[go: up one dir, main page]

RU2004133202A - METHOD OF INTENSIFICATION OF THE GAS COMBUSTION PROCESS AND BURNER DEVICE FOR ITS IMPLEMENTATION - Google Patents

METHOD OF INTENSIFICATION OF THE GAS COMBUSTION PROCESS AND BURNER DEVICE FOR ITS IMPLEMENTATION Download PDF

Info

Publication number
RU2004133202A
RU2004133202A RU2004133202/06A RU2004133202A RU2004133202A RU 2004133202 A RU2004133202 A RU 2004133202A RU 2004133202/06 A RU2004133202/06 A RU 2004133202/06A RU 2004133202 A RU2004133202 A RU 2004133202A RU 2004133202 A RU2004133202 A RU 2004133202A
Authority
RU
Russia
Prior art keywords
gas
collector
burner
gaseous fuel
flame
Prior art date
Application number
RU2004133202/06A
Other languages
Russian (ru)
Other versions
RU2287110C2 (en
Inventor
Виктор Ташеевич Чумак (RU)
Виктор Ташеевич Чумак
Original Assignee
Виктор Ташеевич Чумак (RU)
Виктор Ташеевич Чумак
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 Виктор Ташеевич Чумак (RU), Виктор Ташеевич Чумак filed Critical Виктор Ташеевич Чумак (RU)
Priority to RU2004133202/06A priority Critical patent/RU2287110C2/en
Publication of RU2004133202A publication Critical patent/RU2004133202A/en
Application granted granted Critical
Publication of RU2287110C2 publication Critical patent/RU2287110C2/en

Links

Landscapes

  • Gas Burners (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)

Claims (4)

1. Способ интенсификации процессов сжигания топлива и горелочное устройство для его реализации, включающий подачу первичного воздуха и вторичного, закрученного лопаточными завихрителями, газообразного топлива из коллектора через осевые и радиальные газовые отверстия и жидкого топлива посредством форсунки в зону горения, отличающийся тем, что газовый поток, выходящий из множества газовых сопел, расположенных радиально, смешивается со встречным ламинарным потоком воздуха с последующим резким снижением скорости сформированной газовоздушной смеси посредством угла раскрытия факела, предотвращающий проскок пламени вовнутрь горелки или отрыв пламени.1. A method of intensifying fuel combustion processes and a burner device for its implementation, comprising supplying primary air and secondary, swirling with blade swirls, gaseous fuel from the collector through axial and radial gas openings and liquid fuel by means of a nozzle into the combustion zone, characterized in that the gas stream coming out of a multitude of gas nozzles arranged radially is mixed with an oncoming laminar air flow, followed by a sharp decrease in the speed of the gas carrier formed Ear mixture by flame opening angle, which prevents leakage of the flame inside the burner or flame detachment. 2. Грелочное устройство, содержащее корпус с форсункой для подачи жидкого топлива, коллектор газообразного топлива с осевыми и радиальными отверстиями и цилиндрической перегородкой между корпусом горелки и коллектором газообразного топлива, отличающееся тем, что в газовом коллекторе выполнено множество газовых сопел количеством от 18 до 450 штук, диаметром от 1,0 до 7,5 мм, расположенных радиально на коллекторе газа.2. A heating device containing a housing with a nozzle for supplying liquid fuel, a gaseous fuel collector with axial and radial openings and a cylindrical partition between the burner body and the gaseous fuel collector, characterized in that a plurality of gas nozzles are made in the gas manifold from 18 to 450 pieces with a diameter of 1.0 to 7.5 mm located radially on the gas manifold. 3. Устройство по п.2, отличающееся тем, что угол наклона пластинчатых завихрителей должен составлять от 0 до 90°.3. The device according to claim 2, characterized in that the angle of inclination of the plate swirlers should be from 0 to 90 °. 4. Устройство по пп.2 и 3, отличающееся тем, что соотношение общей площади сечения сопел для выхода газа и общей площади сечения для потока воздуха должно быть в пределах 1-(15-25).4. The device according to PP.2 and 3, characterized in that the ratio of the total cross-sectional area of the nozzles for the gas outlet and the total cross-sectional area for the air flow should be within 1- (15-25).
RU2004133202/06A 2004-11-15 2004-11-15 Method for intensification of the process of gas burning and burner device for its realization RU2287110C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2004133202/06A RU2287110C2 (en) 2004-11-15 2004-11-15 Method for intensification of the process of gas burning and burner device for its realization

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2004133202/06A RU2287110C2 (en) 2004-11-15 2004-11-15 Method for intensification of the process of gas burning and burner device for its realization

Publications (2)

Publication Number Publication Date
RU2004133202A true RU2004133202A (en) 2006-04-27
RU2287110C2 RU2287110C2 (en) 2006-11-10

Family

ID=36655375

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2004133202/06A RU2287110C2 (en) 2004-11-15 2004-11-15 Method for intensification of the process of gas burning and burner device for its realization

Country Status (1)

Country Link
RU (1) RU2287110C2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2453767C2 (en) * 2008-05-12 2012-06-20 Виктор Ташеевич Чумак Method to intensify process of fuel burning and burner device for its realisation
FR3003632B1 (en) * 2013-03-19 2016-10-14 Snecma INJECTION SYSTEM FOR TURBOMACHINE COMBUSTION CHAMBER HAVING AN ANNULAR WALL WITH CONVERGENT INTERNAL PROFILE
RU2551439C1 (en) * 2014-05-21 2015-05-27 Тимофей Логинович Басаргин Burner device for burning of gaseous and liquid fuel

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2011847C3 (en) * 1970-03-12 1979-03-08 Kuibyschevskij Filial Vsesojuznogo Nautschno-Issledovatelskogo Instituta Neftepererabatyvajuschei Promyschlennosti, Ussr, Nowokuibyschewsk (Sowjetunion) Burners for gaseous and liquid fuel
DE3446788A1 (en) * 1984-12-21 1986-07-03 L. & C. Steinmüller GmbH, 5270 Gummersbach Flame vaporising-burner with precombustion chamber
RU2122154C1 (en) * 1995-01-17 1998-11-20 Акционерное общество открытого типа "Экотеплогаз" Method and device for raising power characteristics and environmental friendliness of burner devices
JP2003074804A (en) * 2001-09-05 2003-03-12 Mitsubishi Electric Corp Combustion device

Also Published As

Publication number Publication date
RU2287110C2 (en) 2006-11-10

Similar Documents

Publication Publication Date Title
US6282904B1 (en) Full ring fuel distribution system for a gas turbine combustor
RU2012158338A (en) DEVICE CONTAINING FUEL INJECTORS OF GAS TURBINE (OPTIONS)
CN102563701A (en) Premixing nozzle
CN109114592A (en) The method of combustion system and the combustion product for generating tool premixed flame characteristic
CN102401380A (en) Apparatus and method for mixing fuel in gas turbine nozzle
RU2002134603A (en) THE IMPROVED COMBINATION OF THE PRELIMINARY MIXING CHAMBER AND THE COMBUSTION CHAMBER WITH A SMALL EMISSION OF EMISSIONS FOR GAS TURBINES OPERATING LIQUID AND LIQUID-LIQUID
CA2414034A1 (en) Improved combination of a premixing chamber and a combustion chamber, with low emission of pollutants, for gas turbines running on liquid and/or gas fuel
RU2040731C1 (en) Fuel gasification burner
RU2004133202A (en) METHOD OF INTENSIFICATION OF THE GAS COMBUSTION PROCESS AND BURNER DEVICE FOR ITS IMPLEMENTATION
CN112555829A (en) Spray gun capable of generating supersonic airflow
RU182300U1 (en) Annular combustion chamber of a gas turbine plant
CN206755165U (en) A kind of burner with blossom type nozzle
RU38218U1 (en) DEVICE FOR PREPARING AND SUBMITTING A FUEL-AIR MIXTURE TO THE COMBUSTION CHAMBER
CN115451433A (en) Fuel nozzle premixing system for gas turbine combustor
RU2639823C1 (en) Two-flow gas burner
RU114514U1 (en) Gas oil burner
RU179847U1 (en) FURNACE SUPPORT DEVICE
RU2454605C1 (en) Technological vortex ejection gas burner
RU66009U1 (en) TWO-FLOW GAS BURNER
US20240200771A1 (en) HIGH PERFORMANCE LOW NOx BURNER AND SYSTEM
RU2035663C1 (en) Waste gas burning device
US20240401798A1 (en) HIGH PERFORMANCE LOW NOx BURNER AND SYSTEM AND METHOD OF OPERATION
CN223106025U (en) Burners and boilers that can reduce NOx generation
RU194569U1 (en) DEVICE FOR PREPARING FOR GAS FUEL COMBUSTION
RU2791067C1 (en) Burner module with a double-walled atomizer of a low-emission multi-module combustion chamber

Legal Events

Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20141116