SU1666868A1 - Injection gas burner - Google Patents
Injection gas burner Download PDFInfo
- Publication number
- SU1666868A1 SU1666868A1 SU894641090A SU4641090A SU1666868A1 SU 1666868 A1 SU1666868 A1 SU 1666868A1 SU 894641090 A SU894641090 A SU 894641090A SU 4641090 A SU4641090 A SU 4641090A SU 1666868 A1 SU1666868 A1 SU 1666868A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- mixing chamber
- gas
- swirler
- nozzle
- air
- Prior art date
Links
Abstract
Изобретение относитс к энергетике и может быть использовано в технологических печах различных отраслей промышленности с целью повышени качества сжигани . Газ через патрубок 7 поступает в газовый коллектор 4, откуда, интенсивно закручива сь в завихрителе 5, попадает в кольцевой канал 3 и далее в смесительную камеру 1. Благодар разрежению в смесительной камере 1 через сопло 2 Лавал инжектируетс воздух, который, перемешива сь в смесительной камере с топливным газом, образует топливовоздушную смесь, сгорающую при выходе из смесительной камеры 1. Выполнение рассто ни между торцом сопла 2 Лавал и завихрителем 5 равным 0,3...2,4 ширины завихрител 5 позвол ет существенно интенсифицировать процесс образовани топливовоздушной смеси и повысить качество сжигани . 2 ил.The invention relates to energy and can be used in technological furnaces of various industries with the aim of improving the quality of combustion. Gas through pipe 7 enters the gas manifold 4, from which, swirling intensively in the swirler 5, enters the annular channel 3 and further into the mixing chamber 1. Due to the vacuum in the mixing chamber 1, air is injected through the nozzle 2 of Laval, which, mixing in the mixing The chamber with the fuel gas forms an air-fuel mixture that burns out of the mixing chamber 1 when executing. The distance between the end of the Laval nozzle 2 and the swirler 5 of 0.3 ... 2.4 widths of the swirler 5 makes it possible to significantly intensify the process developing the air-fuel mixture and improving the quality of combustion. 2 Il.
Description
фиг.1figure 1
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU894641090A SU1666868A1 (en) | 1989-01-20 | 1989-01-20 | Injection gas burner |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU894641090A SU1666868A1 (en) | 1989-01-20 | 1989-01-20 | Injection gas burner |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1666868A1 true SU1666868A1 (en) | 1991-07-30 |
Family
ID=21424487
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU894641090A SU1666868A1 (en) | 1989-01-20 | 1989-01-20 | Injection gas burner |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1666868A1 (en) |
-
1989
- 1989-01-20 SU SU894641090A patent/SU1666868A1/en active
Non-Patent Citations (1)
Title |
---|
Авторское свидетельство СССР Nfe 1588991, кл. F 23 D 14/04. 1989. * |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1530831A (en) | Low nox burner | |
CA2190063C (en) | Radial inflow dual fuel injector | |
US4893475A (en) | Combustion apparatus for a gas turbine | |
SU1666868A1 (en) | Injection gas burner | |
ATE207594T1 (en) | WHITE BURNER | |
TW362128B (en) | Ultra-low NOx combustor | |
JPS56133506A (en) | Method for effecting combustion generating bright flame | |
US5685705A (en) | Method and appliance for flame stabilization in premixing burners | |
GB1414043A (en) | Burner | |
GB2088474A (en) | I.C. engine cylinder head charge intake system | |
SU1276877A1 (en) | Burner | |
SU1195137A1 (en) | Oil-gas burner | |
SU1040279A1 (en) | Inspirator gas burner | |
CN219414757U (en) | Burner for unstable air source of single-well heating furnace | |
GB2083904A (en) | Improvements in or relating to gas turbine engine dual fuel burners | |
JPH0227307Y2 (en) | ||
JPS5579919A (en) | Flame jet burner | |
RU92006865A (en) | IZHEKTSIONNAYA GAS BURNER OF PARTIAL PRELIMINARY MIX | |
SU1462063A1 (en) | Method and apparatus for burning up gaseous fuel | |
RU2013693C1 (en) | Burner | |
SU1153188A1 (en) | Burner | |
SU1163088A1 (en) | Method of combined burning of dust-like and gaseous fuel | |
JPS6446516A (en) | Burner for radiant tube | |
SU1588991A1 (en) | Injection burner | |
SU1153184A1 (en) | Vortex burner |