JP7037176B2 - Premixed gas burner - Google Patents

Premixed gas burner Download PDF

Info

Publication number
JP7037176B2
JP7037176B2 JP2018060981A JP2018060981A JP7037176B2 JP 7037176 B2 JP7037176 B2 JP 7037176B2 JP 2018060981 A JP2018060981 A JP 2018060981A JP 2018060981 A JP2018060981 A JP 2018060981A JP 7037176 B2 JP7037176 B2 JP 7037176B2
Authority
JP
Japan
Prior art keywords
fuel gas
burner
gas
flow path
combustion air
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.)
Active
Application number
JP2018060981A
Other languages
Japanese (ja)
Other versions
JP2019174016A (en
Inventor
太希 菊池
博史 高島
優希 衛藤
Original Assignee
株式会社サムソン
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 株式会社サムソン filed Critical 株式会社サムソン
Priority to JP2018060981A priority Critical patent/JP7037176B2/en
Publication of JP2019174016A publication Critical patent/JP2019174016A/en
Application granted granted Critical
Publication of JP7037176B2 publication Critical patent/JP7037176B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Gas Burners (AREA)

Description

本発明は、燃焼用空気と燃料ガスを予め混合してバーナヘッドに供給し、予混合ガスを噴射しながら燃焼を行うようにしている予混合ガスバーナに関するものであり、より詳しくは予混合ガスバーナにおける燃焼用空気と燃料ガスの混合性を向上させた予混合ガスバーナに関するものである。 The present invention relates to a premixed gas burner in which combustion air and fuel gas are premixed and supplied to a burner head so that combustion is performed while injecting a premixed gas. More specifically, the present invention relates to a premixed gas burner. It relates to a premixed gas burner with improved mixing properties of combustion air and fuel gas.

特許第2950196号公報に記載があるように、燃焼用空気と燃料ガスを予め混合しておき、予混合ガスを噴射しながら燃焼を行う予混合ガスバーナが知られている。ここで記載の予混合ガスバーナでは、燃焼用空気をバーナヘッドへ向けて流すバーナダクト内に2枚の絞り部材を対面するように配置して、中央部に略ベンチュリ形状のガスミキサ部を形成している。この絞り部材は、絞った先で折り曲げることでバーナダクトと平行な部分を持ち、その下流側にはゆるやかな拡がり角(約5度~10度)を持ったディフューザを設けている。そして絞り部材とバーナダクト壁面で囲まれた部分をガス室とし、前記絞り部材の平行面には、ガス噴出部として複数の小穴を開口している。前記構成の予混合ガスバーナでは、バーナダクトの上流端から供給される燃焼用空気は、絞り部材を配置している部分で流速が高まり、圧力が低下するためのガス噴出部から供給される燃料ガスは、平行面から効果的に剥離されて、燃焼用空気と効率よく予混合されるというものである。 As described in Japanese Patent No. 2950196, there is known a premixed gas burner in which combustion air and fuel gas are mixed in advance and combustion is performed while injecting the premixed gas. In the premixed gas burner described here, two throttle members are arranged so as to face each other in a burner duct that allows combustion air to flow toward the burner head, and a substantially Venturi-shaped gas mixer portion is formed in the central portion. .. This throttle member has a portion parallel to the burner duct by bending at the throttled end, and a diffuser having a gentle spreading angle (about 5 to 10 degrees) is provided on the downstream side thereof. A portion surrounded by the throttle member and the wall surface of the burner duct is used as a gas chamber, and a plurality of small holes are opened as gas ejection portions on the parallel surface of the throttle member. In the premixed gas burner having the above configuration, the combustion air supplied from the upstream end of the burner duct has the fuel gas supplied from the gas ejection part for increasing the flow velocity and decreasing the pressure at the portion where the throttle member is arranged. It is effectively stripped from the parallel planes and efficiently premixed with the combustion air.

燃焼用空気と燃料ガスを予め混合しておき、バーナヘッドでは予混合ガスを噴射して燃焼する予混合ガスバーナでは、バーナヘッドより手前で燃焼用空気と燃料ガスを十分に混合しておく必要がある。燃焼用空気と燃料ガスの混合部から燃焼部までの距離が長いと、予混合ガス内では燃料ガスが均一に分散することになるが、混合促進部の長さを長くした場合には、燃焼装置が大型化する。前記の予混合ガスバーナでは、燃焼用空気の流路を絞って燃焼用空気の流速を高めることで、ガス噴射部から噴射している燃料ガスを吸引する作用を得ることで、燃焼用空気と燃料ガスの混合性を向上させている。このことによって燃焼用空気と燃料ガスを混合する混合促進部の長さを短くすることができるが、それでも燃焼用空気流の中心部分には燃料ガスの割合が少ない部分ができることがあった。装置の小型省スペース化のためには燃焼用空気と燃料ガスの混合をさらに促進させることが望まれており、より混合性を向上させることのできる構造の検討が行われていた。 In a premixed gas burner that mixes combustion air and fuel gas in advance and injects premixed gas at the burner head to burn, it is necessary to sufficiently mix the combustion air and fuel gas before the burner head. be. If the distance from the mixing part of the combustion air and the fuel gas to the burning part is long, the fuel gas will be uniformly dispersed in the premixed gas, but if the length of the mixing promotion part is lengthened, combustion will occur. The equipment becomes large. In the premixed gas burner described above, the flow path of the combustion air is narrowed to increase the flow velocity of the combustion air, thereby obtaining the action of sucking the fuel gas injected from the gas injection section, thereby obtaining the combustion air and the fuel. The mixture of gas is improved. This makes it possible to shorten the length of the mixing promotion section that mixes the combustion air and the fuel gas, but even so, there may be a portion where the proportion of the fuel gas is small in the central portion of the combustion air flow. In order to reduce the size and space of the device, it is desired to further promote the mixing of combustion air and fuel gas, and a structure capable of further improving the mixing property has been studied.

特許2950196号公報Japanese Patent No. 2950196

本発明が解決しようとする課題は、バーナダクトで燃焼用空気と燃料ガスを混合しておいた予混合ガスをバーナヘッドに供給して燃焼する予混合ガスバーナにおいて、燃焼用空気と燃料ガスの混合性をより向上させることにある。 The problem to be solved by the present invention is the mixing property of combustion air and fuel gas in a premixed gas burner in which a premixed gas in which combustion air and fuel gas are mixed in a burner duct is supplied to a burner head for combustion. Is to improve.

請求項1に記載の発明は、送風機からの燃焼用空気をバーナヘッドへ送るバーナダクトには、燃料ガスを供給する燃料ガス配管を接続しておき、バーナダクト内を通して送る燃焼用空気に燃料ガス配管を通して送る燃料ガスを混合することで予混合ガスとして、予混合ガスをバーナヘッドから噴射して燃焼するようにしている予混合ガスバーナにおいて、バーナダクト内にはバーナダクト内を流れる燃焼用空気の流路断面積を縮小する絞り内板と、絞り内板の外側には燃料ガスを流すためのすき間である噴射ガス流路を開けて重ねるように配置した絞り外板を設置し、絞り外板より下流側にバーナダクト内の流路断面積を縮小した状態に維持する円筒状部材を設置し、円筒状部材のさらに下流側にはバーナダクト内の流路面積を拡大する末広がり部材を設置することにより、バーナダクト内の円筒状部材外側に環状空間を形成しておき、燃料ガス配管は該環状空間に燃料ガスを供給することができるように接続しておき、噴射ガス流路はバーナダクト内での燃焼用空気流の中心軸方向に向いたものであって、噴射ガス流路の先端に設けている噴射ノズルから噴射ガス流路の延長線上に燃料ガスを噴射するようにしていることを特徴とする。 According to the first aspect of the present invention, a fuel gas pipe for supplying fuel gas is connected to the burner duct that sends the combustion air from the blower to the burner head, and the fuel gas pipe is passed through the combustion air sent through the burner duct. In a premixed gas burner in which the premixed gas is injected from the burner head to burn as a premixed gas by mixing the fuel gas to be sent, the cross-sectional area of the flow path of the combustion air flowing in the burner duct is inside the burner duct. An inner plate of the throttle that reduces the size of the fuel gas and an outer plate of the throttle that is arranged so as to open and overlap the injection gas flow path, which is a gap for flowing fuel gas, are installed on the outside of the inner plate of the throttle. By installing a cylindrical member that maintains the cross-sectional area of the flow path in the burner duct in a reduced state, and by installing a divergent member that expands the flow path area in the burner duct further downstream of the cylindrical member, the inside of the burner duct is installed. An annular space is formed on the outside of the cylindrical member, the fuel gas pipe is connected so that the fuel gas can be supplied to the annular space, and the injection gas flow path is the combustion air flow in the burner duct. It is oriented in the direction of the central axis, and is characterized in that the fuel gas is injected from the injection nozzle provided at the tip of the injection gas flow path on the extension line of the injection gas flow path.

燃焼用空気流は、絞り内板の内側に沿って流れながら流路面積の縮小によって流速は増加し、絞り内板先端を超えると流路面積が拡大する。この部分では燃焼用空気流に負圧が発生し、周縁の気体を吸引する作用が発生する。また、絞り内板と絞り外板によって挟まれている噴射ガス流路内を流れている燃料ガス流は、噴射ノズルから噴射する際には噴射ガス流路の延長線上に噴射するため、燃焼用空気流の中心軸方向に向けて噴射することになり、バーナダクトの中心部分を流れている燃焼用空気流と混合する方向に流れる。 The flow velocity of the combustion air flow increases along the inside of the inner plate of the throttle due to the reduction of the flow path area, and the flow velocity increases when the tip of the inner plate of the throttle is exceeded. In this part, a negative pressure is generated in the combustion air flow, and the action of sucking the gas around the periphery occurs. Further, the fuel gas flow flowing in the injection gas flow path sandwiched between the throttle inner plate and the throttle outer plate is injected on the extension line of the injection gas flow path when injecting from the injection nozzle, so that it is for combustion. The gas is injected toward the central axis of the air flow, and flows in the direction of mixing with the combustion air flow flowing in the central portion of the burner duct.

そして噴射ガス流路5でも、噴射ガス流路では絞り内板と絞り外板が同じ間隔であっても、絞り内板と絞り外板は先細りとなっているため、噴射ガス流路での流路断面積は縮小することになり、噴射ノズルから噴射する燃料ガスの流速は速くなっていく。流速を高めた燃料ガスを燃焼用空気流に衝突させるものであるため、燃焼用空気と燃料ガスは激しくぶつかり合うことになり、混合部では両者の混合がより促進される。 Even in the injection gas flow path 5, even if the throttle inner plate and the throttle outer plate are at the same distance in the injection gas flow path, the throttle inner plate and the throttle outer plate are tapered, so that the flow in the injection gas flow path The cross-sectional area of the road will be reduced, and the flow velocity of the fuel gas injected from the injection nozzle will increase. Since the fuel gas having an increased flow velocity collides with the combustion air flow, the combustion air and the fuel gas collide violently, and the mixing of the two is further promoted in the mixing portion.

また、燃料ガスはバーナダクト内周縁の環状空間内を流れた後に噴射ノズルから噴射され、噴射ノズルでの流路面積はバーナダクト内周縁環状空間より小さくなるものであるため、バーナダクト内周縁環状空間内で燃料ガスの流れは均一化され、環状の噴射ノズルからは濃淡のない燃料ガスが噴射されるため、予混合ガス流内での燃料ガス分布がより均一化される。 Further, the fuel gas is injected from the injection nozzle after flowing in the annular space on the inner peripheral edge of the burner duct, and the flow path area at the injection nozzle is smaller than the annular space on the inner peripheral edge of the burner duct. The flow of the fuel gas is made uniform, and the fuel gas having no shading is injected from the annular injection nozzle, so that the distribution of the fuel gas in the premixed gas flow is made more uniform.

本発明を実施することで、燃焼用空気と燃料ガスの混合性が向上し、燃焼用空気と燃料ガスの混合部から燃焼部までの距離を短くすることができるため、燃焼装置を小型化することができる。 By implementing the present invention, the mixing property of the combustion air and the fuel gas is improved, and the distance from the mixing portion of the combustion air and the fuel gas to the combustion portion can be shortened, so that the combustion device can be miniaturized. be able to.

本発明を実施している予混合ガスバーナの燃焼用空気と燃料ガス混合部における断面図Cross-sectional view of the combustion air and fuel gas mixing part of the premixed gas burner in which the present invention is carried out. 本発明を実施している予混合ガスバーナ全体のフロー図Flow chart of the whole premixed gas burner carrying out this invention

本発明の一実施例を図面を用いて説明する。図1は本発明を実施している予混合ガスバーナの燃焼用空気と燃料ガス混合部における断面図、図2は本発明を実施している予混合ガスバーナ全体のフロー図である。 An embodiment of the present invention will be described with reference to the drawings. FIG. 1 is a cross-sectional view of a combustion air and fuel gas mixing portion of a premixed gas burner carrying out the present invention, and FIG. 2 is a flow chart of the entire premixed gas burner carrying out the present invention.

本発明の予混合ガスバーナは、燃焼用空気を流すバーナダクト1内に燃料ガスを噴射し、燃焼用空気と燃料ガスを混合した予混合ガスをバーナヘッド2へ送る。バーナダクト1は、送風機9から送られてきた燃焼用空気を流す径の大きなパイプであり、バーナダクト1の途中には、入口面と出口面を開口した同心の円錐台形状である絞り内板3と絞り外板4を、僅かの間をあけて重ねるようにして設置している。絞り内板3と絞り外板4は、同じ絞り角を持つものであり、縦方向の長さは絞り内板3の方が長いものとしており、絞り外板とバーナダクト内壁の間には隙間が空いている。 The premixed gas burner of the present invention injects fuel gas into the burner duct 1 through which the combustion air flows, and sends the premixed gas in which the combustion air and the fuel gas are mixed to the burner head 2. The burner duct 1 is a pipe having a large diameter for flowing combustion air sent from the blower 9, and in the middle of the burner duct 1, a concentric truncated cone-shaped diaphragm inner plate 3 having an inlet surface and an outlet surface opened is formed. The diaphragm outer plates 4 are installed so as to be overlapped with a slight gap. The aperture inner plate 3 and the aperture outer plate 4 have the same aperture angle, and the aperture inner plate 3 has a longer vertical length, and there is a gap between the aperture outer plate and the inner wall of the burner duct. Vacant.

絞り内板3と絞り外板4は、先端側で位置を揃えており、絞り外板4の先側付近に円筒状部材10を設置する。円筒状部材10は、バーナダクト1と同心であってバーナダクト1より径の小さなものとしており、円筒状部材10のさらに先側には、流路面積を拡大する先広がりとなる円錐台形部材を設置する。先側の円錐台形部材は円筒状部材10とバーナダクト内面のそれぞれと接続しており、円筒状部材10とバーナダクト1の間には環状の空間ができる。燃料ガスはこの環状空間内に導入されるように、燃料ガスの供給を行う燃料ガス配管8を接続する。 The diaphragm inner plate 3 and the diaphragm outer plate 4 are aligned on the tip side, and the cylindrical member 10 is installed near the tip side of the diaphragm outer plate 4. The cylindrical member 10 is concentric with the burner duct 1 and has a smaller diameter than the burner duct 1, and a conical trapezoidal member that expands the flow path area is installed further ahead of the cylindrical member 10. .. The conical trapezoidal member on the front side is connected to each of the cylindrical member 10 and the inner surface of the burner duct, and an annular space is formed between the cylindrical member 10 and the burner duct 1. The fuel gas pipe 8 for supplying the fuel gas is connected so that the fuel gas is introduced into the annular space.

絞り内板3と絞り外板4で挟まれた空間を噴射ガス流路5とし、絞り内板3の先端と絞り外板4の先端の間を噴射ノズル7としておき、燃料ガスは噴射ガス流路5内を通り、噴射ノズル7から噴射するようにしておく。絞り内板3と絞り外板4の絞りによる傾斜面が平行になるようにしていると、絞り内板3と絞り外板4の間隔は噴射ガス流路5内では変わらないが、噴射ガス流路5内の下流側ほど噴射ガス流路5の断面積は小さくなるため、燃料ガスの流速は増加する。噴射ガス流路5内を流れてきた燃料ガスは、バーナダクト内の環状空間内に入ると、バーナダクトの中心軸側を流れる燃焼用空気とは逆の方向に流れた後で噴射ガス流路5内を流れ、噴射ガス流路5の延長線上に噴射される。噴射ガス流路5はバーナダクト1の中心軸方向へ向いているため、燃料ガスはバーナダクト1の中心方向へ噴射される。 The space sandwiched between the throttle inner plate 3 and the throttle outer plate 4 is used as the injection gas flow path 5, and the space between the tip of the throttle inner plate 3 and the tip of the throttle outer plate 4 is set as the injection nozzle 7, and the fuel gas is the injection gas flow. It passes through the path 5 and is sprayed from the injection nozzle 7. When the inclined surfaces of the throttle inner plate 3 and the throttle outer plate 4 are made parallel to each other, the distance between the throttle inner plate 3 and the throttle outer plate 4 does not change in the injection gas flow path 5, but the injection gas flow. Since the cross-sectional area of the injection gas flow path 5 becomes smaller toward the downstream side in the path 5, the flow velocity of the fuel gas increases. When the fuel gas flowing in the injection gas flow path 5 enters the annular space in the burner duct, it flows in the direction opposite to the combustion air flowing on the central axis side of the burner duct and then in the injection gas flow path 5. And is injected on the extension line of the injection gas flow path 5. Since the injected gas flow path 5 is directed toward the central axis of the burner duct 1, the fuel gas is injected toward the center of the burner duct 1.

この場合、噴射ノズル7で流路が狭まって圧力が上昇することになり、燃料ガス流の上流側となる環状流路内での燃料ガスの流れは均一化される。環状流路での燃料ガス流を均一化しておくことで、噴射ノズル7から噴射する燃料ガスには片寄りが無くなり、燃焼用空気との混合状態は良好となる。 In this case, the flow path is narrowed by the injection nozzle 7 and the pressure rises, so that the flow of fuel gas in the annular flow path on the upstream side of the fuel gas flow is made uniform. By making the fuel gas flow in the annular flow path uniform, the fuel gas injected from the injection nozzle 7 is not biased, and the mixed state with the combustion air becomes good.

送風機からバーナダクト1内を通して送ってきた燃焼用空気は、絞り内板3の内側面に沿って流れ、絞り内板3によって燃焼用空気が流れる流路断面積は減少していくために燃焼用空気の流速は増加する。燃焼用空気の流路断面積は、絞り内板3によって一端縮小し、円筒状部材10の部分では縮小した状態が維持された後、流路が広がっていく。 Combustion air sent from the blower through the burner duct 1 flows along the inner surface of the throttle inner plate 3, and the cross-sectional area of the flow path through which the combustion air flows by the throttle inner plate 3 decreases, so that the combustion air Flow velocity increases. The cross-sectional area of the flow path of the combustion air is reduced at one end by the throttle inner plate 3, and the flow path is expanded after the reduced state is maintained at the portion of the cylindrical member 10.

絞り内板3によって流速が増加した燃焼用空気流は、絞り内板3の先側に負圧域を発生し、その周囲に流れてくる燃料ガス流を吸引して混合する。また、噴射ノズル7から噴射する燃料ガス流の流れ方向は、燃焼用空気流の中心軸方向へ向いているため、噴射ノズル7から噴射した燃料ガス流は燃焼用空気流内へ入り、燃焼用空気と混合する。 The combustion air flow whose flow velocity is increased by the throttle inner plate 3 generates a negative pressure region on the tip side of the throttle inner plate 3, and sucks and mixes the fuel gas flow flowing around the negative pressure region. Further, since the flow direction of the fuel gas flow injected from the injection nozzle 7 is directed toward the central axis of the combustion air flow, the fuel gas flow injected from the injection nozzle 7 enters the combustion air flow and is used for combustion. Mix with air.

燃焼用空気と燃料ガスが混ざり合った予混合ガスは、バーナダクト1の先にあるバーナヘッド2へ送られる。バーナダクト1の下流に設置しているバーナヘッド2は、パンチングメタルを円筒形に加工し、その周囲をメタルニットで覆ったものとしている。メタルニットは耐熱性の高い金属繊維を編んだものであり、パンチングメタルに溶接することでメタルニットが浮き上がらないようにしておく。パンチングメタルは金属板に多数の穴を開けたものであり、パンチングメタルの外側にメタルニットを被せたことにより、予混合ガスはパンチングメタルの穴を通り、メタルニットの繊維の隙間を通して噴出する。 The premixed gas in which the combustion air and the fuel gas are mixed is sent to the burner head 2 at the tip of the burner duct 1. The burner head 2 installed downstream of the burner duct 1 is formed by processing a punching metal into a cylindrical shape and covering the periphery with a metal knit. The metal knit is made by knitting metal fibers with high heat resistance, and it is welded to the punching metal to prevent the metal knit from rising. Punching metal is made by making a large number of holes in a metal plate, and by covering the outside of the punching metal with a metal knit, the premixed gas is ejected through the holes of the punching metal and through the gaps between the fibers of the metal knit.

予混合ガスバーナのヘッド部分2には、バーナヘッド2の外側表面にパイロット火炎を発生させるパイロットバーナ6を設置している。パイロットバーナ6にてパイロット火炎を燃焼させている状態でバーナヘッド2のメタルニット面から予混合ガスを噴射すると、メタルニットの表面で火炎の燃焼が行われる。 A pilot burner 6 that generates a pilot flame is installed on the outer surface of the burner head 2 in the head portion 2 of the premixed gas burner. When the premixed gas is injected from the metal knit surface of the burner head 2 while the pilot flame is being burned by the pilot burner 6, the flame is burned on the surface of the metal knit.

バーナダクト1内の燃焼用空気に燃料ガスを噴射して燃焼用空気と燃料ガスを混合していく場合、バーナダクト1内のみで十分な混合を行うためには、バーナダクトでの流路を長くする必要があった。しかし、バーナダクト1での流路を長くすると、燃焼装置が大きくなってしまうため、省スペース化のためにはバーナダクト1での流路の長さを抑えながら、予混合ガスの混合性を高くすることが望まれていた。 When fuel gas is injected into the combustion air in the burner duct 1 to mix the combustion air and the fuel gas, it is necessary to lengthen the flow path in the burner duct in order to perform sufficient mixing only in the burner duct 1. was there. However, if the flow path in the burner duct 1 is lengthened, the combustion device becomes large. Therefore, in order to save space, the length of the flow path in the burner duct 1 is suppressed and the mixing property of the premixed gas is increased. Was desired.

本実施例では、燃焼用空気流は、バーナダクト1の途中に設けている絞り内板3部分を通過する際に流路面積が縮小するために流速が増加し、燃料ガス流も絞り内板3と絞り外板4の間に形成した噴射ガス流路5を通す際には流路面積が縮小するために、噴射ガス流路の先端の噴射ノズル7を通して噴射する燃料ガス流の流速も増加する。そしてバーナダクト1では絞り内板3の先端で狭まった後に流路が広がっているため、流路の拡がりによって燃焼用空気流は末広がりに広がる流れとなる。噴射ノズル7の先側では燃焼用空気流に負圧域が発生し、燃焼用空気流の周囲から燃焼用空気流内へ周囲の気体を吸引する流れが発生する。そして、噴射ガス流路5はバーナダクト1の中心に向かっているために、噴射ノズル7の先側ではバーナダクトの中心を流れている燃焼用空気流の中に向かう流れとなる。そのため、燃料ガス流は燃焼用空気流の内側へ入り込み、燃焼用空気流と燃料ガス流の交差部では乱流が発生して燃焼用空気と燃料ガスは混合される。以上のようにしたことで、火炎の燃焼性は保ちながら混合促進部の長さを抑えることができるため、燃焼装置の省スペースを達成することができる。 In this embodiment, the flow velocity of the combustion air flow increases because the flow path area is reduced when passing through the throttle inner plate 3 provided in the middle of the burner duct 1, and the fuel gas flow is also the throttle inner plate 3. When passing through the injection gas flow path 5 formed between the throttle outer plate 4 and the throttle outer plate 4, the flow path area is reduced, so that the flow velocity of the fuel gas flow to be injected through the injection nozzle 7 at the tip of the injection gas flow path also increases. .. In the burner duct 1, since the flow path expands after being narrowed at the tip of the throttle inner plate 3, the combustion air flow spreads toward the end due to the expansion of the flow path. On the tip side of the injection nozzle 7, a negative pressure region is generated in the combustion air flow, and a flow for sucking the surrounding gas from the periphery of the combustion air flow into the combustion air flow is generated. Since the injection gas flow path 5 is directed toward the center of the burner duct 1, the flow toward the tip of the injection nozzle 7 is toward the combustion air flow flowing through the center of the burner duct. Therefore, the fuel gas flow enters the inside of the combustion air flow, and a turbulent flow is generated at the intersection of the combustion air flow and the fuel gas flow, and the combustion air and the fuel gas are mixed. As described above, the length of the mixing promoting portion can be suppressed while maintaining the combustibility of the flame, so that the space saving of the combustion device can be achieved.

なお、本発明は以上説明した実施例に限定されるものではなく、多くの変形が本発明の技術的思想内で当分野において通常の知識を有する者により可能である。例えば実施例では、バーナダクト1は円筒形状としているが、これを断面四角形の四角柱形状にし、絞り内板及び絞り外板も四角錐台形状にするなどしても同様の作用を得ることができる。 It should be noted that the present invention is not limited to the embodiments described above, and many modifications can be made by a person having ordinary knowledge in the art within the technical idea of the present invention. For example, in the embodiment, the burner duct 1 has a cylindrical shape, but the same effect can be obtained by forming the burner duct 1 into a quadrangular column shape having a quadrangular cross section and forming the diaphragm inner plate and the diaphragm outer plate into a quadrangular pyramid shape. ..

1 バーナダクト
2 バーナヘッド
3 絞り内板
4 絞り外板
5 噴射ガス流路
6 パイロットバーナ
7 噴射ノズル
8 燃料ガス配管
9 送風機
10 円筒状部材
1 Burner duct
2 Burner head 3 Squeeze inner plate 4 Squeeze outer plate 5 Injection gas flow path 6 Pilot burner 7 Injection nozzle 8 Fuel gas piping 9 Blower 10 Cylindrical member

Claims (1)

送風機からの燃焼用空気をバーナヘッドへ送るバーナダクトには、燃料ガスを供給する燃料ガス配管を接続しておき、バーナダクト内を通して送る燃焼用空気に燃料ガス配管を通して送る燃料ガスを混合することで予混合ガスとして、予混合ガスをバーナヘッドから噴射して燃焼するようにしている予混合ガスバーナにおいて、バーナダクト内にはバーナダクト内を流れる燃焼用空気の流路断面積を縮小する絞り内板と、絞り内板の外側には燃料ガスを流すためのすき間である噴射ガス流路を開けて重ねるように配置した絞り外板を設置し、燃料ガス配管は前記噴射ガス流路に燃料ガスを供給することができるように接続しておき、前記の噴射ガス流路はバーナダクト内での燃焼用空気流の中心軸方向に向いたものであって、噴射ガス流路の先端に設けている噴射ノズルから噴射ガス流路の延長線上に燃料ガスを噴射するようにしており、絞り外板より下流側にバーナダクト内の流路断面積を縮小した状態に維持する円筒状部材を設置し、円筒状部材のさらに下流側にはバーナダクト内の流路面積を拡大する末広がり部材を設置することにより、バーナダクト内の円筒状部材外側に環状空間を形成しておき、該環状空間に燃料ガスを供給するため燃料ガス配管を接続していることを特徴とする予混合ガスバーナ。 A fuel gas pipe that supplies fuel gas is connected to the burner duct that sends the combustion air from the blower to the burner head, and the fuel gas that is sent through the fuel gas pipe is mixed with the combustion air that is sent through the burner duct. In a premixed gas burner in which a premixed gas is injected from a burner head as a mixed gas for combustion, an inner plate of a throttle for reducing the cross-sectional area of the flow path of combustion air flowing in the burner duct and a throttle are contained in the burner duct. On the outside of the inner plate, a throttle outer plate is installed so as to open and overlap the injection gas flow path, which is a gap for flowing fuel gas, and the fuel gas pipe supplies fuel gas to the injection gas flow path. The injection gas flow path is directed toward the central axis of the combustion air flow in the burner duct, and is injected from the injection nozzle provided at the tip of the injection gas flow path. Fuel gas is injected on the extension of the gas flow path, and a cylindrical member that keeps the flow path cross-sectional area in the burner duct reduced is installed on the downstream side of the throttle outer plate. By installing a divergent member that expands the flow path area in the burner duct on the downstream side, an annular space is formed outside the cylindrical member in the burner duct, and a fuel gas pipe is used to supply fuel gas to the annular space. A premixed gas burner characterized by being connected .
JP2018060981A 2018-03-28 2018-03-28 Premixed gas burner Active JP7037176B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2018060981A JP7037176B2 (en) 2018-03-28 2018-03-28 Premixed gas burner

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2018060981A JP7037176B2 (en) 2018-03-28 2018-03-28 Premixed gas burner

Publications (2)

Publication Number Publication Date
JP2019174016A JP2019174016A (en) 2019-10-10
JP7037176B2 true JP7037176B2 (en) 2022-03-16

Family

ID=68166739

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2018060981A Active JP7037176B2 (en) 2018-03-28 2018-03-28 Premixed gas burner

Country Status (1)

Country Link
JP (1) JP7037176B2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113291817A (en) * 2021-06-13 2021-08-24 湖南顺特粉体输送设备有限公司 Pagoda type powder fluidization disc for pneumatic powder conveying
CN114935144B (en) * 2022-04-29 2023-08-04 东北大学 Rotational flow oxygen-enriched combustor with smoke circulation

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2950196B2 (en) 1995-04-05 1999-09-20 三浦工業株式会社 Premix gas burner
JP2000346317A (en) 1999-05-31 2000-12-15 Ebara Boiler Kk Mixer in premixing plane combustion burner
JP2002188801A (en) 2000-12-18 2002-07-05 Tokyo Gas Co Ltd Gas mixing method, gas mixing device, and burner
JP2010190483A (en) 2009-02-18 2010-09-02 Ngk Insulators Ltd Long flame lng burner

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH08128609A (en) * 1994-10-31 1996-05-21 Miura Co Ltd Fan equipped with fuel gas mixing mechanism
JPH08296812A (en) * 1995-04-24 1996-11-12 Miura Co Ltd Noise prevention means for premixed type gas burner
EP2116768B1 (en) * 2008-05-09 2016-07-27 Alstom Technology Ltd Burner

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2950196B2 (en) 1995-04-05 1999-09-20 三浦工業株式会社 Premix gas burner
JP2000346317A (en) 1999-05-31 2000-12-15 Ebara Boiler Kk Mixer in premixing plane combustion burner
JP2002188801A (en) 2000-12-18 2002-07-05 Tokyo Gas Co Ltd Gas mixing method, gas mixing device, and burner
JP2010190483A (en) 2009-02-18 2010-09-02 Ngk Insulators Ltd Long flame lng burner

Also Published As

Publication number Publication date
JP2019174016A (en) 2019-10-10

Similar Documents

Publication Publication Date Title
RU2569137C2 (en) Intermediate heating burner device and mode of operation of gas-turbine unit with consecutive combustion
US6880340B2 (en) Combustor with turbulence producing device
US20160238255A1 (en) Enhanced turbulent mixing
US20080078183A1 (en) Liquid fuel enhancement for natural gas swirl stabilized nozzle and method
US9664393B2 (en) Burner of gas turbine with fuel nozzles to inject fuel
US8893500B2 (en) Lean direct fuel injector
CN108844068B (en) Full-premix surface type burner gas-air blender
JP3884596B2 (en) Premixing device
TW201812214A (en) Solid fuel burner
JP2011058775A (en) Gas turbine combustor
US8919132B2 (en) Method of operating a gas turbine engine
KR101110144B1 (en) Premixed type gas-turbine combustor having double mixing structure for reducing nox
JPH0587340A (en) Air-fuel mixer for gas turbine combustor
JP2008292138A (en) Combustion equipment and combustion method of burner
JP2009074706A (en) Gas turbine combustor
JP2010216481A (en) Gas turbine burner and method for partially cooling hot gas flow passing through burner
JP7037176B2 (en) Premixed gas burner
EP1592495B1 (en) Mixer
TWI712761B (en) Solid fuel burner
US20180266678A1 (en) Staged burner
US20200284431A1 (en) Combustor and combustor array
JP2019174039A (en) Surface combustion burner
CN203671652U (en) Cover hood capable of achieving distributed air intake and suitable for combustion chamber of gas turbine
EP2948715B1 (en) Burner system having turbulence elements
CN109028059B (en) Full premix surface type burner with efficient gas-air mixing structure

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20210204

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20211130

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20211130

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20211223

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20220224

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20220225

R150 Certificate of patent or registration of utility model

Ref document number: 7037176

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150