Nothing Special   »   [go: up one dir, main page]

JP2630971B2 - Pulse combustion equipment - Google Patents

Pulse combustion equipment

Info

Publication number
JP2630971B2
JP2630971B2 JP3368088A JP3368088A JP2630971B2 JP 2630971 B2 JP2630971 B2 JP 2630971B2 JP 3368088 A JP3368088 A JP 3368088A JP 3368088 A JP3368088 A JP 3368088A JP 2630971 B2 JP2630971 B2 JP 2630971B2
Authority
JP
Japan
Prior art keywords
combustion
chamber
air
passage
air supply
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.)
Expired - Lifetime
Application number
JP3368088A
Other languages
Japanese (ja)
Other versions
JPH01208607A (en
Inventor
宏之 長谷部
富士夫 小林
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.)
OOSAKA GASU KK
Original Assignee
OOSAKA GASU 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 OOSAKA GASU KK filed Critical OOSAKA GASU KK
Priority to JP3368088A priority Critical patent/JP2630971B2/en
Publication of JPH01208607A publication Critical patent/JPH01208607A/en
Application granted granted Critical
Publication of JP2630971B2 publication Critical patent/JP2630971B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Landscapes

  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、燃焼室の一端側に、燃料供給路及び燃焼用
空気供給路を、かつ、他端側に、燃焼排ガスの排出路を
形成するデイルパイプを接続して、爆発に伴う燃焼排ガ
スの動慣性により流体燃料及び燃焼用空気を前記燃焼室
に流入させ、爆発燃焼させるべく構成したパルス燃焼装
置に関する。
DETAILED DESCRIPTION OF THE INVENTION [Industrial Application Field] The present invention forms a fuel supply passage and a combustion air supply passage at one end of a combustion chamber and a combustion exhaust gas discharge passage at the other end. The present invention relates to a pulse combustion device configured to connect a dale pipe to make a fluid fuel and combustion air flow into the combustion chamber by the dynamic inertia of the combustion exhaust gas accompanying the explosion, and to perform explosive combustion.

〔従来の技術〕[Conventional technology]

従来、第3図に示すように、燃料供給路(21)及び燃
焼用空気供給路(22)の夫々に、燃焼室(1)側へのガ
ス流動のみを許容する逆止弁(23)を設け、燃焼室
(1)の圧力変動に伴って逆止弁(23)を開閉して、燃
焼室(1)内が負圧の時にだけ燃料ガスと燃焼用空気が
燃焼室(1)に流入するように構成していた。
Conventionally, as shown in FIG. 3, a check valve (23) that allows only gas flow to the combustion chamber (1) side is provided in each of the fuel supply path (21) and the combustion air supply path (22). The check valve (23) is opened and closed according to the pressure fluctuation of the combustion chamber (1), so that the fuel gas and the combustion air flow into the combustion chamber (1) only when the pressure in the combustion chamber (1) is negative. Had to be configured.

また、燃焼用空気供給路(22)のファン(24)を点火
時のみ駆動して定常燃焼状態では停止するように構成し
ていた。
Further, the fan (24) of the combustion air supply path (22) is driven only at the time of ignition and is stopped in the steady combustion state.

〔発明が解決しようとする課題〕[Problems to be solved by the invention]

しかし、逆止弁(23)において板状の弁体(23a)が
1秒当り50〜100回程度の激しい振動を生じるため、弁
体(23a)の耐久性に問題を生じやすく、弁体(23a)の
振動に伴う騒音が大きくなりやすく、また、部品点数が
多くて複雑な構造の逆止弁(23)が2個も備えられてい
るため、経費、製作、メンテナンスの面でも問題があ
り、一層の改良の余地があった。
However, in the check valve (23), the plate-like valve body (23a) violently vibrates about 50 to 100 times per second, which easily causes a problem in the durability of the valve body (23a). The noise caused by the vibration of 23a) tends to increase, and there are two check valves (23) with a large number of parts and a complicated structure, which poses problems in terms of cost, production and maintenance. There was room for further improvement.

本発明の目的は、流体燃料と燃焼用空気の供給部を、
トラブルや騒音の発生がほとんど無く、経費、製作、メ
ンテナンスの全ての面で有利なものに改良し、さらに
は、高負荷燃焼が可能で、消音構成を小型化できるよう
にする点にある。
An object of the present invention is to provide a fluid fuel and a combustion air supply unit,
The problem is that there is almost no trouble and noise, and the cost, production, and maintenance are improved to be advantageous, and further, high-load combustion is possible, and the noise reduction configuration can be reduced in size.

〔課題を解決するための手段〕[Means for solving the problem]

本発明の特徴構成は、燃焼用空気供給路に空気室を接
続し、その空気室内に燃焼用空気を定常燃焼状態におい
ても加圧供給する給気装置を設け、前記燃焼用空気供給
路を常時開放通路に形成すると共に、前記空気室から前
記燃焼室へのガス流動に対する流動抵抗がその逆向きの
ガス流動に対する流動抵抗より小になる形状に形成し、
常時開放通路に形成した前記燃料供給路から前記燃焼用
空気供給路に流体燃料を加圧供給する開口を設けたこと
にあり、その作用効果は次の通りである。
A characteristic configuration of the present invention is that an air chamber is connected to a combustion air supply path, and an air supply device that pressurizes and supplies combustion air even in a steady combustion state is provided in the air chamber. While being formed in the open passage, the flow resistance to the gas flow from the air chamber to the combustion chamber is formed in a shape that is smaller than the flow resistance to the gas flow in the opposite direction,
An opening is provided to pressurize and supply fluid fuel from the fuel supply passage formed in the normally open passage to the combustion air supply passage, and its operation and effect are as follows.

〔作 用〕(Operation)

つまり、燃料供給路と燃焼用空気供給路の両方を、従
来必要とした逆止弁を設けないで常時開放通路に形成
し、しかも、燃焼室の燃焼に伴う圧力変動に伴って、流
体燃料と燃焼用空気の混合ガスがパルス燃焼に好適な状
態で燃焼室に供給されるように構成したのである。
In other words, both the fuel supply passage and the combustion air supply passage are formed as always open passages without providing the conventionally required check valve. The configuration is such that the mixed gas of the combustion air is supplied to the combustion chamber in a state suitable for pulse combustion.

さらに説明すると、定常燃焼状態において、燃焼室の
内圧が燃焼で上昇すると、燃焼室の燃焼排ガスがテイル
パイプに流れると共に、空気室のクッション作用により
燃焼用空気供給路にも流れ、そして、燃焼後に燃焼室の
内圧が低下すると、テイルパイプと燃焼用空気供給路の
両方からガスが燃焼室に流れるのであるが、流体燃料と
燃焼用空気の両方が加圧供給されて、燃焼用空気供給路
側からテイルパイプ側にガスが流動する傾向になってい
るために、また、燃焼用空気供給路から燃焼室へのガス
流動に対する流動抵抗が逆向きのガス流動に対する流動
抵抗より小さくなっているために、全体として、燃焼排
ガスのほとんどがテイルパイプに流入し、かつ、燃焼用
空気供給路から燃焼室への1回当りのガス流量が逆向き
の1回当りのガス流量よりも多くなって、流体燃料と燃
焼用空気の混合ガスが燃焼室に、供給量が周期変動する
状態で供給されるのである。
More specifically, in the steady combustion state, when the internal pressure of the combustion chamber rises due to combustion, the combustion exhaust gas of the combustion chamber flows to the tail pipe, and also flows to the combustion air supply path by the cushion function of the air chamber, and after combustion. When the internal pressure of the combustion chamber decreases, gas flows from both the tail pipe and the combustion air supply path to the combustion chamber.However, both the fluid fuel and the combustion air are pressurized and supplied from the combustion air supply path side. Because the gas tends to flow to the tail pipe side, and because the flow resistance to the gas flow from the combustion air supply path to the combustion chamber is smaller than the flow resistance to the reverse gas flow, As a whole, most of the flue gas flows into the tail pipe, and the gas flow from the combustion air supply path to the combustion chamber at a time is opposite to the gas flow at a time. It is greater than, a mixed gas of combustion air and fluid fuel combustion chamber, is the supply amount is supplied in a state of periodic variation.

したがって、従来と同様に良好なパルス燃焼を安定し
て継続できながら、従来備えられていた逆止弁を省略す
ることによって、逆止弁に起因する故障、騒音、経費、
製作やメンテナンスの煩わしさ等の問題を一切無くすこ
とができる。
Therefore, while the good pulse combustion can be stably continued as in the past, the failure, noise, cost,
Problems such as troublesome production and maintenance can be completely eliminated.

その上、実験によって確認したところ、燃焼室内の圧
力変動の周波数を、前述の従来技術の50〜100回/secよ
りも大巾に高い150〜250回/secにでき、燃焼室負荷を前
述の従来技術の2〜3×107kcal/hm3よりも充分に大き
い3〜5×107Kcal/hm3にできた。そのように周波数を
高くできると、燃焼騒音が高周波になるために消音器を
小容量のものにできる。
In addition, as confirmed by experiments, the frequency of the pressure fluctuation in the combustion chamber can be set to 150 to 250 times / sec, which is much higher than the above-described conventional technology of 50 to 100 times / sec, and the load of the combustion chamber can be reduced as described above. It was 3-5 × 10 7 Kcal / hm 3 which was sufficiently larger than the conventional 2-3 × 10 7 kcal / hm 3 . If the frequency can be increased in such a manner, the silencer can be made small in size because the combustion noise becomes high frequency.

〔発明の効果〕〔The invention's effect〕

その結果、燃料供給部をトラブルや騒音の発生がほと
んど無く、経費、製作、メンテナンスの全ての面で有利
なものにできると共に、高負荷燃焼及び消音構成の小型
化が可能になり、燃焼性能向上、耐久性向上、騒音防
止、コストダウン、小型化等を一挙に図った極めて高品
質のパルス燃焼装置を提供できるようになった。
As a result, there is almost no trouble or noise in the fuel supply unit, and it can be advantageous in all aspects of cost, production, and maintenance.In addition, high-load combustion and miniaturization of the silencing configuration are possible, and combustion performance is improved. Thus, it has become possible to provide an extremely high-quality pulse combustion device that can improve durability, prevent noise, reduce costs, and reduce the size.

〔実施例〕〔Example〕

次に、第1図及び第2図により実施例を示す。 Next, an embodiment is shown in FIG. 1 and FIG.

燃焼室(1)の一端側に燃焼用空気供給路(2)を接
続し、空気室(3)を燃焼用空気路(2)に接続し、空
気室(3)に燃焼用空気を定常燃焼状態においてもほぼ
一定圧で加圧供給する給気装置(12)を設けてある。
A combustion air supply path (2) is connected to one end of the combustion chamber (1), an air chamber (3) is connected to the combustion air path (2), and combustion air is steadily burned in the air chamber (3). An air supply device (12) is also provided for supplying pressure at a substantially constant pressure even in the state.

燃焼用空気供給路(2)を形成するに、空気室(3)
に接続したほぼ直管状の管路部分(2a)、及び、円錐形
状で小径側で管路部分(2a)にかつ大径側で燃焼室
(1)に接続した先拡がり部分(2b)を設け、管路部分
(2a)に対向する円盤状の壁体(4)を、先拡がり部分
(2b)の大径側中央に配置して支持棒(4a)で取付け、
壁体(4)の外周側にほぼ全周にわたるガス吐出口
(5)を形成し、もって、燃焼用空気供給路(2)を、
逆止弁の無い常時開放通路に形成すると共に、空気室
(3)から燃焼室(1)へのガス流動に対する流動抵抗
がその逆向きのガス流動に対する流動抵抗より小になる
形状に形成してある。
An air chamber (3) for forming the combustion air supply passage (2)
A substantially straight pipe section (2a) connected to the pipe, and a convergent section (2b) connected to the pipe section (2a) on the small diameter side and connected to the combustion chamber (1) on the large diameter side. A disk-shaped wall (4) opposed to the pipe portion (2a) is arranged at the center of the large-diameter side of the flared portion (2b) and attached with a support rod (4a);
A gas discharge port (5) is formed on the outer peripheral side of the wall (4) over substantially the entire circumference, so that a combustion air supply path (2) is formed.
It is formed in a normally open passage without a check valve, and is formed in such a shape that the flow resistance to the gas flow from the air chamber (3) to the combustion chamber (1) is smaller than the flow resistance to the gas flow in the opposite direction. is there.

先拡がり部分(2a)の背部に燃料ガスの分配室(6)
を形成し、逆止弁の無い常時開放通路に形成すると共に
流量調節弁(V)を有する燃料供給路(7)を分配室
(6)に接続し、分配室(6)から燃料ガスを加圧供給
するための多数の小円孔状開口(8)を、先拡がり部分
(2b)に分散接続し、先拡がり部分(2b)で燃料ガスと
燃焼用空気を混合して、その混合ガスをガス吐出口
(5)から燃焼室(1)に供給するように構成してあ
る。
The fuel gas distribution chamber (6) is located behind the divergent portion (2a).
The fuel supply path (7) having a flow control valve (V) is connected to the distribution chamber (6), and the fuel gas is supplied from the distribution chamber (6). A large number of small circular openings (8) for supplying pressure are dispersedly connected to the flared portion (2b), and the fuel gas and the combustion air are mixed at the flared portion (2b). It is configured to supply gas from the gas discharge port (5) to the combustion chamber (1).

空気室(3)に、その内圧上昇を抑制するための圧抜
き路(9)を接続し、燃焼室(1)の他端側に、燃焼排
ガスの排出路を形成するテイルパイプ(10)を接続し、
燃焼室(1)に始動用点火プラグ(11)を付設し、もっ
て、パルス燃焼装置を構成してある。
The air chamber (3) is connected to a pressure release passage (9) for suppressing an increase in the internal pressure, and a tail pipe (10) forming a discharge passage for combustion exhaust gas is provided at the other end of the combustion chamber (1). connection,
A starting spark plug (11) is attached to the combustion chamber (1), thereby constituting a pulse combustion device.

上記パルス燃焼装置の動作について説明する。始動時
に、給気装置(12)を作動させて、燃料ガスと燃焼用空
気を適当混合比で燃焼室(1)に供給し、かつ、点火プ
ラグ(11)により燃焼室(1)内で爆発を生じさせる。
その結果、爆発に伴う燃焼排ガスの動慣性によって、前
記両供給路(2),(7)から適当量づつ燃料ガスと燃
焼用空気が燃焼室(1)に送り込まれ、燃焼室(7)に
残存する炎により着火し、再び爆発が生じ、そして、そ
のような動作が繰返されるのである。尚、点火プラグ
(11)の作動は、パルス燃焼が安定すれば停止させる。
The operation of the pulse combustion device will be described. At start-up, the air supply device (12) is operated to supply the fuel gas and the combustion air at an appropriate mixing ratio to the combustion chamber (1), and explode in the combustion chamber (1) by the ignition plug (11). Cause.
As a result, due to the dynamic inertia of the combustion exhaust gas accompanying the explosion, an appropriate amount of fuel gas and combustion air are sent from the two supply passages (2) and (7) into the combustion chamber (1), and then into the combustion chamber (7). The remaining flame ignites, explodes again, and the operation repeats. The operation of the ignition plug (11) is stopped when the pulse combustion is stabilized.

尚、燃料供給路(7)の燃料ガス圧が200〜300mmH2O
で、インプットを10000Kcal/hrにしてパルス燃焼させる
と、燃焼室(1)の圧力変動巾が1000〜1500mmH2Oから
−500〜−1000mmH2O程になり、その場合、空気室(3)
の平均圧力が300〜500mmH2O程度になるように、燃焼用
空気供給路(2)の圧損に見合って、給気装置(12)の
供給圧と圧抜き路(9)の圧損を設定する。
The fuel gas pressure in the fuel supply passage (7) is 200 to 300 mmH 2 O.
In and by the input to 10000Kcal / hr to pulse combustion becomes more -500~-1000mmH 2 O pressure fluctuation width from 1000~1500mmH 2 O of the combustion chamber (1), in which case, the air chamber (3)
The supply pressure of the air supply device (12) and the pressure loss of the pressure release passage (9) are set in accordance with the pressure loss of the combustion air supply passage (2) so that the average pressure of the air becomes about 300 to 500 mmH 2 O. .

〔別実施例〕(Another embodiment)

次に別実施例を説明する。 Next, another embodiment will be described.

空気室(3)の容積、形状、その他の条件は、パルス
燃焼の特性、燃焼用空気供給路(2)の圧損や固有振動
数などに見合って適当に選定する。
The volume, shape, and other conditions of the air chamber (3) are appropriately selected according to the characteristics of pulse combustion, the pressure loss and the natural frequency of the combustion air supply passage (2), and the like.

給気装置(12)の具体構成は、例えば電動式のブロワ
ーやコンプレッサーなど変更自在であり、定圧維持のた
めのガバナーを組合せてもよい。
The specific configuration of the air supply device (12) can be changed, for example, such as an electric blower or a compressor, and may be combined with a governor for maintaining a constant pressure.

燃焼用空気供給路(2)や燃料供給路(7)は、形
状、寸法、具体構造、その他において適当に変更でき
る。
The combustion air supply path (2) and the fuel supply path (7) can be appropriately changed in shape, dimensions, specific structure, and the like.

燃料ガスを加圧供給する開口(8)は、寸法、個数、
配置、その他において適当に変更でき、例えば管路部分
(2a)のみに接続したり、管路部分(2a)と先拡がり部
分(2b)の両方に接続してもよい。
The opening (8) for pressurizing and supplying the fuel gas has dimensions, numbers,
The arrangement and the like can be appropriately changed. For example, the connection may be made only to the pipe portion (2a), or may be connected to both the pipe portion (2a) and the flared portion (2b).

壁体(4)は形状、寸法、構造、取付構成、その他に
おいて適宜変更可能である。
The wall (4) can be appropriately changed in shape, size, structure, mounting configuration, and the like.

圧抜き路(9)は、空気室(3)を小型化する上で有
効であり、形状、寸法、配置、個数、構造、その他にお
いて適当に変更できるが、省略することも可能である。
The pressure release path (9) is effective in reducing the size of the air chamber (3), and can be appropriately changed in shape, dimensions, arrangement, number, structure, and the like, but can be omitted.

燃料としては、都市ガス、天然ガス、プロパンガス等
のガス燃料を主として利用するが、油等の液体燃料も利
用でき、要するに流体燃料であればよい。
As the fuel, gas fuel such as city gas, natural gas, propane gas or the like is mainly used, but liquid fuel such as oil can also be used.

パルス燃焼装置は、例えば、気流乾燥装置や液加熱装
置のように流体中に燃焼室(1)やテイルパイプ(10)
等を位置させて流体を加熱する等の各種加熱目的、ある
いは、熱風発生器のように排気エネルギーと熱を利用す
る目的等に利用でき、また、具体的構成において適宜変
更自在である。
The pulse combustion device includes, for example, a combustion chamber (1) or a tail pipe (10) in a fluid such as a flash drying device or a liquid heating device.
It can be used for various heating purposes, such as heating a fluid by positioning it, etc., or for the purpose of utilizing exhaust energy and heat as in a hot air generator, and the specific configuration can be changed as appropriate.

尚、特許請求の範囲の項に図面との対照を便利にする
為に符号を記すが、該記入により本発明は添付図面の構
造に限定されるものではない。
In the claims, reference numerals are provided for convenience of comparison with the drawings, but the present invention is not limited to the structure shown in the attached drawings.

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

第1図は本発明の実施例を示す概略断面図、第2図は第
1図のII−II線矢視図である。第3図は従来例の概略断
面図である。 (1)……燃焼室、(2)……燃焼用空気供給路、
(3)……空気室、(4)……壁体、(5)……ガス吐
出口、(7)……燃料供給路、(8)……開口、(9)
……圧抜き路、(10)……テイルパイプ、(12)……給
気装置。
FIG. 1 is a schematic sectional view showing an embodiment of the present invention, and FIG. 2 is a view taken along the line II-II of FIG. FIG. 3 is a schematic sectional view of a conventional example. (1) ... combustion chamber, (2) ... combustion air supply path,
(3) ... air chamber, (4) ... wall, (5) ... gas discharge port, (7) ... fuel supply path, (8) ... opening, (9)
…… Pressure release path, (10)… Tail pipe, (12) …… Air supply device.

Claims (3)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】燃焼室(1)の一端側に、燃料供給路
(7)及び燃焼用空気供給路(2)を、かつ、他端側
に、燃焼排ガスの排出路を形成するテイルパイプ(10)
を接続して、爆発に伴う燃焼排ガスの動慣性により流体
燃料及び燃焼用空気を前記燃焼室(1)に流入させ、爆
発燃焼させるべく構成したパルス燃焼装置であって、前
記燃焼用空気供給路(2)に空気室(3)を接続し、そ
の空気室(3)内に燃焼用空気を定常燃焼状態において
も加圧供給する給気装置(12)を設け、前記燃焼用空気
供給路(2)を常時開放通路に形成すると共に、前記空
気室(3)から前記燃焼室(1)へのガス流動に対する
流動抵抗がその逆向きのガス流動に対する流動抵抗より
小になる形状に形成し、常時開放通路に形成した前記燃
料供給路(7)から前記燃焼用空気供給路(2)に流体
燃料を加圧供給する開口(8)を設けてあるパルス燃焼
装置。
1. A tail pipe forming a fuel supply passage (7) and a combustion air supply passage (2) at one end of a combustion chamber (1) and a discharge passage of combustion exhaust gas at the other end. Ten)
A pulse combustion device configured to cause fluid fuel and combustion air to flow into the combustion chamber (1) by dynamic inertia of flue gas accompanying the explosion and to perform explosive combustion, wherein the combustion air supply passage is provided. An air chamber (3) is connected to (2), and an air supply device (12) is provided in the air chamber (3) for pressurizing and supplying combustion air even in a steady combustion state. 2) is formed as an always open passage, and is formed in a shape such that the flow resistance to the gas flow from the air chamber (3) to the combustion chamber (1) is smaller than the flow resistance to the gas flow in the opposite direction. A pulse combustion apparatus having an opening (8) for pressurizing and supplying fluid fuel from the fuel supply path (7) formed as a normally open passage to the combustion air supply path (2).
【請求項2】前記燃焼用空気供給路(2)を形成する
に、前記空気室(3)に接続したほぼ直管状の管路部分
(2a)、小径側で前記管路部分(2a)にかつ大径側で前
記燃焼室(1)に接続した先拡がり部分(2b)、及び、
その先拡がり部分(2b)の大径側中心部に前記管路部分
(2a)と対向する状態で配置した壁体(4)を設けて、
その壁体(4)の外周側にガス吐出口(5)を形成し、
前記流体燃料加圧供給用の多数の開口(8)を前記先拡
がり部分(2b)に分散接続してある請求項1記載のパル
ス燃焼装置。
2. The method according to claim 1, wherein the combustion air supply passage is formed in a substantially straight pipe section connected to the air chamber, and on a small diameter side of the pipe section. And a flared portion (2b) connected to the combustion chamber (1) on the large diameter side, and
A wall (4) is provided at a central portion of the enlarged portion (2b) on the large diameter side so as to face the pipe portion (2a),
A gas discharge port (5) is formed on the outer peripheral side of the wall (4),
2. The pulse combustion device according to claim 1, wherein the plurality of openings for pressurized supply of the fluid fuel are dispersedly connected to the flared portion.
【請求項3】前記空気室(3)に、その内圧上昇を抑制
するための圧抜き路(9)を接続してある請求項1又は
2記載のパルス燃焼装置。
3. A pulse combustion apparatus according to claim 1, wherein a pressure relief passage (9) for suppressing an increase in the internal pressure is connected to said air chamber (3).
JP3368088A 1988-02-16 1988-02-16 Pulse combustion equipment Expired - Lifetime JP2630971B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3368088A JP2630971B2 (en) 1988-02-16 1988-02-16 Pulse combustion equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3368088A JP2630971B2 (en) 1988-02-16 1988-02-16 Pulse combustion equipment

Publications (2)

Publication Number Publication Date
JPH01208607A JPH01208607A (en) 1989-08-22
JP2630971B2 true JP2630971B2 (en) 1997-07-16

Family

ID=12393153

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3368088A Expired - Lifetime JP2630971B2 (en) 1988-02-16 1988-02-16 Pulse combustion equipment

Country Status (1)

Country Link
JP (1) JP2630971B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009198036A (en) * 2008-02-20 2009-09-03 Hiroshima Univ Pulse combustion device and pulse combustion method

Also Published As

Publication number Publication date
JPH01208607A (en) 1989-08-22

Similar Documents

Publication Publication Date Title
JP2001241663A (en) Multi-stage multi-plane combustion system for gas turbine engine
US4881373A (en) Pulse combustion device
JPH01306705A (en) Pulse burner
US5010728A (en) Solid fuel turbine engine
JP2630971B2 (en) Pulse combustion equipment
GB2041081A (en) Heater for gaseous fluid
JP2905627B2 (en) Pulse combustor
JPH01269803A (en) Pulse burner
US4574745A (en) Compact pulse combustion burner with enhanced heat transfer
JP4285910B2 (en) How to start a combustion device
JP2001289441A (en) Gas turbine combustor
US1160145A (en) Internal-combustion turbine.
JP2000088202A (en) Method for recovering heat from combustion product and fuel burning device
JPS5974410A (en) Heating device
US6584774B1 (en) High frequency pulsed fuel injector
CN102057221B (en) Gas flame stabilization method and apparatus
US4934923A (en) Pulse combustion apparatus
JPH0555764B2 (en)
RU2084676C1 (en) Two-regime rocket engine
JPH0549885B2 (en)
JPH0144885Y2 (en)
US4875851A (en) Steady state fuel burner assembly for a heat exchanger and method of operating same
JPS611904A (en) Pulse combustion device
JPS60207812A (en) Multi-connection type pulse burner
JPS60248910A (en) Pulse burning device