JPS5835308A - Combustion method preventing resonance and its apparatus - Google Patents

Combustion method preventing resonance and its apparatus

Info

Publication number
JPS5835308A
JPS5835308A JP13403281A JP13403281A JPS5835308A JP S5835308 A JPS5835308 A JP S5835308A JP 13403281 A JP13403281 A JP 13403281A JP 13403281 A JP13403281 A JP 13403281A JP S5835308 A JPS5835308 A JP S5835308A
Authority
JP
Japan
Prior art keywords
fuel spray
burner
hole
combustion
main
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
JP13403281A
Other languages
Japanese (ja)
Other versions
JPH0151721B2 (en
Inventor
Manabu Orimoto
折本 学
Iwao Akiyama
秋山 巖
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.)
Mitsubishi Power Ltd
Original Assignee
Babcock Hitachi 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 Babcock Hitachi KK filed Critical Babcock Hitachi KK
Priority to JP13403281A priority Critical patent/JPS5835308A/en
Publication of JPS5835308A publication Critical patent/JPS5835308A/en
Publication of JPH0151721B2 publication Critical patent/JPH0151721B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D17/00Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D17/00Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
    • F23D17/002Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel gaseous or liquid fuel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2210/00Noise abatement

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Abstract

PURPOSE:To certainly prevent resonance during combustion is on a burner, by composing the burner, with a plurality of fuel spray tubes being equipped, in order to perform a combustion which shows a vibrational change in the rate of heat generation, which is different from an acoustical mode of vibration, which occurs in a combustion furnace, such as an industrial furnace. CONSTITUTION:A heavy oil burner 12a, to which end a flame holder 12 is fitted, is installed in the center part of a burner 8. The primary air is fed into the burner 12a from tubes 12b which encircle the burner 12a, and the secondary air is fed into the burner, passing through the secondary vanes 11. A plurality of fuel spray tubes 3 are annularly arranged to the outer circumference of tubular bodies 11a, encircling the secondary vanes 11. In this case, there are two types of fuel spray tube 3. One is that to which a gas nozzle 13, having a main fuel spray hole 6 which performs both main- hole fuel spray 6' and auxiliary-hole fuel spray 7', and an auxiliary fuel spray hole 7, are equipped. The other is that to which a gas nozzle 13'', having a main fuel spray hole 6 which performs a main-hole fuel spray 6'' only, is equipped. Both types are arranged alternately. With such an arrangement, the pattern of change of the rate of heat generation is made complicated, so that the burner is prevented from resonance during combustion.

Description

【発明の詳細な説明】 この発明はボイラの火炉等において生ずることのある共
鳴振動を防止する燃焼方法及びその装置に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a combustion method and apparatus for preventing resonance vibrations that may occur in a boiler furnace or the like.

化石燃料を使用するボイラ、工業用炉において、石油燃
料の不足から天燃ガスや石炭燃料への転換が行なわれて
いる。とりわけ天燃ガスは硫黄分が極めて少なく5Ox
(硫黄酸化物)の心配がなく、かつ窒素酸化物(NOx
 )の防止が容易なことからクリーンエネルギーとして
注目されている。しかし天燃ガスはその性格上短炎を形
成するので新たに火炉の共鳴振動を生起するという問題
を生じ、その解決が要望されているところである。
BACKGROUND OF THE INVENTION Boilers and industrial furnaces that use fossil fuels are being converted to natural gas or coal fuels due to a shortage of petroleum fuels. In particular, natural gas has extremely low sulfur content, 5Ox.
(sulfur oxides) and nitrogen oxides (NOx).
) is attracting attention as a clean energy source because it can be easily prevented. However, natural gas, by its nature, forms short flames, which creates a new problem of generating resonance vibrations in the furnace, and a solution to this problem is desired.

一般的に燃焼炉としてはボイラにおいては、第1図に示
す如く矩形横断面をもつ中空の立方体で示され、横形の
ものとしては第2図に示す如く筒状横形の工業用炉があ
る。この場合における気柱圧力振動のモードとしては、
固定壁を誉響学的振動の最大振幅部(腹部)にもつ1次
から0次の音響学的振動を生ずることとなる。
In general, a combustion furnace is a hollow cube with a rectangular cross section as shown in FIG. 1, and a horizontal type of combustion furnace is a cylindrical horizontal industrial furnace as shown in FIG. In this case, the mode of air column pressure vibration is:
Acoustic vibrations from the first to the zeroth orders are generated with the fixed wall at the maximum amplitude part (abdomen) of the euphonic vibrations.

第1図のボイラについては幅(W)奥行(D)高さくH
)のいづれについても第3図に示すような両端閉の振動
となっており、第2図の工業用炉については筒の長さく
L)方向について片側閉の第4図に示すようなものとな
っている。
For the boiler shown in Figure 1, width (W), depth (D) and height H
), both ends are closed as shown in Figure 3, and the industrial furnace shown in Figure 2 has one end closed in the cylinder length L) direction as shown in Figure 4. It has become.

バーナ8aへの天燃ガスの供給装置は第5図に示すよう
に管路3aから燃料ガス流量調節弁1as燃料ガス遮断
弁2aを経由し分岐する管路によりガス人口弁4aを経
由してバーナ8aに天燃ガスを供給している。符号5a
、 6aはガスベント弁、符号7aはガスベント管を示
す。
As shown in FIG. 5, the natural gas supply device to the burner 8a is constructed by a pipe line that branches from a pipe line 3a via a fuel gas flow rate adjustment valve 1as and a fuel gas cutoff valve 2a, and supplies the natural gas to the burner via a gas population valve 4a. 8a is supplied with natural gas. Code 5a
, 6a is a gas vent valve, and 7a is a gas vent pipe.

第6図はそのバーナ8aの軸心を含む断面図で、第7図
は第6図のA−A視図(正面図)である。
FIG. 6 is a sectional view including the axis of the burner 8a, and FIG. 7 is a view taken along line AA (front view) of FIG.

火炉1の木管壁14にはバーナ8aがバーナスロート5
と同軸心にしてそのノズルを火炉1に向けて取付けされ
る。バーナ8aの中心に位置する重油/< −+ 12
aの端部には保炎板12が取付けされ、これを囲む筒1
2bから一次空気が供給され、二次ベーン11を経由し
て二次空気10が供給される。
A burner 8a is attached to a burner throat 5 on the wood pipe wall 14 of the furnace 1.
It is installed coaxially with the furnace 1 with its nozzle facing the furnace 1. Heavy oil located at the center of burner 8a/< -+ 12
A flame holding plate 12 is attached to the end of a, and the cylinder 1 surrounding it
Primary air is supplied from 2b, and secondary air 10 is supplied via secondary vane 11.

二次ベーン11を囲む筒状体11aの外周にはスロート
5と同軸心にガスエレメント(燃料噴霧管)3が複数本
(図示では8本)位置する。このガスエレメント3の前
端にはガスノズル13が取付けされている。ガスノズル
13には主燃料噴霧孔6と副燃料噴霧孔7が設けられ、
第7図に示すように主孔燃料噴霧6′、副孔燃料噴霧γ
′が噴出する。副孔燃料噴霧は図示の如くインペラ12
を囲むようにして燃焼し、燃焼用空気流れにより保炎域
4を形成する。何れも主燃料噴霧6′と副燃料噴霧7′
の保炎板12に対する噴霧方向の相対位置方向を同じく
するようにガスノズル13を設けている。このようなガ
スバーナ8aでガスを燃焼させるときはほぼ一定した形
状の燃焼、即ちほぼ一定する振動的発熱率変化をする。
A plurality of gas elements (fuel spray pipes) 3 (eight in the figure) are located coaxially with the throat 5 on the outer periphery of the cylindrical body 11a surrounding the secondary vane 11. A gas nozzle 13 is attached to the front end of this gas element 3. The gas nozzle 13 is provided with a main fuel spray hole 6 and an auxiliary fuel spray hole 7,
As shown in Fig. 7, main hole fuel spray 6', sub hole fuel spray γ
' gushes out. The sub-hole fuel spray is carried out by the impeller 12 as shown in the figure.
It burns in such a way as to surround it, and a flame holding area 4 is formed by the combustion air flow. Both are main fuel spray 6' and auxiliary fuel spray 7'.
The gas nozzles 13 are provided so that the relative positions of the spraying directions with respect to the flame stabilizing plate 12 are the same. When gas is combusted in such a gas burner 8a, the combustion takes place in a substantially constant shape, that is, the oscillatory heat generation rate changes in a substantially constant manner.

その燃焼に伴う炉内の圧力変動は添付する表1の欄l「
安定」の欄に示す圧力変動の「波形特性」の線図で示す
ようなものとなる。その圧力振幅と周波数の関係は平均
した3つの山をもつような周波数分布を示す。
The pressure fluctuation inside the furnace due to its combustion is shown in column 1 of attached Table 1.
The result will be something like the diagram of the "waveform characteristics" of pressure fluctuation shown in the "Stability" column. The relationship between the pressure amplitude and frequency shows a frequency distribution with three average peaks.

しかしこの波形特性がその炉の固有の振動学的振動モー
ド(波形と周波数)と近似したものとなるときはr、 
n、mの順にその波形特性は変化して行き、■に示す如
く周波数特性で大きな圧力振幅を一つもつ所謂共鳴振動
を生じ遂には炉を破損するに至るものである。
However, when this waveform characteristic approximates the unique vibrational vibration mode (waveform and frequency) of the furnace, r,
The waveform characteristics change in the order of n and m, and as shown in (2), a so-called resonant vibration with one large pressure amplitude occurs in the frequency characteristics, eventually leading to damage to the furnace.

共鳴振動に成長する条件としては、 (1)必要条件としては、圧力振動の振幅の最大なとこ
ろ、所謂圧力の腹(ml傍とな る。)に箋熱位町すること。
The conditions for the development of resonance vibration are as follows: (1) The necessary condition is that the temperature should be at the point where the amplitude of the pressure vibration is maximum, the so-called pressure antinode (near ml).

(2)十分条件としては、圧力変動と発熱変動が同期す
ること である。
(2) A sufficient condition is that pressure fluctuations and heat generation fluctuations are synchronized.

しかしく1)の必要条件はボイラ等燃焼炉の構造上バー
ナは所謂片側閉になる水管壁に取付けされるものであり
避けることができない。従って(2)の条件を満たさな
いようにすることが共鳴振動防止上必要である。
However, the requirement 1) cannot be avoided because the burner is attached to the wall of the water pipe which is closed on one side due to the structure of the combustion furnace such as a boiler. Therefore, it is necessary to prevent the condition (2) from being satisfied in order to prevent resonance vibration.

この発明はこのような十分条件を満たさないように燃料
噴霧管を配置し、共鳴振動を起こすような燃焼モードを
形成しないような燃焼をさせる方法とその装置を提案す
ることを目的とする0 要するにこの発明は燃焼炉のもつ音響学的振動モードと
異なる振動的発熱率変化をする燃焼をするように複数本
の燃料噴霧管をもつバーナに燃料を供給する共鳴振動防
止燃焼方法であることを特徴とする。
The purpose of this invention is to propose a method and apparatus for arranging fuel spray pipes so as not to satisfy such sufficient conditions, and to perform combustion in a manner that does not form a combustion mode that causes resonance vibration. The present invention is characterized by a resonance vibration prevention combustion method for supplying fuel to a burner having a plurality of fuel spray pipes so as to perform combustion with an oscillatory change in heat generation rate different from the acoustic vibration mode of the combustion furnace. shall be.

さらにまたこの発明は、燃料噴霧方向と燃料噴霧量を異
にするノズル付き燃料噴霧管2本以上よりなる燃料噴霧
管の組をバーナスロート内周に沿い複数組配置した共鳴
振動防止燃焼装置であることを特徴とする。
Furthermore, the present invention provides a resonance vibration prevention combustion device in which a plurality of sets of fuel spray pipes each consisting of two or more fuel spray pipes with nozzles having different fuel spray directions and fuel spray amounts are arranged along the inner periphery of a burner throat. It is characterized by

この発明の実施にか\る装置を第8図〜第11図により
説明する。なお第8図、第9図で添付する符号で、第6
図、第7図と同一のものは同一部材を示す。この発明の
実施にかかるバーナ8では燃料噴霧管3はガスノズルが
主燃料噴霧孔6と副燃料噴霧孔7をもつガスノズル13
を装着したものと、主燃料噴霧孔6のみを有するガスノ
ズル13r装着したものとの2種類とし、バーナスロー
ト5の内周に沿い第9図に示す如くガスノズル13装着
の燃料噴霧管とガスノズル13′を装着した燃料噴霧管
との組を複数組(第9図では4組)設けるものである。
An apparatus for carrying out this invention will be explained with reference to FIGS. 8 to 11. In addition, the reference numerals attached in Figures 8 and 9 indicate No. 6.
The same parts as those in the figures and FIG. 7 indicate the same members. In the burner 8 according to the embodiment of the present invention, the fuel spray pipe 3 is a gas nozzle 13 having a main fuel spray hole 6 and an auxiliary fuel spray hole 7.
There are two types: one equipped with a gas nozzle 13r having only the main fuel spray hole 6, and one equipped with a gas nozzle 13r having only the main fuel spray hole 6. Along the inner circumference of the burner throat 5, as shown in FIG. A plurality of sets (four sets in FIG. 9) are provided with a fuel spray pipe equipped with a fuel spray pipe.

即ちガスノズル13とガスノズル13′はバーナスロー
ト内周に沿い交互に位置する形となる。このような組合
せをすると発熱率変化のパターンは第11図に示すql
<qtの3つの形態のものが複合した形となり、複雑な
波形のものとなって炉の固有の音響学的゛振動モードと
異なる波形の発熱率変化をすることとなり炉の共鳴振動
を生ずることがない。
That is, the gas nozzles 13 and 13' are arranged alternately along the inner periphery of the burner throat. When such a combination is used, the pattern of heat generation rate change is ql as shown in Figure 11.
The three forms of <qt become a composite form, resulting in a complex waveform, which causes the heat generation rate to change in a waveform different from the unique acoustic vibration mode of the furnace, resulting in resonance vibration of the furnace. There is no.

また第101Jに示す如くガスノズルA1は主燃料噴霧
孔6のみをまたは主燃料噴霧孔6と副燃料噴霧孔7をも
つものとし、ガスノズルB、は主燃料噴霧孔6のみをも
つものとし、ガスノズルCIは副燃料噴霧孔7のみをも
つものとし、このA1B1 c、の組を複数組(図示例
では3組)バーナスロート内周に沿って配置してもよい
。この場合主燃料噴霧孔からのガス噴出方向は図示の如
< 6At 6sと内周接線方向についてαA、αBと
変化させるとよい。
Further, as shown in No. 101J, the gas nozzle A1 has only the main fuel spray hole 6 or the main fuel spray hole 6 and the auxiliary fuel spray hole 7, the gas nozzle B has only the main fuel spray hole 6, and the gas nozzle CI has only the auxiliary fuel spray holes 7, and a plurality of sets (three in the illustrated example) of A1B1c may be arranged along the inner periphery of the burner throat. In this case, the direction of gas ejection from the main fuel nozzle hole may be changed to <6At 6s and αA, αB in the tangential direction of the inner circumference, as shown in the figure.

また燃料供給量はガスノズルごとに変化させることもよ
い。
Further, the amount of fuel supplied may be changed for each gas nozzle.

副燃料噴霧孔からの燃料噴出量と主燃料噴霧孔からの燃
料噴出量の比は通常0.1〜0.5のものを採用してい
る。
The ratio of the amount of fuel jetted from the auxiliary fuel nozzle to the amount of fuel jetted from the main fuel nozzle is usually 0.1 to 0.5.

第12図は振動指数(%)と二段燃焼比(に)との関係
を示すもゐで、イ曲線は従来のバーナ、口曲線はこの発
明にかかるバーナを使用したときのものを示す。ここに
振動指数とは火炉ドラフトの変動を検出し周波数分析を
し、炉の気柱の固有振動数と共鳴する共鳴成分周波数が
どの位の比率で存在するかを示すものであり、二段燃焼
比率とは第二段のバーナに供給する燃料と第一段バーナ
との燃料供給量との比率を言う。実験に供した実験炉は
火炉奥行2m、バーナ2個、燃料としてLPG使用、燃
焼量 7.5 mN / hr 。
FIG. 12 shows the relationship between the vibration index (%) and the two-stage combustion ratio, where the A curve shows the conventional burner and the N curve shows the burner according to the present invention. Here, the vibration index is a measure that detects fluctuations in the furnace draft, performs frequency analysis, and indicates the proportion of resonant component frequencies that resonate with the natural frequency of the air column of the furnace. The ratio refers to the ratio between the amount of fuel supplied to the second-stage burner and the amount of fuel supplied to the first-stage burner. The experimental furnace used in the experiment was 2 m deep, had 2 burners, used LPG as fuel, and had a combustion rate of 7.5 mN/hr.

空気過剰率 10%の条件のものである。The condition is that the excess air ratio is 10%.

この実験の結果でも本願発明にかかるものが振動指数は
従来のバーナより常に低いものであることが確かめられ
た。
The results of this experiment also confirmed that the vibration index of the burner according to the present invention was always lower than that of the conventional burner.

また実嬢動しているボイラにもこの発明にかかるバーナ
を装着し実施した結果、共鳴振動発生を防止する効果の
大であることが確認された。
Furthermore, as a result of installing the burner according to the present invention in an actual boiler in operation, it was confirmed that it is highly effective in preventing the occurrence of resonance vibrations.

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

第1図はボイラの火炉の斜視図、第2図は工業用炉の斜
視図、第3図は第1図の奥行きD1炉幅W、 炉高Hの
いずれについてもの気柱の固有振動パターン、第4図は
第2図に対応する気柱の固有振動パターン、第5図はガ
ス燃料配管の模式斜視図、第6図は従来のバーナの側断
面図、第7図は第6図のA−A親図、第8図はこの発明
にかかるバーナの側断面図、第9図は第8図のB−B親
図、第10図はこの発明の他の実施例を示すバーナ正面
図、第11図はこの発明の実施の場合の発熱率変化と時
間線図、第12図は振動指数と二段燃焼比の関係m図で
ある。 1・・・火炉    3・・・燃料噴霧管6・・・主燃
料噴霧孔  7・・・副燃料噴霧孔8.8a・・・バー
ナ   13・・・ガスノズル第2図 第4図 3;Xト≧シ
Figure 1 is a perspective view of a boiler furnace, Figure 2 is a perspective view of an industrial furnace, and Figure 3 is the natural vibration pattern of the air column for each of the depth D1 furnace width W and furnace height H in Figure 1. Fig. 4 is the natural vibration pattern of the air column corresponding to Fig. 2, Fig. 5 is a schematic perspective view of the gas fuel piping, Fig. 6 is a side sectional view of a conventional burner, and Fig. 7 is A of Fig. 6. -A main view, FIG. 8 is a side sectional view of the burner according to the present invention, FIG. 9 is a B-B main view of FIG. 8, and FIG. 10 is a front view of the burner showing another embodiment of the present invention. FIG. 11 is a diagram of changes in heat generation rate and time diagram in the case of implementing the present invention, and FIG. 12 is a diagram showing the relationship between the vibration index and the two-stage combustion ratio. 1...Furnace 3...Fuel spray pipe 6...Main fuel spray hole 7...Auxiliary fuel spray hole 8.8a...Burner 13...Gas nozzle Fig. 2 Fig. 4 3; ≧S

Claims (1)

【特許請求の範囲】 1、燃焼炉のもつ音響学的振動モードと異なる振動的発
熱率変化をする燃焼をするように複数本の燃料噴霧管を
もつバーナに燃料を供給することを特徴とする共鳴振動
防止燃焼方法02、燃料噴霧方向と燃料噴霧量を異にす
るノズル付き燃料噴霧管2本以上よりなる燃料噴霧管の
組をバーナスロート内周に沿い複数組配置したことを特
徴とする共鳴振動防止燃焼装置。 3、主燃料噴霧孔のみを有するノズル付き燃料噴霧管と
、主燃料噴霧孔と副燃料噴霧孔とを有するノズル付き燃
料噴霧管とをバーナスロート内周に沿い交互配置したこ
とを特徴とする特許請求の範囲第1項記載の共鳴振動防
止燃焼装置。
[Claims] 1. The present invention is characterized in that fuel is supplied to a burner having a plurality of fuel spray pipes so as to perform combustion with an oscillatory heat generation rate change different from the acoustic vibration mode of the combustion furnace. Resonance vibration prevention combustion method 02, a resonance characterized in that a plurality of sets of fuel spray pipes each consisting of two or more fuel spray pipes with nozzles having different fuel spray directions and fuel spray amounts are arranged along the inner periphery of the burner throat. Anti-vibration combustion device. 3. A patent characterized in that fuel spray pipes with nozzles having only main fuel spray holes and fuel spray pipes with nozzles having main fuel spray holes and auxiliary fuel spray holes are arranged alternately along the inner periphery of the burner throat. A resonance vibration prevention combustion device according to claim 1.
JP13403281A 1981-08-28 1981-08-28 Combustion method preventing resonance and its apparatus Granted JPS5835308A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13403281A JPS5835308A (en) 1981-08-28 1981-08-28 Combustion method preventing resonance and its apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13403281A JPS5835308A (en) 1981-08-28 1981-08-28 Combustion method preventing resonance and its apparatus

Publications (2)

Publication Number Publication Date
JPS5835308A true JPS5835308A (en) 1983-03-02
JPH0151721B2 JPH0151721B2 (en) 1989-11-06

Family

ID=15118774

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13403281A Granted JPS5835308A (en) 1981-08-28 1981-08-28 Combustion method preventing resonance and its apparatus

Country Status (1)

Country Link
JP (1) JPS5835308A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0145381A2 (en) * 1983-11-22 1985-06-19 Babcock Power Limited Improvements in or relating to burner tips
WO1999056059A1 (en) * 1998-04-23 1999-11-04 Siemens Aktiengesellschaft Combustion chamber assembly
EP0952392A3 (en) * 1998-04-15 2000-07-19 Mitsubishi Heavy Industries, Ltd. Combustor
JP2023163447A (en) * 2022-04-28 2023-11-10 三菱重工パワーインダストリー株式会社 gas burner

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5514422A (en) * 1978-07-17 1980-01-31 Babcock Hitachi Kk Prevention of combustion knock

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5514422A (en) * 1978-07-17 1980-01-31 Babcock Hitachi Kk Prevention of combustion knock

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0145381A2 (en) * 1983-11-22 1985-06-19 Babcock Power Limited Improvements in or relating to burner tips
EP0952392A3 (en) * 1998-04-15 2000-07-19 Mitsubishi Heavy Industries, Ltd. Combustor
US6267583B1 (en) * 1998-04-15 2001-07-31 Mistubishi Heavy Industries, Ltd. Combustor
WO1999056059A1 (en) * 1998-04-23 1999-11-04 Siemens Aktiengesellschaft Combustion chamber assembly
JP2023163447A (en) * 2022-04-28 2023-11-10 三菱重工パワーインダストリー株式会社 gas burner

Also Published As

Publication number Publication date
JPH0151721B2 (en) 1989-11-06

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