US20100119984A1 - Abatement system - Google Patents

Abatement system Download PDF

Info

Publication number
US20100119984A1
US20100119984A1 US12/613,883 US61388309A US2010119984A1 US 20100119984 A1 US20100119984 A1 US 20100119984A1 US 61388309 A US61388309 A US 61388309A US 2010119984 A1 US2010119984 A1 US 2010119984A1
Authority
US
United States
Prior art keywords
abatement system
fuel
combustion chamber
vacuum generator
generator device
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US12/613,883
Inventor
Allen G. Fox
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Applied Materials Inc
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US12/613,883 priority Critical patent/US20100119984A1/en
Priority to CN2009801449462A priority patent/CN102210006A/en
Priority to KR1020117013222A priority patent/KR20110095305A/en
Priority to PCT/US2009/063692 priority patent/WO2010054291A2/en
Assigned to APPLIED MATERIALS, INC. reassignment APPLIED MATERIALS, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: FOX, ALLEN G.
Publication of US20100119984A1 publication Critical patent/US20100119984A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L21/00Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
    • H01L21/02Manufacture or treatment of semiconductor devices or of parts thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D53/00Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols
    • B01D53/34Chemical or biological purification of waste gases
    • B01D53/38Removing components of undefined structure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23GCREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
    • F23G7/00Incinerators or other apparatus for consuming industrial waste, e.g. chemicals
    • F23G7/06Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases
    • F23G7/061Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases with supplementary heating
    • F23G7/065Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases with supplementary heating using gaseous or liquid fuel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23JREMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTION RESIDUES; FLUES 
    • F23J15/00Arrangements of devices for treating smoke or fumes
    • F23J15/06Arrangements of devices for treating smoke or fumes of coolers
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L21/00Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D2258/00Sources of waste gases
    • B01D2258/02Other waste gases
    • B01D2258/0216Other waste gases from CVD treatment or semi-conductor manufacturing

Definitions

  • Embodiments of the present invention pertain to the field of abatement systems and, in particular, to a fuel burner ring for a combustion chamber in an abatement system and to a fuel flow control for an abatement system.
  • Abatement systems can provide environmental abatement solutions for the semiconductor, solar and display industries.
  • a wide range of point-of-use scrubbing systems are available, including wet, dry, thermal and integrated technologies for abatement of toxic and hazardous exhaust gases for a variety of applications.
  • some abatement systems handle complex effluent challenges ranging from a single unit to an entire fabrication facility.
  • Embodiments of the present invention include abatement systems.
  • an abatement system in an embodiment, includes a combustion chamber.
  • the abatement system also includes a fuel burner ring.
  • the fuel burner ring is coupled with the combustion chamber.
  • an abatement system in another embodiment, includes a combustion chamber.
  • the abatement system also includes a fuel flow control mechanism.
  • the fuel flow control mechanism is coupled with the combustion chamber.
  • an abatement system in yet another embodiment, includes a combustion chamber.
  • the abatement system also includes a fuel burner ring and a fuel flow control mechanism. Both the a fuel burner ring and the fuel flow control mechanism are coupled with the combustion chamber.
  • FIG. 1 illustrates a block-diagram of an abatement system, in accordance with an embodiment of the present invention.
  • FIG. 2 illustrates a cross-sectional view of an abatement system, in accordance with an embodiment of the present invention.
  • FIG. 3 illustrates a cross-sectional view of a conventional arrangement of four process gas inlet tubes, each surrounded by four nozzles for injection combustion fuel.
  • FIG. 4 illustrates a cross-sectional view of an arrangement of four process gas inlet tubes, each surrounded by a burner ring for injecting combustion fuel, in accordance with an embodiment of the present invention.
  • FIG. 5 is a temperature distribution map representing temperature distribution for a ring burner used approximately in a temperature range of 300-900 Kelvin, in accordance with an embodiment of the present invention.
  • FIG. 6 is a temperature distribution map representing temperature distribution for four conventional nozzles used approximately in a temperature range of 300-2200 Kelvin.
  • FIG. 7 illustrates various views of a portion of an abatement system including a combustion chamber having a fuel burner ring, in accordance with an embodiment of the present invention.
  • FIG. 8 illustrates various views of a burner ring for use in an abatement system including a combustion chamber, in accordance with an embodiment of the present invention.
  • FIG. 9 illustrates a diagram of a vacuum generator device, in accordance with an embodiment of the present invention.
  • an abatement system includes a combustion chamber and a fuel burner ring coupled with the combustion chamber. In one embodiment, an abatement system includes a combustion chamber and a fuel flow control mechanism coupled with the combustion chamber. In one embodiment, an abatement system includes a combustion chamber, a fuel burner ring, and a fuel flow control mechanism, both the fuel burner ring and the fuel flow control mechanism coupled with the combustion chamber.
  • an abatement system destroys residual process gases through active flame oxidation and combustion for reliable and safe abatement.
  • effluent gases are heated by a flame in the main chamber of the system which provides ignition of flammable and pyrophoric gas by-products.
  • the advanced design of the flame ignition system ensures a stable flame with high inert gas flow.
  • an abatement system provides wet-scrubbing solutions that support up to four process effluent streams including those from challenging processes such as epitaxial silicon deposition and metal etch.
  • the abatement system handles perfluorocarbons (PFCs) and global-warming gasses.
  • the treatment of hydride and acid-based gases is performed in an abatement system.
  • process gases and by-products react with resin to form nonvolatile solids, an irreversible process that traps by-products and ensures safe disposal of the resin.
  • an abatement system may include a combustion chamber or reactor.
  • FIG. 1 illustrates a block-diagram of an abatement system, in accordance with an embodiment of the present invention.
  • abatement system 100 includes a gas inlet 102 , a combustion chamber or reactor 104 , a cooling chamber 106 , a receiving tank 108 , a scrubber 110 , and an exhaust 112 .
  • combustion chamber or reactor 104 includes a burner.
  • cooling chamber 106 is a waterfall cooling chamber configured with spray jets to spray water into a gas stream.
  • receiving tank 108 includes a large tank holding an amount of water at the bottom of the tank with space over-head for gas that is moving through the abatement system.
  • scrubber 110 sits directly above receiving tank 108 .
  • scrubber 110 includes a spray shower for spraying water into a stream of effluent gases.
  • FIG. 2 illustrates a cross-sectional view of an abatement system, in accordance with an embodiment of the present invention.
  • abatement system 200 includes a gas inlet 202 , a combustion chamber or reactor 204 , a cooling chamber 206 , a receiving tank 208 , a scrubber 210 , and an exhaust 212 .
  • combustion chamber or reactor 204 includes a burner.
  • cooling chamber 206 is a waterfall cooling chamber configured with spray jets to spray water into a gas stream.
  • receiving tank 208 includes a large tank holding an amount of water at the bottom of the tank with space over-head for gas that is moving through the abatement system, as is depicted in FIG. 2 .
  • scrubber 210 sits directly above receiving tank 208 , as is also depicted in FIG. 2 .
  • scrubber 210 includes a spray shower for spraying water into a stream of effluent gases.
  • An abatement system may include a combustion chamber having a fuel burner ring.
  • an abatement system uses combustion to heat a process gas to a sufficiently to a sufficiently high temperature and for a sufficient duration for abatement.
  • an abatement system using burners composed of one or a few large jets may provide non-uniform temperature and flow distributions, which can degrade the performance of the abatement system. The degraded performance may result from some of the process gas not reaching a required temperature and, thus, high velocity gas may exit a reaction chamber before a combustion reaction is complete.
  • a burner ring with many small ports is used and is coupled to the combustion chamber of an abatement system. In a specific embodiment, by using a burner ring with many small ports, a more uniform flow pattern is generated along the length of the reaction chamber.
  • the reaction chamber of an ErikaTM abatement system is equipped with a fuel burner ring instead of a conventional arrangement process using four nozzles.
  • the reaction chamber of an Integrated Subfab System (ISS) abatement system or a MarathonTM abatement system is equipped with a fuel burner ring instead of a conventional arrangement process using four nozzles.
  • gases are introduced to a reaction chamber of the abatement system through four inlet tubes.
  • each inlet tube is surrounded by up to four nozzles. For example, FIG.
  • FIG. 3 illustrates a cross-sectional view of a conventional arrangement of four process gas inlet tubes 300 , each surrounded by four nozzles 302 for injecting combustion fuel.
  • FIG. 4 illustrates a cross-sectional view of an arrangement of four process gas inlet tubes 400 , each surrounded by a burner ring 402 having holes 404 for injecting combustion fuel, in accordance with an embodiment of the present invention.
  • the holes 404 in each burner ring 402 are coupled to a single plenum to obtain uniform flow around the ring.
  • the velocity at each burner ring is reduced to be approximately the same as the velocity of a process gas in each process gas inlet tube 400 .
  • a range of approximately 8-30 holes 404 are included in each burner ring 402 .
  • heating in a combustion chamber of an abatement system is more uniform, improving the overall performance of the abatement system.
  • FIG. 5 is a temperature distribution map 500 representing temperature distribution for a ring burner used approximately in a temperature range of 300-900 Kelvin, in accordance with an embodiment of the present invention.
  • FIG. 6 is a temperature distribution map 600 representing temperature distribution for four conventional nozzles used approximately in a temperature range of 300-2200 Kelvin.
  • FIG. 7 illustrates various views of a portion of an abatement system including a combustion chamber having a fuel burner ring, in accordance with an embodiment of the present invention.
  • a bottom view 790 of a cover 710 of a reaction chamber for an abatement system includes four process gas inlet tubes 700 , each surrounded by a burner ring 702 having holes 704 for injecting combustion fuel.
  • a top view 799 of a cover 710 of a reaction chamber for an abatement system includes four process gas inlet tubes 700 .
  • FIG. 8 illustrates various views of a burner ring for use in an abatement system including a combustion chamber, in accordance with an embodiment of the present invention.
  • a burner ring 802 includes holes 804 for injecting combustion fuel into a reaction chamber in an abatement system.
  • an abatement system with a fuel burner ring may be provided.
  • an abatement system includes a combustion chamber and a fuel burner ring coupled with the combustion chamber.
  • the fuel burner ring includes a plurality of ports.
  • the plurality of ports is arranged to provide an approximately uniform flow pattern of a fuel provided to the plurality of ports.
  • the approximately uniform flow pattern of the fuel is provided along a length of the combustion chamber.
  • the abatement system further includes a process gas inlet tube to introduce a process gas into the combustion chamber, the process gas inlet tube surrounded by the fuel burner ring.
  • the abatement further includes one or more additional process gas inlet tubes, each of the one or more additional process gas inlet tubes surrounded by a fuel burner ring.
  • the fuel burner ring includes a number of ports approximately in the range of 8-30 ports.
  • an abatement system may include a fuel flow control mechanism.
  • the ratio of fuel to air in a pilot or main burner in a combustion abatement device are controlled to prevent flashback, loss of flame, and sooting.
  • Conventional systems may require several devices or software control to maintain the proper ratio while still allowing for variable set-points.
  • Other designs do not even allow for adequate mixing of the air and the fuel. Accordingly, in some facilities, e.g. facilities with low fuel pressure, the fuel pressure supplied by the facility may be too low for some flow control devices.
  • an abatement system is equipped with a vacuum generator device that is driven by high pressure air.
  • the high pressure air creates a slight vacuum to draw gaseous fuel into the device, even when supply pressure is too low.
  • the fuel is a gas such as, but not limited to, methane or a natural gas composition.
  • the fuel to air ratio is determined by the design of the vacuum generator device.
  • the vacuum generator device can be used alone with no other control required. In a specific embodiment, this eliminates the need for separate flow controllers and software input on the air and fuel lines.
  • the fuel pressure is fixed by a pressure regulator.
  • FIG. 9 illustrates a diagram of a vacuum generator device 900 , in accordance with an embodiment of the present invention.
  • vacuum generator device 900 is a venturi device, as illustrated in FIG. 9 .
  • an abatement system with a fuel flow control mechanism includes a combustion chamber and a fuel flow control mechanism coupled with the combustion chamber.
  • the fuel flow control mechanism includes a vacuum generator device configured to be driven by a high pressure airflow.
  • the vacuum generator device is configured such that the high pressure airflow creates a slight vacuum for drawing gaseous fuel into the vacuum generator device.
  • the vacuum generator device is the sole fuel flow control mechanism in the abatement system.
  • the vacuum generator device is further coupled with a pressure regulator as an additional fuel flow control mechanism in the abatement system.
  • the vacuum generator device is further configured to mix a fuel flow and an airflow.
  • an abatement system may include a fuel burner ring and a fuel flow control mechanism.
  • an abatement system includes a combustion chamber, a fuel burner ring coupled with the combustion chamber, and a fuel flow control mechanism also coupled with the combustion chamber.
  • the fuel burner ring includes a plurality of ports
  • the fuel flow control mechanism includes a vacuum generator device configured to be driven by a high pressure airflow.
  • the vacuum generator device is configured such that the high pressure airflow creates a slight vacuum for drawing a fuel into the vacuum generator device, and the plurality of ports is arranged to provide an approximately uniform flow pattern of the fuel provided to the plurality of ports.
  • the approximately uniform flow pattern of the fuel is provided along a length of the combustion chamber, and the vacuum generator device is the sole fuel flow control mechanism in the abatement system.
  • the vacuum generator device is further coupled with a pressure regulator as an additional fuel flow control mechanism in the abatement system, and the abatement system further includes a process gas inlet tube to introduce a process gas into the combustion chamber, the process gas inlet tube surrounded by the fuel burner ring.
  • the vacuum generator device is further configured to mix a fuel flow and an airflow, and the abatement system further includes one or more additional process gas inlet tubes, each of the one or more additional process gas inlet tubes surrounded by a fuel burner ring.
  • the fuel burner ring includes a number of ports approximately in the range of 8-30 ports.
  • an abatement system includes a combustion chamber and a fuel burner ring coupled with the combustion chamber.
  • the fuel burner ring includes a plurality of ports.
  • an abatement system includes a combustion chamber and a fuel flow control mechanism coupled with the combustion chamber.
  • the fuel flow control mechanism includes a vacuum generator device configured to be driven by a high pressure airflow.

Landscapes

  • Engineering & Computer Science (AREA)
  • Environmental & Geological Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • General Chemical & Material Sciences (AREA)
  • Condensed Matter Physics & Semiconductors (AREA)
  • Analytical Chemistry (AREA)
  • Health & Medical Sciences (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Physics & Mathematics (AREA)
  • Biomedical Technology (AREA)
  • General Physics & Mathematics (AREA)
  • Manufacturing & Machinery (AREA)
  • Computer Hardware Design (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Power Engineering (AREA)
  • Incineration Of Waste (AREA)

Abstract

Abatement systems are described. An abatement system includes a combustion chamber and a fuel burner ring coupled with the combustion chamber. Another abatement system includes a combustion chamber and a fuel flow control mechanism coupled with the combustion chamber.

Description

    CROSS REFERENCE TO RELATED APPLICATIONS
  • This application claims the benefit of U.S. Provisional Application No. 61/113,143, filed Nov. 10, 2008, the entire contents of which are hereby incorporated by reference herein.
  • BACKGROUND
  • 1) Field
  • Embodiments of the present invention pertain to the field of abatement systems and, in particular, to a fuel burner ring for a combustion chamber in an abatement system and to a fuel flow control for an abatement system.
  • 2) Description of Related Art
  • Abatement systems can provide environmental abatement solutions for the semiconductor, solar and display industries. A wide range of point-of-use scrubbing systems are available, including wet, dry, thermal and integrated technologies for abatement of toxic and hazardous exhaust gases for a variety of applications. For example, some abatement systems handle complex effluent challenges ranging from a single unit to an entire fabrication facility.
  • SUMMARY
  • Embodiments of the present invention include abatement systems.
  • In an embodiment, an abatement system includes a combustion chamber. The abatement system also includes a fuel burner ring. The fuel burner ring is coupled with the combustion chamber.
  • In another embodiment, an abatement system includes a combustion chamber. The abatement system also includes a fuel flow control mechanism. The fuel flow control mechanism is coupled with the combustion chamber.
  • In yet another embodiment, an abatement system includes a combustion chamber. The abatement system also includes a fuel burner ring and a fuel flow control mechanism. Both the a fuel burner ring and the fuel flow control mechanism are coupled with the combustion chamber.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 illustrates a block-diagram of an abatement system, in accordance with an embodiment of the present invention.
  • FIG. 2 illustrates a cross-sectional view of an abatement system, in accordance with an embodiment of the present invention.
  • FIG. 3 illustrates a cross-sectional view of a conventional arrangement of four process gas inlet tubes, each surrounded by four nozzles for injection combustion fuel.
  • FIG. 4 illustrates a cross-sectional view of an arrangement of four process gas inlet tubes, each surrounded by a burner ring for injecting combustion fuel, in accordance with an embodiment of the present invention.
  • FIG. 5 is a temperature distribution map representing temperature distribution for a ring burner used approximately in a temperature range of 300-900 Kelvin, in accordance with an embodiment of the present invention.
  • FIG. 6 is a temperature distribution map representing temperature distribution for four conventional nozzles used approximately in a temperature range of 300-2200 Kelvin.
  • FIG. 7 illustrates various views of a portion of an abatement system including a combustion chamber having a fuel burner ring, in accordance with an embodiment of the present invention.
  • FIG. 8 illustrates various views of a burner ring for use in an abatement system including a combustion chamber, in accordance with an embodiment of the present invention.
  • FIG. 9 illustrates a diagram of a vacuum generator device, in accordance with an embodiment of the present invention.
  • DETAILED DESCRIPTION
  • Abatement systems are described. In the following description, numerous specific details are set forth, such as system configuration, in order to provide a thorough understanding of embodiments of the present invention. It will be apparent to one skilled in the art that embodiments of the present invention may be practiced without these specific details. In other instances, well-known features, such as facility layouts, are not described in detail in order to not unnecessarily obscure embodiments of the present invention. Furthermore, it is to be understood that the various embodiments shown in the Figures are illustrative representations and are not necessarily drawn to scale.
  • Disclosed herein are abatement systems. In one embodiment, an abatement system includes a combustion chamber and a fuel burner ring coupled with the combustion chamber. In one embodiment, an abatement system includes a combustion chamber and a fuel flow control mechanism coupled with the combustion chamber. In one embodiment, an abatement system includes a combustion chamber, a fuel burner ring, and a fuel flow control mechanism, both the fuel burner ring and the fuel flow control mechanism coupled with the combustion chamber.
  • In accordance with an embodiment of the present invention, an abatement system destroys residual process gases through active flame oxidation and combustion for reliable and safe abatement. In one embodiment, effluent gases are heated by a flame in the main chamber of the system which provides ignition of flammable and pyrophoric gas by-products. In a specific embodiment, the advanced design of the flame ignition system ensures a stable flame with high inert gas flow. In an embodiment, an abatement system provides wet-scrubbing solutions that support up to four process effluent streams including those from challenging processes such as epitaxial silicon deposition and metal etch. In one embodiment, the abatement system handles perfluorocarbons (PFCs) and global-warming gasses. In another embodiment, the treatment of hydride and acid-based gases is performed in an abatement system. In one embodiment, by utilizing chemisorptive technology, process gases and by-products react with resin to form nonvolatile solids, an irreversible process that traps by-products and ensures safe disposal of the resin.
  • In an aspect of the present invention, an abatement system may include a combustion chamber or reactor. FIG. 1 illustrates a block-diagram of an abatement system, in accordance with an embodiment of the present invention. Referring to FIG. 1, abatement system 100 includes a gas inlet 102, a combustion chamber or reactor 104, a cooling chamber 106, a receiving tank 108, a scrubber 110, and an exhaust 112. In one embodiment, combustion chamber or reactor 104 includes a burner. In another embodiment, cooling chamber 106 is a waterfall cooling chamber configured with spray jets to spray water into a gas stream. In an embodiment, receiving tank 108 includes a large tank holding an amount of water at the bottom of the tank with space over-head for gas that is moving through the abatement system. In another embodiment, scrubber 110 sits directly above receiving tank 108. In a specific embodiment, scrubber 110 includes a spray shower for spraying water into a stream of effluent gases.
  • FIG. 2 illustrates a cross-sectional view of an abatement system, in accordance with an embodiment of the present invention. Referring to FIG. 2, abatement system 200 includes a gas inlet 202, a combustion chamber or reactor 204, a cooling chamber 206, a receiving tank 208, a scrubber 210, and an exhaust 212. In one embodiment, combustion chamber or reactor 204 includes a burner. In another embodiment, cooling chamber 206 is a waterfall cooling chamber configured with spray jets to spray water into a gas stream. In an embodiment, receiving tank 208 includes a large tank holding an amount of water at the bottom of the tank with space over-head for gas that is moving through the abatement system, as is depicted in FIG. 2. In another embodiment, scrubber 210 sits directly above receiving tank 208, as is also depicted in FIG. 2. In a specific embodiment, scrubber 210 includes a spray shower for spraying water into a stream of effluent gases.
  • An abatement system may include a combustion chamber having a fuel burner ring. In accordance with an embodiment of the present invention, an abatement system uses combustion to heat a process gas to a sufficiently to a sufficiently high temperature and for a sufficient duration for abatement. However, an abatement system using burners composed of one or a few large jets may provide non-uniform temperature and flow distributions, which can degrade the performance of the abatement system. The degraded performance may result from some of the process gas not reaching a required temperature and, thus, high velocity gas may exit a reaction chamber before a combustion reaction is complete. Instead, in one embodiment, a burner ring with many small ports is used and is coupled to the combustion chamber of an abatement system. In a specific embodiment, by using a burner ring with many small ports, a more uniform flow pattern is generated along the length of the reaction chamber.
  • In an exemplary embodiment of the present invention, the reaction chamber of an Erika™ abatement system, available from Applied Materials, Inc., is equipped with a fuel burner ring instead of a conventional arrangement process using four nozzles. In another exemplary embodiment of the present invention, the reaction chamber of an Integrated Subfab System (ISS) abatement system or a Marathon™ abatement system, available from Applied Materials, Inc., is equipped with a fuel burner ring instead of a conventional arrangement process using four nozzles. In an embodiment, gases are introduced to a reaction chamber of the abatement system through four inlet tubes. In a conventional arrangement, each inlet tube is surrounded by up to four nozzles. For example, FIG. 3 illustrates a cross-sectional view of a conventional arrangement of four process gas inlet tubes 300, each surrounded by four nozzles 302 for injecting combustion fuel. By contrast, FIG. 4 illustrates a cross-sectional view of an arrangement of four process gas inlet tubes 400, each surrounded by a burner ring 402 having holes 404 for injecting combustion fuel, in accordance with an embodiment of the present invention. In an embodiment, the holes 404 in each burner ring 402 are coupled to a single plenum to obtain uniform flow around the ring. In one embodiment, by distributing the fuel flow over a large number of holes, the velocity at each burner ring is reduced to be approximately the same as the velocity of a process gas in each process gas inlet tube 400. In a specific embodiment, a range of approximately 8-30 holes 404 are included in each burner ring 402. In an embodiment, by reducing the fuel velocity surrounding each process gas inlet tube 400, heating in a combustion chamber of an abatement system is more uniform, improving the overall performance of the abatement system.
  • By using a fuel burner ring, the temperature distribution in a reaction chamber may be more uniform. For example, FIG. 5 is a temperature distribution map 500 representing temperature distribution for a ring burner used approximately in a temperature range of 300-900 Kelvin, in accordance with an embodiment of the present invention. By contrast, FIG. 6 is a temperature distribution map 600 representing temperature distribution for four conventional nozzles used approximately in a temperature range of 300-2200 Kelvin.
  • FIG. 7 illustrates various views of a portion of an abatement system including a combustion chamber having a fuel burner ring, in accordance with an embodiment of the present invention. Referring to FIG. 7, in one embodiment, a bottom view 790 of a cover 710 of a reaction chamber for an abatement system includes four process gas inlet tubes 700, each surrounded by a burner ring 702 having holes 704 for injecting combustion fuel. Referring to FIG. 7, in another embodiment, a top view 799 of a cover 710 of a reaction chamber for an abatement system includes four process gas inlet tubes 700. FIG. 8 illustrates various views of a burner ring for use in an abatement system including a combustion chamber, in accordance with an embodiment of the present invention. Referring to FIG. 8, a burner ring 802 includes holes 804 for injecting combustion fuel into a reaction chamber in an abatement system.
  • Thus, an abatement system with a fuel burner ring may be provided. In an embodiment, an abatement system includes a combustion chamber and a fuel burner ring coupled with the combustion chamber. In one embodiment, the fuel burner ring includes a plurality of ports. In a specific embodiment, the plurality of ports is arranged to provide an approximately uniform flow pattern of a fuel provided to the plurality of ports. In a particular embodiment, the approximately uniform flow pattern of the fuel is provided along a length of the combustion chamber. In another particular embodiment, the abatement system further includes a process gas inlet tube to introduce a process gas into the combustion chamber, the process gas inlet tube surrounded by the fuel burner ring. In another particular embodiment, the abatement further includes one or more additional process gas inlet tubes, each of the one or more additional process gas inlet tubes surrounded by a fuel burner ring. In an embodiment, the fuel burner ring includes a number of ports approximately in the range of 8-30 ports.
  • In another aspect of the present invention, an abatement system may include a fuel flow control mechanism. In accordance with an embodiment of the present invention, the ratio of fuel to air in a pilot or main burner in a combustion abatement device are controlled to prevent flashback, loss of flame, and sooting. Conventional systems may require several devices or software control to maintain the proper ratio while still allowing for variable set-points. Other designs do not even allow for adequate mixing of the air and the fuel. Accordingly, in some facilities, e.g. facilities with low fuel pressure, the fuel pressure supplied by the facility may be too low for some flow control devices.
  • Instead, in accordance with an embodiment of the present invention, an abatement system is equipped with a vacuum generator device that is driven by high pressure air. In one embodiment, the high pressure air creates a slight vacuum to draw gaseous fuel into the device, even when supply pressure is too low. In a specific embodiment, the fuel is a gas such as, but not limited to, methane or a natural gas composition. In an embodiment, for a given fuel pressure, the fuel to air ratio is determined by the design of the vacuum generator device. In one embodiment, the vacuum generator device can be used alone with no other control required. In a specific embodiment, this eliminates the need for separate flow controllers and software input on the air and fuel lines. In another embodiment, the fuel pressure is fixed by a pressure regulator. In accordance with an embodiment of the present invention, air flow is adjusted in the vacuum generator device for various operating condition selection. In one embodiment, the adjustment is performed by a flow or pressure control device coupled to the vacuum generator device. In another embodiment, the vacuum generator device also acts as a mixer for the fuel and air, improving the stability of a flame within a reaction chamber of an abatement system. In an exemplary embodiment, FIG. 9 illustrates a diagram of a vacuum generator device 900, in accordance with an embodiment of the present invention. In a specific embodiment, vacuum generator device 900 is a venturi device, as illustrated in FIG. 9.
  • Thus, an abatement system with a fuel flow control mechanism may be provided. In an embodiment, an abatement system includes a combustion chamber and a fuel flow control mechanism coupled with the combustion chamber. In one embodiment, the fuel flow control mechanism includes a vacuum generator device configured to be driven by a high pressure airflow. In a specific embodiment, the vacuum generator device is configured such that the high pressure airflow creates a slight vacuum for drawing gaseous fuel into the vacuum generator device. In a particular embodiment, the vacuum generator device is the sole fuel flow control mechanism in the abatement system. In another particular embodiment, the vacuum generator device is further coupled with a pressure regulator as an additional fuel flow control mechanism in the abatement system. In another particular embodiment, the vacuum generator device is further configured to mix a fuel flow and an airflow.
  • In another aspect of the present invention, an abatement system may include a fuel burner ring and a fuel flow control mechanism. In an embodiment, an abatement system includes a combustion chamber, a fuel burner ring coupled with the combustion chamber, and a fuel flow control mechanism also coupled with the combustion chamber. In one embodiment, the fuel burner ring includes a plurality of ports, and the fuel flow control mechanism includes a vacuum generator device configured to be driven by a high pressure airflow. In a specific embodiment, the vacuum generator device is configured such that the high pressure airflow creates a slight vacuum for drawing a fuel into the vacuum generator device, and the plurality of ports is arranged to provide an approximately uniform flow pattern of the fuel provided to the plurality of ports. In a particular embodiment, the approximately uniform flow pattern of the fuel is provided along a length of the combustion chamber, and the vacuum generator device is the sole fuel flow control mechanism in the abatement system. In another particular embodiment, the vacuum generator device is further coupled with a pressure regulator as an additional fuel flow control mechanism in the abatement system, and the abatement system further includes a process gas inlet tube to introduce a process gas into the combustion chamber, the process gas inlet tube surrounded by the fuel burner ring. In another particular embodiment, the vacuum generator device is further configured to mix a fuel flow and an airflow, and the abatement system further includes one or more additional process gas inlet tubes, each of the one or more additional process gas inlet tubes surrounded by a fuel burner ring. In an embodiment, the fuel burner ring includes a number of ports approximately in the range of 8-30 ports.
  • Thus, abatement systems have been disclosed. In accordance with an embodiment of the present invention, an abatement system includes a combustion chamber and a fuel burner ring coupled with the combustion chamber. In one embodiment, the fuel burner ring includes a plurality of ports. In accordance with another embodiment of the present invention, an abatement system includes a combustion chamber and a fuel flow control mechanism coupled with the combustion chamber. In one embodiment, the fuel flow control mechanism includes a vacuum generator device configured to be driven by a high pressure airflow.

Claims (20)

1. An abatement system, comprising:
a combustion chamber; and
a fuel burner ring coupled with the combustion chamber.
2. The abatement system of claim 1, wherein the fuel burner ring comprises a plurality of ports.
3. The abatement system of claim 2, wherein the plurality of ports is arranged to provide an approximately uniform flow pattern of a fuel provided to the plurality of ports.
4. The abatements system of claim 3, wherein the approximately uniform flow pattern of the fuel is provided along a length of the combustion chamber.
5. The abatement system of claim 4, further comprising:
a process gas inlet tube to introduce a process gas into the combustion chamber, the process gas inlet tube surrounded by the fuel burner ring.
6. The abatement system of claim 5, further comprising:
one or more additional process gas inlet tubes, each of the one or more additional process gas inlet tubes surrounded by a fuel burner ring.
7. The abatement system of claim 2, wherein the fuel burner ring comprises a number of ports approximately in the range of 8-30 ports.
8. An abatement system, comprising:
a combustion chamber; and
a fuel flow control mechanism coupled with the combustion chamber.
9. The abatement system of claim 8, wherein the fuel flow control mechanism comprises a vacuum generator device configured to be driven by a high pressure airflow.
10. The abatement system of claim 9, wherein the vacuum generator device is configured such that the high pressure airflow creates a slight vacuum for drawing gaseous fuel into the vacuum generator device.
11. The abatement system of claim 10, wherein the vacuum generator device is the sole fuel flow control mechanism in the abatement system.
12. The abatement system of claim 10, wherein the vacuum generator device is further coupled with a pressure regulator as an additional fuel flow control mechanism in the abatement system.
13. The abatement system of claim 10, wherein the vacuum generator device is further configured to mix a fuel flow and an airflow.
14. An abatement system, comprising:
a combustion chamber;
a fuel burner ring coupled with the combustion chamber; and
a fuel flow control mechanism coupled with the combustion chamber.
15. The abatement system of claim 14, wherein the fuel burner ring comprises a plurality of ports, and wherein the fuel flow control mechanism comprises a vacuum generator device configured to be driven by a high pressure airflow.
16. The abatement system of claim 15, wherein the vacuum generator device is configured such that the high pressure airflow creates a slight vacuum for drawing a fuel into the vacuum generator device, and wherein the plurality of ports is arranged to provide an approximately uniform flow pattern of the fuel provided to the plurality of ports.
17. The abatements system of claim 16, wherein the approximately uniform flow pattern of the fuel is provided along a length of the combustion chamber, and wherein the vacuum generator device is the sole fuel flow control mechanism in the abatement system.
18. The abatement system of claim 17, wherein the vacuum generator device is further coupled with a pressure regulator as an additional fuel flow control mechanism in the abatement system, the abatement system further comprising:
a process gas inlet tube to introduce a process gas into the combustion chamber, the process gas inlet tube surrounded by the fuel burner ring.
19. The abatement system of claim 18, wherein the vacuum generator device is further configured to mix a fuel flow and an airflow, the abatement system further comprising:
one or more additional process gas inlet tubes, each of the one or more additional process gas inlet tubes surrounded by a fuel burner ring.
20. The abatement system of claim 15, wherein the fuel burner ring comprises a number of ports approximately in the range of 8-30 ports.
US12/613,883 2008-11-10 2009-11-06 Abatement system Abandoned US20100119984A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US12/613,883 US20100119984A1 (en) 2008-11-10 2009-11-06 Abatement system
CN2009801449462A CN102210006A (en) 2008-11-10 2009-11-09 Abatement system
KR1020117013222A KR20110095305A (en) 2008-11-10 2009-11-09 Abatement system
PCT/US2009/063692 WO2010054291A2 (en) 2008-11-10 2009-11-09 Abatement system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11314308P 2008-11-10 2008-11-10
US12/613,883 US20100119984A1 (en) 2008-11-10 2009-11-06 Abatement system

Publications (1)

Publication Number Publication Date
US20100119984A1 true US20100119984A1 (en) 2010-05-13

Family

ID=42153609

Family Applications (1)

Application Number Title Priority Date Filing Date
US12/613,883 Abandoned US20100119984A1 (en) 2008-11-10 2009-11-06 Abatement system

Country Status (4)

Country Link
US (1) US20100119984A1 (en)
KR (1) KR20110095305A (en)
CN (1) CN102210006A (en)
WO (1) WO2010054291A2 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090214991A1 (en) * 2008-02-18 2009-08-27 Applied Materials, Inc. Apparatus and methods for supplying fuel employed by abatement systems to effectively abate effluents
US20160146458A1 (en) * 2013-07-17 2016-05-26 Edwards Limited A head assembly for a radiant burner
US10269600B2 (en) 2016-03-15 2019-04-23 Applied Materials, Inc. Methods and assemblies for gas flow ratio control
US10453721B2 (en) 2016-03-15 2019-10-22 Applied Materials, Inc. Methods and assemblies for gas flow ratio control
WO2020008177A1 (en) * 2018-07-03 2020-01-09 Edwards Limited Gas abatement apparatus
US11517831B2 (en) * 2019-06-25 2022-12-06 George Andrew Rabroker Abatement system for pyrophoric chemicals and method of use

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20190085358A (en) 2018-01-10 2019-07-18 김진홍 An apparatus and a method for removing harmful fluoride by using aqueous methanol solution
GB2608816A (en) * 2021-07-13 2023-01-18 Edwards Ltd Abatement apparatus

Citations (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1871783A (en) * 1928-02-27 1932-08-16 Cleveland Heater Co Dual gas burner
US2369235A (en) * 1941-05-10 1945-02-13 Servel Inc Gas burner
US2573502A (en) * 1945-05-23 1951-10-30 Gen Motors Corp Multichambered gas burner with selective gas supply
US2992531A (en) * 1958-07-11 1961-07-18 Westinghouse Electric Corp Turbine apparatus
US3302684A (en) * 1965-04-15 1967-02-07 Aero Flow Dynamics Inc Combination gas and liquid fuel burner
US3308869A (en) * 1965-12-17 1967-03-14 Combustion Eng Liquid fuel burner for wide range of load
US3376098A (en) * 1966-08-29 1968-04-02 Phillips Petroleum Co Two-chamber burner and process
US3615213A (en) * 1969-05-01 1971-10-26 Air Reduction Method and apparatus for the production of carbon black
US3644077A (en) * 1970-11-02 1972-02-22 S I Johnson Co Flame stabilizing system for power gas burners
US3729285A (en) * 1972-05-22 1973-04-24 G Schwedersky Burner and method of operating it to control the production of nitrogen oxides
US3827851A (en) * 1972-10-03 1974-08-06 Peabody Gordon Piatt Combination, oil, gas, and/or solid burner
US3859935A (en) * 1972-10-03 1975-01-14 Peabody Gordon Piatt Process using a combination, oil, gas, and/or solid burner
US3905753A (en) * 1972-08-26 1975-09-16 Hilmar Vits Compact burner for dryers
US4105394A (en) * 1976-10-18 1978-08-08 John Zink Company Dual pressure flare
US4122674A (en) * 1976-12-27 1978-10-31 The Boeing Company Apparatus for suppressing combustion noise within gas turbine engines
US4475885A (en) * 1983-07-28 1984-10-09 Bloom Engineering Company, Inc. Adjustable flame burner
US4480559A (en) * 1983-01-07 1984-11-06 Combustion Engineering, Inc. Coal and char burner
US5178210A (en) * 1989-10-24 1993-01-12 Gaz De France Vapor pump employing counterflow exchange between air and combustion products without an intermediate fluid
US5203692A (en) * 1990-01-29 1993-04-20 F. L. Smidth & Co. A/S Burner for solid and liquid or gaseous fuel
US20010019815A1 (en) * 1998-11-09 2001-09-06 Jakob Keller Method for preventing flow instabilities in a burner
US20020182553A1 (en) * 2000-12-23 2002-12-05 Paschereit Christian Oliver Burner for the production of a hot gas
US6655137B1 (en) * 2001-06-25 2003-12-02 Amir A. Sardari Advanced combined cycle co-generation abatement system
US20040023179A1 (en) * 2000-09-12 2004-02-05 Gerhard Grob Spray burner for the thermal decomposition of sulphur-containing residues
US20040168900A1 (en) * 2003-02-27 2004-09-02 Peter Tung Staged heat and mass transfer applications
US20050037305A1 (en) * 1999-12-15 2005-02-17 Koji Moriya Fluid distributor, burner apparatus, gas turbine engine and co-generation system
US20050147934A1 (en) * 2002-03-16 2005-07-07 George Stephens Burner with high capacity venturi
US6916172B2 (en) * 2003-08-25 2005-07-12 L & S Cryogenics, Inc. Burner apparatus
US20050250062A1 (en) * 2004-05-06 2005-11-10 New Power Concepts Llc Gaseous fuel burner
US20050271990A1 (en) * 2004-02-25 2005-12-08 Coen Company, Inc. Energy efficient low NOx burner and method of operating same
US20070053803A1 (en) * 2005-09-02 2007-03-08 Clean Systems Korea Inc. Scrubber for processing semiconductor waste gas
US7214349B2 (en) * 1996-12-31 2007-05-08 Applied Materials, Inc. Effluent gas stream treatment system having utility for oxidation treatment of semiconductor manufacturing effluent gases
US20080003150A1 (en) * 2006-02-11 2008-01-03 Applied Materials, Inc. Methods and apparatus for pfc abatement using a cdo chamber
US20080213714A1 (en) * 2005-11-11 2008-09-04 Alexander Knoch Rotary Furnace Burner
US20080280237A1 (en) * 2007-05-10 2008-11-13 Siemens Aktiengesellschaft Oil gasification burner for ash-free liquid fuel
US20080318174A1 (en) * 2006-04-14 2008-12-25 Christophe Leclerc Gas burner for oven

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7569193B2 (en) * 2003-12-19 2009-08-04 Applied Materials, Inc. Apparatus and method for controlled combustion of gaseous pollutants
US7736599B2 (en) * 2004-11-12 2010-06-15 Applied Materials, Inc. Reactor design to reduce particle deposition during process abatement
US7682574B2 (en) * 2004-11-18 2010-03-23 Applied Materials, Inc. Safety, monitoring and control features for thermal abatement reactor
CN101300411B (en) * 2005-10-31 2012-10-03 应用材料公司 Process abatement reactor

Patent Citations (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1871783A (en) * 1928-02-27 1932-08-16 Cleveland Heater Co Dual gas burner
US2369235A (en) * 1941-05-10 1945-02-13 Servel Inc Gas burner
US2573502A (en) * 1945-05-23 1951-10-30 Gen Motors Corp Multichambered gas burner with selective gas supply
US2992531A (en) * 1958-07-11 1961-07-18 Westinghouse Electric Corp Turbine apparatus
US3302684A (en) * 1965-04-15 1967-02-07 Aero Flow Dynamics Inc Combination gas and liquid fuel burner
US3308869A (en) * 1965-12-17 1967-03-14 Combustion Eng Liquid fuel burner for wide range of load
US3376098A (en) * 1966-08-29 1968-04-02 Phillips Petroleum Co Two-chamber burner and process
US3615213A (en) * 1969-05-01 1971-10-26 Air Reduction Method and apparatus for the production of carbon black
US3644077A (en) * 1970-11-02 1972-02-22 S I Johnson Co Flame stabilizing system for power gas burners
US3729285A (en) * 1972-05-22 1973-04-24 G Schwedersky Burner and method of operating it to control the production of nitrogen oxides
US3905753A (en) * 1972-08-26 1975-09-16 Hilmar Vits Compact burner for dryers
US3827851A (en) * 1972-10-03 1974-08-06 Peabody Gordon Piatt Combination, oil, gas, and/or solid burner
US3859935A (en) * 1972-10-03 1975-01-14 Peabody Gordon Piatt Process using a combination, oil, gas, and/or solid burner
US4105394A (en) * 1976-10-18 1978-08-08 John Zink Company Dual pressure flare
US4122674A (en) * 1976-12-27 1978-10-31 The Boeing Company Apparatus for suppressing combustion noise within gas turbine engines
US4480559A (en) * 1983-01-07 1984-11-06 Combustion Engineering, Inc. Coal and char burner
US4475885A (en) * 1983-07-28 1984-10-09 Bloom Engineering Company, Inc. Adjustable flame burner
US5178210A (en) * 1989-10-24 1993-01-12 Gaz De France Vapor pump employing counterflow exchange between air and combustion products without an intermediate fluid
US5203692A (en) * 1990-01-29 1993-04-20 F. L. Smidth & Co. A/S Burner for solid and liquid or gaseous fuel
US7214349B2 (en) * 1996-12-31 2007-05-08 Applied Materials, Inc. Effluent gas stream treatment system having utility for oxidation treatment of semiconductor manufacturing effluent gases
US20010019815A1 (en) * 1998-11-09 2001-09-06 Jakob Keller Method for preventing flow instabilities in a burner
US20050037305A1 (en) * 1999-12-15 2005-02-17 Koji Moriya Fluid distributor, burner apparatus, gas turbine engine and co-generation system
US20040023179A1 (en) * 2000-09-12 2004-02-05 Gerhard Grob Spray burner for the thermal decomposition of sulphur-containing residues
US20020182553A1 (en) * 2000-12-23 2002-12-05 Paschereit Christian Oliver Burner for the production of a hot gas
US6655137B1 (en) * 2001-06-25 2003-12-02 Amir A. Sardari Advanced combined cycle co-generation abatement system
US20050147934A1 (en) * 2002-03-16 2005-07-07 George Stephens Burner with high capacity venturi
US20040168900A1 (en) * 2003-02-27 2004-09-02 Peter Tung Staged heat and mass transfer applications
US6916172B2 (en) * 2003-08-25 2005-07-12 L & S Cryogenics, Inc. Burner apparatus
US20050271990A1 (en) * 2004-02-25 2005-12-08 Coen Company, Inc. Energy efficient low NOx burner and method of operating same
US20050250062A1 (en) * 2004-05-06 2005-11-10 New Power Concepts Llc Gaseous fuel burner
US7934926B2 (en) * 2004-05-06 2011-05-03 Deka Products Limited Partnership Gaseous fuel burner
US20070053803A1 (en) * 2005-09-02 2007-03-08 Clean Systems Korea Inc. Scrubber for processing semiconductor waste gas
US20080213714A1 (en) * 2005-11-11 2008-09-04 Alexander Knoch Rotary Furnace Burner
US20080003150A1 (en) * 2006-02-11 2008-01-03 Applied Materials, Inc. Methods and apparatus for pfc abatement using a cdo chamber
US20080318174A1 (en) * 2006-04-14 2008-12-25 Christophe Leclerc Gas burner for oven
US20080280237A1 (en) * 2007-05-10 2008-11-13 Siemens Aktiengesellschaft Oil gasification burner for ash-free liquid fuel

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090214991A1 (en) * 2008-02-18 2009-08-27 Applied Materials, Inc. Apparatus and methods for supplying fuel employed by abatement systems to effectively abate effluents
US20160146458A1 (en) * 2013-07-17 2016-05-26 Edwards Limited A head assembly for a radiant burner
US11162676B2 (en) * 2013-07-17 2021-11-02 Edwards Limited Head assembly for a radiant burner
US10269600B2 (en) 2016-03-15 2019-04-23 Applied Materials, Inc. Methods and assemblies for gas flow ratio control
US10453721B2 (en) 2016-03-15 2019-10-22 Applied Materials, Inc. Methods and assemblies for gas flow ratio control
US10943803B2 (en) 2016-03-15 2021-03-09 Applied Materials, Inc. Methods and assemblies for gas flow ratio control
US11462426B2 (en) 2016-03-15 2022-10-04 Applied Materials, Inc. Methods and assemblies for gas flow ratio control
US11923221B2 (en) 2016-03-15 2024-03-05 Applied Materials, Inc. Methods and assemblies for gas flow ratio control
WO2020008177A1 (en) * 2018-07-03 2020-01-09 Edwards Limited Gas abatement apparatus
US11517831B2 (en) * 2019-06-25 2022-12-06 George Andrew Rabroker Abatement system for pyrophoric chemicals and method of use

Also Published As

Publication number Publication date
WO2010054291A2 (en) 2010-05-14
WO2010054291A3 (en) 2010-07-29
CN102210006A (en) 2011-10-05
KR20110095305A (en) 2011-08-24

Similar Documents

Publication Publication Date Title
US20100119984A1 (en) Abatement system
EP2396598B1 (en) Method of treating an exhaust gas stream
KR101417181B1 (en) Combustive destruction of noxious substances
US7736608B2 (en) Methods and systems for reducing the emissions from combustion gases
US9023303B2 (en) Extended or multiple reaction zones in scrubbing apparatus
JP7091312B2 (en) Ammonia injection regulation for gas turbine selective catalytic reduction system
JPWO2008096466A1 (en) Gas processing apparatus, gas processing system and gas processing method using the apparatus
KR101640251B1 (en) Method and burner for burning with oxygen
TW201938248A (en) Abatement
US20200033000A1 (en) Method and apparatus for exhaust gas abatement under reduced pressure
CN105873662A (en) Arrangement of combustor and device for selective non catalytic reduction and pulsed injection method
US20100143222A1 (en) Exhaust condensate removal apparatus for abatement system
CN103813861B (en) surface processing device and method
TW201029727A (en) Abatement system
KR102676559B1 (en) Nozzle and related method for transporting plasma stream for plasma reduction
GB2568772A (en) Gas treating apparatus
KR102064662B1 (en) Environmentally hazardous waste gas processing system and burner structure used thereof
Kishi et al. Characteristics of hydrogen combustion in an experimental lean premixed combustor
JP2000213726A (en) Method and device for dioxin reduction
KR100879800B1 (en) Hybrid gas scrubber
Sharma et al. Influence of fuel volatility on combustion and emission characteristics in a gas turbine combustor at different inlet pressures and swirl conditions
JPH1151312A (en) Low nox combustion equipment for liquid fuel
KR20200001585A (en) Environmentally hazardous waste gas processing system and burner structure used thereof
KR20200062218A (en) Nozzle and related method for transferring plasma stream for plasma reduction
CN117242302A (en) Combustion apparatus

Legal Events

Date Code Title Description
AS Assignment

Owner name: APPLIED MATERIALS, INC.,CALIFORNIA

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:FOX, ALLEN G.;REEL/FRAME:023836/0020

Effective date: 20100111

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION