JPS6339545Y2 - - Google Patents
Info
- Publication number
- JPS6339545Y2 JPS6339545Y2 JP1983068157U JP6815783U JPS6339545Y2 JP S6339545 Y2 JPS6339545 Y2 JP S6339545Y2 JP 1983068157 U JP1983068157 U JP 1983068157U JP 6815783 U JP6815783 U JP 6815783U JP S6339545 Y2 JPS6339545 Y2 JP S6339545Y2
- Authority
- JP
- Japan
- Prior art keywords
- nozzle
- combustion gas
- cooling air
- combustion
- combustion chamber
- 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
- 239000000567 combustion gas Substances 0.000 claims description 22
- 238000002485 combustion reaction Methods 0.000 claims description 18
- 238000001816 cooling Methods 0.000 claims description 17
- 239000002737 fuel gas Substances 0.000 description 3
- 230000003685 thermal hair damage Effects 0.000 description 3
- 239000000446 fuel Substances 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 229910052581 Si3N4 Inorganic materials 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Gas Burners (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
Description
【考案の詳細な説明】
〔産業上の利用分野〕
本考案は、内側壁部内に燃焼室を形成し、その
燃焼室の燃焼ガス噴出口を前記燃焼室よりも小径
に形成し、前記内側壁部の外側に、それに対する
冷却用空気流動のための中空部を形成し、その中
空部から冷却用空気を噴出するノズルを形成した
高速バーナ、詳しくは、冷却用空気噴出のための
ノズルの配置改良に関する。[Detailed description of the invention] [Industrial application field] The present invention forms a combustion chamber within an inner wall, and forms a combustion gas outlet of the combustion chamber with a diameter smaller than that of the combustion chamber. A high-speed burner that has a hollow part formed outside of the part for the flow of cooling air, and a nozzle for jetting cooling air from the hollow part, specifically, the arrangement of the nozzle for jetting the cooling air. Regarding improvements.
従来、例えば実公昭53−11869号公報や実開昭
55−162725号公報に示されるように、燃焼室を形
成する内側壁部に対して冷却作用した冷却用空気
を、中空部から燃焼室内に噴出するように、冷却
用空気噴出のためのノズルを配置していた。
Previously, for example, Utility Model Publication No. 53-11869 and Utility Model Publication No. 11869
As shown in Japanese Patent No. 55-162725, a nozzle for jetting cooling air is installed so that the cooling air that has a cooling effect on the inner wall forming the combustion chamber is jetted from the hollow part into the combustion chamber. It was placed.
しかし、燃焼室内でのほぼ完全燃焼によつて発
生した高圧で高温の燃焼ガスが燃焼ガス噴出口か
ら高速で噴出するに際し、燃焼ガス噴出口の周部
に位置するバーナ本体の先端部分が、高温の燃焼
ガスに直に接触するために極めて高温になり、早
期に熱損傷する欠点があつた。
However, when the high-pressure and high-temperature combustion gas generated by almost complete combustion in the combustion chamber is ejected from the combustion gas nozzle at high speed, the tip of the burner body located around the combustion gas nozzle becomes hot. Because they come into direct contact with combustion gases, they reach extremely high temperatures, resulting in early thermal damage.
本考案の目的は、ノズルの配置に改良を加える
だけの極めて簡単な手段でもつて、バーナ本体の
先端部分における熱損傷を十分に抑制できるよう
にする点にある。 An object of the present invention is to make it possible to sufficiently suppress thermal damage at the tip of the burner body by an extremely simple means that only improves the nozzle arrangement.
本考案の特徴構成は、冷却用空気噴出のための
ノズルを、燃焼ガス噴出口のほぼ全周にわたつ
て、かつ、その燃焼ガス噴出口からの燃焼ガス噴
出方向に対して同方向にほぼ平行に冷却用空気が
噴出される方向で配置したことにあり、その作用
効果は次の通りである。
The characteristic configuration of the present invention is that the nozzle for jetting cooling air is arranged around the entire circumference of the combustion gas nozzle and approximately parallel to the direction in which the combustion gas is jetted from the combustion gas nozzle. The cooling air is disposed in the direction in which the cooling air is blown out, and its effects are as follows.
つまり、ノズルからの冷却用空気は、燃焼ガス
噴出流のほぼ全周にわたつてほぼ平行に噴出され
るから、バーナ本体の先端部分と燃焼ガス噴出流
の間にエアーカーテンを形成し、バーナ本体と燃
焼ガスとの接触を抑制すると共にバーナ本体を強
制冷却する。
In other words, since the cooling air from the nozzle is ejected almost parallel to the entire circumference of the combustion gas jet, an air curtain is formed between the tip of the burner body and the combustion gas jet. This suppresses the contact between the burner and the combustion gas and forcibly cools the burner body.
したがつて、高温の燃焼ガスが高速で噴出され
るにもかかわらず、バーナ本体の先端部分におけ
る熱損傷を効果的に抑制できる。 Therefore, even though high-temperature combustion gas is ejected at high speed, thermal damage to the tip portion of the burner body can be effectively suppressed.
その結果、ノズルの配置改良という製作面及び
コスト面で有利な手段でもつて、耐久性向上を十
分に図れ、一段と寿命の長い高速バーナを提供で
きるようになつた。
As a result, it has become possible to sufficiently improve durability and provide a high-speed burner with a longer lifespan by improving the nozzle arrangement, which is advantageous in terms of manufacturing and cost.
次に、図面により実施例を示す。 Next, examples will be shown with reference to drawings.
二重壁構造のバーナ本体において、内側壁部1
1A内に燃焼室2を形成し、燃焼ガス噴出口1を
燃焼室2よりもかなり小径に形成してバーナ本体
の先端部分に設け、渦巻型燃焼器3を燃焼室1に
接続してバーナ本体の後端側に取付けてある。 In the burner body with a double wall structure, the inner wall portion 1
A combustion chamber 2 is formed in the burner body 1A, a combustion gas jet nozzle 1 is formed with a diameter considerably smaller than that of the combustion chamber 2, and is provided at the tip of the burner body, and a spiral combustor 3 is connected to the combustion chamber 1 and It is attached to the rear end of the.
渦巻型燃焼器を形成するに、ガスポート7に接
続した有底筒状の燃料ノズル9の周部に、多数の
燃料ガス用噴出孔8,10を形成し、エアポート
4に接続した燃焼用空気吸込口5からの噴出によ
つて空気旋回室6内で旋回流動する燃焼用空気に
噴出孔8,10からの燃料ガスを混合するように
構成し、空燃混合ガスを燃焼室2内で旋回させな
がら燃焼させるようにしてある。 To form a spiral combustor, a large number of fuel gas injection holes 8 and 10 are formed around the periphery of a bottomed cylindrical fuel nozzle 9 connected to the gas port 7, and combustion air connected to the air port 4 is formed. The fuel gas from the ejection holes 8 and 10 is mixed with the combustion air that swirls in the air swirling chamber 6 due to the ejection from the suction port 5, and the air-fuel mixture is swirled in the combustion chamber 2. It is designed so that it burns while it is burning.
内側壁部11Aの外側に外側壁部11により中
空部12を形成し、中空部12をエアポート4に
給気口14で接続し、中空部12での冷却用空気
流動により内側壁部11Aの焼損を抑制してあ
る。 A hollow part 12 is formed by the outer wall part 11 on the outside of the inner wall part 11A, and the hollow part 12 is connected to the air port 4 through the air supply port 14, and the inner wall part 11A is burnt out due to the flow of cooling air in the hollow part 12. has been suppressed.
中空部12から冷却用空気を噴出するノズル1
3を、燃焼ガス噴出口1のほぼ全周にわたつて、
かつ、燃焼ガス噴出方向に対して同方向にほぼ平
行に冷却用空気が噴出される方向で配置し、ノズ
ル13からの冷却用空気によるエアーカーテンに
よつて、燃焼ガス噴出流によるバーナ本体の先端
部分における焼損を抑制してある。 Nozzle 1 that blows out cooling air from hollow part 12
3 over almost the entire circumference of the combustion gas nozzle 1,
The cooling air is jetted out in the same direction as the combustion gas jetting direction, and the air curtain of the cooling air from the nozzle 13 prevents the tip of the burner body from being blown out by the jetting flow of the combustion gas. Burnout in some parts is suppressed.
内外側壁部11A,11は金属や焼成耐火物
(炭化硅素、窒化硅素、アルミナなど)から成つ
ている。 The inner and outer wall portions 11A, 11 are made of metal or fired refractory (silicon carbide, silicon nitride, alumina, etc.).
ノズル13からの空気噴出量は、燃料ガスの燃
焼に要する理論空気量の5〜30%が望ましい。 The amount of air ejected from the nozzle 13 is preferably 5 to 30% of the theoretical amount of air required for combustion of the fuel gas.
次に別実施例を説明する。 Next, another embodiment will be described.
ノズル13は燃焼ガス噴出口1の周方向におい
て複数に分割形成するか、環状に連続させるかの
いずれかである。 The nozzle 13 is either divided into a plurality of parts in the circumferential direction of the combustion gas injection port 1 or continuous in an annular shape.
燃焼器3の型式は不問である。 The type of combustor 3 does not matter.
図面は、本考案の実施例を示す断面図である。
1……燃焼ガス噴出口、2……燃焼室、11A
……内側壁部、12……中空部、13……ノズ
ル。
The drawings are cross-sectional views showing embodiments of the present invention. 1... Combustion gas outlet, 2... Combustion chamber, 11A
...Inner wall part, 12...Hollow part, 13...Nozzle.
Claims (1)
焼室2の燃焼ガス噴出口1を前記燃焼室2よりも
小径に形成し、前記内側壁部11Aの外側に、そ
れに対する冷却用空気流動のための中空部12を
形成し、その中空部12から冷却用空気を噴出す
るノズル13を形成した高速バーナであつて、前
記ノズル13を前記燃焼ガス噴出口1のほぼ全周
にわたつて、かつ、その燃焼ガス噴出口1からの
燃焼ガス噴出方向に対して同方向にほぼ平行に冷
却用空気が噴出される方向で配置してある高速バ
ーナ。 A combustion chamber 2 is formed within the inner wall portion 11A, a combustion gas outlet 1 of the combustion chamber 2 is formed to have a smaller diameter than the combustion chamber 2, and a cooling air flow is provided outside the inner wall portion 11A. A high-speed burner having a hollow part 12 formed therein, and a nozzle 13 for spouting cooling air from the hollow part 12, the nozzle 13 extending over almost the entire circumference of the combustion gas outlet 1, The high-speed burner is arranged in a direction in which cooling air is ejected substantially parallel to the direction in which the combustion gas is ejected from the combustion gas ejection port 1.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP6815783U JPS59175845U (en) | 1983-05-06 | 1983-05-06 | high speed burner |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP6815783U JPS59175845U (en) | 1983-05-06 | 1983-05-06 | high speed burner |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS59175845U JPS59175845U (en) | 1984-11-24 |
JPS6339545Y2 true JPS6339545Y2 (en) | 1988-10-18 |
Family
ID=30198343
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP6815783U Granted JPS59175845U (en) | 1983-05-06 | 1983-05-06 | high speed burner |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS59175845U (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS63194112A (en) * | 1987-02-06 | 1988-08-11 | Katsuyoshi Inai | Method of heating and generating infrared rays and apparatus thereof |
JPH0318818Y2 (en) * | 1987-08-21 | 1991-04-22 | ||
JP3634325B2 (en) * | 2002-05-30 | 2005-03-30 | 住重機器システム株式会社 | Supersonic jet burner |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5311869U (en) * | 1976-07-14 | 1978-01-31 |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6238107Y2 (en) * | 1979-05-08 | 1987-09-29 |
-
1983
- 1983-05-06 JP JP6815783U patent/JPS59175845U/en active Granted
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5311869U (en) * | 1976-07-14 | 1978-01-31 |
Also Published As
Publication number | Publication date |
---|---|
JPS59175845U (en) | 1984-11-24 |
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