JP2001329862A - Flame detecting device for gas turbine - Google Patents
Flame detecting device for gas turbineInfo
- Publication number
- JP2001329862A JP2001329862A JP2000147243A JP2000147243A JP2001329862A JP 2001329862 A JP2001329862 A JP 2001329862A JP 2000147243 A JP2000147243 A JP 2000147243A JP 2000147243 A JP2000147243 A JP 2000147243A JP 2001329862 A JP2001329862 A JP 2001329862A
- Authority
- JP
- Japan
- Prior art keywords
- combustion chamber
- flame
- ultraviolet
- waveguide
- gas turbine
- 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.)
- Withdrawn
Links
Landscapes
- Control Of Combustion (AREA)
- Photometry And Measurement Of Optical Pulse Characteristics (AREA)
Abstract
Description
【０００１】[0001]
【発明の属する技術分野】本発明は、ガスタービン燃焼
器の着火状況を検出する火炎検出装置に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a flame detecting device for detecting an ignition state of a gas turbine combustor.
【０００２】[0002]
【従来の技術】発電プラントに適用されるガスタービン
は、圧縮機で圧縮された空気と燃料が混合さた混合気を
燃焼器で燃焼することで、その燃焼ガスによって駆動さ
れる。ガスタービンの燃焼器での着火は点火栓により行
なわれ、燃焼器には火炎を紫外線によって検出する火炎
検出装置が備えられている。火炎検出装置により着火状
態（失火状態）を検出し、失火が生じた場合には燃料の
供給停止等の措置を講じている。2. Description of the Related Art A gas turbine applied to a power plant is driven by a combustion gas by burning a mixture of air and fuel compressed by a compressor in a combustor. Ignition in a combustor of a gas turbine is performed by an ignition plug, and the combustor is provided with a flame detection device that detects a flame by ultraviolet rays. An ignition state (misfire state) is detected by a flame detection device, and if a misfire occurs, measures such as stopping supply of fuel are taken.
【０００３】従来の火炎検出装置は、燃焼室を臨むガラ
ス管を燃焼器の本体に設置し、ガラス管の端部にUV光電
管が取り付けられている。UV光電管により燃焼室内に火
炎特有の短波長の紫外線が有るか否かを検出し、燃焼器
が着火されたかを判断している。In a conventional flame detecting device, a glass tube facing a combustion chamber is installed in a main body of a combustor, and a UV photoelectric tube is attached to an end of the glass tube. The UV photoelectric tube detects whether there is a short wavelength ultraviolet ray unique to the flame in the combustion chamber, and determines whether the combustor is ignited.
【０００４】[0004]
【発明が解決しようとする課題】ガスタービンの燃焼器
は高温（例えば1500℃）となるため、ガラス管を介して
UV光電管を取り付けても、UV光電管は高温環境にさらさ
れることになると共に、振動が生じる箇所である。この
ため、従来では、振動や高温に対処できる特殊なUV光電
管を用いたり、水冷設備を付加しており、コストが高く
装置も複雑になっていた。また、UV光電管の交換等のメ
ンテナンスを行う場合、水冷設備等の付帯設備の交換等
の作業が必要となっていた。Since the combustor of a gas turbine is at a high temperature (for example, 1500 ° C.), the temperature of the combustor is increased through a glass tube.
Even if the UV phototube is attached, the UV phototube is exposed to a high-temperature environment and is a place where vibration occurs. For this reason, conventionally, a special UV photoelectric tube capable of coping with vibration and high temperature was used, or a water-cooling device was added, so that the cost was high and the device was complicated. In addition, when maintenance such as replacement of the UV photoelectric tube is performed, work such as replacement of ancillary equipment such as water cooling equipment has been required.
【０００５】また、ガスタービンの燃焼器は円周方向に
多数設けられ、各燃焼器は伝播管によってつながれ、下
部の燃焼器が着火され順番に上方の燃焼器に火炎が伝播
し最終的に最上部の燃焼器に着火されるようになってい
るため、炎検出装置は最後に着火される上部の燃焼器に
装着されている。このため、高所作業となり、また、運
転を停止した状態での作業となっていた。[0005] Further, a large number of combustors are provided in a circumferential direction in a gas turbine, and each combustor is connected by a propagation pipe, a lower combustor is ignited, and a flame propagates to an upper combustor in order, and finally reaches a maximum. Since the upper combustor is ignited, the flame detection device is mounted on the upper combustor which is ignited last. For this reason, the operation was performed at a high place, and the operation was stopped.
【０００６】光ファイバを用いて紫外線を燃焼器から離
れた場所に導き、光ファイバで導かれた紫外線をUV光電
管で検出することも考えられるが、光ファイバは折れや
すく曲線状態に曲げて任意の場所に導くことが困難であ
り、また、紫外線を伝送する光ファイバは特殊で高価に
なってしまう。It is conceivable to use an optical fiber to guide ultraviolet light to a place away from the combustor, and to detect the ultraviolet light guided by the optical fiber with a UV photoelectric tube. However, the optical fiber is easily broken and bent into a curved state. It is difficult to guide to the place, and the optical fiber transmitting the ultraviolet light is special and expensive.
【０００７】本発明は上記状況に鑑みてなされたもの
で、簡素な構成で交換作業等のメンテナンスが容易なガ
スタービンの火炎検出装置を提供することを目的とす
る。SUMMARY OF THE INVENTION The present invention has been made in view of the above circumstances, and has as its object to provide a gas turbine flame detecting device which has a simple configuration and facilitates maintenance such as replacement work.
【０００８】[0008]
【課題を解決するための手段】上記目的を達成するため
の本発明の構成は、導波管の一端をタービン燃焼室に連
結してタービン燃焼室内を臨ませ、導波管の他端に紫外
線を検出する紫外線検出手段を設け、導波管を通してタ
ービン燃焼室内の紫外線を紫外線検出手段で検出するこ
とでタービン燃焼室内の火炎の有無を検知することを特
徴とする。In order to achieve the above-mentioned object, according to the present invention, one end of a waveguide is connected to a turbine combustion chamber to face the turbine combustion chamber, and the other end of the waveguide is exposed to ultraviolet light. Is provided, and the presence or absence of a flame in the turbine combustion chamber is detected by detecting ultraviolet rays in the turbine combustion chamber through the waveguide with the ultraviolet detection means.
【０００９】また、上記目的を達成するための本発明の
構成は、円周方向に多数のタービン燃焼室を備えたガス
タービンにおいて、導波管の一端を最終着火位置にある
タービン燃焼室である最終燃焼室に連結して最終燃焼室
を臨ませ、導波管の他端に紫外線を検出する紫外線検出
手段を設け、導波管を通して最終燃焼室内の紫外線を紫
外線検出手段で検出することで最終燃焼室内の火炎の有
無を検知して全てのタービン燃焼室の着火状態を判断す
ることを特徴とする。According to another aspect of the present invention, there is provided a gas turbine having a plurality of turbine combustion chambers in a circumferential direction, wherein one end of a waveguide is located at a final ignition position. The final combustion chamber is connected to the final combustion chamber, and the other end of the waveguide is provided with ultraviolet ray detecting means for detecting ultraviolet rays. The ultraviolet ray in the final combustion chamber is detected by the ultraviolet ray detecting means through the waveguide. It is characterized in that the presence or absence of a flame in the combustion chamber is detected to determine the ignition state of all turbine combustion chambers.
【００１０】そして、最終燃焼室には一対の導波管の一
端が連結され、それぞれの導波管の他端には少なくとも
２つの紫外線検出手段が設けられ、複数の紫外線検出手
段の検出情報を総合して最終燃焼室内の火炎の有無を検
知することを特徴とする。また、３つの紫外線検出手段
が導波管の他端に設けられ、２つ以上の紫外線検出手段
の検出情報が同じになったときに最終燃焼室内の火炎の
有無を検知することを特徴とする。[0010] One end of a pair of waveguides is connected to the final combustion chamber, and at least two ultraviolet detecting means are provided at the other end of each of the waveguides. It is characterized in that the presence or absence of a flame in the final combustion chamber is detected comprehensively. Further, three ultraviolet detecting means are provided at the other end of the waveguide, and the presence or absence of a flame in the final combustion chamber is detected when detection information of two or more ultraviolet detecting means becomes the same. .
【００１１】[0011]
【発明の実施の形態】図１には本発明の一実施形態例に
係る火炎検出装置を備えたガスタービンの概略構成、図
２には燃焼器の状況を表す断面、図３には図２中の要部
拡大状況、図４にはUV光電管の取り付き状況を示してあ
る。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS FIG. 1 is a schematic configuration of a gas turbine provided with a flame detecting device according to an embodiment of the present invention, FIG. 2 is a cross section showing the condition of a combustor, and FIG. FIG. 4 shows a state where the main part is enlarged, and FIG. 4 shows a state where UV phototubes are attached.
【００１２】図１、図２に示すように、ガスタービン装
置１は、複数の燃焼器（図１には４本、図２には１８
本）２が備えられ、燃焼器２を介して供給される燃焼ガ
スでガスタービン３が回転駆動される。図２に示すよう
に、複数の燃焼器２は円周状態に取り付けられ、燃焼器
２のタービン燃焼室（燃焼室）同士は伝播管４によって
連結されている。最下部の燃焼器２ａには点火栓５が設
けられ、燃焼器２ａが着火され順番に上方の燃焼器２に
火炎が伝播し最終的に最上部の２つの燃焼器２ｂの燃焼
室（最終燃焼室）が着火されるようになっている。ガス
タービン装置１には圧縮機６が備えられ、圧縮機６はガ
スタービン３によって回転駆動して圧縮空気を燃焼器２
に供給する。図中の符号で７はガスタービン装置１で運
転される発電機である。As shown in FIGS. 1 and 2, the gas turbine device 1 has a plurality of combustors (four in FIG. 1 and 18 in FIG. 2).
The gas turbine 3 is rotatably driven by the combustion gas supplied through the combustor 2. As shown in FIG. 2, the plurality of combustors 2 are attached in a circumferential state, and turbine combustion chambers (combustion chambers) of the combustor 2 are connected to each other by a transmission pipe 4. The lowermost combustor 2a is provided with an ignition plug 5, and the combustor 2a is ignited, and the flame propagates to the upper combustor 2 in order, and finally the combustion chambers of the two uppermost combustors 2b (final combustion). Room) is ignited. The gas turbine device 1 is provided with a compressor 6. The compressor 6 is rotationally driven by the gas turbine 3 to supply compressed air to the combustor 2.
To supply. Reference numeral 7 in the figure denotes a generator operated by the gas turbine device 1.
【００１３】最終着火位置にある２つの燃焼器２ｂの燃
焼室に連結して、それぞれ２本の導波管１１の一端が燃
焼室内を臨むように連結されている。導波管１１の他端
は、ガスタービン装置１の熱の影響を受けず作業がしや
すい場所、例えば、ガスタービン装置１の設置面近傍で
大気温度の環境で振動が生じない場所に導かれ、それぞ
れの導波管１１の他端には紫外線検出手段１２が設けら
れている。導波管１１は、例えば、ステンレス製または
銅製のパイプで構成され、内部を紫外線が導波されるよ
うになっている。導波管１１の内面にAlメッキやAgメッ
キを施してもよい。[0013] The two waveguides 11 are connected to the combustion chambers of the two combustors 2b at the final ignition position, and one end of each of the two waveguides 11 is connected to face the combustion chamber. The other end of the waveguide 11 is guided to a place where it is easy to work without being affected by the heat of the gas turbine device 1, for example, a place near the installation surface of the gas turbine device 1 where vibration does not occur in an environment of atmospheric temperature. The other end of each waveguide 11 is provided with an ultraviolet detecting means 12. The waveguide 11 is made of, for example, a pipe made of stainless steel or copper, so that ultraviolet rays are guided inside. The inner surface of the waveguide 11 may be plated with Al or Ag.
【００１４】図３に示すように、燃焼器２ｂの燃焼室に
は２本の石英ガラス管２０が取り付けられ、石英ガラス
管２０の先端には本体フランジ１４が設けられている。
本体フランジ１４には導波管１１側のフランジ１５がボ
ルト等により固定され、フランジ１５には導波管１１の
一端がねじ結合等により固定されている。これにより、
導波管１１の一端は石英ガラス管２０を介して燃焼器２
ｂの燃焼室内を臨むようになっている。紫外線検出手段
１２はUV光電管１３が３個一組となって構成され、３個
のUV光電管１３は、図４に示すように、三角形状に配置
されている。３個のUV光電管１３は図示しない制御装置
に連結され、３個のUV光電管１３のうちの２個以上のUV
光電管１３が検出した情報が紫外線検出手段１２の検出
情報となるようにされている。As shown in FIG. 3, two quartz glass tubes 20 are attached to the combustion chamber of the combustor 2b, and a main body flange 14 is provided at the tip of the quartz glass tube 20.
A flange 15 on the waveguide 11 side is fixed to the main body flange 14 by a bolt or the like, and one end of the waveguide 11 is fixed to the flange 15 by a screw connection or the like. This allows
One end of the waveguide 11 is connected to the combustor 2 through a quartz glass tube 20.
b, facing the combustion chamber. The ultraviolet detecting means 12 is constituted by a set of three UV phototubes 13, and the three UV phototubes 13 are arranged in a triangular shape as shown in FIG. The three UV phototubes 13 are connected to a controller (not shown), and two or more of the three UV phototubes 13
The information detected by the photoelectric tube 13 is used as the detection information of the ultraviolet detector 12.
【００１５】尚、上述した実施形態例では、２つの燃焼
器２ｂの燃焼室にそれぞれ２本の導波管１１の一端を連
結したが、２つの燃焼器２ｂの燃焼室に１本の導波管１
１を連結したり、１つの燃焼器２ｂの燃焼室に２本また
は１本の導波管１１を連結することも可能である。In the embodiment described above, one end of each of the two waveguides 11 is connected to the combustion chamber of the two combustors 2b. However, one waveguide is connected to the combustion chamber of the two combustors 2b. Tube 1
1 or two or one waveguide 11 can be connected to the combustion chamber of one combustor 2b.
【００１６】上記構成の火炎検出装置を備えたガスター
ビン装置１では、点火栓５により最下部の燃焼器２ａが
着火され、順番に上方の燃焼器２に火炎が伝播し最終的
に最上部の２つの燃焼器２ｂの燃焼室が着火されるよう
になっている。そして、燃焼器２ｂの燃焼室内の紫外線
が導波管１１を導波して紫外線検出手段１２に送られ
る。３個のUV光電管１３により紫外線が検出されると、
即ち、２個以上のUV光電管１３により紫外線が検出され
ると、燃焼器２ｂの燃焼室内の火炎が確認されて燃焼器
２の着火が認識される。また、２個以上のUV光電管１３
により紫外線が確認されないと、燃焼器２が失火してい
ると認識され、燃料停止等の処置が実行される。In the gas turbine device 1 provided with the flame detecting device having the above structure, the lowermost combustor 2a is ignited by the ignition plug 5, and the flame propagates to the upper combustor 2 in order, and finally the uppermost combustor 2a. The combustion chambers of the two combustors 2b are ignited. Then, the ultraviolet light in the combustion chamber of the combustor 2 b is guided to the ultraviolet light detecting means 12 through the waveguide 11. When ultraviolet rays are detected by the three UV photoelectric tubes 13,
That is, when ultraviolet rays are detected by two or more UV photoelectric tubes 13, the flame in the combustion chamber of the combustor 2b is confirmed, and ignition of the combustor 2 is recognized. In addition, two or more UV photoelectric tubes 13
If no ultraviolet ray is detected, it is recognized that the combustor 2 has misfired, and measures such as stopping the fuel are executed.
【００１７】上述した火炎検出装置は、導波管１１によ
り燃焼器２ｂから遠い場所の良好な環境の場所まで紫外
線を導波し、そこでUV光電管１３により紫外線を検出し
ているので、高温で振動が発生する環境下にUV光電管１
３を設置する必要がなく、安価なUV光電管を適用するこ
とができ、容易に３個のUV光電管を用いて紫外線検出手
段１２とすることができ、冷却設備等が不要になる。従
って、温度や振動等によるUV光電管１３の故障が無くな
って信頼性が向上し、火炎検出装置を安価に構成するこ
とができると共に、壊れたUV光電管１３のみの交換が可
能になり、しかも、運転中の交換が可能になる。また、
UV光電管１３の使用環境が厳しくないため、安価なUV光
電管１３であっても長期にわたり使用することができ、
ランニングコストを大幅に安くすることができる。In the above-described flame detecting device, the ultraviolet rays are guided by the waveguide 11 to a place in a favorable environment far from the combustor 2b, and the ultraviolet rays are detected by the UV photoelectric tube 13 there. Photovoltaic tube 1
3, there is no need to install, an inexpensive UV photoelectric tube can be applied, and the UV detecting means 12 can be easily formed by using three UV photoelectric tubes, so that cooling equipment and the like become unnecessary. Therefore, the failure of the UV photoelectric tube 13 due to temperature, vibration, or the like is eliminated, reliability is improved, the flame detection device can be configured at low cost, and only the broken UV photoelectric tube 13 can be replaced. Exchange during is possible. Also,
Because the usage environment of the UV photoelectric tube 13 is not severe, even an inexpensive UV photoelectric tube 13 can be used for a long time,
The running cost can be significantly reduced.
【００１８】[0018]
【発明の効果】本発明のガスタービンの火炎検出装置
は、導波管の一端をタービン燃焼室に連結してタービン
燃焼室内を臨ませ、導波管の他端に紫外線を検出する紫
外線検出手段を設け、導波管を通してタービン燃焼室内
の紫外線を紫外線検出手段で検出することでタービン燃
焼室内の火炎の有無を検知するようにしたので、燃焼室
から遠い場所の良好な環境の場所まで紫外線を導波し、
そこで紫外線検出手段により紫外線を検出して火炎を検
出することができる。この結果、高温で振動が発生する
環境下に紫外線検出手段を設置する必要がなく、安価な
紫外線検出手段を適用することができ、冷却設備等が不
要になり、簡素な構成で交換作業等のメンテナンスが容
易なガスタービンの火炎検出装置とすることができる。The flame detecting device for a gas turbine according to the present invention has an ultraviolet detecting means for connecting one end of a waveguide to a turbine combustion chamber so as to face the turbine combustion chamber and detecting ultraviolet light at the other end of the waveguide. Is provided, and the presence or absence of a flame in the turbine combustion chamber is detected by detecting ultraviolet rays in the turbine combustion chamber through the waveguide with the ultraviolet ray detecting means. Guided,
Therefore, the flame can be detected by detecting the ultraviolet ray by the ultraviolet ray detecting means. As a result, there is no need to install ultraviolet detecting means in an environment where vibrations occur at high temperatures, an inexpensive ultraviolet detecting means can be applied, cooling equipment and the like become unnecessary, and a simple configuration for replacement work and the like can be achieved. A flame detector for a gas turbine that can be easily maintained can be provided.
【００１９】また、本発明のガスタービンの火炎検出装
置は、円周方向に多数のタービン燃焼室を備えたガスタ
ービンにおいて、導波管の一端を最終着火位置にあるタ
ービン燃焼室である最終燃焼室に連結して最終燃焼室を
臨ませ、導波管の他端に紫外線を検出する紫外線検出手
段を設け、導波管を通して最終燃焼室内の紫外線を紫外
線検出手段で検出することで最終燃焼室内の火炎の有無
を検知して全てのタービン燃焼室の着火状態を判断する
ようにしたので、最終燃焼室から遠い場所の良好な環境
の場所まで紫外線を導波し、そこで紫外線検出手段によ
り紫外線を検出して全てのタービン燃焼室の火炎を検出
することができる。この結果、高温で振動が発生する環
境下に紫外線検出手段を設置する必要がなく、安価な紫
外線検出手段を適用することができ、冷却設備等が不要
になり、簡素な構成で交換作業等のメンテナンスが容易
なガスタービンの火炎検出装置とすることができる。Further, according to the gas turbine flame detecting device of the present invention, in a gas turbine having a plurality of turbine combustion chambers in a circumferential direction, one end of a waveguide is a final combustion position of a turbine combustion chamber at a final ignition position. The other end of the waveguide is provided with ultraviolet ray detection means for detecting ultraviolet rays, and the ultraviolet ray in the final combustion chamber is detected by the ultraviolet ray detection means through the waveguide. The presence or absence of the flame is detected to determine the ignition state of all turbine combustion chambers, so that ultraviolet light is guided to a place in a favorable environment far from the final combustion chamber, where the ultraviolet light is detected by ultraviolet light detection means. It is possible to detect and detect the flames of all the turbine combustion chambers. As a result, there is no need to install ultraviolet detecting means in an environment where vibrations occur at high temperatures, an inexpensive ultraviolet detecting means can be applied, cooling equipment and the like become unnecessary, and a simple configuration for replacement work and the like can be achieved. A flame detector for a gas turbine that can be easily maintained can be provided.
【００２０】また、最終燃焼室には一対の導波管の一端
が連結され、それぞれの導波管の他端には少なくとも２
つの紫外線検出手段が設けられ、複数の紫外線検出手段
の検出情報を総合して最終燃焼室内の火炎の有無を検出
するようにしたので、確実に火炎の有無を検知すること
ができる。Further, one end of a pair of waveguides is connected to the final combustion chamber, and at least two ends are connected to the other end of each waveguide.
One ultraviolet detecting means is provided, and the presence or absence of the flame in the final combustion chamber is detected by integrating the detection information of the plurality of ultraviolet detecting means, so that the presence or absence of the flame can be reliably detected.
【００２１】また、３つの紫外線検出手段が導波管の他
端に設けられ、２つ以上の紫外線検出手段の検出情報が
同じになったときに最終燃焼室内の火炎の有無を検知す
るようにしたので、安価な構成で確実に火炎の有無を検
知することができる。Also, three ultraviolet detecting means are provided at the other end of the waveguide, and the presence or absence of a flame in the final combustion chamber is detected when the detection information of the two or more ultraviolet detecting means becomes the same. Therefore, it is possible to reliably detect the presence or absence of a flame with an inexpensive configuration.
【図面の簡単な説明】[Brief description of the drawings]
【図１】本発明の一実施形態例に係る火炎検出装置を備
えたガスタービンの概略構成図。FIG. 1 is a schematic configuration diagram of a gas turbine including a flame detection device according to an embodiment of the present invention.
【図２】燃焼器の状況を表す断面図。FIG. 2 is a cross-sectional view illustrating a state of a combustor.
【図３】図２中の要部拡大図。FIG. 3 is an enlarged view of a main part in FIG. 2;
【図４】UV光電管の取り付き状況説明図。FIG. 4 is an explanatory diagram of a mounting state of a UV photoelectric tube.
１ ガスタービン装置 ２ 燃焼器 ３ ガスタービン ４ 伝播管 ５ 点火栓 ６ 圧縮機 １１ 導波管 １２ 紫外線検出手段 １３ UV光電管 DESCRIPTION OF SYMBOLS 1 Gas turbine apparatus 2 Combustor 3 Gas turbine 4 Propagation tube 5 Spark plug 6 Compressor 11 Waveguide 12 Ultraviolet ray detection means 13 UV photoelectric tube
Claims (4)
てタービン燃焼室内を臨ませ、導波管の他端に紫外線を
検出する紫外線検出手段を設け、導波管を通してタービ
ン燃焼室内の紫外線を紫外線検出手段で検出することで
タービン燃焼室内の火炎の有無を検知することを特徴と
するガスタービンの火炎検出装置。An end of a waveguide is connected to a turbine combustion chamber to face the turbine combustion chamber, and the other end of the waveguide is provided with ultraviolet detecting means for detecting ultraviolet light. A flame detection device for a gas turbine, wherein the presence or absence of a flame in a turbine combustion chamber is detected by detecting ultraviolet light by an ultraviolet light detection means.
たガスタービンにおいて、導波管の一端を最終着火位置
にあるタービン燃焼室である最終燃焼室に連結して最終
燃焼室を臨ませ、導波管の他端に紫外線を検出する紫外
線検出手段を設け、導波管を通して最終燃焼室内の紫外
線を紫外線検出手段で検出することで最終燃焼室内の火
炎の有無を検知して全てのタービン燃焼室の着火状態を
判断することを特徴とするガスタービンの火炎検出装
置。2. In a gas turbine having a plurality of turbine combustion chambers in a circumferential direction, one end of a waveguide is connected to a final combustion chamber which is a turbine combustion chamber at a final ignition position to face the final combustion chamber. The other end of the waveguide is provided with an ultraviolet ray detecting means for detecting ultraviolet rays, and the ultraviolet rays in the final combustion chamber are detected by the ultraviolet ray detecting means through the waveguide to detect the presence or absence of a flame in the final combustion chamber. A flame detection device for a gas turbine, which determines an ignition state of a combustion chamber.
の導波管の一端が連結され、それぞれの導波管の他端に
は少なくとも２つの紫外線検出手段が設けられ、複数の
紫外線検出手段の検出情報を総合して最終燃焼室内の火
炎の有無を検知することを特徴とするガスタービンの火
炎検出装置。3. The ultraviolet detector according to claim 2, wherein one end of a pair of waveguides is connected to the final combustion chamber, and at least two ultraviolet detecting means are provided at the other end of each waveguide. A flame detection device for a gas turbine, which detects presence or absence of a flame in a final combustion chamber by integrating detection information of the means.
段が導波管の他端に設けられ、２つ以上の紫外線検出手
段の検出情報が同じになったときに最終燃焼室内の火炎
の有無を検知することを特徴とするガスタービンの火炎
検出装置。4. The flame according to claim 2, wherein three ultraviolet detecting means are provided at the other end of the waveguide, and the presence or absence of a flame in the final combustion chamber when two or more ultraviolet detecting means have the same detection information. A flame detection device for a gas turbine, wherein the flame is detected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2000147243A JP2001329862A (en) | 2000-05-19 | 2000-05-19 | Flame detecting device for gas turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2000147243A JP2001329862A (en) | 2000-05-19 | 2000-05-19 | Flame detecting device for gas turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JP2001329862A true JP2001329862A (en) | 2001-11-30 |
Family
ID=18653449
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2000147243A Withdrawn JP2001329862A (en) | 2000-05-19 | 2000-05-19 | Flame detecting device for gas turbine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2001329862A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2008169835A (en) * | 2007-01-12 | 2008-07-24 | Rosemount Aerospace Inc | Combustion condition monitoring device for gas turbine engine |
| CN100414271C (en) * | 2002-05-07 | 2008-08-27 | 株式会社山武 | Ultraviolet detector |
-
2000
- 2000-05-19 JP JP2000147243A patent/JP2001329862A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100414271C (en) * | 2002-05-07 | 2008-08-27 | 株式会社山武 | Ultraviolet detector |
| JP2008169835A (en) * | 2007-01-12 | 2008-07-24 | Rosemount Aerospace Inc | Combustion condition monitoring device for gas turbine engine |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP1036308B1 (en) | Method and apparatus for characterizing a combustion flame | |
| US6135760A (en) | Method and apparatus for characterizing a combustion flame | |
| US7928854B2 (en) | Techniques for smoke detection | |
| US8418475B2 (en) | Attachment structure of combustion oscillation detecting device | |
| JP2006083730A (en) | Firing detection method for gas turbine | |
| CN105509890A (en) | On-line infrared measurement apparatus for hearth flue-gas temperature | |
| JP2011202943A (en) | Optical fuel nozzle flashback detector | |
| CN206958962U (en) | Flame detector | |
| JP2001329862A (en) | Flame detecting device for gas turbine | |
| AU601503B2 (en) | Combined ignition and monitoring device for burners | |
| CN215062201U (en) | Flame detection device for boiler combustion system | |
| CN107228017B (en) | Gas turbine plant provided with thermoacoustic instability detection and method for controlling the same | |
| EP3222918B1 (en) | Gas-turbine burner assembly with optical probe | |
| GB2282221A (en) | A flame detector | |
| CN213207923U (en) | Micro-oil ignition ultraviolet flame detection light guide device for boiler of thermal power plant | |
| JP2020063869A (en) | Unburned gas detection device | |
| KR200330737Y1 (en) | Burner Flame Image Receiver | |
| CN216557203U (en) | Double-probe flame detection system | |
| JP2014055851A (en) | Flame detector, and burner ignition torch equipped with the same | |
| CN217715035U (en) | Fire detection measuring tube cooling device with temperature monitoring function | |
| JPH055425A (en) | Method and device for detecting burner deterioration | |
| JPH0697187B2 (en) | Flame monitoring device using optical fiber | |
| JP3529161B2 (en) | Furnace combustion vibration monitoring device | |
| KR101140998B1 (en) | Flame sensor for buner | |
| JPS6339559Y2 (en) |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A300 | Withdrawal of application because of no request for examination |
Free format text: JAPANESE INTERMEDIATE CODE: A300 Effective date: 20070807 |