CN110345498A - A kind of cavity jet pipe of combustion-type POU equipment - Google Patents
A kind of cavity jet pipe of combustion-type POU equipment Download PDFInfo
- Publication number
- CN110345498A CN110345498A CN201910709518.5A CN201910709518A CN110345498A CN 110345498 A CN110345498 A CN 110345498A CN 201910709518 A CN201910709518 A CN 201910709518A CN 110345498 A CN110345498 A CN 110345498A
- Authority
- CN
- China
- Prior art keywords
- jet pipe
- section
- outer layer
- aditus laryngis
- cavity
- 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.)
- Pending
Links
- 239000011261 inert gas Substances 0.000 claims abstract description 49
- 239000007921 spray Substances 0.000 claims abstract description 34
- 239000002912 waste gas Substances 0.000 claims abstract description 17
- 239000007789 gas Substances 0.000 claims description 67
- 238000002485 combustion reaction Methods 0.000 abstract description 4
- 239000000428 dust Substances 0.000 abstract description 3
- 238000006243 chemical reaction Methods 0.000 description 7
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000002347 injection Methods 0.000 description 3
- 239000007924 injection Substances 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 230000000903 blocking effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 239000000377 silicon dioxide Substances 0.000 description 2
- 150000001336 alkenes Chemical class 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 229910052743 krypton Inorganic materials 0.000 description 1
- DNNSSWSSYDEUBZ-UHFFFAOYSA-N krypton atom Chemical compound [Kr] DNNSSWSSYDEUBZ-UHFFFAOYSA-N 0.000 description 1
- 210000000867 larynx Anatomy 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 229910052754 neon Inorganic materials 0.000 description 1
- GKAOGPIIYCISHV-UHFFFAOYSA-N neon atom Chemical compound [Ne] GKAOGPIIYCISHV-UHFFFAOYSA-N 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000007747 plating Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 238000000197 pyrolysis Methods 0.000 description 1
- 238000012797 qualification Methods 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910052724 xenon Inorganic materials 0.000 description 1
- FHNFHKCVQCLJFQ-UHFFFAOYSA-N xenon atom Chemical compound [Xe] FHNFHKCVQCLJFQ-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
- F23G5/00—Incineration of waste; Incinerator constructions; Details, accessories or control therefor
- F23G5/44—Details; Accessories
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
- F23G7/00—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals
- F23G7/06—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases
Abstract
The present invention relates to technical field of waste gas treatment, more particularly to a kind of cavity jet pipe of combustion-type POU equipment.The cavity jet pipe includes at least core jet pipe, outer layer jet pipe, inert gas spray head, the outlet of the core jet pipe is located at the inside of the outer layer jet pipe and towards the outlet of outer layer jet pipe, and the notch setting of inert gas spray head is on the tube wall of the outer layer jet pipe and towards inside outer layer jet pipe.Cavity jet pipe of the invention is for solving the problems, such as the spout of exhaust piping in the prior art and combustion chamber wall surface dust incrustation.
Description
Technical field
The present invention relates to technical field of waste gas treatment, more particularly to a kind of cavity jet pipe of combustion-type POU equipment.
Background technique
The exhaust gas of strong corrosive would generally be generated in semiconductor technology, these exhaust gas all have human body or environment certain
Harmfulness, it is therefore desirable to can be just discharged into atmosphere after being handled exhaust gas.Often pass through combustion-type POU equipment at present for exhaust gas
It is discharged after oxidation and pyrolysis, but the dust incrustation of the spout of exhaust piping and combustion chamber wall surface always is modern POU equipment
Key problem, this leads to the frequent maintenance of equipment.
To solve the above-mentioned problems, the present invention provides a kind of cavity jet pipe of combustion-type POU equipment.
Summary of the invention
In view of the foregoing deficiencies of prior art, the purpose of the present invention is to provide a kind of chambers of combustion-type POU equipment
Body jet pipe, for solving the problems, such as the spout of exhaust piping in the prior art and combustion chamber wall surface dust incrustation.
In order to achieve the above objects and other related objects, the present invention provides a kind of cavity jet pipe of combustion-type POU equipment, institute
Cavity jet pipe is stated including at least core jet pipe, outer layer jet pipe, inert gas spray head, the outlet of the core jet pipe is located at described outer
Layer jet pipe inside and towards the outlet of outer layer jet pipe, the notch setting of inert gas spray head is on the tube wall of the outer layer jet pipe
And towards inside outer layer jet pipe.
The core jet pipe includes connected the first flared section and the first slot section, first flared section and the first slot
Section is connected by the first aditus laryngis.The outer layer jet pipe includes connected the second flared section and the second slot section, second flaring
Section is connect with the second slot section by the second aditus laryngis.
First flared section is provided with exhaust gas inlet, and the second slot section is provided with waste gas outlet.
First flared section is gradually reduced by exhaust gas inlet to the first aditus laryngis internal diameter, and second flared section is by starting point
It is gradually reduced to the second aditus laryngis internal diameter.
The first slot section is remained unchanged by the first aditus laryngis to outlet end internal diameter.
The first slot section can also be gradually increased by the first aditus laryngis to outlet end internal diameter.
The first aditus laryngis section is at the bore minimum of the core jet pipe, and the second aditus laryngis section is center spray
At the bore minimum of pipe.
The core jet pipe is for conveying exhaust gas.It is accelerated in the first slot section exhaust gas.
The second slot section is remained unchanged by the second aditus laryngis to waste gas outlet end internal diameter.
The second slot section can also be gradually increased by the second aditus laryngis to waste gas outlet end internal diameter.
The first slot section is located at the inside of the outer layer jet pipe and towards the waste gas outlet of outer layer jet pipe.
Preferably, the first flared section exhaust gas inlet end extends to outside the second flared section of the outer layer jet pipe, institute
The first slot section outlet end is stated to extend at second flared section 2/5ths.
First flared section and second flared section are to be tightly connected.
The outer layer jet pipe is for conveying exhaust gas and inert gas, exhaust gas and the inert gas quilt in the second slot section
Accelerate.
The notch setting of the inert gas spray head is on the tube wall of the outer layer jet pipe.
Preferably, the inert gas spray head is located on the second flared section tube wall.
As described above, a kind of cavity jet pipe of combustion-type POU equipment of the invention, has the advantages that
By using inert gas as protection gas medium, inert gas is protected in outer layer jet pipe and when leaving outer layer jet pipe
Shield gas still exist in outer layer, exhaust gas can make exhaust gas deferred reaction in internal layer, make waste gas reaction far from spout position into
Row, there is incrustation or blocking spray head in spout tube wall in a large amount of particulate matters such as silica for preventing waste gas reaction from being formed, to change
The case where being apt to intracavitary incrustation reduces maintenance and repair rate.
Detailed description of the invention
Fig. 1 is shown as cavity nozzle structure figure.
Fig. 2 is shown as core jet pipe outlet end gas pressure intensity figure.
Fig. 3 is shown as outer layer jet pipe waste gas outlet end gas pressure intensity figure.
Fig. 4 cavity sprays tube fluid and accelerates figure.
Fig. 5 is shown as core jet pipe exhaust gas flow velocity figure.
Fig. 6 is shown as outer layer jet pipe inert gas cover figure.
Component label instructions
1 exhaust gas inlet
2 core jet pipes
21 first flared sections
22 first slot sections
23 first aditus laryngis
3 outer layer jet pipes
31 second flared sections
32 second slot sections
33 second aditus laryngis
4 inert gas spray heads
5 waste gas outlets
Specific embodiment
Embodiments of the present invention are illustrated by particular specific embodiment below, those skilled in the art can be by this explanation
Content disclosed by book is understood other advantages and efficacy of the present invention easily.
Fig. 1 is please referred to Fig. 6.It should be clear that this specification structure depicted in this specification institute accompanying drawings, ratio, size etc., only to
Cooperate the revealed content of specification, so that those skilled in the art understands and reads, being not intended to limit the invention can be real
The qualifications applied, therefore do not have technical essential meaning, the tune of the modification of any structure, the change of proportionate relationship or size
It is whole, in the case where not influencing the effect of present invention can be generated and the purpose that can reach, it should all still fall in disclosed skill
In the range of art content can cover.Meanwhile in this specification it is cited as "upper", "lower", "left", "right", " centre " and
The term of " one " etc. is merely convenient to being illustrated for narration, rather than to limit the scope of the invention, relativeness
It is altered or modified, under the content of no substantial changes in technology, when being also considered as the enforceable scope of the present invention.
As shown in Figure 1, the present invention provides a kind of cavity jet pipe of combustion-type POU equipment, the cavity jet pipe is included at least
Core jet pipe 2, outer layer jet pipe 3, inert gas spray head 4, the spout of the core jet pipe 2 are located at the inside of the outer layer jet pipe 3
And towards the outlet of outer layer jet pipe 3, the notch setting of inert gas spray head 4 is on the tube wall of the outer layer jet pipe 3 and towards outer
Inside layer jet pipe.
The core jet pipe 2 and outer layer jet pipe 3 are for continuously accelerating fluids within pipes.
The core jet pipe 2 includes connected the first flared section 21 and the first slot section 22, first flared section 21 and
First slot section 22 is connected by the first aditus laryngis 23.In the application, the flared section and slot section are relative concept, are referred to opposite
It is bigger with respect to the opening area of slot section in the opening area of same nozzle body, flared section.
First flared section 21 is provided with exhaust gas inlet 1.
First flared section 21 is gradually reduced by 1 to the first aditus laryngis of exhaust gas inlet, 23 internal diameter.
The first slot section 22 should at least be remained unchanged by the first aditus laryngis 23 to outlet end internal diameter.Preferably, described
One slot section 22 is gradually increased by the first aditus laryngis 23 to outlet end internal diameter.
First flared section, the 21 exhaust gas inlet end internal diameter is less than 31 starting point internal diameter of the second flared section.
Exhaust gas inlet end cross-sectional shape includes but is not limited to circle, and rectangle is trapezoidal, triangle.
In a preferred embodiment, exhaust gas inlet end cross section is circle.
Internal diameter of first slot section, the 22 outlet end internal diameter less than 21 exhaust gas inlet end of the first flared section.
First slot section, the 22 outlet end cross-sectional shape includes but is not limited to circle, and rectangle is trapezoidal, triangle.
In a preferred embodiment, the outlet end cross section is circle.
First aditus laryngis 23 is the pipeline section for connecting the first flared section 21 and the first slot section 22, and first aditus laryngis is institute
It states at the bore minimum of core jet pipe.
First aditus laryngis, 23 length is less than the first flared section 21 or the length of the first slot section 22.
First flared section 21 and 22 length of the first slot section can be equal, can also be unequal.
As shown in figure 5, the core jet pipe 2 is for conveying exhaust gas.It is accelerated in 22 exhaust gas of the first slot section, preferably
, exhaust gas is accelerated as supersonic speed.
As shown in Figure 1, the outer layer jet pipe 3 includes connected the second flared section and the second slot section, second flaring
Section 31 is connect with the second slot section 32 by the second aditus laryngis 33.
Second flared section 31 is gradually reduced by starting point to 33 internal diameter of the second aditus laryngis.
The second slot section 32 should at least be remained unchanged by the second aditus laryngis 33 to 2 outlet end internal diameter of outer layer jet pipe.It is preferred that
, the second slot section 32 is gradually increased by the second aditus laryngis 33 to 2 outlet end internal diameter of outer layer jet pipe.
Second flared section, the 31 starting point internal diameter is greater than 21 exhaust gas inlet end internal diameter of the first flared section, it is preferred that second
31 starting point internal diameter of flared section is 3-5 times of 21 exhaust gas inlet end internal diameter of the first flared section.
Second flared section, the 31 starting point cross-sectional shape includes but is not limited to circle, and rectangle is trapezoidal, triangle.
In a preferred embodiment, the 31 starting point cross-sectional shape of the second flared section is circle.
Second flared section, 31 length is greater than the total length of core jet pipe 2.
Second flared section, the 31 starting point internal diameter is greater than 32 waste gas outlet end internal diameter of the second slot section.Preferably, described
Second flared section, 31 starting point internal diameter is 3-4 times of 32 waste gas outlet end internal diameter of the second slot section.
Second slot section, the 32 outlet end cross section can be circle, and rectangle is trapezoidal, triangle.
In a preferred embodiment, the 32 outlet end cross section of the second slot section is circle.
Second aditus laryngis 33 is the pipeline section for connecting the second flared section 31 and the second slot section 32, and second aditus laryngis 33 is
At the bore minimum of the core jet pipe.
The second aditus laryngis length is the length less than the second flared section 31 or the second slot section 32.
The length of second flared section 31 or the second slot section 32 can be equal, can also be unequal.
The second slot section is provided with waste gas outlet 5.
The combustion chamber of second slot section, the 32 outlet end connection POU equipment.
The first slot section 22 is located at the inside of the outer layer jet pipe 3 and towards the outlet of outer layer jet pipe 3.
Further, the 21 exhaust gas inlet end of the first flared section extends to the second flared section 31 of the outer layer jet pipe 3
Outside, 22 outlet end of the first slot section of the core jet pipe are extended to set on nearly second aditus laryngis 32 of second flared section 31
Place, it is preferred that 22 outlet end of the first slot section is set at away from 31 starting point 3/5ths of the second flared section.
First flared section 21 is to be tightly connected with second flared section 31.
As shown in fig. 6, the outer layer jet pipe 3 is for conveying exhaust gas and inert gas, exhaust gas and inert gas are described the
Continuously accelerated when two slot sections 32.
As shown in Figure 1, the notch setting of the inert gas spray head 4 is on the tube wall of the outer layer jet pipe 3.
In a preferred embodiment, the inert gas spray head 4 is located on 31 tube wall of the second flared section.
In a preferred embodiment, the spout of the inert gas spray head 4 is located at remote second larynx of second flared section 31
On tube wall at mouthful, while being located at the underface of the core jet pipe 2.
The inert gas spray head can spray inert gas perpendicular to 22 axial direction of the first slot section, can also direction
Second flared section, 31 inside any direction sprays inert gas.Preferably, the inert gas spray head is perpendicular to the first slot section
22 axial injection inert gases, are wrapped in internal layer to form inert gas shielding gas-bearing formation for exhaust gas.
The inert gas spray head 4 can be set one, also can be set multiple, such as can be one, and two, three
It is a, four or more.When the inert gas spray head 4 is arranged multiple, it can be set outside the tube wall of the second flared section 31
In circumferential wall.
Dynamic source can be set in the inert gas spray head 4, can also be not provided with power source.When the inert gas sprays
First 4 when being provided with power source, and the exhaust gas and inert gas of the outer layer jet pipe 3 can be accelerated as supersonic speed.
The material of the inert gas spray head 4 can be one or more of following: plating stainless steel, polytetrafluoroethyl-ne
Alkene.
The inert gas spray head 4 for spraying inert gas, the inert gas can be nitrogen, helium, neon, argon, krypton,
Xenon.Preferably, the inert gas is nitrogen.
The inert gas isolation exhaust gas and discord waste gas reaction, the two of injection are accelerated in outer layer jet pipe, inert gas
Inert gas shielding gas-bearing formation is formed in the entire flared section of the second flared section 31, exhaust gas is formed in inert gas shielding gas internal layer
Stable laminar flow.
When in use, exhaust gas enters the first flared section 21 through exhaust gas inlet 1 to the jet pipe of the application in the present invention, and exhaust gas is passing through
It crosses the first aditus laryngis 23 and the first slot section 22 is accelerated, when 1 pressure of exhaust gas inlet is sufficiently large, 22 exit of the first slot section
Air-flow is up to supersonic speed.Enter 31 rear end of the second flared section of outer layer jet pipe after exhaust gas ejection core jet pipe.Such as Fig. 2 and Fig. 3 institute
Show, gas is generated discontinuous due to the unexpected compression by back-pressure Pt ' (pressure at inert gas spray head) outside core jet pipe
Pressure increase because Pe (outlet pressure of core jet pipe) be greater than Pa (pressure of outer layer jet pipe), exhaust gas be in owe expansion shape
State, exhaust gas prolonged expansion and reduce pressure after core jet pipe out, and pressure is gradually lowered to Pa, and in the second flared section 31 due to
The injection of inert gas spray head 4 forms inert gas shielding gas-bearing formation, and the exhaust gas for spurting into the second flared section 31 is wrapped in indifferent gas
Body protects gas internal layer, and the low pressure of 3 core of outer layer jet pipe concentrates exhaust gas, be not easy to spread, and forms stable laminar flow (Pt in Fig. 2
The pressure at exhaust gas inlet end is represented, the direction of inert gas spray head is identical as core jet pipe direction in Fig. 3).In exhaust gas and inertia
Gas is again speeded up when passing through the second aditus laryngis with the second slot section, sprays (exhaust gas and indifferent gas from outer layer nozzle exit later
Airflow condition of the body in each jet pipe refers to fig. 4 to fig. 6).As shown in figure 3, Pe ' (outlet pressure of outer layer jet pipe) is less than
Pa ' (environmental pressure) will form shock wave in outer layer nozzle exit.When exhaust gas leaves outer layer jet pipe 3 inert gas shielding gas according to
So it is present in outer layer, exhaust gas can make exhaust gas deferred reaction in internal layer, carry out waste gas reaction in the position far from spout, prevent
There is incrustation or blocking spray head in jet pipe tube wall in a large amount of particulate matters such as silica that only waste gas reaction is formed, so as to improve intracavitary
The case where incrustation, reduces maintenance and repair rate.
In conclusion the present invention effectively overcomes various shortcoming in the prior art and has high industrial utilization value.
The above-described embodiments merely illustrate the principles and effects of the present invention, and is not intended to limit the present invention.It is any ripe
The personage for knowing this technology all without departing from the spirit and scope of the present invention, carries out modifications and changes to above-described embodiment.Cause
This, institute is complete without departing from the spirit and technical ideas disclosed in the present invention by those of ordinary skill in the art such as
At all equivalent modifications or change, should be covered by the claims of the present invention.
Claims (10)
1. a kind of cavity jet pipe of combustion-type POU equipment, which is characterized in that the cavity jet pipe include at least core jet pipe (2),
Outer layer jet pipe (3), inert gas spray head (4), the outlet of the core jet pipe (2) be located at the inside of the outer layer jet pipe (3) and
Towards the outlet of outer layer jet pipe (3), the notch setting of inert gas spray head (4) is on the tube wall of the outer layer jet pipe (3) and court
Outer layers jet pipe (3) is internal.
2. cavity jet pipe as described in claim 1, which is characterized in that the core jet pipe (2) includes the first connected flaring
Section (21) and the first slot section (22), first flared section (21) and the first slot section (22) are connected by the first aditus laryngis (23)
It connects；The outer layer jet pipe (3) includes connected the second flared section (31) and the second slot section (32), second flared section (31)
It is connect with the second slot section (32) by the second aditus laryngis (33).
3. cavity jet pipe as claimed in claim 2, which is characterized in that further include one or more of following characteristics:
A) first flared section (21) is provided with exhaust gas inlet (1), and the second slot section (22) is provided with waste gas outlet
(5)；
B) first flared section (21) is gradually reduced by starting point to the first aditus laryngis (23) internal diameter；
C) the first slot section (22) is remained unchanged by the first aditus laryngis (23) to core jet pipe outlet end internal diameter；
D) first aditus laryngis (23) is at the bore minimum of the core jet pipe (2)；
E) second flared section (31) is gradually reduced by starting point to the second aditus laryngis (33) internal diameter；
F) the second slot section (32) is remained unchanged by the second aditus laryngis (33) to outer layer nozzle exit end internal diameter；
G) second aditus laryngis (33) is at the bore minimum of the outer layer jet pipe (3).
4. cavity jet pipe as claimed in claim 2, which is characterized in that the first slot section (22) by the first aditus laryngis (23) extremely
Core jet pipe outlet end internal diameter is gradually increased, and/or, the second slot section (32) is gone out by the second aditus laryngis (32) to outer layer jet pipe
Mouth end internal diameter is gradually increased.
5. cavity jet pipe as claimed in claim 2, which is characterized in that the first slot section (22) is for accelerating exhaust gas.
6. cavity jet pipe as described in claim 1, which is characterized in that the core jet pipe outlet end is set to second flaring
At section (31) nearly second aditus laryngis (33).
7. cavity jet pipe as claimed in claim 2, which is characterized in that first flared section (21) and second flared section
(31) it is tightly connected.
8. cavity jet pipe as described in claim 1, which is characterized in that the outer layer jet pipe (3) is for conveying exhaust gas and inertia
Gas, exhaust gas and inert gas are accelerated at the second slot section (32).
9. cavity jet pipe as claimed in claim 1 or 2, which is characterized in that the inert gas spray head (4) is located at described second
On flared section (31) tube wall.
10. cavity jet pipe as claimed in claim 9, which is characterized in that the second flared section of the inert gas spray head direction
(31) internal either direction.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910709518.5A CN110345498A (en) | 2019-08-02 | 2019-08-02 | A kind of cavity jet pipe of combustion-type POU equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910709518.5A CN110345498A (en) | 2019-08-02 | 2019-08-02 | A kind of cavity jet pipe of combustion-type POU equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110345498A true CN110345498A (en) | 2019-10-18 |
Family
ID=68183751
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910709518.5A Pending CN110345498A (en) | 2019-08-02 | 2019-08-02 | A kind of cavity jet pipe of combustion-type POU equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110345498A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2023267A (en) * | 1978-06-15 | 1979-12-28 | Kernforschungsanlage Juelich | Apparatus and method for burning substances entrained as suspended particles in a gas |
| JPH02103311A (en) * | 1988-10-11 | 1990-04-16 | Chiyoda Corp | Method of treatment of poisonous flue gas by combustion |
| CN1047379A (en) * | 1989-05-08 | 1990-11-28 | 联合碳化工业气体技术公司 | Multiple oxidant jet combustion method and device |
| DE19744477A1 (en) * | 1997-10-09 | 1999-04-15 | Centrotherm Elektrische Anlage | Burner for waste gas cleaning installations |
| CN103775253A (en) * | 2014-02-12 | 2014-05-07 | 中国船舶重工集团公司第七一一研究所 | Exhaust gas pretreatment system for diesel engine |
| CN211119393U (en) * | 2019-08-02 | 2020-07-28 | 上海盛剑环境***科技股份有限公司 | Cavity spray pipe of combustion type POU equipment |
-
2019
- 2019-08-02 CN CN201910709518.5A patent/CN110345498A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2023267A (en) * | 1978-06-15 | 1979-12-28 | Kernforschungsanlage Juelich | Apparatus and method for burning substances entrained as suspended particles in a gas |
| JPH02103311A (en) * | 1988-10-11 | 1990-04-16 | Chiyoda Corp | Method of treatment of poisonous flue gas by combustion |
| CN1047379A (en) * | 1989-05-08 | 1990-11-28 | 联合碳化工业气体技术公司 | Multiple oxidant jet combustion method and device |
| DE19744477A1 (en) * | 1997-10-09 | 1999-04-15 | Centrotherm Elektrische Anlage | Burner for waste gas cleaning installations |
| CN103775253A (en) * | 2014-02-12 | 2014-05-07 | 中国船舶重工集团公司第七一一研究所 | Exhaust gas pretreatment system for diesel engine |
| CN211119393U (en) * | 2019-08-02 | 2020-07-28 | 上海盛剑环境***科技股份有限公司 | Cavity spray pipe of combustion type POU equipment |
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