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RU95101416A - Burner assembly - Google Patents

Burner assembly

Info

Publication number
RU95101416A
RU95101416A RU95101416/06A RU95101416A RU95101416A RU 95101416 A RU95101416 A RU 95101416A RU 95101416/06 A RU95101416/06 A RU 95101416/06A RU 95101416 A RU95101416 A RU 95101416A RU 95101416 A RU95101416 A RU 95101416A
Authority
RU
Russia
Prior art keywords
nozzle
liquid
gas
housing
cylindrical portion
Prior art date
Application number
RU95101416/06A
Other languages
Russian (ru)
Other versions
RU2106574C1 (en
Inventor
В.С. Варфоломеев
О.В. Дунай
В.Я. Кузнецов
И.А. Образцов
О.В. Строгонов
В.А. Щукин
Original Assignee
Казанский государственный технический университет им.А.Н.Туполева
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 Казанский государственный технический университет им.А.Н.Туполева filed Critical Казанский государственный технический университет им.А.Н.Туполева
Priority to RU95101416A priority Critical patent/RU2106574C1/en
Publication of RU95101416A publication Critical patent/RU95101416A/en
Application granted granted Critical
Publication of RU2106574C1 publication Critical patent/RU2106574C1/en

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00Combustion technologies with mitigation potential
    • Y02E20/34Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery

Landscapes

  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Abstract

FIELD: heat power engineering; combustion of gaseous and liquid fuels. SUBSTANCE: burner assembly has housing 1, flame tube 2, air supply branch pipe 3, glow plug 4, gas-liquid nozzle 5 and gas-liquid evaporating nozzle 6. Flame tube 2 is installed with clearance along axis of housing 1 forming secondary air supply space 7. Ring swirler 8 is installed at output of burner assembly at end of secondary air supply space. Gas- liquid evaporating nozzle 6 has flat end face portion by means of which it is installed along axis of burner assembly, input cylindrical portion, conical adapter, output cylindrical portion of diameter smaller than that of input portion and tubular evaporating coil 9 with gaseous or liquid fuel supply channel 10. Input cylindrical portion of evaporating gas-liquid nozzle 6 with system of holes to deliver air into end face space 11 of standing flame with swirler 12 placed in each flame, and flat end face portion form end face space 13 together with housing 1. Output cylindrical portion of nozzle 6 has ring manifold 15 with system of chordal holes 16. Output end of tubular evaporating coil 9 is connected with ring manifold 15. Flame damper-stabilizer 18 is installed between output cylindrical portion of nozzle 6 and flame tube 2 at end of channel 17. Glow plug is installed along nozzle axis in its inner space 27. EFFECT: reduced ejection of harmful substances, enlarged range of stable burning. 5 cl

Claims (1)

Изобретение относится к теплоэнергетике и может быть использовано в различных теплотехнических устройствах для сжигания газообразного и жидкого топлива. Цель - снижение выбросов вредных веществ и расширение диапазона устойчивого горения по расходу топлива. Горелочное устройство содержит корпус 1, жаровую трубу 2, воздухоподводящий патрубок 3, свечу зажигания 4, газожидкостную форсунку 5 и газожидкостную испарительную форсунку 6. Жаровая труба 2 установлена по оси корпуса 1 с зазором, образуя полость подвода вторичного воздуха 7, в конце которой на выходе из горелочного устройства, установлен кольцевой завихритель 8. Форсунка 6 включает в себя плоскую торцевую часть, с помощью которой она устанавливается по оси горелочного устройства, входную цилиндрическую часть, конической переходник, выходную цилиндрическую часть меньшего диаметра, чем входная часть и трубчатый испарительный змеевик 9 с каналом подвода газообразного или жидкого топлива 10. Входная цилиндрическая часть испарительной газожидкостной форсунки 6 с системой отверстий для подвода воздуха в торцевую полость 11 дежурного факела, в каждом из которых установлены завихрители 12 и плоская торцевая ее часть, образуют с корпусом 1 торцевую полость 13. Выходная цилиндрическая часть форсунки 6 имеет кольцевой коллектор 15 с системой хордальных отверстий 16. Выходной конец трубчатого испарительного змеевика 9 соединен с кольцевым коллектором 15. В конце канала 17 между выходной цилиндрической частью форсунки 6 и жаровой трубой 2 установлен антифламинг-стабилизатор 18. По оси форсунки 5 в ее внутренней полости 27 установлена свеча зажигания.The invention relates to a power system and can be used in various heat engineering devices for burning gaseous and liquid fuels. The goal is to reduce emissions of harmful substances and expand the range of sustainable combustion for fuel consumption. The burner device comprises a housing 1, a heat pipe 2, an air supply pipe 3, a spark plug 4, a gas-liquid nozzle 5, and a gas-liquid vaporization nozzle 6. The heat pipe 2 is installed along the axis of the housing 1 with a gap, forming a secondary air supply cavity 7, at the end of which there is an outlet an annular swirler is installed from the burner 8. The nozzle 6 includes a flat end part, with which it is installed along the axis of the burner, the inlet cylindrical part, the conical adapter, the outlet a cylindrical part of a smaller diameter than the inlet part and the tubular evaporative coil 9 with a channel for supplying gaseous or liquid fuel 10. The inlet cylindrical part of the vaporizing gas-liquid nozzle 6 with a system of holes for supplying air to the end cavity 11 of the standby torch, in each of which swirls 12 and its flat end part forms an end cavity 13 with the housing 1. The output cylindrical part of the nozzle 6 has an annular collector 15 with a system of chordal openings 16. The output end is tubular second evaporator coil 9 is connected to the annular manifold 15. At the end of the channel 17 between the outlet cylindrical portion of the nozzle 6 and the flame tube 2 is antiflaming stabilizer 18. As the nozzle axis 5 in the inner cavity 27 is set a spark plug.
RU95101416A 1995-01-31 1995-01-31 Burner assembly RU2106574C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU95101416A RU2106574C1 (en) 1995-01-31 1995-01-31 Burner assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU95101416A RU2106574C1 (en) 1995-01-31 1995-01-31 Burner assembly

Publications (2)

Publication Number Publication Date
RU95101416A true RU95101416A (en) 1996-11-20
RU2106574C1 RU2106574C1 (en) 1998-03-10

Family

ID=20164437

Family Applications (1)

Application Number Title Priority Date Filing Date
RU95101416A RU2106574C1 (en) 1995-01-31 1995-01-31 Burner assembly

Country Status (1)

Country Link
RU (1) RU2106574C1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2550370C2 (en) * 2011-05-11 2015-05-10 Альстом Текнолоджи Лтд Centrifugal nozzle with projecting parts
RU2497014C1 (en) * 2012-03-15 2013-10-27 Открытое Акционерное Общество "Российские Железные Дороги" Method to control gas temperature in system of fuel supply of gas turbine locomotives
RU193247U1 (en) * 2019-05-06 2019-10-21 Владимир Антонович Вторых BURNER

Also Published As

Publication number Publication date
RU2106574C1 (en) 1998-03-10

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