This invention generally relates to a fuel injector for a combustion engine. More particularly, this invention relates to a fuel injector that heats fuel to aid the combustion process.
Combustion engine suppliers continually strive to improve emission and combustion performance. One method of improving both emission and combustion performance includes heating or vaporizing fuel before injection into the combustion chamber. Heating the fuel replicates operation of a hot engine, and therefore improves combustion performance. Further, alternate fuels such as ethanol perform poorly in cold conditions, and therefore also benefit from pre-heating of fuel.
Various methods of heating fuel at a fuel injector have been attempted. Such methods include the use of a ceramic heater, or a resistively heated capillary tube within which the fuel passes. These methods require electric power and therefore leads that extend through pressure barriers and walls. Seals required between the wires and pressure barriers are a potential source of fuel leakage and are therefore undesirable. Further, such heat generating devices must be insulated from other fuel injector components and therefore are difficult to implement and support within a fuel injector.
Accordingly, it is desirable to design and develop a method of heating fuel without creating additional fuel leak paths, or insulating structures while still providing for the heating and vaporization of fuel.
An example fuel injector assembly includes a first coil that induces a magnetic field into a second coil that is utilized to heat fuel flowing through the fuel injector.
The example fuel injector includes a primary coil that receives a first signal from a driver to generate a first magnetic field that moves an armature between an open and closed position. A secondary coil is utilized to heat a component in thermal contact with the fuel flow that in turn heats fuel before exiting the fuel injector. The heated fuel exiting the fuel injector assembly is heated to a temperature that substantially vaporizes the liquid fuel to achieve a high level of atomization that in turn improves combustion performance.
The secondary coil generates a second magnetic field generated by a current induced by the first coil into the second coil. The induced current is generated by a second signal that is sent to the first coil in addition to the first signal. The second signal is an alternating current signal that produces a time varying second magnetic field. The frequency of the alternating current that generates the second magnetic field is such that movement of the armature is not induced. The frequency of the alternating current results in a time varying and reversing second magnetic field. The time varying second magnetic field produces a flux flow in the surface of the material that alternates direction to generate heat.
Because no hard leads are required to induce the desired second time varying magnetic field, the second coil can be placed within sealed compartments and still provide the desired inductive heating performance.
These and other features of the present invention can be best understood from the following specification and drawings, the following of which is a brief description.
Referring to
The component in thermal contact with the fuel flow 18 in this example is a portion of the armature 26. The armature 26 includes an armature tube 22 disposed within the fuel flow 18. The armature tube 22 is fabricated from a magnetically active material that responds to a magnetic field. The secondary coil 16 generates the second magnetic field surrounding and interacting with the armature tube 22. The second magnetic field is generated by a current induced by the first coil 14 into the second coil 16. The induced current is generated by a second signal that is sent to the first coil 14 in addition to the first signal. The second signal is an alternating current signal that produces a time varying second magnetic field in the secondary coil 16.
The frequency of the alternating current that generates the second magnetic field is such that movement of the armature 26 is not induced. No movement of the armature 26 is induced because the frequency of the alternating current results in a time varying and reversing second magnetic field. Heat inside the armature tube 22 is generated by hysteretic and eddy-current loses that are induced by the time varying second magnetic field. Although the armature tube 22 temperature is elevated, the secondary coil 16 remains relatively cool and therefore does not require any special thermal insulation accommodations. The amount of heat generated is determined by the specific resistivity of the material of the armature tube 22 and the magnitude of the second magnetic field. The time varying second magnetic field produces a flux flow in the surface of the material that alternates direction to generate heat. The higher the resistivity of the material the better the generation of heat responsive to the second magnetic field. The specific material utilized for the armature tube 22 is selected to provide the desired generation of thermal energy required to elevate and vaporize fuel within the fuel injector assembly 10.
Referring to
The second alternating current 32 directed to the first coil 14 is utilized to induce the second magnetic field in the second coil 16. As appreciated, by providing a desired ratio of windings between the first coil 14 and the second coil 16 a desired magnitude of the second time varying magnetic field is provided. Further, the alternating current signal 32 interposed onto the first direct current signal 30, generates the desired alternating and time varying magnetic field that generates inductive heating of the armature tube 22 within the fuel flow 18.
Referring to
Referring to
Because no hard leads are required to induce the desired second time varying magnetic field, it can be placed within sealed compartments and still provide the desired inductive heating performance. Further, placement of the secondary coil 16 is only limited by the capability of producing a second time varying magnetic field of a desired strength to produce the desired inductive heating to attain the desired level of vaporized fuel.
Although a preferred embodiment of this invention has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this invention. For that reason, the following claims should be studied to determine the true scope and content of this invention.
The application claims priority to U.S. Provisional Application No. 60/784,260 which was filed on Mar. 21, 2006.
Number | Name | Date | Kind |
---|---|---|---|
3601110 | Kamazuka | Aug 1971 | A |
3839906 | Hanson | Oct 1974 | A |
4572436 | Stettner et al. | Feb 1986 | A |
4934907 | Kroner | Jun 1990 | A |
5040497 | Dingle | Aug 1991 | A |
5159915 | Saito et al. | Nov 1992 | A |
5201341 | Saito et al. | Apr 1993 | A |
5487114 | Dinh | Jan 1996 | A |
5550452 | Shirai et al. | Aug 1996 | A |
5758826 | Nines | Jun 1998 | A |
5787857 | Simons | Aug 1998 | A |
5915626 | Awarzamani et al. | Jun 1999 | A |
5959433 | Rohde | Sep 1999 | A |
6109543 | Bright et al. | Aug 2000 | A |
6315217 | Park | Nov 2001 | B1 |
6422481 | Ren et al. | Jul 2002 | B2 |
6550458 | Yamakado et al. | Apr 2003 | B2 |
6561168 | Hokao et al. | May 2003 | B2 |
6578775 | Hokao | Jun 2003 | B2 |
6650128 | Sanders | Nov 2003 | B2 |
6651602 | Hiraku et al. | Nov 2003 | B2 |
6721158 | Heinke | Apr 2004 | B2 |
6728602 | Husted et al. | Apr 2004 | B2 |
20010052553 | Hokao | Dec 2001 | A1 |
20020139872 | Hokao | Oct 2002 | A1 |
20030048254 | Huang | Mar 2003 | A1 |
20030178009 | Pellizzari et al. | Sep 2003 | A1 |
20050258266 | Elia et al. | Nov 2005 | A1 |
20050279867 | Ismailov | Dec 2005 | A1 |
20070200006 | Czimmek | Aug 2007 | A1 |
20070221748 | Hornby et al. | Sep 2007 | A1 |
20070221874 | Hornby et al. | Sep 2007 | A1 |
20070235086 | Hornby et al. | Oct 2007 | A1 |
20070235557 | Hornby et al. | Oct 2007 | A1 |
Number | Date | Country |
---|---|---|
4431189 | Mar 1996 | DE |
10057630 | May 2002 | DE |
2307513 | May 1997 | GB |
05288131 | Nov 1993 | JP |
09264224 | Oct 1997 | JP |
10238424 | Sep 1998 | JP |
2002180919 | Jun 2002 | JP |
2002180919 | Jun 2002 | JP |
Number | Date | Country | |
---|---|---|---|
20070221874 A1 | Sep 2007 | US |
Number | Date | Country | |
---|---|---|---|
60784260 | Mar 2006 | US |