CN104033903B - Composite burner - Google Patents

Composite burner Download PDF

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Publication number
CN104033903B
CN104033903B CN201310067386.3A CN201310067386A CN104033903B CN 104033903 B CN104033903 B CN 104033903B CN 201310067386 A CN201310067386 A CN 201310067386A CN 104033903 B CN104033903 B CN 104033903B
Authority
CN
China
Prior art keywords
burner
fuel
fuel injection
pipe
induction tunnel
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 - Fee Related
Application number
CN201310067386.3A
Other languages
Chinese (zh)
Other versions
CN104033903A (en
Inventor
包寅戈
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.)
Taizhou Zaobao Cooker Co Ltd
Original Assignee
Taizhou Zaobao Cooker 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 Taizhou Zaobao Cooker Co Ltd filed Critical Taizhou Zaobao Cooker Co Ltd
Priority to CN201310067386.3A priority Critical patent/CN104033903B/en
Publication of CN104033903A publication Critical patent/CN104033903A/en
Application granted granted Critical
Publication of CN104033903B publication Critical patent/CN104033903B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The invention discloses a kind of composite burner, including a bracing frame, a homogenizing plate and one first fuel injection pipe, described composite burner also include a burner and one second fuel injection pipe, be provided with an annular groove on described bracing frame, one first fuel enters pipe and one first induction tunnel support, the size of described homogenizing plate adapts with the size of described annular groove, and the first described fuel injection pipe is connected with the first described induction tunnel support.The advantage of the composite burner of the present invention is: with two fuel injection pipes of horizontally disposed and vertical layout, the fuel and the air that simultaneously enter burner are more, and heating power is relatively big, and range is wide.

Description

Composite burner
Technical field
The present invention relates to a kind of burner, more precisely a kind of composite burner.
Background technology
Combustion furnace is a kind of for by clean-burning for combustion gas equipment, being widely used in productive life, but combustion furnace of the prior art only includes a fuel injection pipe, fuel and the lack of air of burner is entered in unit interval, the heat of release is less, and heating power is less, and range is narrower.
Summary of the invention
The present invention mainly solves the technical problem existing for prior art, thus a kind of two fuel injection pipes with horizontally disposed and vertical layout are provided, the fuel and the air that simultaneously enter burner are more, and heating power is relatively big, the composite burner that range is wide.
The above-mentioned technical problem of the present invention is mainly addressed by following technical proposals:
A kind of composite burner, including a bracing frame, a homogenizing plate and one first fuel injection pipe, described composite burner also include a burner and one second fuel injection pipe, be provided with an annular groove on described bracing frame, one first fuel enters pipe and one first induction tunnel support, the size of described homogenizing plate adapts with the size of described annular groove, and the first described fuel injection pipe is connected with the first described induction tunnel support.
As preferred embodiment of the present invention, be evenly arranged equal discharge orifice on described homogenizing plate, one second fuel enters pipe and one second induction tunnel support, being placed with a honeycomb type current-sharing block in described equal discharge orifice, the second described fuel injection pipe is connected with the second described induction tunnel support.
As preferred embodiment of the present invention, the bottom of described burner is provided with a fuel inlet, and described fuel inlet enters pipe with the second described fuel and is connected.
As preferred embodiment of the present invention, the sidewall of the end of the first described fuel injection pipe being provided with perforation, the structure of the second described fuel injection pipe is identical with the structure of the first described fuel injection pipe.
As preferred embodiment of the present invention, the kind of described burner includes infrared stove head and floated burner, and the present invention preferentially uses infrared stove head, the bottom of floated burner to include a fuel inlet.
The advantage of the composite burner of the present invention is: with two fuel injection pipes of horizontally disposed and vertical layout, the fuel and the air that simultaneously enter burner are more, and heating power is relatively big, and range is wide.
Accompanying drawing explanation
In order to be illustrated more clearly that the embodiment of the present invention or technical scheme of the prior art, the accompanying drawing used required in embodiment or description of the prior art will be briefly described below, apparently, accompanying drawing in describing below is only some embodiments of the present invention, for those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings.
Fig. 1 is the perspective view of the composite burner of the present invention;
Fig. 2 is the perspective view of the bracing frame of the composite burner in Fig. 1;
Fig. 3 is the perspective view of the homogenizing plate in Fig. 1;
Fig. 4 is the perspective view of the honeycomb type current-sharing block in Fig. 3;
Fig. 5 is the perspective view of the infrared stove head that the burner in Fig. 1, the i.e. present invention preferentially use;
Fig. 6 is the perspective view of the floated burner in Fig. 1;
Fig. 7 is the perspective view of the first fuel injection pipe in Fig. 1;
Wherein:
1, bracing frame;11, annular groove;12, the first fuel enters pipe;
13, the first induction tunnel support;
2, homogenizing plate;21, equal discharge orifice;22, honeycomb type current-sharing block;23, the second fuel enters pipe;
24, the second induction tunnel support;
3, the first fuel injection pipe;31, perforation;
4, burner;41, fuel inlet;
5, floated burner;51, floated burner fuel inlet;
6, the second fuel injection pipe.
Detailed description of the invention
Below in conjunction with the accompanying drawings the preferred embodiments of the present invention are described in detail, so that advantages and features of the invention can be easier to be readily appreciated by one skilled in the art, thus protection scope of the present invention are made apparent clear and definite defining.
The advantage of the composite burner of the present invention is: with two fuel injection pipes of horizontally disposed and vertical layout, the fuel and the air that simultaneously enter burner are more, and heating power is relatively big, and range is wide.
As shown in Figure 1, Figure 2, Figure 5, a kind of composite burner, including bracing frame 1, homogenizing plate 2 and an one first fuel injection pipe 3, this composite burner also include burner 4 and an one second fuel injection pipe 6, it is provided with annular groove 11,1 first fuel on this bracing frame 1 and enters pipe 12 and one first induction tunnel support 13, the size of this homogenizing plate 2 adapts with the size of this annular groove 11, and this first fuel injection pipe 3 is connected with this first induction tunnel support 13.
As shown in Fig. 1, Fig. 3, Fig. 4, it is evenly arranged equal discharge orifice 21,1 second fuel on this homogenizing plate 2 and enters pipe 23 and one second induction tunnel support 24, being placed with a honeycomb type current-sharing block 22 in this equal discharge orifice 21, this second fuel injection pipe 6 is connected with this second induction tunnel support 24.
As shown in Figure 5, Figure 6, this burner 4 uses infrared stove head, and the bottom of this burner is provided with a fuel inlet 41, and this fuel inlet 41 enters pipe 23 with this second fuel and is connected.
As it is shown in fig. 7, be provided with perforation 31 on the sidewall of the end of this first fuel injection pipe 3.
The mentality of designing of the present invention is below described the most in one embodiment, and in the case of system allows, the present invention can expand to the most external more functional module, thus extends its function to greatest extent.
The above, the only detailed description of the invention of the present invention, but protection scope of the present invention is not limited thereto, any change expected without creative work or replacement, all should contain within protection scope of the present invention.Therefore, protection scope of the present invention should be as the criterion with the protection domain that claims are limited.

Claims (3)

1. a composite burner, draws including a bracing frame (1), a homogenizing plate (2) and one first fuel Penetrate pipe (3), it is characterised in that: described composite burner also include a burner (4) and one second combustion Material induction tunnel (6), described bracing frame (1) is provided with an annular groove (11), one first fuel entrance Pipe (12) and one first induction tunnel support (13), the size of described homogenizing plate (2) is recessed with described annular The size of groove (11) adapts, the first described fuel injection pipe (3) and the first described induction tunnel support (13) it is connected, described homogenizing plate (2) has been evenly arranged equal discharge orifice (21), one second fuel entrance Pipe (23) and one second induction tunnel support (24), be placed with a honeycomb type in described equal discharge orifice (21) equal Stream block (22), the second described fuel injection pipe (6) is connected with the second described induction tunnel support (24), The bottom of described burner (4) is provided with a fuel inlet (41), and described fuel inlet (41) is with described Second fuel enter pipe (23) be connected.
Composite burner the most according to claim 1, it is characterised in that: the first described fuel draws Perforation (31) it is provided with on the sidewall of the end penetrating pipe (3).
Composite burner the most according to claim 2, it is characterised in that: described burner (4) Kind includes infrared-type burner and floated burner.
CN201310067386.3A 2013-03-04 2013-03-04 Composite burner Expired - Fee Related CN104033903B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310067386.3A CN104033903B (en) 2013-03-04 2013-03-04 Composite burner

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310067386.3A CN104033903B (en) 2013-03-04 2013-03-04 Composite burner

Publications (2)

Publication Number Publication Date
CN104033903A CN104033903A (en) 2014-09-10
CN104033903B true CN104033903B (en) 2016-12-28

Family

ID=51464791

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310067386.3A Expired - Fee Related CN104033903B (en) 2013-03-04 2013-03-04 Composite burner

Country Status (1)

Country Link
CN (1) CN104033903B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106859311A (en) * 2017-04-19 2017-06-20 包寅戈 Face bucket is boiled with induction tunnel

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1339672A (en) * 2000-08-22 2002-03-13 湖南迅达集团有限公司 Embedded clean-keeping burner for kitchen range
CN2549325Y (en) * 2002-06-14 2003-05-07 尹华金 Vortex gas saving strong combustor
CN101846339A (en) * 2009-03-23 2010-09-29 王利虹 Method for serially connecting valves and improving burner into gas cooker capably of controlling temperature and intensifying fire to form vigorous fire
CN201652343U (en) * 2010-01-22 2010-11-24 孙贤得 Energy-saving burner
CN201866771U (en) * 2010-11-16 2011-06-15 陈兴贵 Infrared furnace end for multifunctional medium-pressure furnace
CN203240583U (en) * 2013-03-04 2013-10-16 姜堰市灶宝灶具有限公司 Composite burner

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1339672A (en) * 2000-08-22 2002-03-13 湖南迅达集团有限公司 Embedded clean-keeping burner for kitchen range
CN2549325Y (en) * 2002-06-14 2003-05-07 尹华金 Vortex gas saving strong combustor
CN101846339A (en) * 2009-03-23 2010-09-29 王利虹 Method for serially connecting valves and improving burner into gas cooker capably of controlling temperature and intensifying fire to form vigorous fire
CN201652343U (en) * 2010-01-22 2010-11-24 孙贤得 Energy-saving burner
CN201866771U (en) * 2010-11-16 2011-06-15 陈兴贵 Infrared furnace end for multifunctional medium-pressure furnace
CN203240583U (en) * 2013-03-04 2013-10-16 姜堰市灶宝灶具有限公司 Composite burner

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Address after: 225300 room three, building 308, Kowloon shopping mall, Hailing District, Jiangsu, Taizhou

Applicant after: TAIZHOU ZAOBAO KITCHEN RANGE CO.,LTD.

Address before: 225500 M6-108 room, Huadong Hardware City, Jiangyan Economic Development Zone, Taizhou, Jiangsu

Applicant before: TAIZHOU ZAOBAO KITCHEN RANGE CO.,LTD.

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GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20161228

CF01 Termination of patent right due to non-payment of annual fee