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JPS60189708U - pulse combustion device - Google Patents

pulse combustion device

Info

Publication number
JPS60189708U
JPS60189708U JP7545284U JP7545284U JPS60189708U JP S60189708 U JPS60189708 U JP S60189708U JP 7545284 U JP7545284 U JP 7545284U JP 7545284 U JP7545284 U JP 7545284U JP S60189708 U JPS60189708 U JP S60189708U
Authority
JP
Japan
Prior art keywords
air
fuel injection
injection part
air passage
pulse 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
Application number
JP7545284U
Other languages
Japanese (ja)
Other versions
JPH0144884Y2 (en
Inventor
平澤 房男
桜井 耕三
菅野 義裕
坂本 幾久
幸利 高橋
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.)
Toshiba Corp
Tokyo Gas Co Ltd
Original Assignee
Toshiba Corp
Tokyo Gas Co Ltd
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 Toshiba Corp, Tokyo Gas Co Ltd filed Critical Toshiba Corp
Priority to JP7545284U priority Critical patent/JPS60189708U/en
Publication of JPS60189708U publication Critical patent/JPS60189708U/en
Application granted granted Critical
Publication of JPH0144884Y2 publication Critical patent/JPH0144884Y2/ja
Granted legal-status Critical Current

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  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

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

、第1図および第2図はこの考案の一実施例を示すもの
で、第1図はパルス燃焼装置における燃料噴出部近傍の
概略構成を示す縦断面図、第2図は第1図の■−■線断
面図、第3図乃至第5図は従来例を示すもので、第3図
はラジアントチューブ    −バーナ全体の概略構成
を示す縦断面図、第4図は空気フラッパバルブ機構の概
略構成を示す縦断面図、第5図は空気フランパバルブ機
構を一部切欠して示す横断面図である。 ′9・・・燃料噴出部、11・・・燃焼室、25・・・
空気通路、32・・・空気渦流形成部材。 第1図 第2図
, FIG. 1 and FIG. 2 show an embodiment of this invention. FIG. 1 is a vertical cross-sectional view showing a schematic structure near the fuel injection part in a pulse combustion device, and FIG. - sectional view taken along the ■ line; Figures 3 to 5 show a conventional example; Figure 3 is a radiant tube; - a longitudinal sectional view showing a schematic configuration of the entire burner; and Figure 4 is a schematic configuration of the air flapper valve mechanism. FIG. 5 is a cross-sectional view, with a portion of the air flapper valve mechanism cut away. '9... Fuel injection part, 11... Combustion chamber, 25...
Air passage, 32... air vortex forming member. Figure 1 Figure 2

Claims (2)

【実用新案登録請求の範囲】[Scope of utility model registration request] (1)パルス燃焼用の燃焼室と、この燃焼室の上流側に
連通し燃焼室への空気を供給させる空気通路と、この空
気通路内の略中央に形成し空気の流通方向に対し略直角
方向に燃料を噴射する燃、−料噴出部と、この燃料噴出
部の上流側外周部分における空気通路に形成した燃料噴
出部側へ送られる空気流を旋回させるための空気渦流形
成部材とを具備したことを特徴とするパルス燃焼装置。
(1) A combustion chamber for pulse combustion, an air passage that communicates with the upstream side of this combustion chamber and supplies air to the combustion chamber, and an air passage that is formed approximately in the center of this air passage and is approximately perpendicular to the direction of air flow. The fuel injection part includes a fuel injection part that injects fuel in the direction of the fuel injection part, and an air vortex forming member for swirling the air flow sent to the fuel injection part side, which is formed in the air passage in the upstream outer peripheral part of the fuel injection part. A pulse combustion device characterized by:
(2)空気渦流形成部材は空気通路の空気流通方向に対
し傾斜状態で形成された空気渦流形成用の゛ 複数のガ
イド孔を備え、かつ各ガイド孔間の隔壁によって形成さ
れる固定翼部を空気の流通方向に対し上流側から下流側
まで同一幅寸法に形成させた形状または下流側に比べて
上流側か先細となる形状の何れかの形状にしたことを特
徴とする実用新案登録請求の範囲第(1)項記載のパル
ス燃焼装置。
(2) The air vortex forming member is provided with a plurality of guide holes for forming an air vortex formed at an angle with respect to the air flow direction of the air passage, and has a fixed wing portion formed by a partition wall between each guide hole. A claim for utility model registration characterized by having a shape that has the same width dimension from upstream to downstream in the direction of air circulation, or a shape that is tapered on the upstream side compared to the downstream side. A pulse combustion device according to scope (1).
JP7545284U 1984-05-23 1984-05-23 pulse combustion device Granted JPS60189708U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7545284U JPS60189708U (en) 1984-05-23 1984-05-23 pulse combustion device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7545284U JPS60189708U (en) 1984-05-23 1984-05-23 pulse combustion device

Publications (2)

Publication Number Publication Date
JPS60189708U true JPS60189708U (en) 1985-12-16
JPH0144884Y2 JPH0144884Y2 (en) 1989-12-26

Family

ID=30616684

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7545284U Granted JPS60189708U (en) 1984-05-23 1984-05-23 pulse combustion device

Country Status (1)

Country Link
JP (1) JPS60189708U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2016503482A (en) * 2012-11-07 2016-02-04 エクスポネンシャル テクノロジーズ, インコーポレイテッドExponential Technologies, Inc. Pressure gain combustion apparatus and method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2016503482A (en) * 2012-11-07 2016-02-04 エクスポネンシャル テクノロジーズ, インコーポレイテッドExponential Technologies, Inc. Pressure gain combustion apparatus and method

Also Published As

Publication number Publication date
JPH0144884Y2 (en) 1989-12-26

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