CN203517172U - High pressure antiseeping grouting machine - Google Patents
High pressure antiseeping grouting machine Download PDFInfo
- Publication number
- CN203517172U CN203517172U CN201320510539.2U CN201320510539U CN203517172U CN 203517172 U CN203517172 U CN 203517172U CN 201320510539 U CN201320510539 U CN 201320510539U CN 203517172 U CN203517172 U CN 203517172U
- Authority
- CN
- China
- Prior art keywords
- high pressure
- fuselage
- machine body
- heater
- suction tude
- 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
Links
- 239000000463 material Substances 0.000 claims description 5
- 230000001105 regulatory effect Effects 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 3
- 239000002994 raw material Substances 0.000 abstract 2
- 239000002981 blocking agent Substances 0.000 description 9
- 238000000034 method Methods 0.000 description 2
- 238000004064 recycling Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
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Abstract
The utility model provides a high pressure antiseeping grouting machine which comprises a machine body. An air inlet pipe is arranged on one side of the machine body, a pressure valve is arranged on the air inlet pipe, a feed pipe is arranged on one side, close to the air inlet pipe, of the upper portion of the machine body, a raw material tank is arranged on the upper portion of the feed pipe, a feed port is formed in the upper portion of the raw material tank, the air inlet pipe and the feed pipe join on a discharge pipe, the discharge pipe penetrates through the bottom of the machine body and extends outwards, a discharge port is formed in the output end of the discharge pipe, a heater is arranged on one side, away from the air inlet pipe, of the upper portion of the machine body, a gun head is arranged on the lower portion of the heater, the gun head penetrates through the bottom of the machine body and extends outwards, and a support is arranged on the bottom of the machine body. The high pressure antiseeping grouting machine has the advantages that the structure is simple, using is convenient, plugging agents are jetted to a leaking point by using high pressure, the plugging agents are dried by using the heater, and the leaking stoppage effect is good.
Description
(1) technical field
The utility model relates to a kind of leak stoppers, particularly relates to a kind of high pressure leaking stoppage grouter.
(2) background technique
Along with the development in city, increasing city auxiliary facility is installed in city now.The transportation of now a lot of things all needs tube road to complete, and still, along with the lengthening of service time, pipeline can leak unavoidably, and the leakage of pipeline not only can cause the waste of resource, also can affect the construction in city simultaneously.Existing leak stoppers is just simply put electric leakage into lost circulation plug, but can not tackle the problem at its root.Therefore, be necessary existing leak stoppers to improve, make it utilize high pressure that blocking agent is ejected into dew point, recycling heater is dried blocking agent, and plugging effect is good.
(3) model utility content
In order to overcome the deficiency of existing leak stoppers, the utility model provides a kind of high pressure leaking stoppage grouter.
The technical solution of the utility model is achieved in that
A kind of high pressure leaking stoppage grouter of this programme, comprises fuselage, and a side of described fuselage is provided with suction tude; In described suction tude, be provided with pressure valve; Described back is provided with supply pipe near a side of suction tude; The top of described supply pipe is provided with head tank; The top of described head tank is provided with material feeding mouth; Described suction tude and supply pipe are intersected in discharge nozzle; Described discharge nozzle stretches to outside through the bottom of fuselage; The output terminal of described discharge nozzle is provided with discharge port; Described back is provided with heater away from a side of suction tude; The bottom of described heater is provided with rifle head; Described rifle head stretches to outside through the bottom of fuselage; The distance that described rifle head is liftoff is a little more than the liftoff distance of discharge port; The bottom of described fuselage is provided with support.
Further, on described discharge port, be provided with Flow valve.
Further, on described heater, be provided with flame regulating valve.
Usefulness of the present utility model is: simple in structure, easy to use, and utilize high pressure that blocking agent is ejected into dew point, recycling heater is dried blocking agent, and plugging effect is good.
(4) accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Wherein: 1-fuselage, 2-suction tude, 3-pressure valve, 4-supply pipe, 5-head tank, 6-material feeding mouth, 7-discharge nozzle, 8-discharge port, 9-heater, 10-rifle head, 11-support.
(5) embodiment
Below in conjunction with accompanying drawing, a kind of mode of execution of the present utility model is made to brief description.
A kind of high pressure leaking stoppage grouter as Fig. 1, comprises fuselage 1, and a side of described fuselage 1 is provided with suction tude 2; In described suction tude 2, be provided with pressure valve 3; Described fuselage 1 top is provided with supply pipe 4 near a side of suction tude 2; The top of described supply pipe 4 is provided with head tank 5; The top of described head tank 5 is provided with material feeding mouth 6; Described suction tude 2 and supply pipe 3 are intersected in discharge nozzle 7; Described discharge nozzle 7 stretches to outside through the bottom of fuselage 1; The output terminal of described discharge nozzle 7 is provided with discharge port 8; Described fuselage 1 top is provided with heater 9 away from a side of suction tude 2; The bottom of described heater 9 is provided with rifle head 10; Described rifle head 10 stretches to outside through the bottom of fuselage 1; The distance that described rifle head 10 is liftoff is a little more than the liftoff distance of discharge port 8; The bottom of described fuselage 1 is provided with support 11; On described discharge port 8, be provided with Flow valve; On described heater 9, be provided with flame regulating valve.
The working procedure of this example: when using the utility model, first, blocking agent is joined from material feeding mouth 6 to head tank 5, pressurizer is added to air pressure in equipment by suction tude 2, then, blocking agent in head tank 5 enters into discharge nozzle 7 after pressurization, blocking agent after pressurization is ejected into dew point by discharge port 8,9 pairs of rifle heads 10 of heater heat, finally, the route that rifle head 10 is advanced along discharge port 8 heats blocking agent, and blocking agent hardening after heating, can thoroughly shut dew point.
Above an embodiment of the present utility model is had been described in detail, but described content is only preferred embodiment of the present utility model, can not be considered to for limiting practical range of the present utility model.All equalization variations of doing according to the utility model application range and improvement etc., within all should still belonging to patent covering scope of the present utility model.
Claims (3)
1. a high pressure leaking stoppage grouter, comprises fuselage (1), it is characterized in that: a side of described fuselage (1) is provided with suction tude (2); In described suction tude (2), be provided with pressure valve (3); Described fuselage (1) top is provided with supply pipe (4) near a side of suction tude (2); The top of described supply pipe (4) is provided with head tank (5); The top of described head tank (5) is provided with material feeding mouth (6); Described suction tude (2) and supply pipe (3) are intersected in discharge nozzle (7); Described discharge nozzle (7) stretches to outside through the bottom of fuselage (1); The output terminal of described discharge nozzle (7) is provided with discharge port (8); Described fuselage (1) top is provided with heater (9) away from a side of suction tude (2); The bottom of described heater (9) is provided with rifle head (10); Described rifle head (10) stretches to outside through the bottom of fuselage (1); The distance that described rifle head (10) is liftoff is a little more than the liftoff distance of discharge port (8); The bottom of described fuselage (1) is provided with support (11).
2. a kind of high pressure leaking stoppage grouter according to claim 1, is characterized in that: described discharge port is provided with Flow valve on (8).
3. a kind of high pressure leaking stoppage grouter according to claim 1, is characterized in that: described heater is provided with flame regulating valve on (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320510539.2U CN203517172U (en) | 2013-08-20 | 2013-08-20 | High pressure antiseeping grouting machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320510539.2U CN203517172U (en) | 2013-08-20 | 2013-08-20 | High pressure antiseeping grouting machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203517172U true CN203517172U (en) | 2014-04-02 |
Family
ID=50376103
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320510539.2U Expired - Fee Related CN203517172U (en) | 2013-08-20 | 2013-08-20 | High pressure antiseeping grouting machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203517172U (en) |
-
2013
- 2013-08-20 CN CN201320510539.2U patent/CN203517172U/en not_active Expired - Fee Related
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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: 20140402 Termination date: 20140820 |
|
| EXPY | Termination of patent right or utility model |