CN210801187U - Turbine furnace shell - Google Patents
Turbine furnace shell Download PDFInfo
- Publication number
- CN210801187U CN210801187U CN201921401392.7U CN201921401392U CN210801187U CN 210801187 U CN210801187 U CN 210801187U CN 201921401392 U CN201921401392 U CN 201921401392U CN 210801187 U CN210801187 U CN 210801187U
- Authority
- CN
- China
- Prior art keywords
- turbine
- furnace end
- gas
- air
- injection pipe
- 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
Links
Images
Abstract
The utility model belongs to the technical field of gas-cooker spare part, especially, relate to a turbine stove outer covering, draw the pipe including furnace end and the turbine shape of setting in furnace end one side, the turbine shape draws the import of penetrating the pipe for the air intake that is used for advancing the air, and the turbine shape draws the outside lateral wall of penetrating the pipe to offer the air inlet that is used for advancing the gas, and the turbine shape draws the inside turbine that is equipped with to be used for mixing air and gas to mix the chamber, and the turbine shape draws penetrating pipe and furnace end junction to have seted up the wind gas export, and the turbine mixes the chamber and is linked together through wind gas export and furnace end inside. The utility model discloses make air and gas draw by the air intake and the air inlet of turbine shape injection pipe respectively to mix the intracavity at the turbine and carry out intensive mixing, send into the furnace end through the wind gas export at last and inside burning, can make the gas combustion more abundant, effectively improve combustion efficiency, reduce the wasting of resources and air pollution because of incomplete burning causes.
Description
Technical Field
The utility model belongs to the technical field of gas-cooker spare part, especially, relate to a turbine furnace shell.
Background
Gas cookers have become a widely used kitchen utensil and require air to be consumed during combustion. The air mixed with the gas in the burner in advance is called primary air, and for the gas stove adopting an injection structure, the gas is injected from the nozzle, and the air sucked at the injection pipe is the primary air. When the fuel gas is burnt, the air reabsorbed by the flame is secondary air. The intake of primary air and the mixing degree of the primary air and the fuel gas are related to whether the fuel gas is fully combusted, and the heat efficiency of the gas stove is directly influenced.
In the existing gas stove on the market, primary air and fuel gas are sucked by negative pressure generated by an injection structure and are directly sent to a stove head, the process is relatively quick, the primary air cannot be fully mixed with the fuel gas, the combustion is easy to be insufficient, and the heat efficiency of the gas stove is influenced.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the shortcomings of the prior art, and provides a turbine furnace shell which can better mix air and gas and improve the combustion efficiency.
The utility model aims at solving the problems by the following technical scheme:
a turbine furnace shell is characterized in that: the novel gas burner comprises a burner body and a turbine-shaped injection pipe arranged on one side of the burner body, wherein the inlet of the turbine-shaped injection pipe is an air inlet for air inlet, the outer side wall of the turbine-shaped injection pipe is provided with an air inlet for gas inlet, the turbine-shaped injection pipe is internally provided with a turbine mixing cavity for mixing air and gas, the turbine-shaped injection pipe and the burner body are connected at the joint of the turbine-shaped injection pipe and the burner body, and the turbine mixing cavity is communicated with the inside of the burner body through the air outlet.
Based on above-mentioned structure, air and gas are inhaled by air intake and the air inlet of turbine shape injection pipe respectively to mix the intracavity at the turbine and carry out intensive mixing, send into the furnace end through the wind gas export at last and inside burning, can make the gas combustion more abundant, effectively improve combustion efficiency.
Preferably, the furnace end of the utility model is a barrel-shaped structure with an opening at the top.
Furthermore, the outer side wall of the top of the furnace end of the utility model is provided with a horizontally arranged disc-shaped support lug, the support lug is provided with a plurality of fixed hole sites, and the central axis of the disc-shaped support lug is coincided with the central axis of the furnace end; the horizontal plane of the support lug is lower than the top of the furnace end and higher than the turbine-shaped injection pipe.
Furthermore, ignition pinhole, response pinhole, little fire tube hole and offal tube hole have been seted up to the furnace end bottom surface.
Preferably, the ignition needle hole, the induction needle hole and the small fire tube hole are uniformly distributed at the center of the bottom surface of the furnace end along a circumference.
Preferably, the sewer hole of the utility model is positioned on one side of the bottom surface of the furnace end.
Preferably, ignition pinhole, response pinhole, little fire tube hole are circular through-hole.
Preferably, the outlet hole of the utility model is a circular through hole.
Compared with the prior art the utility model has the following characteristics and beneficial effect:
air and gas are respectively inhaled by air intake and the air inlet of turbine shape injection pipe to mix the intracavity at the turbine and carry out intensive mixing, send into the furnace end through the wind gas export at last inside burning, can make the gas combustion more abundant, effectively improve combustion efficiency, reduce the wasting of resources and air pollution because of incomplete burning causes.
Drawings
Fig. 1 is a schematic view of a three-dimensional structure of the present invention.
Fig. 2 is a schematic view of a three-dimensional structure of the present invention.
Fig. 3 is a schematic view of the top view structure of the present invention.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
As shown in the figures 1 and 2, the turbine furnace shell comprises a furnace end 1 and a turbine-shaped injection pipe 2 arranged on one side of the furnace end 1, wherein an air inlet 3 for air inlet is formed in an inlet of the turbine-shaped injection pipe 2, an air inlet 4 for gas inlet is formed in the outer side wall of the turbine-shaped injection pipe 2, a turbine mixing cavity 5 for mixing air and gas is formed in the turbine-shaped injection pipe 2, an air outlet 6 is formed in the joint of the turbine-shaped injection pipe 2 and the furnace end 1, and the turbine mixing cavity 5 is communicated with the interior of the furnace end 1 through the air outlet 6.
Based on above-mentioned structure, in the course of the work, air and gas are inhaled by air intake 3 and air inlet 4 of turbine shape injection pipe 2 respectively to carry out intensive mixing in turbine mixes the chamber 5, send into furnace end 1 inside through wind gas outlet 6 at last and burn, can make the gas burning more abundant, effectively improve combustion efficiency.
Preferably, the furnace end 1 is a barrel-shaped structure with an opening at the top.
Further, a disc-shaped support lug 7 which is horizontally arranged is arranged on the outer side wall of the top of the furnace end 1, a plurality of fixing hole positions 8 are arranged on the support lug 7, and the central axis of the disc-shaped support lug 7 is coincided with the central axis of the furnace end 1; the horizontal plane of the support lug 7 is lower than the top of the furnace end 1 and higher than the turbine-shaped injection pipe 2.
Further, as shown in fig. 2 and 3, an ignition pinhole 9, an induction pinhole 10, a small fire tube hole 11 and a lower water tube hole 12 are formed on the bottom surface of the burner 1. The ignition needle hole 9, the induction needle hole 10 and the small fire tube hole 11 are positioned in the center of the bottom surface of the furnace end 1 and are uniformly distributed along a circumference. The water outlet pipe hole 12 is positioned at one side of the bottom surface of the furnace end 1. The ignition pinhole 9, the induction pinhole 10 and the small fire tube hole 11 are circular through holes. The drain pipe hole 12 is a circular through hole.
The utility model discloses a turbine shape is drawn and is penetrated pipe 2 and can mix air and gas better, makes the gas combustion abundant, improves combustion efficiency, reduces wasting of resources and air pollution because of incomplete combustion causes.
The specific embodiments described herein are merely illustrative of the spirit of the invention. Various modifications, additions and substitutions for the specific embodiments described herein may be made by those skilled in the art without departing from the spirit of the invention or exceeding the scope of the invention as defined in the accompanying claims.
Claims (8)
1. A turbine furnace shell is characterized in that: the novel gas burner comprises a burner body and a turbine-shaped injection pipe arranged on one side of the burner body, wherein the inlet of the turbine-shaped injection pipe is an air inlet for air inlet, the outer side wall of the turbine-shaped injection pipe is provided with an air inlet for gas inlet, the turbine-shaped injection pipe is internally provided with a turbine mixing cavity for mixing air and gas, the turbine-shaped injection pipe and the burner body are connected at the joint of the turbine-shaped injection pipe and the burner body, and the turbine mixing cavity is communicated with the inside of the burner body through the air outlet.
2. The turbine shell according to claim 1, wherein: the furnace end is of a barrel-shaped structure with an opening at the top.
3. The turbine shell according to claim 2, wherein: the outer side wall of the top of the furnace end is provided with a horizontally arranged disc-shaped support lug, the support lug is provided with a plurality of fixing hole positions, and the central axis of the disc-shaped support lug is coincided with the central axis of the furnace end; the horizontal plane of the support lug is lower than the top of the furnace end and higher than the turbine-shaped injection pipe.
4. The turbine shell according to claim 1 or 2 or 3, wherein: the bottom surface of the furnace end is provided with an ignition pinhole, an induction pinhole, a small fire tube hole and a drainage tube hole.
5. The turbine shell according to claim 4, wherein: the ignition needle hole, the induction needle hole and the small fire tube hole are arranged in the center of the bottom surface of the furnace end and are uniformly distributed along a circumference.
6. The turbine shell according to claim 5, wherein: the water outlet pipe hole is positioned on one side of the bottom surface of the furnace end.
7. The turbine shell according to claim 5, wherein: the ignition pinhole, the induction pinhole and the small fire tube hole are circular through holes.
8. The turbine shell according to claim 6, wherein: the water outlet pipe hole is a circular through hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921401392.7U CN210801187U (en) | 2019-08-27 | 2019-08-27 | Turbine furnace shell |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921401392.7U CN210801187U (en) | 2019-08-27 | 2019-08-27 | Turbine furnace shell |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210801187U true CN210801187U (en) | 2020-06-19 |
Family
ID=71241984
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921401392.7U Active CN210801187U (en) | 2019-08-27 | 2019-08-27 | Turbine furnace shell |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210801187U (en) |
-
2019
- 2019-08-27 CN CN201921401392.7U patent/CN210801187U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN202733890U (en) | Stove burner using blast type to supplement secondary air | |
| CN206958922U (en) | Three-ring distributor and three-ring combustor using same | |
| CN103453549B (en) | A kind of Draught gas burner binary channels mixing injector | |
| CN201180997Y (en) | Multi-point ejection stereo air intake combustor | |
| CN108644772A (en) | A kind of upper inlet wind type burner | |
| CN210801187U (en) | Turbine furnace shell | |
| CN212537832U (en) | Gas distribution blast structure and gas-cooker | |
| CN108592090A (en) | A kind of sthenic fire range | |
| CN211232869U (en) | Furnace end capable of improving combustion effect | |
| CN204880259U (en) | Liquid fuel special furnace end that burns | |
| CN107062213A (en) | The electric preheating of premix combustion voluntarily gasification liquid fuel burner | |
| CN207990686U (en) | A kind of full top intaking air gas combustion stove of oxygen-enriched combusting | |
| CN208332336U (en) | A kind of sthenic fire range | |
| CN111140889A (en) | Turbine furnace shell | |
| CN217464426U (en) | Stable combustion furnace end | |
| CN215175013U (en) | Three-ring fire burner | |
| CN213513876U (en) | Mixing furnace for combustion machine | |
| CN111425896B (en) | Household gas stove pot rack based on TVC standing vortex structure | |
| CN213146557U (en) | Energy-saving stove | |
| CN218064870U (en) | Multi-port air inlet type stove burner | |
| CN221237864U (en) | Energy-saving burner | |
| CN210462993U (en) | Superposition mixed air turbulent effect combustor | |
| CN212204513U (en) | Multi-injection single-cavity combustor and stove | |
| CN215675179U (en) | Double-channel central gas channel structure and burner thereof | |
| CN214949220U (en) | Lower air inlet direct-injection strong fire stove |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Turbine shell Effective date of registration: 20201123 Granted publication date: 20200619 Pledgee: Taizhou Linhai sub branch of Zhejiang Mintai Commercial Bank Co., Ltd Pledgor: BOLI STOVE TECHNOLOGY Co.,Ltd. Registration number: Y2020330001002 |