WO2002048610A1 - Dispositif de combustion catalytique avec vaporisation de combustible liquide sur parois chaudes - Google Patents
Dispositif de combustion catalytique avec vaporisation de combustible liquide sur parois chaudes Download PDFInfo
- Publication number
- WO2002048610A1 WO2002048610A1 PCT/FR2001/003850 FR0103850W WO0248610A1 WO 2002048610 A1 WO2002048610 A1 WO 2002048610A1 FR 0103850 W FR0103850 W FR 0103850W WO 0248610 A1 WO0248610 A1 WO 0248610A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- fuel
- zone
- combustion
- wall
- hot
- Prior art date
Links
- 239000000446 fuel Substances 0.000 title claims abstract description 73
- 239000007788 liquid Substances 0.000 title claims abstract description 30
- 238000007084 catalytic combustion reaction Methods 0.000 title claims abstract description 18
- 238000009834 vaporization Methods 0.000 title claims description 12
- 238000002485 combustion reaction Methods 0.000 claims abstract description 59
- 230000003197 catalytic effect Effects 0.000 claims abstract description 30
- 238000002156 mixing Methods 0.000 claims abstract description 9
- 238000002347 injection Methods 0.000 claims description 17
- 239000007924 injection Substances 0.000 claims description 17
- 239000000203 mixture Substances 0.000 claims description 17
- 238000005507 spraying Methods 0.000 claims description 13
- 230000008016 vaporization Effects 0.000 claims description 11
- 230000000977 initiatory effect Effects 0.000 claims description 7
- 238000011084 recovery Methods 0.000 claims description 4
- 238000009835 boiling Methods 0.000 claims description 3
- 239000011810 insulating material Substances 0.000 claims description 2
- 239000007921 spray Substances 0.000 abstract description 2
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 15
- 238000009826 distribution Methods 0.000 description 8
- 239000007789 gas Substances 0.000 description 8
- 239000000243 solution Substances 0.000 description 5
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 4
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 4
- 229910002091 carbon monoxide Inorganic materials 0.000 description 4
- 239000003054 catalyst Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 3
- 239000003344 environmental pollutant Substances 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 230000003647 oxidation Effects 0.000 description 3
- 238000007254 oxidation reaction Methods 0.000 description 3
- 231100000719 pollutant Toxicity 0.000 description 3
- 238000002360 preparation method Methods 0.000 description 3
- 238000006722 reduction reaction Methods 0.000 description 3
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- 229910021529 ammonia Inorganic materials 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 239000000758 substrate Substances 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 238000004523 catalytic cracking Methods 0.000 description 1
- 238000010531 catalytic reduction reaction Methods 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 239000002283 diesel fuel Substances 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 239000003546 flue gas Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 238000013467 fragmentation Methods 0.000 description 1
- 238000006062 fragmentation reaction Methods 0.000 description 1
- 239000002737 fuel gas Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- VUZPPFZMUPKLLV-UHFFFAOYSA-N methane;hydrate Chemical compound C.O VUZPPFZMUPKLLV-UHFFFAOYSA-N 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical group [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 1
- 239000010970 precious metal Substances 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C13/00—Apparatus in which combustion takes place in the presence of catalytic material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D9/00—Burners in which a stream of liquid fuel impinges intermittently on a hot surface
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/40—Continuous combustion chambers using liquid or gaseous fuel characterised by the use of catalytic means
Definitions
- the present invention relates to a catalytic combustion device with vaporization of liquid fuel on a hot wall, thereby making it possible to optimize the preparation of the air-fuel mixture in a combustion zone.
- this technology is based on lowering the combustion temperatures. It allows the NO x to drop to around 20 ppm, but this reduction is often done to the detriment of carbon monoxide and unburnt fuel emissions, which are increased.
- Catalytic combustion is an attractive solution to meet the increasing severity of pollutant standards.
- the catalytic combustion chamber advantageously replaces the conventional burners, because it allows better control of the total oxidation of the fuel in a very wide range of values of the air / fuel ratio, thus making it possible to work under optimal conditions which reduce high emissions of nitrogen oxides, unburnt fuels and carbon monoxide.
- the essential characteristic of this particular type of combustion is to ensure the complete oxidation of the fuels at a relatively low temperature (below 1000 ° C.), compared with conventional combustion.
- catalytic combustion makes it possible to burn a wide variety of compounds.
- catalytic combustion is thus multiple: radiant panels and tubes, catalytic stoves, gas turbines, cogeneration, burners for boilers, catalytic sleeves for tubular reaction systems, production of hot gases in the field of direct contact heating and reactors with catalytic plates, etc.
- the possible fields of application of catalytic combustion are described in the literature for example in “Catalytic Combustion: Current Status and Implications for Energy Efficiency in the Process Industries, Heat recovery System & CHP, 13, n ° 5, pp 383-390 , 1993 ".
- Combustion catalysts are generally prepared from a monolithic substrate, ceramic or metal, on which is deposited a thin support layer consisting of one or more refractory oxides, with a surface and porosity greater than that of the monolithic substrate . On this support layer is dispersed the active phase most often comprising essentially metals of the platinum group.
- the most common reactor configuration is a reactor comprising several catalytic zones: the inlet catalyst (s) being more specifically dedicated upon initiation of the combustion reaction, the following serving to stabilize the combustion reaction
- This mixture must be produced as quickly as possible, and in the most homogeneous manner while limiting the risks of auto-ignition.
- the invention relates to a catalytic combustion device comprising a main combustion zone comprising at least one catalytic stage, at least one air / fuel mixing zone, said mixing zone comprising at least one pressurized air inlet, and means for injecting a liquid fuel, characterized in that the injection means project the liquid fuel onto a wall heated by the combustion of the air / fuel mixture in the area of main combustion so as to allow the vaporization of said fuel in contact with this wall.
- the invention it is possible to very substantially reduce the diameter of the liquid droplets by sending a primary liquid jet over a surface of temperature greater than the maximum boiling temperature of said fuel under the pressure conditions of the combustion zone.
- This primary liquid jet can advantageously come from any injector or spraying system known to those skilled in the art.
- injectors are used which allow primary spraying of the fuel with liquid droplets whose average diameter is between 5 and 60 ⁇ m (10 " ⁇ meter), preferably between 10 and 40 ⁇ m.
- the surface temperature of the wall encountered by the primary jet is substantially equal to or greater, at the pressure considered, at a first temperature TN of the wall corresponding to a maximum boiling temperature of the liquid.
- ⁇ a temperature above or below 100 ° C at said temperature, preferably a temperature above or below 50 ° C at said temperature and very preferably a temperature above or below 20 ° C at said temperature.
- Control of the temperature of the wall will therefore condition the size of the droplets and may be carried out according to any technique known to those skilled in the art.
- Such an injection strategy has many advantages during the preparation of the air-fuel mixture, in catalytic combustion: - Compared to a conventional configuration of catalytic combustion device with premixer and catalytic section, an arrangement having such a mode injection allows faster vaporization of the liquid fuel, especially those with fairly high final vaporization temperatures. This is the case for certain diesel fuels for example. Under these conditions, the air-fuel premix can be obtained more quickly.
- the arrangement object of the present invention can also contribute to the cooling of the walls of the combustion or post-combustion zones or of the zone which conveys the hot gases to the expansion turbine.
- the hot wall on which the fuel is sprayed is the wall of the combustion or post-combustion zone or of the zone carrying the hot gases from the combustion or that of the starting equipment which can be for example , a flame combustion chamber, an electric heater or any other device known to man ] of Art.
- the means allowing the injection of the liquid fuel are injectors carrying out a primary spraying whose orientation and characteristics are calculated to obtain the most homogeneous possible distribution of the fuel in the air of combustion and the size of the droplets from said injector is between 5 and 60 ⁇ m, preferably between 10 and 40 ⁇ m and very preferably between 20 and 30 ⁇ m.
- the hot wall of the zone opposite said injection means has a substantially planar shape.
- the hot wall of the zone opposite the injectors prefferably has a curved shape, for example concave.
- the zone receiving the impact of the fuel jets is equipped with devices making it possible to increase the transfer of heat from the hot zone to the spraying zone.
- the device according to the present invention finds, for example, its application in gas turbines having a heat recovery unit or in combustion chambers with annular geometry.
- FIGS. 1 and 2 give, by way of nonlimiting example of the invention, two different embodiments of the device according to the invention:
- FIG. 1 shows an exemplary embodiment in which the injection of fuel is carried out on a hot wall of a device for initiating combustion constituted by a pilot burner.
- FIG. 2 shows another embodiment in which the fuel injection is carried out on a hot wall of an afterburner zone.
- the combustion device shown diagrammatically in FIG. 1 comprises an inlet for pressurized air 1 coming from a compressor (not shown in the figure). This air circulates in a peripheral annular space 2 before arriving in a distribution box 3 where it is shared between a flow intended for a device for initiating combustion, here a pilot burner 4, and a flow directed towards a section catalytic 5.
- a device not shown in the figure can be placed at the level of this distribution box 3, in order to share the air optimally, whatever the speed of the machine.
- the pilot burner shown in Figure 1 is a conventional flame burner. It comprises a central fuel supply rod 6, an air box 7, means 8, such as for example blades, for adjusting the speed and rotation of the combustion air before it enters the combustion zone. 9 of the pilot burner, a smoke outlet zone 10 produced by the pilot burner, said outlet passing right through the catalytic section 5.
- This pilot burner can also be equipment known to those skilled in the art and reputed to emit little nitrogen oxides, such as for example systems in which combustion air is rotated in blades, with injection. fuel inside the blades, or part of the blades, or in the immediate vicinity of these blades.
- this comprises an air-fuel mixing zone 11 situated downstream of the distribution box 3, liquid fuel injectors with mechanical spraying 12 distributed evenly for example around the periphery of the mixing zone 1 1 and the catalytic section 5.
- the injectors 12 produce a jet of liquid fuel directed towards the hot wall 13 of the pilot burner 4, and make it possible to carry out a primary spraying of this fuel with liquid droplets whose average diameter is between 5 and 60 ⁇ m (10 '6 meter ) and preferably between 10 and 40 ⁇ m.
- This jet is preferably substantially perpendicular to the hot wall.
- substantially perpendicular it is understood that the angle between the surface of the hot wall with respect to the axis of the jet is very preferably between 80 ° and 100 °.
- this angle can be between 40 ° and 140 ° and preferably between 60 ° and 120 °.
- the wall 13 is heated by the combustion of the air / fuel mixture in section 5 and in contact with the hot wall, the liquid fuel is vaporized by dividing into very fine droplets of a few microns ⁇ (10 "s m) of average diameter which are entrained by the combustion air.
- the number of injectors, their orientation relative to the hot surface and the characteristics of the injectors are calculated by a person skilled in the art for obtain the most homogeneous distribution of the fuel in the gas flow, once the fine droplets are sprayed in.
- the air-fuel gas mixture then enters the catalytic section 5, which most often consists of one or more monoliths in parallel and or in series, in order to limit the pressure drops
- the catalytic section 5 most often consists of one or more monoliths in parallel and or in series, in order to limit the pressure drops
- the wall 15 which is in contact with the post-combustion zone 14 or the catalytic section 5 is also a heated wall by burning) fuel-air mixture into the catalytic section 5 and it may be contemplated to arrange the injectors 12 look at this wall.
- the wall 13 of the pilot burner 4 opposite the injectors may have a substantially flat shape, or even curved concave so that all the droplets of liquid fuel emitted by the injector, have the most impact perpendicularly possible the hot surface where they must fragment and pulverize.
- FIG. 1 is another possible illustration of the invention.
- combustion air supply 101 from the compressor (not shown in the figure), a combustion ignition device 102 (or pilot burner) and the main combustion zone 200 with its catalytic section 103 proper.
- the combustion air circulates in a substantially annular peripheral space 104.
- the fuel is introduced by means of injectors 105 fixed and substantially evenly distributed on the external wall 106 of the external wall of the annular space 104.
- injectors can be mechanical (without spraying assistance) or pneumatic (with spraying fluid assistance) or any other equivalent device.
- the jets produced by these injectors are directed towards the hot wall 107 which separates the annular space 104 from the zone 108 which can be an after-combustion zone or even simply a connection zone between the catalytic section 103 and the expansion turbine (not shown in the figure) and, in contact with this hot wall, the liquid fuel is sprayed into very fine droplets.
- the injectors 105 produce a fuel jet with a primary spray containing liquid droplets whose average diameter is between 5 and 60 ⁇ m (10 's meter), preferably between 10 and 40 ⁇ m.
- certain parts of the wall 107 can be covered with insulating materials in order to avoid hot spots which can cause premature ignition of the air-fuel mixture.
- the zone 120 of the wall 107 which receives the impact of the jets can be equipped with devices such as fins, in order to increase the heat transfer from the hot zone 108 to the spraying zone 104.
- the annular zone 104 ends with a distributor 109 which distributes the air-fuel mixture between the pilot burner 102 and the main catalytic section 103.
- This distribution can be obtained for example by a mobile shutter 110 which is placed alternately opposite the inlet 111 of the catalytic section 103 or opposite the inlet 112 of the pilot burner 102, depending on the operating conditions of the machine.
- the pilot burner can be a device like that presented in FIG. 1. It can also be according to the system indicated in FIG. 2, that is to say consisting of a catalytic initiation section 121, supplied by a circuit 1 13 located after the distributor 109.
- This catalytic section can be a metallic monolith, preheated by the Joule effect, by virtue of an electrical supply consisting of any source of electricity 114, of two metallic connectors 115 situated at each end of the monolith and an electrical connection 116 connecting said connectors 115 to the source of electricity 114.
- the main catalytic section 103 includes a distribution box 117 for the air-fuel mixture, this box being able to be equipped for example with a perforated plate 118 intended to ensure a homogeneous supply of all the constituent channels of the monolith.
- This plate 118 can also be a very thin monolith, intended to block any flame in the case of an unwanted self-ignition of the air-fuel mixture, in the space 1 19 located between said plate 118 and the catalytic section.
- main 103 This may consist of one or more monoliths placed in series or in parallel.
- a free space 108 before the expansion turbine (not shown in the figure), intended to complete the combustion of the air-mixture fuel, in case it has not completely burned in the catalytic section.
- the catalytic sections 102 and 103 can use catalysts of different natures.
- the catalyst of the pilot burner 102 may for example have a high content of precious metals known for their efficiency in catalytic combustion and thus allow combustion to start from 200 or 250 ° C.
- the invention can also be applied to configurations of gas turbines having a heat recovery unit or to combustion chambers with annular geometry.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Spray-Type Burners (AREA)
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/433,792 US20040048211A1 (en) | 2000-12-11 | 2001-12-05 | Catalytic combustion device with liquid fuel vaporisation on hot walls |
JP2002549886A JP2004515741A (ja) | 2000-12-11 | 2001-12-05 | 高温の壁上で液体燃料を気化させる触媒燃焼装置 |
DE60125412T DE60125412T2 (de) | 2000-12-11 | 2001-12-05 | Katalytische verbrennungsvorrichtung mit flüssigbrennstoffverdampfung auf heissen wänden |
EP01270733A EP1344000B1 (fr) | 2000-12-11 | 2001-12-05 | Dispositif de combustion catalytique avec vaporisation de combustible liquide sur parois chaudes |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0016107A FR2817946B1 (fr) | 2000-12-11 | 2000-12-11 | Dispositif de combustion catalytique avec pulverisation de combustible liquide sur parois chaudes |
FR00/16107 | 2000-12-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2002048610A1 true WO2002048610A1 (fr) | 2002-06-20 |
Family
ID=8857509
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/FR2001/003850 WO2002048610A1 (fr) | 2000-12-11 | 2001-12-05 | Dispositif de combustion catalytique avec vaporisation de combustible liquide sur parois chaudes |
Country Status (7)
Country | Link |
---|---|
US (1) | US20040048211A1 (fr) |
EP (1) | EP1344000B1 (fr) |
JP (1) | JP2004515741A (fr) |
AT (1) | ATE348979T1 (fr) |
DE (1) | DE60125412T2 (fr) |
FR (1) | FR2817946B1 (fr) |
WO (1) | WO2002048610A1 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1650499A3 (fr) * | 2004-10-20 | 2009-05-06 | United Technologies Corporation | Procédé et dispositif de combustion catalytique riche/pauvre |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7117676B2 (en) * | 2003-03-26 | 2006-10-10 | United Technologies Corporation | Apparatus for mixing fluids |
US7007486B2 (en) * | 2003-03-26 | 2006-03-07 | The Boeing Company | Apparatus and method for selecting a flow mixture |
US7127899B2 (en) * | 2004-02-26 | 2006-10-31 | United Technologies Corporation | Non-swirl dry low NOx (DLN) combustor |
US20070130830A1 (en) * | 2005-12-14 | 2007-06-14 | Balachandar Varatharajan | Staged combustion for a fuel reformer |
FR2899956B1 (fr) * | 2006-04-14 | 2008-07-25 | Thirode Grandes Cuisines Poligny | Bruleur a gaz pour four de cuisine |
US20080020333A1 (en) * | 2006-06-14 | 2008-01-24 | Smaling Rudolf M | Dual reaction zone fuel reformer and associated method |
SE536578C2 (sv) * | 2012-05-15 | 2014-03-04 | Reformtech Heating Holding Ab | Bränsleinsprutningssystem för användning i en katalytisk värmare och reaktor för utförande av katalytisk förbränning avflytande bränslen |
WO2014154931A1 (fr) * | 2013-03-27 | 2014-10-02 | Oilon Oy | Procédé et appareil pour brûler des hydrocarbures et d'autres liquides et gaz |
FR3011911B1 (fr) * | 2013-10-14 | 2015-11-20 | Cogebio | Bruleur de gaz pauvre |
DE102014103813A1 (de) * | 2014-03-20 | 2015-09-24 | Webasto SE | Verdampferbrenneranordnung für ein mobiles, mit flüssigem Brennstoff betriebenes Heizgerät |
CN113640337B (zh) * | 2021-07-23 | 2024-04-05 | 哈尔滨工业大学 | 研究碳氢燃料液滴在微小尺度热壁面蒸发结焦的实验装置及其实验方法 |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4040252A (en) * | 1976-01-30 | 1977-08-09 | United Technologies Corporation | Catalytic premixing combustor |
US4067190A (en) * | 1975-09-29 | 1978-01-10 | Westinghouse Electric Corporation | Catalytic gas turbine combustor with a fuel-air premix chamber |
JPS5913831A (ja) * | 1982-07-16 | 1984-01-24 | Toshiba Corp | ガスタ−ビン燃焼器 |
US4561257A (en) * | 1981-05-20 | 1985-12-31 | Rolls-Royce Limited | Gas turbine engine combustion apparatus |
JPH06249414A (ja) * | 1993-02-26 | 1994-09-06 | Matsushita Electric Ind Co Ltd | 触媒燃焼装置 |
FR2732447A1 (fr) * | 1995-03-31 | 1996-10-04 | Samsung Electronics Co Ltd | Structure de bruleur du type a orifices pour appareil de combustion de petrole lampant |
JPH11264514A (ja) * | 1998-03-18 | 1999-09-28 | Corona Corp | 触媒燃焼装置 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4013396A (en) * | 1975-08-25 | 1977-03-22 | Tenney William L | Fuel aerosolization apparatus and method |
DE2912519C2 (de) * | 1979-03-29 | 1984-03-15 | Kernforschungsanlage Jülich GmbH, 5170 Jülich | Brenner für flüssigen Brennstoff und Verbrennungsluft |
US4381187A (en) * | 1980-03-24 | 1983-04-26 | United Technologies Corporation | Process for gasifying liquid hydrocarbon fuels |
CA1303477C (fr) * | 1988-06-06 | 1992-06-16 | Yoichiro Ohkubo | Dispositif de combustion catalytique |
US5203690A (en) * | 1988-07-08 | 1993-04-20 | Nippon Chemical Plant Consultant Co., Ltd. | Combustion apparatus |
JPH06235519A (ja) * | 1993-02-08 | 1994-08-23 | Toshiba Corp | ガスタービン用燃焼器 |
KR100662168B1 (ko) * | 1999-08-19 | 2006-12-27 | 마츠시타 덴끼 산교 가부시키가이샤 | 촉매연소장치 및 연료기화장치 |
-
2000
- 2000-12-11 FR FR0016107A patent/FR2817946B1/fr not_active Expired - Fee Related
-
2001
- 2001-12-05 EP EP01270733A patent/EP1344000B1/fr not_active Expired - Lifetime
- 2001-12-05 US US10/433,792 patent/US20040048211A1/en not_active Abandoned
- 2001-12-05 WO PCT/FR2001/003850 patent/WO2002048610A1/fr active IP Right Grant
- 2001-12-05 AT AT01270733T patent/ATE348979T1/de not_active IP Right Cessation
- 2001-12-05 JP JP2002549886A patent/JP2004515741A/ja active Pending
- 2001-12-05 DE DE60125412T patent/DE60125412T2/de not_active Expired - Lifetime
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4067190A (en) * | 1975-09-29 | 1978-01-10 | Westinghouse Electric Corporation | Catalytic gas turbine combustor with a fuel-air premix chamber |
US4040252A (en) * | 1976-01-30 | 1977-08-09 | United Technologies Corporation | Catalytic premixing combustor |
US4561257A (en) * | 1981-05-20 | 1985-12-31 | Rolls-Royce Limited | Gas turbine engine combustion apparatus |
JPS5913831A (ja) * | 1982-07-16 | 1984-01-24 | Toshiba Corp | ガスタ−ビン燃焼器 |
JPH06249414A (ja) * | 1993-02-26 | 1994-09-06 | Matsushita Electric Ind Co Ltd | 触媒燃焼装置 |
FR2732447A1 (fr) * | 1995-03-31 | 1996-10-04 | Samsung Electronics Co Ltd | Structure de bruleur du type a orifices pour appareil de combustion de petrole lampant |
JPH11264514A (ja) * | 1998-03-18 | 1999-09-28 | Corona Corp | 触媒燃焼装置 |
Non-Patent Citations (3)
Title |
---|
PATENT ABSTRACTS OF JAPAN vol. 008, no. 100 (M - 295) 11 May 1984 (1984-05-11) * |
PATENT ABSTRACTS OF JAPAN vol. 018, no. 644 (M - 1718) 7 December 1994 (1994-12-07) * |
PATENT ABSTRACTS OF JAPAN vol. 1999, no. 14 22 December 1999 (1999-12-22) * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1650499A3 (fr) * | 2004-10-20 | 2009-05-06 | United Technologies Corporation | Procédé et dispositif de combustion catalytique riche/pauvre |
Also Published As
Publication number | Publication date |
---|---|
EP1344000B1 (fr) | 2006-12-20 |
DE60125412T2 (de) | 2007-09-27 |
EP1344000A1 (fr) | 2003-09-17 |
ATE348979T1 (de) | 2007-01-15 |
DE60125412D1 (de) | 2007-02-01 |
FR2817946B1 (fr) | 2003-03-21 |
FR2817946A1 (fr) | 2002-06-14 |
US20040048211A1 (en) | 2004-03-11 |
JP2004515741A (ja) | 2004-05-27 |
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