RU96112593A - BURNER - Google Patents
BURNERInfo
- Publication number
- RU96112593A RU96112593A RU96112593/06A RU96112593A RU96112593A RU 96112593 A RU96112593 A RU 96112593A RU 96112593/06 A RU96112593/06 A RU 96112593/06A RU 96112593 A RU96112593 A RU 96112593A RU 96112593 A RU96112593 A RU 96112593A
- Authority
- RU
- Russia
- Prior art keywords
- swirl
- sleeve
- precamera
- annular
- blades
- Prior art date
Links
- 239000000446 fuel Substances 0.000 claims 2
Claims (3)
l = k•h•cosφ,
где k - эмпирический коэффициент (k = 2,3 - 2,9);
h - высота лопатки завихрителя;
φ - угол закрутки потока в завихрителе.2. The burner according to claim 1, characterized in that the axial blade swirl is installed between the fuel distributing device and the output of the annular precamera, while the length of the annular precamera is determined by the formula
l = k • h • cosφ,
where k is an empirical coefficient (k = 2.3 - 2.9);
h is the height of the blade of the swirl;
φ is the swirl angle of the flow in the swirl.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU96112593A RU2099639C1 (en) | 1996-06-21 | 1996-06-21 | Burner |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU96112593A RU2099639C1 (en) | 1996-06-21 | 1996-06-21 | Burner |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2099639C1 RU2099639C1 (en) | 1997-12-20 |
RU96112593A true RU96112593A (en) | 1998-01-27 |
Family
ID=20182272
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU96112593A RU2099639C1 (en) | 1996-06-21 | 1996-06-21 | Burner |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2099639C1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2971038B1 (en) * | 2011-01-31 | 2013-02-08 | Snecma | INJECTION DEVICE FOR A TURBOMACHINE COMBUSTION CHAMBER |
RU2451878C1 (en) * | 2011-02-07 | 2012-05-27 | Открытое акционерное общество "Газпром" | Method for preliminary preparation and combustion of "lean" air-fuel mixture in low-emission burner |
RU2548525C1 (en) * | 2014-02-12 | 2015-04-20 | Открытое акционерное общество "Газпром" | Method to burn preliminary prepared lean air-fuel mixture in double-circuit low-emission burner with diffusion stabilising flare used |
CN104266228B (en) * | 2014-09-22 | 2018-02-09 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | Gas-turbine combustion chamber axial direction two-stage swirl nozzle in opposite direction |
RU205048U1 (en) * | 2020-09-07 | 2021-06-24 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Саратовский государственный технический университет имени Гагарина Ю.А." (СГТУ имени Гагарина Ю.А.) | High-speed gas burner |
-
1996
- 1996-06-21 RU RU96112593A patent/RU2099639C1/en not_active IP Right Cessation
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