JPS5860111A - Ceramic burner for high temperature - Google Patents

Ceramic burner for high temperature

Info

Publication number
JPS5860111A
JPS5860111A JP15741381A JP15741381A JPS5860111A JP S5860111 A JPS5860111 A JP S5860111A JP 15741381 A JP15741381 A JP 15741381A JP 15741381 A JP15741381 A JP 15741381A JP S5860111 A JPS5860111 A JP S5860111A
Authority
JP
Japan
Prior art keywords
air
fuel gas
cooling
burner
nozzle
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.)
Granted
Application number
JP15741381A
Other languages
Japanese (ja)
Other versions
JPS6410728B2 (en
Inventor
Kiyoshi Naito
内藤 清
Akio Shiyukutani
宿谷 昭夫
Kiyoshiro Moriuchi
森内 清白
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shinagawa Refractories Co Ltd
Shinagawa Shiro Renga KK
Original Assignee
Shinagawa Refractories Co Ltd
Shinagawa Shiro Renga KK
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 Shinagawa Refractories Co Ltd, Shinagawa Shiro Renga KK filed Critical Shinagawa Refractories Co Ltd
Priority to JP15741381A priority Critical patent/JPS5860111A/en
Publication of JPS5860111A publication Critical patent/JPS5860111A/en
Publication of JPS6410728B2 publication Critical patent/JPS6410728B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/20Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • F23D14/22Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Gas Burners (AREA)

Abstract

PURPOSE:To obtain stable characteristics in a burner even in high temperature, by using a ceramic which is durable to the thermal shock for the material to make a protective cylinder and an air nozzle, and by making the joint part of a ceramic with a metal part in a structure not being affected by expansion difference. CONSTITUTION:A burner body is composed in such a manner that a fuel gas pipe 1 is provided in the center part, around which air pipes 7 are provided at regular intervals, and surrounding the air pipes 7, a protective cylinder 18 is provided. The air pipe 7 has an air nozzle 9, which is joined to the tip of an air pipe 7 by an air nozzle fitting member 8. A cooling air ventilating channel 22 is formed on the external periphery of an air nozzle fitting member 8. In this case, a protective cylinder 18 and an air nozzle 9 are made of ceramic material. By using this material, stable characteristics can be obtained in a burner even in high temperature, and at the same time, the burner can be used for a long time with a small rate of air even in an air-cooled mode.

Description

【発明の詳細な説明】 本発@祉炉内11度1.400’t: −1,900c
c(D高Brに使用されるバーナ機構の改良に関するも
のであ夛、)ぐ−ナ部からの熱損失を減少させる省エネ
ルギー型ガス/4−すを提供することを目的とする。
Detailed description of the invention This invention @ 11 degrees inside the welfare furnace 1.400't: -1,900c
c (Regarding the improvement of the burner mechanism used in D-high Br) The object of the present invention is to provide an energy-saving gas/four-stove that reduces heat loss from the burner section.

1.400 cc〜I 、900°cOi111F、4
111C)71Jl’ルンに使用されている従来のバー
ナは、  1.4000C〜1.900℃とiう炉内か
らの高温1s囲気及び温度55G’e −1,200℃
の高−二次空気からバーナ先端部を保護するため水冷管
を併用している。
1.400 cc~I, 900°cOi111F, 4
111C) The conventional burner used in the 71Jl' run has a high temperature of 1s from inside the furnace of 1.4000C to 1.900℃ and a temperature of 55G'e -1,200℃.
A water-cooled pipe is also used to protect the burner tip from the high secondary air.

さらに最近は、省エネルギーの一環として、廃ガス顕熱
を燃焼用二次空気として回収利用することが益々多くな
ってお)、そのため燃焼用二次空気の温度上昇に伴い、
従来の金属製ノズルを有するバーナでは、高温酸化勢の
短命化の方向tたどってい為−こO高温化からバーナの
先端を保鰻するためこの種の多くの一苛−すは水冷方式
を採用している。
Furthermore, recently, as part of energy conservation, waste gas sensible heat is increasingly being recovered and used as secondary air for combustion), and as a result, as the temperature of secondary air for combustion increases,
In conventional burners with metal nozzles, the lifespan of high-temperature oxidation forces has been shortened.In order to protect the tip of the burner from high temperatures, many of these types of burners adopt a water-cooling system. are doing.

しかしこのような水冷式バーナは下記のごとき欠点を有
している。すなわち水冷による熱損失がバーナ1本当り
8.000〜12.000 Kcal / hr  と
多く、かつ水冷管の漏水トラブル及び先端部へのカーボ
ン付着等の問題もあシパーナの保守管理に多くの労力を
必要とする。例えばバーナ本数が16本のトンネルキル
ンの場合の全水冷熱損失は128.000〜192.0
00 Kcal / hrとなる。そして六とえ水冷方
式を採用しても、高温炉に使用する場合はその寿命が短
く、長期使用Kd不向きであるという欠点があった。
However, such water-cooled burners have the following drawbacks. In other words, the heat loss due to water cooling is as high as 8,000 to 12,000 Kcal/hr per burner, and there are also problems such as leakage of water cooling pipes and carbon adhesion to the tips, which requires a lot of effort to maintain and manage the Sipana. I need. For example, in the case of a tunnel kiln with 16 burners, the total water cooling heat loss is 128.000 to 192.0.
00 Kcal/hr. Even if a water-cooling system is adopted, the service life is short when used in a high-temperature furnace, and the Kd is unsuitable for long-term use.

本発明は前記の水冷式バーナの諸量mを解決すべくなさ
れ良ものである。
The present invention has been made in order to solve the above-described various quantities m of the water-cooled burner.

高温バーナの水冷を行なわない場合にill、%金属に
代る高温耐火部材が必要であル、これには、一般にセラ
きツク材料が考えられるが、セラミック材料には(1)
熱衡撃に弱い (2)金属とセラミック材料との膨張差
による損傷尋の問題がある。このため、バーナを構成す
る各部材の中で、tず先端部と外周部保■筒を材質的に
セラきツク化することを考え、先端の受ける輻射熱と高
温二次空気からの貫流熱による影響を抑制することとし
1本発明に使用するセラミック材料は十分熱衝撃に耐え
うる材質のものを遺足し、また、金属との結合部は膨張
差が比較的悪影譬を及ぼさない構造を有し、さらに内側
の金属部分の蓄熱の[1−化と過熱防止のために少量の
冷却空気を使用することKよっても充分空冷効果を有す
る構造としたこと゛を特長とするバーナである。
When a high-temperature burner is not water-cooled, a high-temperature refractory material is required in place of metal. Ceramic materials are generally considered for this, but ceramic materials (1)
Weak against thermal shock (2) There is a problem of damage caused by the difference in expansion between metal and ceramic materials. For this reason, we considered using ceramic material for the tip end and outer peripheral retaining cylinder of each member constituting the burner. In order to suppress the influence, 1. The ceramic material used in the present invention is made of a material that can sufficiently withstand thermal shock, and the joint part with the metal has a structure in which the difference in expansion does not have a relatively negative effect. Furthermore, this burner is characterized by a structure that has a sufficient air cooling effect by using a small amount of cooling air to reduce heat accumulation in the inner metal part and prevent overheating.

次に本発明の一実施例を示す添附図面に基づいて具体的
に説明する。
Next, an embodiment of the present invention will be described in detail based on the accompanying drawings.

第1図は本発明の一実施例の一部分縦断面を示し。FIG. 1 shows a partial longitudinal section of an embodiment of the present invention.

第2図は111図の先端部の拡大縦断面図である。FIG. 2 is an enlarged longitudinal sectional view of the tip of FIG. 111.

本発明に係るバーナはlljl図に示すごとく中心部に
燃料ガスパイプ1が設けてあシ、その外周K −足の間
txt有してエアーノーイブ7を周設し、さらに最外肩
部に一定の間隙を設けて空冷)fイブ16及び保■箇1
8t−周設して構成されるバーナ本体であって、燃料ガ
スノ譬イデ1は第2図に示すごとくその先端部に、燃料
ガスノズル取付部材2によって接合される燃料ガスノズ
ル6を有する。
The burner according to the present invention has a fuel gas pipe 1 provided in the center as shown in the figure, an air nove 7 is provided around the outer circumference K and the space between the legs txt, and a certain gap is provided at the outermost shoulder. air cooling)
The fuel gas nozzle 1 has a fuel gas nozzle 6 connected to it by a fuel gas nozzle attachment member 2 at its tip, as shown in FIG.

前記燃料ガスノズル取付部材2 ”K Fi外周−上に
一次空気通気孔141が形成され、鎖部の外周がエアー
ノズルデ7およびエアーノズル取付部材8とエアーノズ
ル9との内面に部分的に当接される。
A primary air vent 141 is formed on the outer periphery of the fuel gas nozzle mounting member 2 ``K Fi, and the outer periphery of the chain part partially contacts the inner surfaces of the air nozzle 7 and the air nozzle mounting member 8 and the air nozzle 9. .

燃料ガスノズル6の外周には一次空気溝12が形成され
、#部の外周が燃料ガスノズル取付部材2にお妙ると同
様エアーノズル9の内面に部分的に当接される。さらに
燃料ガスノズル6の壁iiiに一次空気通気孔14が穿
設され、燃料ガスノズル6内に接合されたインサート、
部材4の先端部に形成された中心噴出孔15と連通して
いる。イノサート部材4の外周上の一部分には燃料ガス
通過溝5が形成され、鎖部の外周が燃料ガスノズル6の
内面に部分的に当接される。6Fi燃料ガス噴出孔であ
る。
A primary air groove 12 is formed on the outer periphery of the fuel gas nozzle 6, and when the outer periphery of the # part is attached to the fuel gas nozzle mounting member 2, it partially contacts the inner surface of the air nozzle 9. Furthermore, a primary air vent 14 is drilled in the wall iii of the fuel gas nozzle 6, and an insert joined within the fuel gas nozzle 6;
It communicates with a central jet hole 15 formed at the tip of the member 4. A fuel gas passage groove 5 is formed in a part of the outer circumference of the inosert member 4, and the outer circumference of the chain part partially contacts the inner surface of the fuel gas nozzle 6. 6Fi fuel gas nozzle.

エアー・母イゾ7は@2&Jに示すごとく、その先端部
にエアーノズル取付部材8によって接合されるエアーノ
ズル9を有する。該エア−ノズル取付部材80外周上に
は冷却空気通気溝22が形成8れ腋部の外周面が空冷ノ
譬イゾ16の先端部に!!絖部材17によって連接され
た保鰻簡16の内面に部分的に当接される。1sは一次
空気噴出孔である・ エアー・譬イデ7の全長の中間部位においては外周上に
冷却空気通気溝21を有する芯出し部材10を有し、腋
部の外゛周面が接続部材17の内面に部分的KJllI
Iされる。
As shown in @2&J, the air master tube 7 has an air nozzle 9 connected to its tip by an air nozzle attachment member 8. A cooling air ventilation groove 22 is formed on the outer periphery of the air nozzle mounting member 80, and the outer circumferential surface of the armpit portion is the tip of the air cooling nozzle 16! ! It is partially abutted against the inner surface of the eel protector 16 connected by the thread member 17. 1s is a primary air outlet. The centering member 10 has a cooling air ventilation groove 21 on the outer periphery at the middle part of the entire length of the air guide 7, and the outer circumferential surface of the armpit part is connected to the connecting member 17. Partial KJllI on the inner surface of
I will be treated.

円周上に冷却空気分岐孔20を有する空冷・譬イデ16
および保膜筒18Iri接続部材17によって相互、に
接合されるallll柱部材17饅筒受部片にtri接
続部材通気溝67を形成しておシ、バーナ取付部材s1
の内面と該部外周面は部分的に当接される。保鏝箇18
め一先端部分には、必l!に応じて断熱カバー19を固
着してもよい。
Air cooling model 16 having cooling air branch holes 20 on the circumference
A ventilation groove 67 is formed in the columnar member 17 and the tube receiving piece of the columnar member 17, which are connected to each other by the membrane retaining cylinder 18Iri connection member 17, and the burner mounting member s1 is formed.
The inner surface and the outer circumferential surface of the portion are partially in contact with each other. Safety bullet 18
A must for the tip of the eyelid! The heat insulating cover 19 may be fixed depending on the situation.

2墨は冷却空気噴出孔である。オイルパイプ1゜エアー
ノ臂イデ7.空冷ノ臂イブ16の各基端の開口IBは夫
々、燃料ガス配管24.−次空気配管26、空冷配管2
9と接合される。28#i空冷パイプ増付部材、25は
エアーノズル取付部材である。
The two ink are cooling air vents. Oil pipe 1゜air arm ide 7. The opening IB at each base end of the air-cooled arm eve 16 is connected to the fuel gas pipe 24 . -Next air piping 26, air cooling piping 2
It is joined with 9. 28#i is an air cooling pipe additional member, and 25 is an air nozzle mounting member.

前記のごとく構成されたノ4−す本体は第1図に示スと
とく炉1159にボックス型のノ櫂−す取付部材61を
用いてセットされる・44は炉内、40社バーナータイ
ル、46はスロート部、41は二次空気通路、42は二
次空気室である。ノ櫂−す取付部材る1の炉内側外周は
断熱材32で包囲され炉内44からの高iixm気から
保■される・58はバーナの保護筒18と断熱材s2と
の関に設けた円すい柱状の空間である・ バーナ本体の炉壁&9への取付方法は炉壁69に予め嵌
設されている/4−す取付部材る1の炉外11M口部よ
シ%接続部材17に形成された接続部甘過気溝IS7の
外周をバーナ取付部材is1の内面に内接しながら挿入
し、シール材墨4を内′設したシール材保持金具66を
螺合等の方法で接着し、セットボルト65でバーナ本体
の傾斜を真Ill、?固定する。&6はバーナ取付部材
31と空冷ノ9イア’14によって形成された空間であ
るO前記のごとく構成された本バーナは長さ約1000
−2保III筒18の外径が約70−の寸法を有する。
The nozzle main body constructed as described above is set in the furnace 1159 using the box-shaped paddle mounting member 61 as shown in FIG. 46 is a throat portion, 41 is a secondary air passage, and 42 is a secondary air chamber. The outer periphery of the paddle attachment member 1 inside the furnace is surrounded by a heat insulating material 32 to protect it from high IIXM air from the inside of the furnace 44. 58 is provided between the burner protection cylinder 18 and the heat insulating material s2. The burner body is a conical columnar space.The method of attaching the burner body to the furnace wall &9 is to use the connecting member 17 from the outside of the furnace 11M of the mounting member 1 which is fitted in advance to the furnace wall 69. Insert the outer periphery of the connected part sweet air groove IS7 while inscribing it into the inner surface of the burner mounting member IS1, and glue the sealing material holding fitting 66 with the sealing material ink 4 inside by screwing or other method, and set it. Ill tilt the burner body with bolt 65? Fix it. &6 is the space formed by the burner mounting member 31 and the air cooling hole 14.The burner constructed as described above has a length of about 1000 mm.
The outer diameter of the -2 protection III cylinder 18 has a dimension of approximately 70 mm.

本i4−すにおいて燃料ガスは燃料ガス配管24から供
給され燃料!スノ帯イデ1内部を通り燃料ガスノズル墨
内部の燃料ガス通過1115を過シ燃料ガス噴出孔6よ
)噴霧される− 一次空気は一次空気配管26よ#)0・1〜0−1tk
#/312の圧力て供給されエアーノ!イデアの内部を
通り一次9気過気壽11及び−夜空気溝12を過多、−
大空気噴出孔1墨よ)噴出される。又−部は一次空気通
気孔14を通シ、中心噴出孔1Sから一噴出される・−
夜空気量コントロールはコントロールバルブ27で行う
In this case, the fuel gas is supplied from the fuel gas pipe 24, and the fuel gas is supplied from the fuel gas pipe 24. The primary air is sprayed through the primary air pipe 26 through the fuel gas passage 1115 inside the fuel gas nozzle through the fuel gas nozzle 1. The primary air is sprayed through the primary air pipe 26.
# / 312 pressure is supplied to the air! Passing through the interior of the idea, the primary 9 air passes 11 and the night air groove 12 passes through the air, -
Large air vent 1 ink) is ejected. Also, the part passes through the primary air vent 14 and is ejected from the central jet hole 1S.
The control valve 27 controls the amount of air at night.

冷却空気は冷却空気配管29から200〜400−H2
Qの圧力で供給され、冷却空気量のコントロール社コン
トロールパルツ墨0で行われる。供給すれ要冷却空気#
i、空冷Δイブ16の内部を通グ、一部は冷却空気分岐
孔20を通シ、空間66に至夛接続部材17にある接続
部材通気$57を過シ、空間Sat経て二次空気室42
に入る・ζ0@に冷却空気分岐孔20を通った冷却空気
は接続部材17と保護筒18の一部、及びノ櫂−す取付
部材111の一部を適当に冷却しつつ、加熱され燃焼用
空気の一部として利用される・残シの冷却空気は芯出し
部材1o上に#)る冷却空気通気W21を通)、保護筒
18.エアー・々イf7.エアーノズル取付部材8.エ
アー/Ikgを冷却熱交換しながら通過し、冷却空気噴
出孔2iSよ〕噴出され、燃焼用空・気の一部となる・
・9一ナ取付部材31の内部においては冷却空気分岐孔
20よ〕8良冷却空気が炉外にもれない様空間&6社シ
ール材保持金具&る内に取付もれたシール材114でシ
ールされる。高温二次空気(1,200〜550cc)
は二次空気通路41を経て、二次空気1142に入シ、
バーナメイル40内部のスロート部4墨を通過して炉内
44に入る゛。
Cooling air is from cooling air pipe 29 to 200-400-H2
It is supplied at a pressure of Q, and the amount of cooling air is set to 0. Cooling air required to be supplied #
i, through the inside of the air cooling Δ Eve 16, a part of which passes through the cooling air branch hole 20, passes through the connection member ventilation $57 in the connection member 17 to the space 66, and passes through the space Sat to the secondary air chamber. 42
The cooling air that has passed through the cooling air branch hole 20 into the ζ0@ is heated while suitably cooling the connecting member 17, a part of the protective tube 18, and a part of the paddle mounting member 111, and is heated for combustion. The remaining cooling air, which is used as part of the air, passes through the cooling air vent W21 above the centering member 1o, and the protection tube 18. Air tii f7. Air nozzle mounting member 8. It passes through the air/Ikg while exchanging cooling heat, is ejected from the cooling air outlet 2iS, and becomes part of the combustion air/air.
・Inside the cooling air branch hole 20 of the 9-in-1 mounting member 31, seal with the sealing material 114 installed inside the space & 6 sealing material retaining metal fittings so that the cooling air does not leak out of the furnace. be done. High temperature secondary air (1,200~550cc)
enters the secondary air 1142 through the secondary air passage 41,
It passes through the throat section 4 inside the burna mail 40 and enters the furnace interior 44.

保護筒18.エアーノズル9Fi窒化珪素等のセラミッ
ク材料よシな〕、超高温炉(1,400〜1.go。
Protective tube 18. Air nozzle 9Fi (ceramic material such as silicon nitride), ultra-high temperature furnace (1,400~1.go).

℃)でも長期安定使用が可能であゐ、これら保護筒18
.エアーノズル9はお0おO接続部材17及びエアーノ
ズル取付部材8により取付、交換が野鳥に可能な構造と
なっている・ 前記構造と構成によシ冷却空気は最終的には燃焼用空気
と&−るが、燃料ffi量とは無関係に、ノ4−すl1
1011111気温度により11が決定′され、少量で
充分効果を発揮することが出来え一 本発@ID*論例の超高温トンネル中ルンにおける爽績
によれば一次空気と冷却空気の合計量は。
These protective tubes can be used stably for a long time even at
.. The air nozzle 9 has a structure that allows it to be installed and replaced by a wild bird using the O0O connecting member 17 and the air nozzle mounting member 8. Due to the above structure and configuration, the cooling air is ultimately converted into combustion air. However, regardless of the amount of fuel ffi,
1011111 11 is determined by the air temperature, and it can be sufficiently effective with a small amount.According to the results of an ultra-high temperature tunnel run in a single air @ID* paper, the total amount of primary air and cooling air is .

理論燃焼空気量のlO〜II IGの範囲であ)、この
割合が25悌以上の場合は省エネルゼーの点から好重し
くない。
The theoretical combustion air amount is in the range of 1O to IIIG), and if this ratio is 25 degrees or more, it is not favorable from the point of view of energy saving.

本発明のバーナでは下記の効果があった。The burner of the present invention had the following effects.

■ 保護筒、エアーノズルにセラミック材を使用・し喪
ので高slにおいても安定し友脣性を得ることが出来、
かつ冷却方法の改真によ)、空冷方式でも少量の空気量
で−(−すの長期使用が可能となつ九。
■ Ceramic material is used for the protection tube and air nozzle, making it stable and compatible even at high SL.
Moreover, with the reform of the cooling method, long-term use is possible with a small amount of air even with an air-cooling system.

′■ 上記■の結果、冷却熱損失が大幅に減少し従来の
水冷バーナ使用時と比し燃料(オイル)が約7憾O省エ
ネルイーとなつ友。
'■ As a result of the above (■), the cooling heat loss is greatly reduced and the fuel (oil) is approximately 7 O energy saving compared to when using a conventional water-cooled burner.

■ 水冷設備が軍費とな夛バーナの保守管理の面でも従
来Cバーナエpfjkt′L″tいる。
■ Water-cooling equipment is a military expense, and in terms of maintenance and management of burners, conventional C burners are still expensive.

従って1本発明セラミックバーナはトンネルキルン以外
oairi潟雰囲気炉用として好適である・
Therefore, the ceramic burner of the present invention is suitable for use in oairi lagoon atmosphere furnaces other than tunnel kilns.

【図面の簡単な説明】[Brief explanation of drawings]

II1図は本発明高温用セラミックバーナの一実施例を
示す部分縦断面図、@2図ti第1図の先端部の拡大縦
断面図であシ、図中、1は燃料ガス・母イブ、  2は
燃料ガスノズル取付部材、  墨は燃料ガスノズル、 
  4Fiインサ一ト部材1.5は燃料ガス通過It、
   7#iエアーノ普イブ、  aFiエアーノズル
取付部材、  9はエアーノズル、10は芯出し部材、
  11は一次空気通気溝、12は一次空気配管  1
4は一次空気通気孔、  15は中心噴出孔、  16
は空冷ノ9イグ、17.は接続部材、  18#i保護
筒、  2QU冷却空気分岐孔、 21は冷却空気通気
溝、  22は冷却空気通気溝、  24は燃料ガス配
管、  26は一次空気配管、  29は空冷配管・
Fig. II1 is a partial vertical sectional view showing an embodiment of the high temperature ceramic burner of the present invention, and Fig. 2 is an enlarged longitudinal sectional view of the tip of Fig. 1. In the figure, 1 is a fuel gas/mother tube; 2 is the fuel gas nozzle mounting member, black is the fuel gas nozzle,
4Fi insert member 1.5 is a fuel gas passage It,
7 #i air nozzle, aFi air nozzle mounting member, 9 is air nozzle, 10 is centering member,
11 is the primary air ventilation groove, 12 is the primary air piping 1
4 is the primary air vent, 15 is the central ejection hole, 16
is air-cooled 9ig, 17. are connection members, 18#i protection tube, 2QU cooling air branch hole, 21 is cooling air ventilation groove, 22 is cooling air ventilation groove, 24 is fuel gas piping, 26 is primary air piping, 29 is air cooling piping.

Claims (1)

【特許請求の範囲】[Claims] バーナの中心部に、その先端に、−次空気通気譚を外周
の制御に形成した燃料ガスノズル取付部材を介して内部
に中心噴出孔を形成し九インサート部材を一次空気通気
孔と連通し、かつ燃料ガス通過溝を隔てて内蔵する外周
の一部分に=次空気溝を形成しえ燃料Iメノズルを取付
部てなる燃料ガスノダイブを配設し、燃料ガス/fイ!
の外側に燃料ガスパイプとの関に適宜の間隔を設けて、
冷却空気通気W?′・有するエアーノズル取付部材を介
してセラミツタ製エアーノズルを蝋付け、かつ空冷;讐
イデと保験筒の接続部材の内側に冷却空気通気溝を形成
した芯出し部材を設けてなるエアーノ譬イブを配設し、
エアー・譬イデの外側に炉内側に−にう2ツクJIO保
護筒を接続部材を介して取付け、かつ冷却空気分岐孔を
穿設してなる空冷ノ々イデを配設し、燃料ガスノ々イデ
、エアー/臂イfおよび空冷パイプの各基端m會夫々燃
料ガス配管、−次空気配管、空冷配管と連結可能に構成
してなる高温用セラ2ツクバーナ。
In the center of the burner, at its tip, a central jet hole is formed inside through a fuel gas nozzle mounting member formed with a secondary air vent on the outer periphery, and a nine insert member communicates with the primary air vent; An air groove is formed in a part of the built-in outer periphery across the fuel gas passage groove, and a fuel gas nodive consisting of a fuel I nozzle mounting part is provided, and the fuel gas/f i!
Provide an appropriate distance between the outside of the fuel gas pipe and the fuel gas pipe.
Cooling air ventilation W? '・A ceramic air nozzle is brazed through the air nozzle mounting member and is air cooled; an air nozzle is provided with a centering member with a cooling air ventilation groove formed inside the connection member between the air nozzle and the test tube. and
On the outside of the air outlet, two JIO protection tubes are attached to the inside of the furnace via connecting members, and an air cooling outlet is provided with cooling air branch holes. , an air/arm f, and each proximal end m of an air-cooled pipe are configured to be connectable to a fuel gas pipe, a secondary air pipe, and an air-cooled pipe, respectively.
JP15741381A 1981-10-05 1981-10-05 Ceramic burner for high temperature Granted JPS5860111A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15741381A JPS5860111A (en) 1981-10-05 1981-10-05 Ceramic burner for high temperature

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15741381A JPS5860111A (en) 1981-10-05 1981-10-05 Ceramic burner for high temperature

Publications (2)

Publication Number Publication Date
JPS5860111A true JPS5860111A (en) 1983-04-09
JPS6410728B2 JPS6410728B2 (en) 1989-02-22

Family

ID=15649089

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15741381A Granted JPS5860111A (en) 1981-10-05 1981-10-05 Ceramic burner for high temperature

Country Status (1)

Country Link
JP (1) JPS5860111A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01107012A (en) * 1987-09-10 1989-04-24 Shell Internatl Res Maatschappij Bv Ceramic burner for partial oxidation of fuel containing hydrocarbon
EP0582521A1 (en) * 1992-08-06 1994-02-09 L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Oxyfuel burners
US5823769A (en) * 1996-03-26 1998-10-20 Combustion Tec, Inc. In-line method of burner firing and NOx emission control for glass melting
JP2011520084A (en) * 2008-04-03 2011-07-14 レール・リキード−ソシエテ・アノニム・プール・レテュード・エ・レクスプロワタシオン・デ・プロセデ・ジョルジュ・クロード Combustion tool with quarl block and injector, assembly of the tool and furnace with the tool

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01107012A (en) * 1987-09-10 1989-04-24 Shell Internatl Res Maatschappij Bv Ceramic burner for partial oxidation of fuel containing hydrocarbon
EP0582521A1 (en) * 1992-08-06 1994-02-09 L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Oxyfuel burners
FR2694623A1 (en) * 1992-08-06 1994-02-11 Air Liquide Oxyfuel burners.
US5823769A (en) * 1996-03-26 1998-10-20 Combustion Tec, Inc. In-line method of burner firing and NOx emission control for glass melting
JP2011520084A (en) * 2008-04-03 2011-07-14 レール・リキード−ソシエテ・アノニム・プール・レテュード・エ・レクスプロワタシオン・デ・プロセデ・ジョルジュ・クロード Combustion tool with quarl block and injector, assembly of the tool and furnace with the tool

Also Published As

Publication number Publication date
JPS6410728B2 (en) 1989-02-22

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