention provides all the advantages and eliminates the disadvantages of a fuel rail at high injection pressures. In that regard, preferably the total storage volume, intensifier plus storage in porting and storage 50, is less than that that would cause a hydraulic lock in the engine cylinder is dumped into the cylinder on breakage of the injector tip. Also, the storage volume should not be so large as to jeopardize the structural integrity of the injector. Of course, while one exemplary form of direct needle control has been disclosed for purposes of setting the environment for the present invention, substantially any form of direct needle control may be used. Also while the check valve 54 is shown as a ball valve, other forms of check valves may also be used.
The exemplary embodiment of injector disclosed herein also uses intensifier actuation fluid for direct needle control. Alternatively, intensified fuel pressure may be used for direct needle control. This is not preferred however, because of the valving difficulties at the intensified pressure. Of course, substantially any method of direct needle control may be used with the present invention, as it is the combination of direct needle control, however done, together with the ability to store fuel at the intensified pressure, that provides the performance and efficiency characteristics of the present invention.
Now referring to
In the embodiment of
The operation of the embodiment of
The preferred method of operating the present invention is to operate the intensifier throughout the full duration of the injection event, recycling the intensifier only between injection events. This has the advantages of maintaining the highest pressure, and a uniform pressure, throughout the injection event, providing maximum atomization and repeatability in the injector operation.
Thus one aspect of the present invention is that it can very substantially reduce the energy loss of prior art intensifier type fuel injectors and methods of operation thereof by using (injecting) all or substantially all the fuel at the intensified pressure before intensifying another fuel charge. This may allow a single intensification for use over multiple injection events (injection over multiple combustion cycles), particularly at low engine power settings, where depressurizing (de-intensifying) and re-intensification a large part of the intensified fuel not used in an injection event is particularly wasteful of the quite substantial energy used for intensification.
While certain preferred embodiments of the present invention have been disclosed and described herein for purposes of illustration and not for purposes of limitation, it will be understood by those skilled in the art that various changes in form and detail may be made therein without departing from the spirit and scope of the invention.
This application is a divisional of U.S. patent application Ser. No. 12/502,827 filed Jul. 14, 2009 which claims the benefit of U.S. Provisional Patent Application No. 61/080,955 filed Jul. 15, 2008, U.S. Provisional Patent Application No. 61/101,925 filed Oct. 1, 2008 and U.S. Provisional Patent Application No. 61/145,874 filed Jan. 20, 2009.
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Number | Date | Country | |
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20130075498 A1 | Mar 2013 | US |
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61080955 | Jul 2008 | US | |
61101925 | Oct 2008 | US | |
61145874 | Jan 2009 | US |
Number | Date | Country | |
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Parent | 12502827 | Jul 2009 | US |
Child | 13683044 | US |