JPS60117008A - Burner - Google Patents
BurnerInfo
- Publication number
- JPS60117008A JPS60117008A JP22425783A JP22425783A JPS60117008A JP S60117008 A JPS60117008 A JP S60117008A JP 22425783 A JP22425783 A JP 22425783A JP 22425783 A JP22425783 A JP 22425783A JP S60117008 A JPS60117008 A JP S60117008A
- Authority
- JP
- Japan
- Prior art keywords
- fuel
- chamber
- air
- premixture
- combustion
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
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
Description
【発明の詳細な説明】
本発明は燃焼器に関し、特に予蒸発予混合式とした逆流
缶形の燃焼器に関する。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a combustor, and more particularly to a counterflow can type combustor of a pre-evaporation and pre-mixing type.
従来のこの種の燃焼器としては、図には示さないが例え
ば本願人が特願昭3g −772797号として出願中
のものがある。この出願中の例では、内筒と外筒とが設
けられている逆流缶形燃焼器のヘッドに近い内筒と外筒
との間に環状の予蒸発予混合室を設け、この予蒸発予混
合室に主燃料噴射弁から燃料を噴射させて流入空気中で
予蒸発予混合を行わせ、これをヘッドから燃焼室に導く
ように構成されており、希薄燃焼と組合せたことによっ
て従来の拡散燃焼方式に比して一様な希薄混合気の供給
と安定した火炎とが得られることからNO,の排出量を
大巾に低減させることができる特徴を有する。As a conventional combustor of this type, although not shown in the drawings, for example, there is a combustor currently pending as Japanese Patent Application No. 3G-772797 by the present applicant. In the example in this application, an annular pre-evaporation premixing chamber is provided between the inner cylinder and the outer cylinder near the head of a counterflow can type combustor provided with an inner cylinder and an outer cylinder. It is configured to inject fuel from the main fuel injection valve into the mixing chamber to perform pre-evaporation and pre-mixing in the incoming air, and guide this through the head to the combustion chamber. Compared to the combustion method, this method provides a uniform supply of a lean air-fuel mixture and a stable flame, so it has the feature of significantly reducing NO emissions.
しかしながら、このような従来の燃焼器にあっては、逆
流缶型の環状通路に予蒸発予混合室を設ける形態に構成
されているため、−璽焼筒の大きさもそれなりに変らず
、現状通路自体の半径方向の幅が狭いので、ここに設け
られている予蒸発予混合室では燃料の均一な分散が難し
い。However, in such conventional combustors, the pre-evaporation and pre-mixing chamber is provided in the annular passage in the form of a counterflow can, so the size of the burner tube remains unchanged, and the current passage Due to its narrow radial width, it is difficult to uniformly distribute the fuel in the pre-evaporation premixing chamber provided here.
本発明の目的は、このような問題点に着目し、十分な予
混合気が得られてしかも燃焼器の全長が従来型の拡散燃
焼器程度に抑えられ、耐久性に富み、製作台が従来より
著しく廉価な予蒸発予混合式の燃焼器を提供することに
ある。The purpose of the present invention is to solve these problems, and to achieve sufficient premixture, the overall length of the combustor can be reduced to the same level as a conventional diffusion combustor, it is highly durable, and the production table can be used in a manner similar to that of a conventional diffusion combustor. The object of the present invention is to provide a pre-evaporation and pre-mixing type combustor which is significantly cheaper.
かかる目的を達成するために2本発明では5独立した円
筒形の予蒸発予混合室を燃焼室と並列の位置に配置する
と共に環状通路の空気が逆流型と同様な方向からとの予
蒸発予混合室に導かれるようになし、更にこの予混合室
で得られた予混合気を燃焼器ヘッドに設けた連通室によ
り頭部燃焼室に導くように構成するっ
以下に5図面に基づいて本発明の詳細な説明する。In order to achieve this object, in the present invention, five independent cylindrical pre-evaporation premixing chambers are arranged in parallel with the combustion chamber, and the air in the annular passage is pre-evaporated from the same direction as in the counterflow type. The premixture obtained in the premixing chamber is introduced into the head combustion chamber through a communication chamber provided in the combustor head. Detailed description of the invention.
第1図および第2図は本発明の一実施例を示し、ここで
、/は円筒形予蒸発予混合室、コは燃焼室であシ、並列
に配置したこれらの予混合室lと燃焼室コとを1本例で
は断熱を兼ねた一体の成形ブロックJとしてキャスタブ
ル着しくはマシナブルな断熱材料を用いて成形する。な
お、ブロック3はヘッドケーシング371側と燃焼室ケ
ーシングダB側とに分離したものとなし、ケーシングダ
の組立時に一体に成形されるようにして、それぞれのブ
ロック3を接着剤(プライマ)等によってケーシング+
Aおよび+Bの壁面に固定する。1 and 2 show an embodiment of the present invention, where / is a cylindrical pre-evaporation premixing chamber, C is a combustion chamber, and these premixing chambers L and combustion are arranged in parallel. In this example, the chambers are molded as an integral molded block J that also serves as heat insulation, using castable or machinable heat insulation material. The block 3 is separated into the head casing 371 side and the combustion chamber casing dam B side, and the blocks 3 are molded into one body when the casing dam is assembled, and each block 3 is attached with adhesive (primer) or the like. Casing +
Fix it to the walls of A and +B.
S ハへラドケーシング9A側のブロック3に形成した
連通室であり、Aは燃焼室ケ〜シングllB側のブロッ
ク3の頂部に嵌込んで双方のブロック3の間に保持させ
たバックル板であって、このバッフル板乙により連通室
Sと燃焼室コとの間を画定すると共忙、バッフル板6と
保炎器7とによって燃焼室コへの環状ノズルとを形成す
る。S is a communication chamber formed in the block 3 on the side of the casing 9A, and A is a buckle plate fitted into the top of the block 3 on the side of the combustion chamber casing 11B and held between both blocks 3. When this baffle plate 6 defines a space between the communication chamber S and the combustion chamber 7, the baffle plate 6 and the flame stabilizer 7 form an annular nozzle to the combustion chamber 7.
?は保炎器7とその中心を合わせてヘッドケーシング4
(Aの外部から着脱自在に挿着した補助燃料噴射弁であ
シ、lθは予混合室lにケーシング<cHの外部から挿
着した主燃料噴射弁、更にl/は燃焼室コに送られる予
混合気Mを点火させる点火せんである。? Align the center of the flame holder 7 with the head casing 4.
(This is the auxiliary fuel injection valve that is removably inserted from the outside of A, lθ is the main fuel injection valve that is inserted from the outside of the casing <cH into the premixing chamber l, and l/ is sent to the combustion chamber This is an ignition lamp that ignites the premixture M.
また、ブロック3のうち円筒形に形成した燃焼室コの下
流側には希釈孔/コを設けた希釈筒13が嵌合されてお
り、希釈筒/3の更に下流側にはスクロール入口部/&
が一体に成形されている。Further, a dilution cylinder 13 having a dilution hole / is fitted on the downstream side of the cylindrical combustion chamber / in the block 3 , and a scroll inlet / / is further downstream of the dilution cylinder / 3 . &
are integrally molded.
次に、このように構成した燃焼器−おける燃焼動作につ
いて述べると、希釈筒isの外周部KGって流入する燃
焼用空気Aはまづ予混合室lに導かれ、ここで主燃料噴
射弁10からの噴射により霧化された燃料Fと混合【7
、予混合気Mとなって連通室Sへと導かれる。Next, to describe the combustion operation in the combustor configured in this way, the combustion air A flowing in through the outer peripheral part KG of the dilution tube IS is first led to the premixing chamber I, where it is connected to the main fuel injection valve. Mixed with fuel F atomized by injection from 10 [7
, it becomes a premixture M and is guided to the communication chamber S.
しかして、予混合室/の頂部から連通室5には。Thus, from the top of the premixing chamber/to the communication chamber 5.
第2図に示すように予混合気Mがその接線方向か−ら導
入されるようにしであるので、予混合気Nは保炎器7の
周りの旋回流となり、更にここで反転させられた予混合
気は環状ノズルgから燃焼室コに導かれる。かくして十
分気化された予混合気Mは燃焼室−で燃焼されながら更
にその下流側で希釈孔/2から供給される希釈空気A′
によって希釈され、希薄混合気としての燃焼が継続され
て、得られる高温ガスはスクロールに送られる。As shown in Figure 2, since the premixture M is introduced from the tangential direction, the premixture N becomes a swirling flow around the flame stabilizer 7, and is further reversed here. The premixture is guided from the annular nozzle g to the combustion chamber. The thus sufficiently vaporized premixture M is combusted in the combustion chamber, and further downstream, dilution air A' is supplied from the dilution hole /2.
The resulting high-temperature gas is diluted by the gas mixture and continues to burn as a lean mixture, and the resulting hot gas is sent to the scroll.
上述したように、本例の燃焼器にあっては、燃焼室コや
予混合室lなどか一体の断熱材料で成形されているので
、従来のように特別な燃焼筒やその断熱材の配置および
支持構造を必要とせず、また、予混合室lを円筒形状に
形成しているので燃料Fの一様な拡散分布によって均一
な予混合気Mの生成が容易となる。As mentioned above, in the combustor of this example, the combustion chamber, premixing chamber, etc. are made of integral heat insulating material, so there is no need to arrange the special combustion tube and its heat insulating material as in the conventional case. Further, since the premixing chamber l is formed in a cylindrical shape, a uniform premixture M can be easily generated due to the uniform diffusion distribution of the fuel F.
また、バッフル板6や保炎器7を別体の部品として着脱
自在なように構成しているので、これらの部品に要求さ
れる工作上の精度や耐熱性をそれぞれ独自に選定して組
合わせることができる。In addition, since the baffle plate 6 and flame stabilizer 7 are configured to be detachable as separate parts, the required machining precision and heat resistance of these parts can be independently selected and combined. be able to.
なお、補助噴射弁gは予蒸発予混合燃焼システムには必
須のものではないが、始動時や急加速時。Although the auxiliary injection valve g is not essential for the pre-evaporation premix combustion system, it is used during startup and sudden acceleration.
更に高負荷時などに補助噴射弁gを補助に併用すること
によって、このような負荷変動を受ける燃焼器に幅の広
い運転性能を保持させる効果がある。Furthermore, by using the auxiliary injection valve g as an aid during times of high load, etc., there is an effect that the combustor, which is subject to such load fluctuations, can maintain a wide range of operating performance.
以上説明してきたように、本発明によれば、霧化された
燃料を予蒸発予混合する独立した円筒形の予混合室と、
予混合気を燃焼させる燃焼室とを並列に配置すると共に
、燃焼室の頂部と予混合室の頂部との間に予混合気を燃
焼室に導くための連通室を設けて、予混合室からの予混
合気が連通室で反転されて燃焼室に導かれるようKする
と共K。As explained above, according to the present invention, an independent cylindrical premixing chamber for pre-evaporating and premixing atomized fuel;
The combustion chamber for combusting the premixture is arranged in parallel, and a communication chamber for guiding the premixture to the combustion chamber is provided between the top of the combustion chamber and the top of the premixing chamber. The premixture is reversed in the communication chamber and guided to the combustion chamber.
これらの予混合室と燃焼室および連通室をそれぞれ一体
の断熱材忙よシ成形したので、従来のこの種の予蒸発予
混合式燃焼器に使用されているような内筒型の燃焼筒を
構成する必要がなく、またスクロール入口部に連なる流
路と一体化した希釈筒な燃焼室に接合させているので部
品点数が少なくてすむのみならず組立が容易で、しかも
燃焼器の全長−が従来の拡散燃焼器程度の長さですみ、
耐久性に優れているのみならずその製作費も極めて廉価
である。These premixing chambers, combustion chambers, and communication chambers are each made of integral heat insulating material, making it possible to create an internal combustion tube similar to that used in conventional preevaporation and premixing type combustors. In addition, since the combustion chamber is connected to the dilution cylinder that is integrated with the flow path connected to the scroll inlet, the number of parts is reduced and assembly is easy, and the overall length of the combustor is shortened. It is only as long as a conventional diffusion combustor,
Not only is it highly durable, but its manufacturing cost is also extremely low.
また、予混合室を独立した円筒形としたことによって燃
料を均一に拡散分布させることができ、理想的な予混金
気が得られる。更にまた、補助噴射弁を併用する仁とに
よりJ始動や急加速時などの激しい負荷変*に対して優
れた追従性を保持させることができ、幅広い運転性能を
持たせるこ゛とができる。Further, by forming the premixing chamber into an independent cylindrical shape, the fuel can be uniformly diffused and distributed, and an ideal premixed gas can be obtained. Furthermore, by using an auxiliary injection valve in combination, it is possible to maintain excellent followability against severe load changes* such as during J start or sudden acceleration, and a wide range of operating performance can be achieved.
第1図は本発明燃焼器の構成の一例を示す断面図、 第2図は第1図のB−B線断面図である。 l・・・予混合室、 a・・・燃焼室、 3・・・ブロック、 弘、ダA、lIB・・・ケーシング、 S・・・連通室、 6・・・バッフル板、 7・・・保炎器、 g・・・環状ノズル、 t・・・補助燃料噴射弁、 10・・・主燃料噴射弁、 l/・・・点火せん、 /2・・・希釈孔、 13・・・希釈筒。 /44・・・スクロール入口部。 第1 1 第2図 図 FIG. 1 is a sectional view showing an example of the configuration of the combustor of the present invention; FIG. 2 is a sectional view taken along the line B--B in FIG. 1. l... premixing chamber, a... combustion chamber, 3...Block, Hiroshi, DaA, lIB...Casing, S...Communication room, 6... baffle board, 7...Flame holder, g... annular nozzle, t...auxiliary fuel injection valve, 10... Main fuel injection valve, l/... No ignition, /2... dilution hole, 13... Dilution cylinder. /44...Scroll entrance section. 1st 1 Figure 2 figure
Claims (1)
室と、前記予混合室と並列に配置され予混合気を燃焼さ
せる燃焼室と、前記予混合室で得られた前記予混合気の
流れを反転させて前記燃焼室に導く連通室とを具えたこ
とを特徴とする燃焼器っ 2、特許請求の範囲第1項に記載の燃焼器において、前
記予混合室および前記燃焼室を断熱材で一体に形成し、
前記連通室を前記断熱材で別体に形成して5該連通室を
前記予混合室および前記燃焼室に着脱自在にしたことを
特徴とする燃焼器。[Scope of Claims] 1) An independent cylindrical premixing chamber that performs pre-evaporation and premixing of fuel, a combustion chamber that is arranged in parallel with the premixing chamber and combusts the premixed mixture, and A combustor according to claim 1, further comprising a communication chamber for reversing the flow of the obtained premixture and guiding it to the combustion chamber. The mixing chamber and the combustion chamber are integrally formed with a heat insulating material,
5. A combustor characterized in that the communication chamber is formed separately from the heat insulating material, and the communication chamber is detachably attached to the premixing chamber and the combustion chamber.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP22425783A JPS60117008A (en) | 1983-11-30 | 1983-11-30 | Burner |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP22425783A JPS60117008A (en) | 1983-11-30 | 1983-11-30 | Burner |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS60117008A true JPS60117008A (en) | 1985-06-24 |
JPH0559323B2 JPH0559323B2 (en) | 1993-08-30 |
Family
ID=16810942
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP22425783A Granted JPS60117008A (en) | 1983-11-30 | 1983-11-30 | Burner |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS60117008A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5085575A (en) * | 1989-12-19 | 1992-02-04 | Asea Brown Boveri | Method for premixed combustion of a liquid fuel |
WO2024156685A1 (en) * | 2023-01-24 | 2024-08-02 | MPS-Consulting GmbH | Combustion chamber for a gas turbine, and gas turbine |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5317773A (en) * | 1976-08-02 | 1978-02-18 | Hitachi Ltd | Minute particle detector |
JPS5833373U (en) * | 1981-08-29 | 1983-03-04 | 三上 正夫 | Fixture for retaining wire for ceiling lining in automobiles |
-
1983
- 1983-11-30 JP JP22425783A patent/JPS60117008A/en active Granted
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5317773A (en) * | 1976-08-02 | 1978-02-18 | Hitachi Ltd | Minute particle detector |
JPS5833373U (en) * | 1981-08-29 | 1983-03-04 | 三上 正夫 | Fixture for retaining wire for ceiling lining in automobiles |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5085575A (en) * | 1989-12-19 | 1992-02-04 | Asea Brown Boveri | Method for premixed combustion of a liquid fuel |
WO2024156685A1 (en) * | 2023-01-24 | 2024-08-02 | MPS-Consulting GmbH | Combustion chamber for a gas turbine, and gas turbine |
Also Published As
Publication number | Publication date |
---|---|
JPH0559323B2 (en) | 1993-08-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP3628747B2 (en) | Nozzle for diffusion mode combustion and premixed mode combustion in a turbine combustor and method for operating a turbine combustor | |
US5069029A (en) | Gas turbine combustor and combustion method therefor | |
EP0722065B1 (en) | Fuel injector arrangement for gas-or liquid-fuelled turbine | |
US20070033948A1 (en) | Multi-point staging strategy for low emission and stable combustion | |
KR20150065782A (en) | Combustor with radially staged premixed pilot for improved operability | |
CN102679399B (en) | There is the gas turbine combustion chamber of fixing flare fuel nozzle | |
US6874323B2 (en) | Low emissions hydrogen blended pilot | |
JP2006258041A (en) | Gas turbine combustor and its igniting method | |
JP3990678B2 (en) | Gas turbine combustor | |
JPH0293210A (en) | Gas turnbine combustor | |
JPS60117008A (en) | Burner | |
JP3826200B2 (en) | Premix combustor | |
CN111630321B (en) | Burner device | |
JPH1114055A (en) | Gas turbine combustor and its combustion method | |
JP3482718B2 (en) | Gas turbine combustor | |
JPH1163417A (en) | Two stage combustor | |
US8128398B2 (en) | Burner and pilot burner | |
JPH06174233A (en) | Gas turbine combustor | |
JPH03247908A (en) | Gas burner | |
JPH0539290Y2 (en) | ||
JPH0645149Y2 (en) | Combustor | |
JPH01118023A (en) | Gas turbine combustor | |
JP2666114B2 (en) | Gas turbine premix combustor | |
JPH06281146A (en) | Burner for combustor | |
JPH0875165A (en) | Gas turbine burner |