CN203980624U - Living beings forward type gas-fired turbofurnace unit - Google Patents

Living beings forward type gas-fired turbofurnace unit Download PDF

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Publication number
CN203980624U
CN203980624U CN201420463083.3U CN201420463083U CN203980624U CN 203980624 U CN203980624 U CN 203980624U CN 201420463083 U CN201420463083 U CN 201420463083U CN 203980624 U CN203980624 U CN 203980624U
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CN
China
Prior art keywords
combustion chamber
heater
fired
turbofurnace
type gas
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
CN201420463083.3U
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Chinese (zh)
Inventor
刘春峰
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Gloomy Tyke Harbin Renewable Sources Of Energy Technological Development Co Ltd
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Gloomy Tyke Harbin Renewable Sources Of Energy Technological Development Co Ltd
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Priority to CN201420463083.3U priority Critical patent/CN203980624U/en
Application granted granted Critical
Publication of CN203980624U publication Critical patent/CN203980624U/en
Anticipated expiration legal-status Critical
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Abstract

Living beings forward type gas-fired turbofurnace unit, relates to combustion apparatus field.The utility model is in order to solve the problem that existing boiler combustion is insufficient, the thermal efficiency is low.Scheme: body of heater surrounding is water wall, body of heater top is provided with chimney, bottom of furnace body is provided with fire grate, fire grate below is provided with ash bin, ash bin is provided with ash hole, furnace body inside top is provided with water pipe, living beings forward type gas-fired turbofurnace unit also comprises radiation heat pipe, radiation heat pipe is divided into first-stage firing chamber and secondary combustion chamber from the bottom to top body of heater, on the bottom of radiation heat pipe and the inwall of first-stage firing chamber, be equipped with fire-resistant soil layer, front side at body of heater is provided with gasification combustion chamber, gasification combustion chamber is communicated with first-stage firing chamber by the outlet flue on first-stage firing chamber sidewall, gasification combustion chamber is communicated with secondary combustion chamber with the smoke inlet by secondary combustion chamber's sidewall.The utility model sufficient combustion, the thermal efficiency is high.

Description

Living beings forward type gas-fired turbofurnace unit
Technical field
The utility model relates to a kind of cyclone furnace, specifically relates to a kind of living beings forward type gas-fired turbofurnace unit, belongs to combustion apparatus field.
Background technology
Existing boiler furnace is simple in structure, generally adopts a rectangle combustion chamber, in combustion process because oxygen can not fully mix with fuel, cause burning insufficient, the thermal efficiency is lower, generally also only can use the traditional fuels such as coal simultaneously.Therefore, urgently relate to a kind of sufficient combustion, living beings forward type gas-fired turbofurnace unit that the thermal efficiency is high.
Utility model content
The utility model is to solve that existing boiler combustion is insufficient, problem that the thermal efficiency is low, and then a kind of sufficient combustion, living beings forward type gas-fired turbofurnace unit that the thermal efficiency is high are provided.
The utility model for solving the problems of the technologies described above taked technical scheme is:
Living beings forward type gas-fired turbofurnace unit of the present utility model comprises body of heater, body of heater surrounding is water wall, body of heater top is provided with chimney, bottom of furnace body is provided with fire grate, fire grate below is provided with ash bin, ash bin is provided with ash hole, furnace body inside top is provided with water pipe, living beings forward type gas-fired turbofurnace unit also comprises radiation heat pipe, radiation heat pipe is divided into first-stage firing chamber and secondary combustion chamber from the bottom to top body of heater, on the bottom of radiation heat pipe and the inwall of first-stage firing chamber, be equipped with fire-resistant soil layer, front side at body of heater is provided with gasification combustion chamber, gasification combustion chamber is communicated with first-stage firing chamber by the outlet flue on first-stage firing chamber sidewall, gasification combustion chamber is communicated with secondary combustion chamber with the smoke inlet by secondary combustion chamber's sidewall.
In such scheme, radiation heat pipe is divided into first-stage firing chamber and secondary combustion chamber from the bottom to top body of heater, on the bottom of radiation heat pipe and the inwall of first-stage firing chamber, be equipped with fire-resistant soil layer, front side at body of heater is provided with gasification combustion chamber, gasification combustion chamber is communicated with first-stage firing chamber by the outlet flue on first-stage firing chamber sidewall, and gasification combustion chamber is communicated with secondary combustion chamber with the smoke inlet by secondary combustion chamber's sidewall.This structure can be utilized fuel half fired state produces in first-stage firing chamber carbon monoxide and flue gas, heating seat clay, and radiant heat, to radiation heat pipe, completes once and heats; Carbon monoxide and the flue gas of first-stage firing chamber arrive gasification combustion chamber by outlet flue, burn in gasification combustion chamber, and enter secondary combustion chamber by smoke inlet and fully burn along speed, thereby reach the comprehensive heating pipe of flame and focus and Shui Bi, reach best hot water effect, solved on the whole the insufficient and low problem of the thermal efficiency of burning.
Scheme is further designed: in order to make fire-resistant soil layer, heat conduction is to radiation heat pipe better, and fire-resistant the thickness of the layer is 250mm.
Scheme is further designed: in order to ensure the gentle fully burning of adding of fuel, the volume of first-stage firing chamber is 2/5 of body of heater volume.
Scheme is further designed: in order to ensure that carbon monoxide and flue gas enter gasification combustion chamber from first-stage firing chamber, then enter secondary combustion chamber by gasification combustion chamber and be fully burned, the wall that gasification combustion chamber is connected with body of heater tilts.
Scheme is further designed: the wall that gasification combustion chamber is connected with body of heater and horizontal direction are 30 degree angles.
The utility model sufficient combustion, the thermal efficiency are high, can be used as combustion apparatus and promote.
Brief description of the drawings
Fig. 1 is living beings forward type gas-fired turbofurnace unit structure chart;
1-first-stage firing chamber in figure, 2-secondary combustion chamber, 3-gasification combustion chamber, 4-outlet flue, 5-smoke inlet, 6-radiation heat pipe, the fire-resistant soil layer of 7-, 8-fire grate, 9-ash bin, 10-ash hole, 11-water pipe, 12-water wall, 13-chimney.
Detailed description of the invention
Detailed description of the invention: describe in conjunction with Fig. 1, the living beings forward type gas-fired turbofurnace unit of present embodiment comprises body of heater, body of heater surrounding is water wall, body of heater top is provided with chimney, bottom of furnace body is provided with fire grate, fire grate below is provided with ash bin, ash bin is provided with ash hole, furnace body inside top is provided with water pipe, living beings forward type gas-fired turbofurnace unit also comprises radiation heat pipe, radiation heat pipe is divided into first-stage firing chamber and secondary combustion chamber from the bottom to top body of heater, on the bottom of radiation heat pipe and the inwall of first-stage firing chamber, be equipped with fire-resistant soil layer, front side at body of heater is provided with gasification combustion chamber, gasification combustion chamber is communicated with first-stage firing chamber by the outlet flue on first-stage firing chamber sidewall, gasification combustion chamber is communicated with secondary combustion chamber with the smoke inlet by secondary combustion chamber's sidewall.。Fuel carbon monoxide and flue gas that in first-stage firing chamber 1, half fired state produces, the seat clay 7 contacting with radiation heat pipe 6 by heating, radiant heat, to radiation heat pipe 6, completes once and heats; The carbon monoxide of first-stage firing chamber 1 and flue gas arrive gasification combustion chamber 3 by outlet flue 4, burn in gasification combustion chamber 3, and enter secondary combustion chamber 2 by smoke inlet 5 rapidly and fully burn, thereby reach flame and the comprehensive heating pipe of focus and Shui Bi, reach best hot water effect.
Present embodiment is the exemplary illustration to this patent just, does not limit its protection domain, and those skilled in the art can also change its part, as long as no the Spirit Essence that exceeds this patent, all in the protection domain of this patent.

Claims (5)

1. living beings forward type gas-fired turbofurnace unit, comprise body of heater, body of heater surrounding is water wall (12), body of heater top is provided with chimney (13), bottom of furnace body is provided with fire grate (8), fire grate (8) below is provided with ash bin (9), ash bin (9) is provided with ash hole (10), furnace body inside top is provided with water pipe (11), it is characterized in that: living beings forward type gas-fired turbofurnace unit also comprises radiation heat pipe (6), radiation heat pipe (6) is divided into first-stage firing chamber (1) and secondary combustion chamber (2) from the bottom to top body of heater, on the inwall of the bottom of radiation heat pipe (6) and first-stage firing chamber (1), be equipped with fire-resistant soil layer (7), be provided with gasification combustion chamber (3) in the front side of body of heater, gasification combustion chamber (3) is communicated with first-stage firing chamber (1) by the outlet flue (4) on first-stage firing chamber (1) sidewall, gasification combustion chamber (3) is communicated with secondary combustion chamber (2) with the smoke inlet (5) by secondary combustion chamber (2) sidewall.
2. living beings forward type gas-fired turbofurnace unit according to claim 1, is characterized in that: the thickness of fire-resistant soil layer (7) is 250mm.
3. living beings forward type gas-fired turbofurnace unit according to claim 1, is characterized in that: the volume of first-stage firing chamber (1) is 2/5 of body of heater volume.
4. according to the living beings forward type gas-fired turbofurnace unit described in claim 1,2 or 3, it is characterized in that: the wall that gasification combustion chamber (3) is connected with body of heater tilts.
5. living beings forward type gas-fired turbofurnace unit according to claim 4, is characterized in that: the wall that gasification combustion chamber (3) is connected with body of heater and horizontal direction are 30 degree angles.
CN201420463083.3U 2014-08-15 2014-08-15 Living beings forward type gas-fired turbofurnace unit Expired - Fee Related CN203980624U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420463083.3U CN203980624U (en) 2014-08-15 2014-08-15 Living beings forward type gas-fired turbofurnace unit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420463083.3U CN203980624U (en) 2014-08-15 2014-08-15 Living beings forward type gas-fired turbofurnace unit

Publications (1)

Publication Number Publication Date
CN203980624U true CN203980624U (en) 2014-12-03

Family

ID=51978055

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420463083.3U Expired - Fee Related CN203980624U (en) 2014-08-15 2014-08-15 Living beings forward type gas-fired turbofurnace unit

Country Status (1)

Country Link
CN (1) CN203980624U (en)

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

Granted publication date: 20141203

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