CN103089434A - Combustible gas engine - Google Patents

Combustible gas engine Download PDF

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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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CN
China
Prior art keywords
gas
engine
impeller
main shaft
driving wheel
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
Application number
CN2011103364311A
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Chinese (zh)
Inventor
李慧明
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanxi Qinxin Energy Group Co Ltd
Original Assignee
Shanxi Qinxin Energy Group Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Shanxi Qinxin Energy Group Co Ltd filed Critical Shanxi Qinxin Energy Group Co Ltd
Priority to CN2011103364311A priority Critical patent/CN103089434A/en
Publication of CN103089434A publication Critical patent/CN103089434A/en
Pending legal-status Critical Current

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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

A kind of gas burning engine
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.
Gas compressor 3 is assemblied on main shaft 2 with impeller 14, supports same axle center by bearing 5 and moves in the direction of the clock, and air is entered by suction port 4, is pressed into the firing chamber by gas compressor 3 through inlet hole 6; Fuel pot is inflammable gas pressurization pot type liquefied gas tank, after solenoid valve 8 is opened, enter burner through air pipe 7, solenoid valve 8, modulating valve 9, run into the air that enters the firing chamber, at this moment spark ignitor flame, fully burning in the firing chamber, during burning, flame temperature can reach 1300 ℃ of-2000 ℃ of based on fuel different temperatures differences, make burning indoor gas rapid expansion, gas sprays with flank speed through nozzle 13, promote impeller 14 and drive in the direction of the clock 1 rotation of motor driving wheel, thus externally acting.Gas after acting is discharged by relief opening 15.Modulating valve 9 can adjustment of combustion gas flow size, the adjusting rotary speed size is to control the size of outputting power, when shut electromagnetic valve 8, the fuel supply is cut off, engine operation stops.
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).
CN2011103364311A 2011-10-31 2011-10-31 Combustible gas engine Pending CN103089434A (en)

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
CN (1) CN103089434A (en)

Citations (3)

* Cited by examiner, † Cited by third party
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

Patent Citations (3)

* Cited by examiner, † Cited by third party
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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Application publication date: 20130508