Method and apparatus for conditioning liquid hydrocarbon fuels

Information

  • Patent Grant
  • 8702420
  • Patent Number
    8,702,420
  • Date Filed
    Thursday, December 8, 2005
    18 years ago
  • Date Issued
    Tuesday, April 22, 2014
    10 years ago
Abstract
In one embodiment of a method for vaporizing liquids such as fuels, the liquid is sprayed into a chamber such that the spray does not impinge on any surface. The energy for vaporization is supplied through the injection of a hot diluent such as nitrogen or oxygen depleted air. Additional heat is added through the surface. In another embodiment, the liquid is sprayed onto a hot surface using a geometry such that the entire spray is intercepted by the surface. Heat is added through the surface to maintain an internal surface temperature above the boiling point of the least volatile component of the liquid. The liquid droplets impinging on the surface are thus flash vaporized. A carrier gas may also be flowed through the vaporizer to control the dew point of the resultant vapor phase mixture.
Description
BACKGROUND INFORMATION

Low emissions from combustion devices are obtained by burning a lean mixture of fuel and air obtained by pre-mixing gaseous fuel and air. Dry Low NOx (DLN) technology gas turbines, for example, typically burn natural gas under lean, pre-mixed conditions. Liquid fuels, by contrast, are typically burned by injecting a fuel spray directly into the combustor. This results in a diffusion flame in which the fuel is burned in a locally stoichiometric fuel/air mixture and causes high emissions. Under certain conditions, burning a liquid fuel is more desirable than burning a gaseous fuel. However, it would be desirable to avoid the high emissions associated with diffusion flames when burning such liquid fuels.


SUMMARY

A method and apparatus for conditioning liquid fuels at a location external to a combustion device so that the resulting vapor phase fuel may be pre-mixed with air and burned under lean conditions, thus achieving low emissions, is described herein. Preferably, the liquid fuel is conditioned such that it may be used in a combustor configured for natural gas without modification to the combustor/fuel metering system. In one embodiment, the liquid fuel is sprayed into a vaporization chamber such that the spray does not impinge on any surface. The energy for vaporization is supplied through the injection of a hot diluent such as nitrogen or oxygen depleted air. Additional heat is added through the surface of the chamber to prevent heat loss and to maintain an internal surface temperature above the boiling point of the least volatile component of the liquid. The diluent gas also serves to control the dew point of the resultant vapor phase mixture. Additional heating to augment the vaporization process in the event that the diluent flow or temperature fall below the minimum levels needed for complete vaporization is supplied by internal heaters.


In another embodiment, the liquid fuel is sprayed onto a hot surface using a geometry such that the entire spray is intercepted by the surface. Heat is added through the surface to maintain an internal surface temperature above the boiling point of the least volatile component of the liquid fuel. The liquid droplets impinging on the surface are thus flash vaporized such that there is no build up of bulk liquid or a liquid film in the vaporizer. A carrier gas, such as nitrogen or air, may also be flowed through the vaporizer to control the dew point of the resultant vapor phase mixture. In some embodiments, a fuel nozzle is mounted at one end (the enclosed end) of a cylindrical chamber. The nozzle forms a hollow cone type spray with a spray angle chosen such that all of the spray impinges on the cylinder surface (in other embodiments a solid cone type spray nozzle is used). The preferred orientation is vertical, with the spray downward, so that the impingement of the spray on the walls is even. Two or more such chambers can be joined to a common manifold to accommodate higher capacities.





BRIEF DESCRIPTION OF THE FIGURES

The features and advantages of the present invention will become more apparent from the detailed description set forth below when taken in conjunction with the drawings in which like reference numbers indicate identical or functionally similar elements.



FIG. 1 is a schematic drawing of a fuel vaporizer according to a first embodiment of the invention.



FIG. 2 is a schematic drawing of a single nozzle vaporizer according to a second embodiment of the invention.



FIG. 3 is a schematic drawing of a plurality of the vaporizers of FIG. 2 joined to a common manifold according to a third embodiment of the invention.



FIG. 4 is a block diagram showing electrical components of the fuel vaporizer of FIG. 1.



FIG. 5 illustrates a cross sectional view of the spray pattern of the single nozzle vaporizer of FIG. 2.



FIG. 6
a illustrates an embodiment in which a preheater is used to preheat a liquid fuel supply.



FIG. 6
b illustrates an embodiment in which a preheater is used to preheat a diluent gas supply.





DETAILED DESCRIPTION

Various embodiments of methods and apparatuses for conditioning liquid fuels are discussed below. Specific details are set forth in order to provide a thorough understanding of the present invention. The specific embodiments described below should not be understood to limit the invention. Additionally, for ease of understanding, certain method steps are delineated as separate steps. These steps should not be understood as necessarily distinct or order-dependent in their performance unless so indicated.


The complete disclosure of U.S. patent application Ser. No. 10/682,408, which was filed Oct. 10, 2003 (now U.S. Pat. No. 7,089,745), and which describes methods and devices for vaporizing, mixing, and delivering liquid fuels or liquefied gases which have been pre-vaporized with a reduced oxygen content air stream for use in combustion devices, is fully incorporated herein by reference. In addition, U.S. Patent Application Ser. No. 60/535,716, filed Jan. 12, 2004, and 11/033,180, filed Jan. 12, 2005 (now U.S. Pat. No. 7,435,080), which disclose systems and methods for flame stabilization and control, are both also fully incorporated herein by reference.


In some embodiments of a method and apparatus for conditioning liquids, such as hydrocarbon fuels, the liquid is sprayed into a chamber such that the spray does not impinge on any surface. The energy for vaporization is supplied through the injection of a hot diluent such as nitrogen or oxygen depleted air. Additional heat is added through the surface to prevent heat loss and to maintain an internal surface temperature above the boiling point of the least volatile component of the liquid. The diluent gas also serves to control the dew point of the resultant vapor phase mixture. Additional heating to augment the vaporization process in the event that the diluent flow or temperature fall below the minimum levels needed for complete vaporization is supplied by internal heaters. One application of the invention is the vaporization of liquid fuels, such as kerosene and heating oil, for introduction into a combustion device, such as a gas turbine. Pre-vaporizing the fuel in this manner allows the operation of the gas turbine in the lean, premixed mode, resulting in extremely low pollutant emissions.



FIG. 1 illustrates a fuel conditioner 100 according to such an embodiment of the invention. The fuel conditioner 100 includes a cylindrical vaporization chamber 110. Liquid fuel is sprayed into the chamber 110 through nozzles 120 mounted on the sidewall 112 of the chamber 110. The nozzles 120 are pressure atomizing spray nozzles in some embodiments. In other embodiments, the nozzles 120 may be two-fluid nozzles (such as filming or “air” blast type nozzles), in which case the diluent (or carrier) gas may enter the chamber 110 through such two-fluid nozzles. In an alternative embodiment, the nozzles are mounted on a manifold which runs parallel to the axis of the cylindrical chamber and which gets installed from an end of the chamber.


In some embodiments, the sidewall and/or end wall of the chamber 110 are heated. In some embodiments, heating tape or heat tracing (MI cable) (not shown in FIG. 1) is used to heat the sidewall and/or end wall. As discussed above, the heating of the sidewall and/or end wall of the chamber 110 serves to prevent heat loss and maintain an internal surface temperature above that of the boiling point for least volatile component of the liquid fuel.


In the embodiment of FIG. 1, the nozzles 120 are arranged in rings spaced around the circumference of the cylinder, with each column of nozzles 120 supplied by one of a plurality of manifolds 130. Diluent gas is supplied through an inlet 140 that is in fluid communication with a plenum 150 formed by a space between the top end wall 160 of the chamber 110 and a perforated plate 160. The diluent gas enters the interior of the chamber 110 through perforations in the plate 160. The diluent gas is preferably a gas that has less oxygen than ambient air, such as nitrogen, steam, methane, oxygen depleted air, or exhaust gas from a combustion device. The diluent gas is preferably heated to at least the boiling point of the liquid such that the diluent gas supplies the heat required for vaporization of the liquid fuels entering the chamber 110 through the nozzles 120. As discussed above, the diluent gas also serves to lower the dew point of the vapor phase mixture. Lowering the dew point temperature is desirable so that downstream components, such as the line connecting the vaporizer to the combustion device, can be maintained at a temperature lower than that required for the initial vaporization. The use of an inert carrier gas can also serve to limit chemical reaction in the conditioner 100 and transfer lines connecting the conditioner 100 to a combustor, thus suppressing coking. Vaporized fuel exits the chamber through one or more exit ports 170 for transport to the combustion device.


In alternative embodiments, the diluent gas is introduced into the chamber 110 through nozzles arranged on the sidewall of the chamber 110 and positioned, for example, between the nozzles 120 and or on one of the end walls of the chamber 110. Depending on the location and method in which the diluent gas is introduced into the chamber 110, the diluent gas may be introduced in a co-flow arrangement, a counter-flow arrangement, and/or at various angles in order to, for example, induce a swirling flow inside the chamber 110.


Referring now back to FIG. 1, an optional spool section 180 is attached to the chamber 110 in some embodiments. The length of the spool section 180 is chosen to increase the vaporizer residence time so that it is sufficient for complete evaporation of the fuel droplets. The spool section 180 preferably has a plurality of heating elements 190 disposed therein (two concentric rings of heating elements 190 are illustrated in FIG. 1). The heating elements 190 preferably extend the length of the spool section 180, and may be electrical bayonet heaters, heat exchange tubes, or any other type of heating element. In some embodiments, each heating element 190a-n is provided with a separate temperature control 401a-n as shown in FIG. 4.


The spool section 180 also includes one or more exit ports 182, similar to those of the chamber 110, through which vaporized liquid may exit the spool section 182. A drain 186 passes through the end cap 184 of the spool section 180 to allow any unvaporized liquids to be removed from the conditioner 100.


The spool section 180 may include a particulate collection device (not shown in FIG. 1) in some embodiments. The particulate collection device controls particulate or droplet carryover exiting the conditioner 100. Possible particulate control devices include mist eliminators, cyclones, and filter elements.


In some embodiments, a preheater (not shown in FIG. 1) is used to pre-heat the liquid prior to entry into the chamber 110. This lowers the amount of heat needed to vaporize the liquid in the chamber 110. Preheating also lowers the viscosity of the liquid, which improves the quality of the spray produced by the nozzles 120.


It should be understood that the number of nozzles 120, the length of the chamber 110 and the spool section 180 can be modified to suit desired operating conditions (e.g., volume of fuel needed, type of liquid fuel to be conditioned, etc.). Thus, the design illustrated in FIG. 1 is easily scalable for a variety of operating conditions.


In the embodiments discussed above in connection with FIG. 1, the liquid fuel does not impinge on any interior surface. In other embodiments, such as those illustrated in FIGS. 2 and 3, the liquid fuel does impinge on interior surfaces of a vaporization chamber. In such embodiments, the energy for vaporization is supplied by heat transfer through the walls of the vaporization chamber. The essential design feature of a fuel conditioner operating in this manner is the match of the heat transfer rate through the walls to the heat required to vaporize the liquid. This is achieved by matching the surface area used for vaporization with the liquid flow rate and the achievable heat flow through the walls. Since the heat requirement is different in different sections of the vaporizer, the heat input may be staged with separate temperature control for each stage.



FIG. 2 is a schematic drawing of a single nozzle vaporizer 200 according to a second embodiment of the invention. Liquid fuel is sprayed into the vaporizer 200 through a nozzle 210 mounted on the end flange 220. A carrier gas such as nitrogen or air, which is preferably pre-heated to supply some of the heat required for vaporization, is also introduced through ports 230 on the end flange 220. As with the embodiment of FIG. 1, the use of a carrier gas serves two purposes: 1) to aid in removing the vapor from vaporizing chamber, and 2) to lower the dew point temperature of the vapor. Lowering the dew point temperature is desirable so that downstream components, such as the line connecting the vaporizer to a combustion device, can be maintained at a temperature lower than that required for the initial vaporization. The use of an inert carrier gas can also serve to limit chemical reaction in the vaporizer and transfer lines, thus suppressing coking. There are many possible ways to introduce the carrier gas such as, but not limited to: in each vaporizer module, in the main body of the vaporizer, in an axial direction, and in a tangential direction to induce swirl. In the vaporizer 200, the carrier gas is injected tangentially at two ports 230 to induce a swirling co-flow.


The resulting spray from the nozzle that impinges on the interior cylindrical surface 240 of the vaporizer 200, and is evaporated due to heat input through the surface and from the hot carrier gas. As shown in the cross sectional view 500 of FIG. 5 (not to scale), the nozzle 210 (shown in block form in FIG. 5) preferably forms a hollow cone type spray with a spray angle chosen such that all of the spray impinges on the cylinder surface. The carrier gas nozzles 211 supply the carrier gas in a direction tangential to a direction of the spray from the nozzle 210 to induce a swirling co-flow 270. Referring now back to FIG. 2, the surface 240 is heated by a combination of electrical heating tape 250 and band heaters 260 in this embodiment. In other embodiments, the heat input may be supplied by heat exchange with a hot liquid or gas (such as steam or hot combustion products.



FIG. 3 is a schematic diagram of a fuel conditioning system 300 with multiple single nozzle vaporization units 200. In order to maintain the optimum surface area to volume ratio for spray vaporization, additional capacity is obtained by grouping multiple vaporizer “legs” onto a common manifold 310. The body of the manifold 310 is also heated, in this case with heating tape 350. A rupture disc 370 is mounted on one end of the manifold 310 for safety. Vapor exits the other end of the manifold 310.


As discussed above, a preheater is used to preheat the liquid fuel prior to entry into the chamber of the vaporizer in some embodiments. An example is shown in FIG. 6a, which illustrates a preheater 610a that accepts liquid fuel and preheats it. The preheated liquid fuel is then fed from the preheater 610 to a vaporizer 620 in accordance with one of the embodiments discussed above. Shown in FIG. 6b is a preheater 610b that preheats the diluent gas as discussed above.


Several embodiments of fuel conditioning devices have been discussed above. Numerous other modifications and variations of the present invention are possible in light of the above teachings. It is therefore to be understood that within the scope of the appended claims, the invention may be practiced otherwise than as specifically described herein.

Claims
  • 1. A fuel conditioning unit comprising: a cylindrical vaporization chamber, the cylindrical vaporization chamber comprising a sidewall and an end wall;a plurality of nozzles mounted along the sidewall and in fluid communication with a liquid fuel supply, the nozzles being configured to spray liquid fuel radially inward into the chamber;at least one diluent gas port in fluid communication with the chamber, the diluent gas port being in fluid communication with a supply of heated diluent gas, the diluent gas port being configured to introduce the diluent gas into the chamber;at least one exit port in fluid communication with the chamber, the exit port providing a path for vaporized liquid fuel to exit the chamber;wherein the heated diluent gas supplies a least a portion of the heat required for vaporization of the liquid fuel, and wherein a mixture of the diluent gas and vaporized liquid fuel has an oxygen content below the limiting oxygen index and has a lower dew point than that of the liquid fuel in the absence of the diluent gas; anda spool section attached to a portion of the sidewall opposite the end wall such that the spool section forms an extension of the chamber, the spool section having a heating element disposed therein, the heating element supplying additional heat to vaporize any liquid fuel not vaporized in the portion of the chamber corresponding to the sidewall, the spool section having at least one additional exit port through which any fuel vaporized in the spool section may exit the fuel conditioning unit.
  • 2. The fuel conditioning unit of claim 1, wherein the at least one diluent gas port comprises a plurality of diluent gas ports formed in a perforated plate located within the chamber, the perforated plate, the end wall and a portion of the sidewall forming a plenum in fluid communication with the plurality of diluent gas ports and the supply of heated diluent gas.
  • 3. The fuel conditioning unit of claim 1, wherein the spool section has a plurality of heating elements disposed therein.
  • 4. The fuel conditioning unit of claim 3, wherein each of the plurality of heating elements has an individual temperature control.
  • 5. The fuel conditioning unit of claim 1, wherein the heating element has a length equal to a length of the spool section.
  • 6. The fuel conditioning unit of claim 1, wherein at least a portion of the chamber sidewall or the chamber end wall is heated.
  • 7. The fuel conditioning unit of claim 1, wherein the diluent gas is inert.
  • 8. A method for conditioning a liquid fuel comprising the steps of: spraying the liquid fuel into a cylindrical vaporization chamber through a plurality of nozzles mounted on a sidewall of the chamber and in fluid communication with the chamber such that the liquid fuel does not impinge on any wall of the chamber;supplying a heated diluent gas to the vaporization chamber through a plurality of diluent gas ports formed in a perforated plate located within the chamber and in fluid communication with the chamber; andreceiving a conditioned vaporized fuel gas from at least one exit port in fluid communication with the chamber, the conditioned vaporized fuel gas comprising a mixture of the diluent gas and a vaporized form of the liquid fuel, the conditioned vaporized fuel gas having an oxygen content below the limiting oxygen index and a lower dew point than that of the vaporized form of the liquid fuel in the absence of the diluent gas;wherein the perforated plate, at least one end wall of the chamber, and a portion of the side wall of the chamber form a plenum in fluid communication with the plurality of diluent gas ports and the supply of heated diluent gas.
  • 9. The method of claim 8, wherein the chamber has at least one heating element disposed therein to vaporize any liquid fuel not vaporized by the heat supplied by the diluent gas.
  • 10. The method of claim 9, wherein the at least one heating element comprises a plurality of heating elements.
  • 11. The method of claim 10, wherein each of the plurality of heating elements has an individual temperature control.
  • 12. The method of claim 8, further comprising the step of heating at least a portion of a wall of the chamber.
  • 13. The method of claim 8, wherein the diluent gas is inert.
  • 14. A fuel conditioning unit comprising: a vaporization chamber, the vaporization chamber having a sidewall and an end wall;a heating element attached to the sidewall;at least one fuel nozzle mounted on the end wall, the fuel nozzle being in fluid communication with a supply of a liquid fuel consisting essentially of hydrocarbons, the fuel nozzle being configured to produce a spray with a spray angle such that all of the spray impinges on an interior surface of the sidewall; andat least one diluent gas port in fluid communication with the vaporization chamber, the diluent gas port being in fluid communication with a supply of diluent gas;wherein the heating element is configured to heat a portion of the sidewall upon which the spray impinges to a temperature above the boiling point of the least volatile component of liquid fuel and sufficient to flash vaporize the liquid fuel spray as it contacts the sidewall, and the diluent gas and vaporized liquid fuel combine to form a mixture that has a lower dew point than that of the liquid fuel in the absence of the diluent gas; andwherein the fuel conditioning unit is configured such that, the mixture is maintained at a temperature above the dew point of the mixture until the mixture reaches a combustor located downstream of the fuel conditioning unit.
  • 15. The fuel conditioning unit of claim 14, wherein the sidewall is cylindrical and the spray is a conical spray.
  • 16. The fuel conditioning unit of claim 14, further comprising at least one additional heating element, the additional heating element being configured to keep a portion of the vaporization chamber apart from a portion on which the spray impinges at a temperature above a dew point of the mixture of the diluent gas and vaporized liquid fuel.
  • 17. The fuel conditioning unit of claim 14, further comprising a preheater located between the nozzle and the liquid fuel supply, the preheater being configured to heat the liquid fuel to a temperature above ambient temperature and below a boiling point of the liquid fuel.
  • 18. The fuel conditioning unit of claim 14, wherein the diluent gas is inert.
  • 19. A fuel conditioning system comprising: a manifold; anda plurality of fuel conditioning units according to claim 14, each of the fuel conditioning units being attached to the manifold to supply a mixture of diluent gas and vaporized liquid fuel to the manifold.
  • 20. A method for conditioning a liquid fuel comprising the steps of: supplying a liquid fuel consisting essentially of hydrocarbons to a vaporization chamber through a nozzle that produces a spray at an angle such that substantially all of the spray impinges upon a heated surface of a vaporization chamber, the heated surface being at a temperature above the boiling point of the least volatile component of liquid fuel and having sufficient heat to flash vaporize the liquid fuel spray, the heated surface being heated by a heating element located outside of the vaporization chamber;supplying a diluent gas to the vaporization chamber such that the vaporized liquid fuel and the diluent gas form a mixture, said mixture having a lower dew point than that of the vaporized liquid fuel in the absence of the diluent gas; andsupplying the mixture to a combustor located downstream of the vaporization chamber such that the mixture is maintained at a temperature above the dew point of the mixture until the mixture undergoes combustion.
  • 21. The method of claim 20, further comprising the step of preheating the liquid fuel to a temperature above ambient temperature and below a boiling point of the liquid fuel.
  • 22. The method of claim 20, wherein the sidewall is cylindrical and the spray is a conical spray.
  • 23. The method of claim 20, further comprising the step of heating a second portion of the vaporization chamber apart from the portion impinged by the spray, the second portion being heated to a temperature above boiling point of a least volatile component of the liquid fuel.
  • 24. The method of claim 20, wherein the diluent gas is inert.
  • 25. The method of claim 20, wherein the diluent gas is supplied in a direction tangential to a direction of the spray to induce a swirling co-flow.
  • 26. The fuel conditioning unit of claim 1, wherein each of the plurality of nozzles is oriented toward a central axis of the vaporization chamber.
  • 27. The fuel conditioning unit of claim 1, further comprising a combustor in fluid communication with the exit port, wherein the fuel conditioning unit is configured such that the mixture remains at a temperature above the dew point for the mixture until it is combusted in the combustor.
  • 28. The method of claim 8, further comprising the step of maintaining the conditioned vaporized fuel above the dew point until the conditioned vaporized fuel is combusted in a combustor in fluid communication with the exit port.
Parent Case Info

This application claims priority from U.S. provisional patent application Ser. No. 60/634,221 filed Dec. 8, 2004, the content of which is incorporated fully herein by reference.

US Referenced Citations (154)
Number Name Date Kind
163323 Martin May 1875 A
696909 McCormick et al Apr 1902 A
964031 Leahy Jul 1910 A
1544607 Emette Jul 1925 A
1755846 Steed Apr 1930 A
2216178 Anton Oct 1940 A
2256785 Dalen et al. Sep 1941 A
2268603 Linder Jan 1942 A
2354179 Blanc Jul 1944 A
2377342 Holicer Jun 1945 A
2701608 Johnson Feb 1955 A
RE24682 Johnson Aug 1959 E
3229464 Mock Jan 1966 A
3254695 Brodlin Jun 1966 A
3545902 Bailey Dec 1970 A
3564847 Wagner Feb 1971 A
3568934 Dunn Mar 1971 A
3576382 Finnstrand Apr 1971 A
3597134 Bailey Aug 1971 A
3602202 Kobayashi Aug 1971 A
3603711 Downs Sep 1971 A
3788065 Markowski Jan 1974 A
3800533 Zankowski Apr 1974 A
3832985 Edde Sep 1974 A
3840321 Moench Oct 1974 A
3847534 Nomaguchi et al. Nov 1974 A
3866585 Kopa Feb 1975 A
3937008 Markowski et al. Feb 1976 A
3973395 Markowski et al. Aug 1976 A
3986815 Miyahara Oct 1976 A
3990831 Syska Nov 1976 A
4004875 Zink et al. Jan 1977 A
4008041 Roffe et al. Feb 1977 A
4013396 Tenney Mar 1977 A
4019314 Springmann Apr 1977 A
4023538 Harpman et al. May 1977 A
4025282 Reed et al. May 1977 A
4028044 Carlisle Jun 1977 A
4033725 Reed et al. Jul 1977 A
4040403 Rose et al. Aug 1977 A
4045956 Markowski et al. Sep 1977 A
4047880 Caldarelli Sep 1977 A
4058977 Markowski et al. Nov 1977 A
4088437 Holzapfel May 1978 A
4094291 Hamburg Jun 1978 A
4099382 Paull et al. Jul 1978 A
4114566 Harpman et al. Sep 1978 A
4140473 Hoehing et al. Feb 1979 A
4148599 Reed et al. Apr 1979 A
4173254 Paull et al. Nov 1979 A
4212163 Mikina Jul 1980 A
4250704 Bruckner et al. Feb 1981 A
4270506 Lowe Jun 1981 A
4289475 Wall et al. Sep 1981 A
4295821 Schilling Oct 1981 A
4302180 Le Mer Nov 1981 A
4318689 Forster et al. Mar 1982 A
4333735 Hardy et al. Jun 1982 A
4375799 Swanson Mar 1983 A
4399079 Lowe Aug 1983 A
4416613 Barisoff Nov 1983 A
4443180 LeFrois Apr 1984 A
4480986 Nelson et al. Nov 1984 A
4483832 Schirmer Nov 1984 A
4588375 Sandstrom May 1986 A
4606720 Harvey Aug 1986 A
4624631 Kobayashi et al. Nov 1986 A
4646705 Babitzka et al. Mar 1987 A
4659743 Rao et al. Apr 1987 A
4697415 Schiffers Oct 1987 A
4729217 Kehlhofer Mar 1988 A
4784599 Garbo Nov 1988 A
4838029 Gleason et al. Jun 1989 A
4907565 Bailey et al. Mar 1990 A
4909192 Forster et al. Mar 1990 A
4909728 Nakamoto et al. Mar 1990 A
4928015 Butler et al. May 1990 A
5015173 Fullemann et al. May 1991 A
5035227 Hansen Jul 1991 A
5138163 Butler et al. Aug 1992 A
5156002 Mowill Oct 1992 A
5165224 Spadaccini et al. Nov 1992 A
5207053 Spadaccini May 1993 A
5238396 Yap Aug 1993 A
5345756 Jahnke et al. Sep 1994 A
5346391 Fullemann et al. Sep 1994 A
5359847 Pillsbury et al. Nov 1994 A
5377483 Mowill Jan 1995 A
5388395 Scharpf et al. Feb 1995 A
5394686 Child et al. Mar 1995 A
5410869 Muller May 1995 A
5417053 Uji May 1995 A
5459994 Drnevich Oct 1995 A
5464344 Hufton Nov 1995 A
5473882 Zarzalis et al. Dec 1995 A
5481866 Mowill Jan 1996 A
5572861 Shao Nov 1996 A
5713195 Bronicki et al. Feb 1998 A
5740673 Smith et al. Apr 1998 A
5756360 Harvey et al. May 1998 A
5775091 Bannister et al. Jul 1998 A
5794431 Utamura et al. Aug 1998 A
5806298 Klosek et al. Sep 1998 A
5848885 Tanaka et al. Dec 1998 A
5901547 Smith et al. May 1999 A
5979183 Smith et al. Nov 1999 A
6039261 Pavese Mar 2000 A
6067789 Dobbeling et al. May 2000 A
6145294 Traver et al. Nov 2000 A
6167691 Yoshikawa et al. Jan 2001 B1
6170264 Viteri et al. Jan 2001 B1
6174160 Lee et al. Jan 2001 B1
6200128 Kobayashi Mar 2001 B1
6220034 Mowill Apr 2001 B1
6282901 Marin et al. Sep 2001 B1
6341486 Hannermann Jan 2002 B2
6343462 Drnevich et al. Feb 2002 B1
6350116 Herrmann Feb 2002 B1
6408612 Hannermann et al. Jun 2002 B2
6430915 Wiant et al. Aug 2002 B1
6434925 Hannermann et al. Aug 2002 B2
6499991 Usami et al. Dec 2002 B1
6508053 Ha et al. Jan 2003 B1
6579086 Fullemann et al. Jun 2003 B2
6588212 Wallace et al. Jul 2003 B1
6596780 Jahnke et al. Jul 2003 B2
6632085 Suzuki et al. Oct 2003 B1
6718794 Brugerolle et al. Apr 2004 B2
6779333 Gerhold Aug 2004 B2
6910335 Viteri et al. Jun 2005 B2
6923642 Sennoun et al. Aug 2005 B2
6928821 Gerhold Aug 2005 B2
6932594 Weclas et al. Aug 2005 B2
6978619 Blomeyer Dec 2005 B2
7089745 Roby et al. Aug 2006 B2
7322198 Roby et al. Jan 2008 B2
7770396 Roby et al. Aug 2010 B2
7823570 Cracknell et al. Nov 2010 B2
20030131582 Anderson et al. Jul 2003 A1
20040065088 Viteri et al. Apr 2004 A1
20040134194 Roby et al. Jul 2004 A1
20040170936 Weclas et al. Sep 2004 A1
20040177617 Frutschi et al. Sep 2004 A1
20040216465 Sheppard et al. Nov 2004 A1
20040247499 Matsuoka et al. Dec 2004 A1
20060127827 Yoshida et al. Jun 2006 A1
20060149423 Barnicki et al. Jul 2006 A1
20070125091 Roby et al. Jun 2007 A1
20070254966 Eskin et al. Nov 2007 A1
20080115502 Roby et al. May 2008 A1
20090031968 Cracknell et al. Feb 2009 A1
20090084082 Martin et al. Apr 2009 A1
20100300063 Palmer et al. Dec 2010 A1
20100300103 Roby et al. Dec 2010 A1
Foreign Referenced Citations (23)
Number Date Country
1564859 Jan 2005 CN
1726371 Jan 2006 CN
43 26 802 Feb 1995 DE
197 28 151 Jan 1999 DE
100 10 546 Sep 2000 DE
0 575 043 Dec 1994 EP
0 877 156 Nov 1998 EP
56-160515 Dec 1981 JP
58-71987 Apr 1983 JP
62108911 May 1987 JP
63080058 Apr 1988 JP
03168505 Jul 1991 JP
04060307 Feb 1992 JP
06-058508 Mar 1994 JP
06-265146 Sep 1994 JP
11-30423 Feb 1999 JP
11-51312 Feb 1999 JP
2003-226884 Aug 2003 JP
2006-503259 Jan 2006 JP
WO 8803249 May 1988 WO
WO 9008962 Aug 1990 WO
WO 02099334 Dec 2002 WO
WO 2005054657 Jun 2005 WO
Non-Patent Literature Citations (92)
Entry
Malte, Philip C., et al., “The Staged Prevaporizing-Premixing Injector: High Pressure Evaluation”, AGTSR Subaward No. 00-01-SR087, Final Report from the University of Washington, Dec. 2002.
“Summary Health Statistics for U.S. Adults: National Health Interview Survey”, Vital and Health Statistics, Series 10, No. 218, 2001.
Ahrens, Marty, “The U.S. Fire Problem Overview Report Leading Causes and Other Patterns and Trends,”, NFPA, Fire Analysis and Research Division, Jun. 2003.
A.H Lefebvre, “Gas Turbine Comubustion,” Emissions, Thermal Sciences and Propulsion Center School of Mechanical Engineering Purdue University, pp. 487-490, Undated.
Stoffel, et al., “Conversion of Liquid to Gaseous Fuels for Lean Premixed Combustion,” Presented at the International Gas Turbine and Aeroengine Congress and Exposition, Houston, TX, Jun. 5-8, 1995 (10 pages).
Turns, S.R., “An Introduction to Combustion Concepts and Applications,” Second Addition, Chapter I, Propulsion Engineering Research Center and Department of Mechanical and Nuclear Engineering, The Pennsylvania State University, McGraw Hill, pp. 6-8, undated.
Wei, et al., “Experimental Investigation of the Prevaporized Premixed (vpl) Combustion Process for Liquid Fuel Lean Combustion,” Chemical Engineering and Processing, vol. 41, pp. 157-164 (2002).
Abstract of Cowell, et al., “Development of a Dual-Fuel Injection System for Lean Premixed Industrial Gas Turbines,” American Society of Mechanical Engineers, New York, NY, vol. 39, p. 3268 (1996).
Davis, L.B., et al., “Dry Low NOx Combustion Systems for GE Heavy-Duty Gas Turbines,” GE Power Systems, GER-3568G, Oct. 2000 (25 pages).
Abstract of Gillispie, et al., “Effects of Fuel Gas Mixtures on Power Limits in a Dual-Fuel Engine,” Natural Gas and Alternative Fuels for Engines American Society of Mechanical Engineers, Internal Combustion Engine Division, vol. 30, p. 2794 (1994).
Hoffmann, S., et al., “Further Devolopment of the Siemens LPP Hybrid Burner,” ASME-IGTI 98-GT-552, presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Stockholm, Sweden, Jun. 2-5, 1998 (7 pages).
Office Action issued in CA 2,501,862, mailed May 8, 2009.
Office Action issued in MX/a/2007/006899, mailed May 30, 2011.
Partial English translation of Office Action issued in MX/a/2007/006899, mailed May 30, 2011.
International Search Report issued in International Application No. PCT/US2003/32423, mailed Aug. 17, 2004.
International Search Report issued in PCT/US2005/04414, dated Nov. 1, 2006.
Written Opinion issued in PCT/US2005/04414, dated Nov. 1, 2006.
International Preliminary Report on Patentability issued in PCT/US2005/04414, dated Jun. 13, 2007.
Japanese Office Action issued in JP 2005-501180, mailed Jun. 16, 2009.
English translation of Japanese Office Action issued in JP 2005-501180, mailed Jun. 16, 2009.
Enlgish language abstract of JP 11-051312, published Feb. 26, 1999.
Machine Enlgish language translation of JP 11-051312, published Feb. 26, 1999.
English language abstract of JP 56-160515, published Dec. 10, 1981.
Office Action issued in CN 200380105739.9, dated Nov. 17, 2006.
English translation of Chinese Office Action issued in CN 200380105739.9, dated Nov. 17, 2006.
Office Action issued in AU 2003284124, dated Oct. 29, 2008.
Office Action issued in KR 10-2005-7006266, dated Jun. 29, 2007.
English translation of Office Action issued in KR 10-2005-7006266, dated Jun. 29, 2007.
Office Action issued in CN 200710166824.6, dated Jun. 5, 2009.
English translation of Office Action issued in CN 200710166824.6, dated Jun. 5, 2009.
Office Action issued in CN 200710166824.6, dated Jan. 8, 2010.
English translation of Office Action issued in CN 200710166824.6, dated Jan. 8, 2010.
Office Action issued in CN 200710166824.6, dated Nov. 15, 2010.
English translation of Office Action issued in CN 200710166824.6, dated Nov. 15, 2010.
Office Action issued in NZ 539362, dated May 1, 2006.
Office Action issued in CN 200580041555.X, dated Feb. 6, 2009.
English translation of Office Action issued in CN 200580041555.X, dated Feb. 6, 2009.
Office Action issued in CN 200580041555.X, dated Jan. 29, 2010.
English translation of Office Action issued in CN 200580041555.X, dated Jan. 29, 2010.
Office Action issued in CN 200580041555.X, dated Nov. 22, 2010.
English translation of Office Action issued in CN 200580041555.X, dated Nov. 22, 2010.
International Search Report issued in PCT/US2007/067891, mailed Mar. 10, 2008.
Written Opinion issued in PCT/US2007/067891, mailed Mar. 10, 2008.
International Preliminary Report on Patentability issued in PCT/US2007/067891, mailed Nov. 13, 2008.
Office Action issued in MX PA/a/2005/003786, mailed Jun. 4, 2010.
Partial English language translation of Office Action issued in MX PA/a/2005/003786, mailed Jun. 4, 2010.
Office Action issued in AU 2005314037, mailed Dec. 21, 2009.
Office Action issued in NZ 555544, mailed Oct. 7, 2010.
Office Action issued in MY PI 20070934, mailed Jun. 30, 2010.
Office Action issued in CN 200780015985.3, mailed Jun. 15, 2011.
Partial English language translation of Office Action CN 200780015985.3, mailed Jun. 15, 2011.
English language abstract of JP 06-058508, published Mar. 1, 1994.
Machine English language translation of JP 06-058508, published Mar. 1, 1994.
English language abstract of JP 06-265146, published September 20, 1994.
Machine English language translation of JP 06-265146, published Sep. 20, 1994.
English language abstract of JP 11-30423, published Feb. 2, 1999.
Machine English language translation of JP 11-30423, published Feb. 2, 1999.
English langauge abstract of CN 1564859, published Jan. 12, 2005.
English language abstract of JP 03-168505, published Jul. 22, 1991.
English language abstract of JP 04-60307, published Feb. 26, 1992.
English language abstract of JP 63-80058, published Apr. 11, 1988.
English language abstract of JP 62-108911, published May 20, 1987.
U.S. Appl. No. 10/682,408.
U.S. Appl. No. 11/464,441.
U.S. Appl. No. 11/929,675.
Abstract of Stoffel, et al., “Conversion of Liquid to Gaseous Fuels for Lean Premixed Combustion,” Presented at the International Gas Turbine and Aeroengine Congress and Exposition, Houston, TX, Jun. 5-8, 1995 (10 pages).
Abstract of Wei, et al., “Experimental Investigation of the Prevaporized Premixed (vpl) Combustion Process for Liquid Fuel Lean Combustion,” Chemical Engineering and Processing, vol. 41, pp. 157-164 (2002).
Arthur H. Lefebvre, “Gas Turbine Combustion; Second Edition”, Printed by Edward brothers 1998, pp. 57-62.
Supplementary European Search Report issued in EP 03 77 6355, Mailed Aug. 4, 2011.
English language abstract of EP 0 877 156, published Nov. 11, 1998.
English language abstract of DE 100 10 546 published Sep. 7, 2000.
English language abstract of DE 43 26 802 published Feb. 2, 1995.
English language abstract of DE 197 28 151 pubslished Jan. 7, 1999.
U.S. Appl. No. 12/851,379.
Office Action issued in Mexican Application No. MX/a/2007/006899, dated Jan. 10, 2012.
Partial English language translation of Office Action issued in Mexican Application No. MX/a/2007/006899, dated Jan. 10, 2012.
Office Action issued in Chinese Application No. 200780015985.3, dated May 3, 2012.
English language translation Office Action issued in Chinese Application No. 200780015985.3, dated May 3, 2012.
Office Action issued in European Application No. EP 03776355.4, dated Jun. 20, 2012.
Office Action issued in Chinese Application No. 200780015985.3, dated Aug. 23, 2012.
English language translation Office Action issued in Chinese Application No. 200780015985.3, dated Aug. 23, 2012.
Office Action issued in Australian Application No. 2007258113, dated Jan. 17, 2012.
Office Action issued in EP 03 776 335.4 dated Apr. 12, 2013.
Office Action issued in KR 10-2008-7029206 dated May 9, 2013.
English language translation of Office Action issued in KR 10-2008-7029206 dated May 9, 2013.
U.S. Appl. No. 11/742,478.
Office Action issued in Japanese Application No. 2009-510013, dated Dec. 4, 2012.
English language translation Office Action issued in Japanese Application No. 2009-510013, dated Dec. 4, 2012.
English language abstract of JP 2003-226884, published Aug. 15, 2003.
Machine English language translation of JP 2003-226884, published Aug. 15, 2003.
English language abstract of JP 2006-503259, published Jan. 26, 2006.
Machine English language translation of JP 2006-503259, published Jan. 26, 2006.
Related Publications (1)
Number Date Country
20060154189 A1 Jul 2006 US
Provisional Applications (1)
Number Date Country
60634221 Dec 2004 US