ES417780A1 - Apparatus for determining air flow to a gas burner - Google Patents
Apparatus for determining air flow to a gas burnerInfo
- Publication number
- ES417780A1 ES417780A1 ES417780A ES417780A ES417780A1 ES 417780 A1 ES417780 A1 ES 417780A1 ES 417780 A ES417780 A ES 417780A ES 417780 A ES417780 A ES 417780A ES 417780 A1 ES417780 A1 ES 417780A1
- Authority
- ES
- Spain
- Prior art keywords
- burners
- air flow
- gas burner
- air
- determining air
- 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.)
- Expired
Links
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
- F23C7/00—Combustion apparatus characterised by arrangements for air supply
- F23C7/008—Flow control devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D17/00—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Regulation And Control Of Combustion (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
- Combustion Of Fluid Fuel (AREA)
Abstract
An apparatus for determining air flow to one or more burners of a furnace or the like wherein an enclosure is provided which surrounds the burners and receives air for supply to the burners. A register assembly is provided in the enclosure and cooperates with the burners to direct a predetermined portion of the air to a combustion zone adjacent each of the burners. A static pressure zone is created for the latter portion of air to enable its static pressure to be measured and the air flow to be determined.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US27883972A | 1972-08-02 | 1972-08-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
ES417780A1 true ES417780A1 (en) | 1976-03-01 |
Family
ID=23066597
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES417780A Expired ES417780A1 (en) | 1972-08-02 | 1973-08-02 | Apparatus for determining air flow to a gas burner |
Country Status (4)
Country | Link |
---|---|
US (1) | US3765824A (en) |
JP (2) | JPS4967223A (en) |
CA (1) | CA976078A (en) |
ES (1) | ES417780A1 (en) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3897199A (en) * | 1974-07-05 | 1975-07-29 | Foster Wheeler Corp | Burner assembly having a tertiary air nozzle |
US4050879A (en) * | 1974-11-18 | 1977-09-27 | Mitsubishi Jukogyo Kabushiki Kaisha | Fuel combustion apparatus |
JPS6122146U (en) * | 1984-07-10 | 1986-02-08 | 日新電機株式会社 | Abnormality detection device for electrical equipment |
JPS62107241U (en) * | 1985-12-24 | 1987-07-09 | ||
US5572862A (en) * | 1993-07-07 | 1996-11-12 | Mowill Rolf Jan | Convectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules |
US5638674A (en) * | 1993-07-07 | 1997-06-17 | Mowill; R. Jan | Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission |
US6220034B1 (en) | 1993-07-07 | 2001-04-24 | R. Jan Mowill | Convectively cooled, single stage, fully premixed controllable fuel/air combustor |
US5924276A (en) * | 1996-07-17 | 1999-07-20 | Mowill; R. Jan | Premixer with dilution air bypass valve assembly |
US6925809B2 (en) | 1999-02-26 | 2005-08-09 | R. Jan Mowill | Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities |
US6327860B1 (en) * | 2000-06-21 | 2001-12-11 | Honeywell International, Inc. | Fuel injector for low emissions premixing gas turbine combustor |
JP2002039533A (en) * | 2000-07-21 | 2002-02-06 | Mitsubishi Heavy Ind Ltd | Combustor, gas turbine, and jet engine |
US20070277530A1 (en) * | 2006-05-31 | 2007-12-06 | Constantin Alexandru Dinu | Inlet flow conditioner for gas turbine engine fuel nozzle |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3486834A (en) * | 1968-04-25 | 1969-12-30 | Combustion Eng | Gas burning system arrangement |
US3700376A (en) * | 1970-12-28 | 1972-10-24 | Babcock & Wilcox Ag | Oil burner |
JPS4711177U (en) * | 1971-02-24 | 1972-10-09 |
-
1972
- 1972-08-02 US US00278839A patent/US3765824A/en not_active Expired - Lifetime
-
1973
- 1973-07-26 CA CA177,397A patent/CA976078A/en not_active Expired
- 1973-07-31 JP JP48086305A patent/JPS4967223A/ja active Pending
- 1973-08-02 ES ES417780A patent/ES417780A1/en not_active Expired
-
1978
- 1978-05-15 JP JP1978064008U patent/JPS542231U/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
US3765824A (en) | 1973-10-16 |
JPS4967223A (en) | 1974-06-29 |
CA976078A (en) | 1975-10-14 |
JPS542231U (en) | 1979-01-09 |
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