CN103089434A - Combustible gas engine - Google Patents
Combustible gas engine Download PDFInfo
- Publication number
- CN103089434A CN103089434A CN2011103364311A CN201110336431A CN103089434A CN 103089434 A CN103089434 A CN 103089434A CN 2011103364311 A CN2011103364311 A CN 2011103364311A CN 201110336431 A CN201110336431 A CN 201110336431A CN 103089434 A CN103089434 A CN 103089434A
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- Prior art keywords
- gas
- engine
- impeller
- main shaft
- driving wheel
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Abstract
The invention discloses a combustible gas engine. The upper portion of a combustion chamber (12) is a fuel supply pipeline, the fuel supply pipeline is sequentially connected with a gas guide tube (7), a solenoid valve (8), an adjustment valve (9) and burners (10), the lower portion of the combustion chamber (12) is connected with an air introducing system and a power output system, the air introducing system comprises a gas inlet (4), gas compressors (3) and a gas inlet pore (6), and the power output system comprises a motor driving wheel (1), a main shaft (2), an impeller (14) and a bearing (5); one end of the main shaft (2) is sequentially connected with the motor driving wheel (1), the impeller (14), the air inlet (4), the gas compressors (3) and the bearing (5), a spark plug (11) is arranged in the combustion chamber body, and one end of the spark plug (11) is a gas nozzle (13); and the bottom of the cylinder body of the engine is provided with a gas outlet (15). The combustible gas engine has the advantages of simple structure, simple making technology, less wear parts, reasonable design, wide application fuel range, use convenience, effective improvement of the heat efficiency of the heat engine, and reduction of the pollution of the discharged gas.
Description
Technical field:
The invention belongs to and a kind ofly can apply to Motor Vehicle, generator set, the motor that boats and ships drive is specifically related to a kind of gas burning engine.
Background technique:
Existing motor car engine, generally all use fuel oil, act as a fuel, claim fossil fuel, as reciprocating engine, turbogenerator, rotary engines etc. are discharged into some harmful gases in atmosphere after its work, cause the severe contamination of ecotope, although people come replacing fuel oil at the fuel of seeking of ideal always, in order to reduce pollution to environment, what can actually be applied has no report always.
Summary of the invention:
The purpose of this invention is to provide in a kind of gas burning engine, improve the heat engine working efficiency, the parts that reduce wear, when effectively reducing engine operation, discharge of noxious gases pollutes.
The technical solution used in the present invention is: a kind of gas burning engine comprises motor
driving wheel 1, main shaft 2, gas compressor 3, suction port 4, bearing 5, inlet hole 6, air pipe 7, solenoid valve 8, modulating valve 9, burner 10, spark plug 11, firing chamber 12, gas nozzle 13, impeller 14, relief opening 15, 12 tops, firing chamber are fuel supply pipe roads, be connected with air pipe 7 on pipeline in turn, solenoid valve 8, modulating valve 9, burner 10, the bottom, firing chamber is connected with air intake system and power output system, air intake system comprises suction port 4, gas compressor 3, inlet hole 6, power output system comprises motor driving wheel 1, main shaft 2, impeller 14, bearing 5, from end connecting motor driving wheel 1 successively, impeller 14, suction port 4, gas compressor 3, bearing 5, firing chamber body are provided with spark plug 11, one ends and are provided with gas nozzle 13 by main shaft 2, the engine cylinder-body foot is provided with relief opening 15.
Advantage of the present invention is: simple in structure, manufacturing process is simple, and wearout parts is few, and is reasonable in design, and applicable fuel range is wide.Easy to use, compare with prior art, the present invention not only can improve the thermal efficiency of heat engine, and fuel relatively in the past, can reduce the pollution of exhausting air, concrete higher use value.
Description of drawings:
Fig. 1 is structural representation of the present invention.
Embodiment
a kind of gas burning engine, comprise motor driving wheel 1, main shaft 2, gas compressor 3, suction port 4, bearing 5, inlet hole 6, air pipe 7, solenoid valve 8, modulating valve 9, burner 10, spark plug 11, firing chamber 12, gas nozzle 13, impeller 14, relief opening 15, 12 tops, firing chamber are fuel supply pipe roads, be connected with air pipe 7 on pipeline in turn, solenoid valve 8, modulating valve 9, burner 10, the bottom, firing chamber is connected with air intake system and power output system, air intake system comprises suction port 4, gas compressor 3, inlet hole 6, power output system comprises motor driving wheel 1, main shaft 2, impeller 14, bearing 5, from end connecting motor driving wheel 1 successively, impeller 14, suction port 4, gas compressor 3, bearing 5, firing chamber body are provided with spark plug 11, one ends and are provided with gas nozzle 13 by main shaft 2, the engine cylinder-body foot is provided with relief opening 15.
Because impeller and gas compressor centrifugal wind wheel are contained on same axle, so suction port to the air of firing chamber is continuous, fuel is also that continuous supplying is to the firing chamber, impeller all is subjected to nozzle to promote acting in 360 ° of slewing areas, maximum speed can reach 3000 rev/mins, rotate smoothness, power output is steady, and the thermal efficiency is high.The fuel that uses is gas, also effectively reduces the pollution of gas discharging.
Claims (1)
1. gas burning engine, comprise motor driving wheel (1), main shaft (2), gas compressor (3), suction port (4), bearing (5), inlet hole (6), air pipe (7), solenoid valve (8), modulating valve (9), burner (10), spark plug (11), firing chamber (12), gas nozzle (13), impeller (14), relief opening (15), it is characterized in that: top, firing chamber (12) is the fuel supply pipe road, be connected with air pipe (7) on pipeline in turn, solenoid valve (8), modulating valve (9), burner (10), the bottom, firing chamber is connected with air intake system and power output system, air intake system comprises suction port (4), gas compressor (3), inlet hole (6), power output system comprises motor driving wheel (1), main shaft (2), impeller (14), bearing (5), from end connecting motor driving wheel successively (1), impeller (14), suction port (4), gas compressor (3), bearing (5), firing chamber body are provided with spark plug (11) by main shaft (2), and an end is provided with gas nozzle (13), the engine cylinder-body foot is provided with relief opening (15).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011103364311A CN103089434A (en) | 2011-10-31 | 2011-10-31 | Combustible gas engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011103364311A CN103089434A (en) | 2011-10-31 | 2011-10-31 | Combustible gas engine |
Publications (1)
Publication Number | Publication Date |
---|---|
CN103089434A true CN103089434A (en) | 2013-05-08 |
Family
ID=48202467
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2011103364311A Pending CN103089434A (en) | 2011-10-31 | 2011-10-31 | Combustible gas engine |
Country Status (1)
Country | Link |
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CN (1) | CN103089434A (en) |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3010281A (en) * | 1957-12-24 | 1961-11-28 | Adolph J Cervenka | Toroidal combustion chamber |
US3238718A (en) * | 1964-01-30 | 1966-03-08 | Boeing Co | Gas turbine engine |
CN202325858U (en) * | 2011-10-31 | 2012-07-11 | 山西沁新能源集团股份有限公司 | Combustible gas engine |
-
2011
- 2011-10-31 CN CN2011103364311A patent/CN103089434A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3010281A (en) * | 1957-12-24 | 1961-11-28 | Adolph J Cervenka | Toroidal combustion chamber |
US3238718A (en) * | 1964-01-30 | 1966-03-08 | Boeing Co | Gas turbine engine |
CN202325858U (en) * | 2011-10-31 | 2012-07-11 | 山西沁新能源集团股份有限公司 | Combustible gas engine |
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C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20130508 |