CN203050885U - Associated gas engine - Google Patents
Associated gas engine Download PDFInfo
- Publication number
- CN203050885U CN203050885U CN 201320024087 CN201320024087U CN203050885U CN 203050885 U CN203050885 U CN 203050885U CN 201320024087 CN201320024087 CN 201320024087 CN 201320024087 U CN201320024087 U CN 201320024087U CN 203050885 U CN203050885 U CN 203050885U
- Authority
- CN
- China
- Prior art keywords
- fuselage
- associated gas
- fuel tank
- flywheel
- automatic
- 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
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Abstract
The utility model discloses an associated gas engine which comprises an engine body. A mixer is placed on one side of the engine body; a spark plug is placed beside the mixer, and is connected with an automatic speed controller; a full-automatic starter is placed beside the automatic speed controller; a belt wheel is placed on the other side of the engine body; a fly wheel is placed on the belt wheel; and a magnetic block and a magneto-electricity high-tension cable package are placed on the fly wheel. Associated gas on an oil well mouth can be efficiently converted to power and is output through the associated gas engine, and the associated gas can be served as a power source of oil pumping, and the associated gas engine is energy-saving and environment-friendly.
Description
Technical field
The utility model belongs to the technical field of engines of oil field oil recovery usefulness, relates to a kind of associated gas motor.
Background technique
At present; in the oil well operation process; well head can produce a large amount of associated gases, directly enters air and can cause pollution of atmosphere, and processing method commonly used now is; associated gas is generated electricity by the natural gas power unit; but because oil well mouth associated gas tolerance is less, and generator set needs a large amount of associated gases, so cause generator set to shut down easily; delay production, so lower to the utilization ratio of associated gas.
Summary of the invention
The purpose of this utility model provides a kind of associated gas motor, to solve the problem that oil well mouth associated gas can not efficiently utilize.
The technological scheme that the utility model adopts is, comprise fuselage, a side of fuselage is provided with fuel tank, fuel tank is provided with spark plug, the fuel tank bottom is provided with the dewatering outlet, be provided with mixer near the fuel tank side on the fuselage, mixer is provided with the mixing air valve, mixing air valve is connected with automatic speed governor by speed control rod, speed control rod and automatic speed governor all are positioned on the face adjacent with fuel tank place face on the fuselage, and speed control rod is provided with speed-regulating handle, and the automatic speed governor side is provided with full-automatic starter, side relative with full-automatic starter place face on the fuselage is provided with belt pulley, be with flywheel on the belt pulley, flywheel is provided with magnetic patch, and the position of corresponding magnetic patch is provided with magnetoelectricity high voltage wire bag on the fuselage, the top of fuselage is provided with sound silencer, and fuselage is provided with cooling unit.
Characteristics of the present utility model also are,
Cooling unit comprises water tank, water tank is provided with fan, fan is connected with fuselage by connector, and connector is positioned at side relative with fuel tank place face on the fuselage, and connector is connected with flywheel by belt, the top of water tank is provided with the filler, the other filling pipe end II that arranges in filler, filling pipe end II is connected with the filling pipe end I that the fuselage top arranges by pipeline, is provided with water pump near the flywheel side on the fuselage, water pump is provided with down mouth of a river I, and following mouth of a river I is connected with the following mouth of a river II that water tank bottom arranges by pipeline.
The beneficial effects of the utility model are, by associated gas motor of the present utility model, can utilize oil well mouth associated gas efficiently, are translated into power output, can be used as the power resources of oil pumping, not only energy-conservation but also environmental protection.
Description of drawings
Fig. 1 is the plan view of the utility model associated gas motor;
Fig. 2 is the rear view of the utility model associated gas motor.
Among the figure, 1. mixer, 2. associated gas import, 3. diesel engine, 4. filling pipe end I, 5. fuselage, 6. filling pipe end II, 7. mouth of a river II is 8. descended, 9. water tank in the filler, 10. fan, 11. full-automatic starters, 12. automatic speed governors, 13. dewatering outlets, 14. fuel tanks, 15. spark plug, 16. magnetic patch, 17. magnetoelectricity high voltage wire bags, 18. sound silencers, 19. following mouth of a river I, 20. water pumps, 21. flywheels, 22. belt pulleys, 23. speed-regulating handle, 24. speed control rods, 25. mix air valve, 26. connectors.
Embodiment
Below in conjunction with the drawings and specific embodiments the utility model is elaborated.
The utility model provides a kind of associated gas motor, referring to Fig. 1, Fig. 2, comprise fuselage 5, a side of fuselage is provided with fuel tank 14, fuel tank 14 is provided with spark plug 15, fuel tank 14 bottoms are provided with dewatering outlet 13, be provided with mixers 1 near fuel tank 14 sides on the fuselage 5, mixer 1 is provided with and mixes air valve 25, mixing air valve 25 is connected with automatic speed governor 12 by speed control rod 24, speed control rod 24 all is positioned on the face adjacent with fuel tank 14 place faces on the fuselage 5 with automatic speed governor 12, speed control rod 24 is provided with speed-regulating handle 23, automatic speed governor 12 sides are provided with full-automatic starter 11, and side relative with full-automatic starter 11 place faces on the fuselage 5 is provided with belt pulley 22, is with flywheel 21 on the belt pulley 22, flywheel 21 is provided with magnetic patch 16, the position of corresponding magnetic patch 16 is provided with magnetoelectricity high voltage wire bag 17 on the fuselage 5, and the top of fuselage 5 is provided with sound silencer 18, and fuselage 5 is provided with cooling unit.
Cooling unit wherein comprises water tank 9, water tank 9 is provided with fan 10, fan 10 is connected with fuselage 5 by connector 26, connector 26 is positioned at side relative with fuel tank 14 place faces on the fuselage 5, connector 26 is connected with flywheel 21 by belt, the top of water tank 9 is provided with filler 7, the filler 7 other filling pipe end II6 that arrange, filling pipe end II6 is connected with the filling pipe end I4 that the fuselage top arranges by pipeline, be provided with water pumps 20 near flywheel 21 sides on the fuselage 5, water pump 20 is provided with down mouth of a river I19, and following mouth of a river I19 is connected with the following mouth of a river II8 that water tank 9 bottoms arrange by pipeline.
During work, depress the starting bar of full-automatic starter 11, start the associated gas motor, driving belt pulley 22 rotates, flywheel 21 is rotated thereupon, magnetic patch 16 is fixed on the flywheel 21, and magnetoelectricity high voltage wire bag 17 is fixed on the fuselage 5, and magnetoelectricity high voltage wire bag 17 produces electric current when flywheel 21 rotates, electric current is by being wired to sparking on the spark plug 15, constitute ignition system, simultaneously, associated gas enters in the cylinder of fuselage by the associated gas import 2 of mixer 1, spark plug is lighted associated gas, drive the connecting rod periodic duty in the fuselage 14, produce kinetic energy, from flywheel 21 outputs.
Automatic speed governor 12 can be regulated the air inflow that enters from associated gas import 2 according to the payload of fuselage 5.
7 feed tanks, 9 water fillings from the filler, current arrive the following mouth of a river I19 of water pump 20 by following mouth of a river II8, enter water tank 9 from filling pipe end I4 and filling pipe end II6 again, and the circulation cooling in the time cooling water will being discharged, only needs water 13 is emitted and got final product from the dewatering outlet.
During the associated gas engine operation, flywheel 21 rotates, and by belt transmission, drives the belt movement on the connector 26, thereby the fan 10 that drives on the water tank 9 rotates, and can accelerate the water in the cooling water tank 9.
When the air pressure of associated gas when 0.2KPa is above, associated gas is entered by mixer 1 in the cylinder of fuselage 5, is provided kinetic energy for motor after spark plug 15 igniting; When associated gas air feed deficiency, air pressure is when 0.2KPa is following, the associated gas import 2 of mixer 1 is plugged, stop air feed, air intlet is opened simultaneously, and filler opening is also connected, regulate the gasoline oil inlet quantity of filler opening by fuel tap, making gasoline and air is that the ratio of 1:7 is mixed according to volume ratio, enters in the cylinder of fuselage 5 again, is provided kinetic energy for motor after spark plug 15 igniting.
By associated gas motor of the present utility model, can make the associated gas motor under the situation of associated gas abundance, utilize associated gas to produce kinetic energy, and can under micro-air feed, intermittent gas supply and the situation of dying, convert the pattern of burns gasoline to, make the associated gas motor still can be normally stable running, can realize utilizing efficiently the purpose of oil well mouth associated gas, associated gas is converted into power output, as the power resources of recovering the oil, not only energy-conservation but also environmental protection.
Claims (2)
1. associated gas motor, it is characterized in that, comprise fuselage (5), a side of fuselage is provided with fuel tank (14), fuel tank (14) is provided with spark plug (15), fuel tank (14) bottom is provided with dewatering outlet (13), fuselage (5) is gone up near the other mixer (1) that is provided with of fuel tank (14), mixer (1) is provided with and mixes air valve (25), mixing air valve (25) is connected with automatic speed governor (12) by speed control rod (24), speed control rod (24) all is positioned at fuselage (5) with automatic speed governor (12) and goes up on the face adjacent with fuel tank (14) place face, speed control rod (24) is provided with speed-regulating handle (23), the other full-automatic starter (11) that is provided with of automatic speed governor (12), fuselage (5) is gone up the side relative with full-automatic starter (11) place face and is provided with belt pulley (22), be with flywheel (21) on the belt pulley (22), flywheel (21) is provided with magnetic patch (16), the position that described fuselage (5) is gone up corresponding magnetic patch (16) is provided with magnetoelectricity high voltage wire bag (17), the top of described fuselage (5) is provided with sound silencer (18), and described fuselage (5) is provided with cooling unit.
2. a kind of associated gas motor as claimed in claim 1, it is characterized in that, described cooling unit comprises water tank (9), water tank (9) is provided with fan (10), fan (10) is connected with fuselage (5) by connector (26), connector (26) is positioned at fuselage (5) and goes up the side relative with fuel tank (14) place face, connector (26) is connected with flywheel (21) by belt, the top of described water tank (9) is provided with filler (7), the other filling pipe end II(6 that arranges in filler (7)), filling pipe end II(6) the filling pipe end I(4 that arranges by pipeline and fuselage top) is connected, fuselage (5) is gone up near the other water pump (20) that is provided with of flywheel (21), water pump (20) is provided with down mouth of a river I(19), following mouth of a river I(19) the following mouth of a river II(8 that arranges by pipeline and water tank bottom) be connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320024087 CN203050885U (en) | 2013-01-17 | 2013-01-17 | Associated gas engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320024087 CN203050885U (en) | 2013-01-17 | 2013-01-17 | Associated gas engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203050885U true CN203050885U (en) | 2013-07-10 |
Family
ID=48733844
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320024087 Expired - Fee Related CN203050885U (en) | 2013-01-17 | 2013-01-17 | Associated gas engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203050885U (en) |
-
2013
- 2013-01-17 CN CN 201320024087 patent/CN203050885U/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 | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130710 Termination date: 20140117 |