CN203037073U - Supersonic speed high temperature ceramic repair welding gun - Google Patents
Supersonic speed high temperature ceramic repair welding gun Download PDFInfo
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- CN203037073U CN203037073U CN 201320037001 CN201320037001U CN203037073U CN 203037073 U CN203037073 U CN 203037073U CN 201320037001 CN201320037001 CN 201320037001 CN 201320037001 U CN201320037001 U CN 201320037001U CN 203037073 U CN203037073 U CN 203037073U
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- circulatory system
- water cooling
- cooling circulatory
- ground floor
- high pressure
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Abstract
The utility model provides a supersonic speed high temperature ceramic repair welding gun and relates to the technical field of ceramic repair. A high pressure oxygen inlet (1) and a gas inlet (2) are communicated with a combustion chamber (14). A gas check valve (12) is arranged between the gas inlet (2) and the combustion chamber (14). The gas inlet (2) is arranged at the outer portion of the high pressure oxygen inlet (1). The supersonic speed high temperature ceramic repair welding gun is characterized in that a high temperature shooting induction device (16) is arranged on the lower portion of the combustion chamber (14). A high pressure inlet (4) is connected with the high temperature shooting induction device (16). Due to the fact that the shooting induction device is arranged on a gun head of the supersonic speed high temperature ceramic repair welding gun, firm combination is formed on a repair-welded fireproof brick wall face, jet velocity reaches a supersonic speed state, a dropping-off phenomenon does not occur and combination intensity is high.
Description
Technical field:
It is exactly the field that the utility model relates to the pottery repairing, is specifically related to a kind of supersonic speed high-temperature ceramic soldering rifle.
Background technology:
Supersonic speed high-temperature ceramic soldering rifle is with in imflammable gas and oxygen or the air input soldering gun burner chamber, ignition system is lighted the back with it and is produced the high temperature and high speed expanded gas flow, the ceramic welding machine is imported the ceramic welding material of output in the air-flow of this speed high speed expansion simultaneously, and the soldering material particle is accelerated and is ejected on the refractory brick metope.Supersonic speed high-temperature ceramic soldering rifle can be applicable to the high temperature kiln internal refractory brick wall face damaged location welding maintenance of industries such as glass factory, glass fibre factory, steel plant, power station, garbage burning factory, metallurgy, steam power plant, petrochemical industry.
The complex structure of at present general ceramic welding rifle, structure is single, the ceramic welding material temperature that ejects is not high enough, the metope of soldering forms firm inadequately, and the soldering material speed of spraying is not high, can not reach supersonic speed, and obscission takes place the pottery after the soldering easily, bond strength is lower, and general ceramic welding rifle does not have the shooting induction installation simultaneously.
The utility model content:
The purpose of this utility model provides a kind of supersonic speed high-temperature ceramic soldering rifle, and its rifle headband has the shooting induction installation, and its soldering refractory brick metope forms strong bonded, and jet velocity can reach the supersonic speed state, obscission can not take place, the bond strength height.
In order to solve the existing problem of background technology, the utility model is by the following technical solutions: it comprises high pressure oxygen inlet 1, fuel gas inlet 2, igniter interface 3, high pressure admission mouth 4, soldering material import 5, ground floor water cooling circulatory system coolant intake 6, ground floor water cooling circulatory system cooling delivery port 7, the ground floor water cooling circulatory system 8, second layer water cooling circulatory system coolant intake 9, second layer water cooling circulatory system cooling delivery port 10, the second layer water cooling circulatory system 11, combustion gas check-valves 12, ignition coil 13, combustion chamber 14, electronics spark plug 15, high temperature shooting induction installation 16, earth terminal 17 and accelerating tube 18; High pressure oxygen inlet 1 and fuel gas inlet 2 are communicated with combustion chamber 14, and be provided with combustion gas check-valves 12 between fuel gas inlet 2 and the combustion chamber 14, fuel gas inlet 2 is arranged on the outside of high pressure oxygen inlet 1, igniter interface 3 is arranged on the outside of high pressure oxygen inlet 1, ignition coil 13 is arranged on the inside of igniter interface 3, electronics spark plug 15 is arranged in the combustion chamber 14, and ignition coil 13 is connected with electronics spark plug 15, one end of accelerating tube 18 is connected with combustion chamber 14, soldering material import 5 is communicated with accelerating tube 18, high pressure admission mouth 4 is arranged on the outside of fuel gas inlet 2, the ground floor water cooling circulatory system 8 is arranged on the outside of high pressure admission mouth 4, ground floor water cooling circulatory system coolant intake 6 is arranged on the left end of the ground floor water cooling circulatory system 8, the terminal outer wall of the ground floor water cooling circulatory system 8 is provided with ground floor water cooling circulatory system cooling delivery port 7, the second layer water cooling circulatory system 11 is arranged on the outside of the ground floor water cooling circulatory system 8, one end of the second layer water cooling circulatory system 11 is provided with second layer water cooling circulatory system coolant intake 9, the terminal outer wall of the second layer water cooling circulatory system 11 is provided with second layer water cooling circulatory system cooling delivery port 10, earth terminal 17 is arranged on the rear side of the outer end of the second layer water cooling circulatory system 11, the bottom of described combustion chamber 14 is provided with high temperature shooting induction installation 16, and high pressure admission mouth 4 is connected with high temperature shooting induction installation 16.
Described high pressure admission mouth 4 is the data wire import.
The utlity model has following beneficial effect: its rifle headband has the shooting induction installation, and its soldering refractory brick metope forms strong bonded, and jet velocity can reach the supersonic speed state, obscission can not take place, the bond strength height.
Description of drawings:
Fig. 1 is structural representation of the present utility model,
Fig. 2 is the A-A cutaway view of Fig. 1,
Fig. 3 is the B-B cutaway view of Fig. 1,
Fig. 4 is that the C portion of Fig. 1 is to view.
The specific embodiment:
Referring to Fig. 1-4, this specific embodiment by the following technical solutions: it comprises high pressure oxygen inlet 1, fuel gas inlet 2, igniter interface 3, high pressure admission mouth 4, soldering material import 5, ground floor water cooling circulatory system coolant intake 6, ground floor water cooling circulatory system cooling delivery port 7, the ground floor water cooling circulatory system 8, second layer water cooling circulatory system coolant intake 9, second layer water cooling circulatory system cooling delivery port 10, the second layer water cooling circulatory system 11, combustion gas check-valves 12, ignition coil 13, combustion chamber 14, electronics spark plug 15, high temperature shooting induction installation 16, earth terminal 17 and accelerating tube 18; High pressure oxygen inlet 1 and fuel gas inlet 2 are communicated with combustion chamber 14, and be provided with combustion gas check-valves 12 between fuel gas inlet 2 and the combustion chamber 14, fuel gas inlet 2 is arranged on the outside of high pressure oxygen inlet 1, igniter interface 3 is arranged on the outside of high pressure oxygen inlet 1, ignition coil 13 is arranged on the inside of igniter interface 3, electronics spark plug 15 is arranged in the combustion chamber 14, and ignition coil 13 is connected with electronics spark plug 15, one end of accelerating tube 18 is connected with combustion chamber 14, soldering material import 5 is communicated with accelerating tube 18, high pressure admission mouth 4 is arranged on the outside of fuel gas inlet 2, the ground floor water cooling circulatory system 8 is arranged on the outside of high pressure admission mouth 4, ground floor water cooling circulatory system coolant intake 6 is arranged on the left end of the ground floor water cooling circulatory system 8, the terminal outer wall of the ground floor water cooling circulatory system 8 is provided with ground floor water cooling circulatory system cooling delivery port 7, the second layer water cooling circulatory system 11 is arranged on the outside of the ground floor water cooling circulatory system 8, one end of the second layer water cooling circulatory system 11 is provided with second layer water cooling circulatory system coolant intake 9, the terminal outer wall of the second layer water cooling circulatory system 11 is provided with second layer water cooling circulatory system cooling delivery port 10, earth terminal 17 is arranged on the rear side of the outer end of the second layer water cooling circulatory system 11, the bottom of described combustion chamber 14 is provided with high temperature shooting induction installation 16, and high pressure admission mouth 4 is connected with high temperature shooting induction installation 16.
Described high pressure admission mouth 4 is the data wire import.
The course of work of this specific embodiment is as follows:
High pressure oxygen is imported the combustion chamber 14 from high pressure oxygen inlet 1, combustion gas is imported from fuel gas inlet 2 and is entered combustion chamber 14 by combustion gas check-valves 12, and ignition coil 13 is inserted in the supersonic speed ceramic welding rifle and with electronics spark plug 15 by igniter interface 3 and is connected.When soldering begins, electronics spark plug 15 to be connected by ignition coil 13 by the external connected electronic igniter, electronics spark plug 15 just begins constant ignition, and the combustion gas in the ignition combustion chamber 14 and the mist of oxygen make it that violent gas-phase combustion reaction take place.Heat energy is emitted in burning acutely expands combustion product, and when this violent gas that expands was flowed through accelerating tube 18, the effect of contraction that is subjected to accelerating tube 18 formed supersonic speed thermal-flame stream.The ceramic welding material is imported in the supersonic speed ceramic welding rifles by soldering material import 5, and enters accelerating tube 18, and the ceramic material particle obtains spraying to the refractory brick metope after heating and the acceleration under the effect of supersonic speed thermal-flame stream, implements the soldering to metope refractory brick.
High temperature shooting induction installation 16 butt welding fettling faces carry out real-time transmission and the monitoring soldering operating process of image, and data are connected output by data wire through data wire import 4 with external display.The high temperature shooting induction installation of pressure-air being imported supersonic speed high-temperature ceramic soldering rifle head by data wire import 4 plays the cooling protection effect simultaneously.
Ground floor water cooling circulatory system coolant intake 6 with in the big-flow high-pressure cooling water input supersonic speed high-temperature ceramic soldering rifle in the water inlet layer of the ground floor water cooling circulatory system 8 to the combustion chamber 14 in the supersonic speed high-temperature ceramic soldering rifle, high temperature shooting induction installation 16, accelerating tube 18 cools off, the water inlet layer outer wall gap of the ground floor water cooling circulatory system 8 is socketed with the water-yielding stratum of the ground floor water cooling circulatory system 8, this water-yielding stratum does not hold outer wall to be provided with ground floor water cooling circulatory system cooling delivery port 7, and the backwater after the circulation is carrying a large amount of heats and discharging from ground floor water cooling circulatory system cooling delivery port 7.The water inlet layer inwall gap of the second layer water cooling circulatory system 11 is socketed with the water-yielding stratum of the ground floor water cooling circulatory system 8, this water inlet layer not end is provided with second layer water cooling circulatory system coolant intake 9, the big-flow high-pressure cooling water is in second layer water cooling circulatory system coolant intake 9 input supersonic speed high-temperature ceramic soldering rifles, the normal operating temperature of supersonic speed high-temperature ceramic soldering rifle and structural strength have been guaranteed through 11 coolings of the second layer water cooling circulatory system, the water inlet layer outer wall gap of the second layer water cooling circulatory system 11 is socketed with the water-yielding stratum of second layer water-cooling circulating system, this water-yielding stratum does not hold outer wall to be provided with second layer water cooling circulatory system cooling delivery port 10, finishes the water of circulating reflux and discharges from second layer water cooling circulatory system cooling delivery port 10.
When using supersonic speed high-temperature ceramic soldering rifle that stove refractory brick metope is carried out the soldering operation, earth terminal 17 should play the effect of ground connection.
The rifle headband of this specific embodiment has the shooting induction installation, and its soldering refractory brick metope forms strong bonded, and jet velocity can reach the supersonic speed state, obscission can not take place, the bond strength height.
Claims (2)
1. supersonic speed high-temperature ceramic soldering rifle, it comprises high pressure oxygen inlet (1), fuel gas inlet (2), igniter interface (3), high pressure admission mouth (4), soldering material import (5), ground floor water cooling circulatory system coolant intake (6), ground floor water cooling circulatory system cooling delivery port (7), the ground floor water cooling circulatory system (8), second layer water cooling circulatory system coolant intake (9), second layer water cooling circulatory system cooling delivery port (10), the second layer water cooling circulatory system (11), combustion gas check-valves (12), ignition coil (13), combustion chamber (14), electronics spark plug (15), high temperature shooting induction installation (16), earth terminal (17) and accelerating tube (18); High pressure oxygen inlet (1) and fuel gas inlet (2) are communicated with combustion chamber (14), and be provided with combustion gas check-valves (12) between fuel gas inlet (2) and combustion chamber (14), fuel gas inlet (2) is arranged on the outside of high pressure oxygen inlet (1), the bottom that it is characterized in that described combustion chamber (14) is provided with high temperature shooting induction installation (16), and high pressure admission mouth (4) is connected with high temperature shooting induction installation (16).
2. supersonic speed high-temperature ceramic soldering rifle according to claim 1, it is characterized in that igniter interface (3) is arranged on the outside of high pressure oxygen inlet (1), ignition coil (13) is arranged on the inside of igniter interface (3), electronics spark plug (15) is arranged in the combustion chamber (14), and ignition coil (13) is connected with electronics spark plug (15), one end of accelerating tube (18) is connected with combustion chamber (14), soldering material import (5) is communicated with accelerating tube (18), high pressure admission mouth (4) is arranged on the outside of fuel gas inlet (2), the ground floor water cooling circulatory system (8) is arranged on the outside of high pressure admission mouth (4), ground floor water cooling circulatory system coolant intake (6) is arranged on the left end of the ground floor water cooling circulatory system (8), the terminal outer wall of the ground floor water cooling circulatory system (8) is provided with ground floor water cooling circulatory system cooling delivery port (7), the second layer water cooling circulatory system (11) is arranged on the outside of the ground floor water cooling circulatory system (8), one end of the second layer water cooling circulatory system (11) is provided with second layer water cooling circulatory system coolant intake (9), the terminal outer wall of the second layer water cooling circulatory system (11) is provided with second layer water cooling circulatory system cooling delivery port (10), and earth terminal (17) is arranged on the rear side of the outer end of the second layer water cooling circulatory system (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320037001 CN203037073U (en) | 2013-01-24 | 2013-01-24 | Supersonic speed high temperature ceramic repair welding gun |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320037001 CN203037073U (en) | 2013-01-24 | 2013-01-24 | Supersonic speed high temperature ceramic repair welding gun |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203037073U true CN203037073U (en) | 2013-07-03 |
Family
ID=48689188
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320037001 Expired - Fee Related CN203037073U (en) | 2013-01-24 | 2013-01-24 | Supersonic speed high temperature ceramic repair welding gun |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203037073U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103075887A (en) * | 2013-01-24 | 2013-05-01 | 张立生 | Supersonic speed high-temperature ceramic repair welding gun |
-
2013
- 2013-01-24 CN CN 201320037001 patent/CN203037073U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103075887A (en) * | 2013-01-24 | 2013-05-01 | 张立生 | Supersonic speed high-temperature ceramic repair welding gun |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130703 Termination date: 20190124 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |