CN209340039U - A kind of Gas Turbine Generating Units high energy ignition unit - Google Patents

A kind of Gas Turbine Generating Units high energy ignition unit Download PDF

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Publication number
CN209340039U
CN209340039U CN201822152182.0U CN201822152182U CN209340039U CN 209340039 U CN209340039 U CN 209340039U CN 201822152182 U CN201822152182 U CN 201822152182U CN 209340039 U CN209340039 U CN 209340039U
Authority
CN
China
Prior art keywords
high energy
gas turbine
generating units
igniter
turbine generating
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
Application number
CN201822152182.0U
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Chinese (zh)
Inventor
周涛
温志宇
刘春杰
王芳
吕祖强
陈希成
张学健
高明
胡中楷
李娜
宫洵
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.)
Chinese Hangfa Power Technology Engineering Co Ltd Harbin Branch
Original Assignee
Chinese Hangfa Power Technology Engineering Co Ltd Harbin Branch
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
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Application filed by Chinese Hangfa Power Technology Engineering Co Ltd Harbin Branch filed Critical Chinese Hangfa Power Technology Engineering Co Ltd Harbin Branch
Priority to CN201822152182.0U priority Critical patent/CN209340039U/en
Application granted granted Critical
Publication of CN209340039U publication Critical patent/CN209340039U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

A kind of Gas Turbine Generating Units high energy ignition unit.Currently, startup of unit curve is solidificated in combustion engine controller, the environment temperature that is adaptable to when being debugged in factory and atmospheric pressure, therefore in actual operation, often there is the phenomenon that fuel gas temperature overtemperature after winter speed hang-up and summer turbine.A kind of Gas Turbine Generating Units high energy ignition unit, its composition includes: igniter (1), firing cable (2) and semiconductor discharge plug (3), the connection of one end of igniter and firing cable, the other end of firing cable is connect with semiconductor discharge plug, igniter is DHZ-72A low pressure point firearm, and semiconductor discharge plug is BDZ-53F sparking plug.The utility model is applied to Gas Turbine Generating Units high energy ignition unit.

Description

A kind of Gas Turbine Generating Units high energy ignition unit
Technical field
The utility model relates to a kind of Gas Turbine Generating Units high energy ignition units.
Background technique
Currently, the combustion engine unit for production is mainly used for emergency power generation, starts band and carry speed and start success rate It is the performance indicator extremely paid close attention to using side.In generating set starting process, after lighting a fire successfully, fire at different ambient temperatures Fuel delivery needed for machine is different, and still, startup of unit curve is solidificated in combustion engine controller, is adaptable to adjust in factory Environment temperature and atmospheric pressure when examination, therefore in actual operation, after often there is winter speed hang-up and summer turbine The phenomenon that fuel gas temperature overtemperature, influences startup of unit success rate.In order to better adapt to market needs, it is necessary to improve startup of unit Success rate, can input for safety emergency in the in case of emergency shortest time.
Utility model content
The purpose of the utility model is to provide a kind of Gas Turbine Generating Units high energy ignition units.
Above-mentioned purpose is realized by following technical scheme:
A kind of Gas Turbine Generating Units high energy ignition unit, composition includes: igniter, firing cable and semiconductor Sparking plug, it is characterized in that: the igniter is connect with one end of the firing cable, the other end of the firing cable It is connect with the semiconductor discharge plug, the igniter DHZ-72A is low pressure point firearm, and the semiconductor discharge plug is BDZ-53F sparking plug.
The Gas Turbine Generating Units high energy ignition unit, the semiconductor discharge plug is interior to be arranged combuster, institute There is light diesel fuel, the ignition end and insulator joint of the semiconductor discharge plug are to use semiconductor in the combustion chamber stated Material wraps up central electrode, and the semiconductor material is filled between central electrode and shell.
The Gas Turbine Generating Units high energy ignition unit, the semiconductor discharge plug material are titanium dioxide.
The utility model beneficial effect achieved is:
1. the utility model can better adapt to market needs, unit starting success rate is improved, it can be urgent In the case of input for safety emergency in the shortest time.The utility model has single spark energy height, surface carbon deposit and tide The wet influence very little that arc discharge is formed to semiconductor surface, and in discharge process, carbon deposit will be burned off, and humidity also will be automatic The advantages that removing, not will lead to spark energy decline.
2. the utility model generates spark using the high electric field pulse of igniter, indoor fuel (the light bavin of burning is lighted Oil).The DH-7 ignition coil used originally is replaced to add SDZ-2A erosion igniter igniting system with low pressure point firearm with semiconductor discharge plug System.The advantages of this improvement is to engine original design change amount minimum, and igniter is constant, and startup program is constant.Pass through improvement Ignition system, ignition energy greatly improve, and other parameters and program are constant.The improved single spark energy of ignition system reaches 1J or more is far longer than the spark energy of original system.
Detailed description of the invention
Attached drawing is used to provide a further understanding of the present invention, and constitutes part of specification, practical with this Novel embodiment is used to explain the utility model together, does not constitute limitations of the present invention.In the accompanying drawings:
Attached drawing 1 is the igniter interface diagram of the utility model.
Attached drawing 2 is the appearance schematic diagram of the semiconductor body sparking plug of the utility model.
Attached drawing 3 is the top view of attached drawing 2.
In figure: 1, igniter, 2, firing cable, 3, semiconductor discharge plug.
Specific embodiment
It is illustrated below in conjunction with preferred embodiment of the attached drawing to the utility model, it should be understood that described herein excellent It selects embodiment to be only used for describing and explaining the present invention, is not used to limit the utility model.
Embodiment 1:
A kind of Gas Turbine Generating Units high energy ignition unit, composition include: igniter 1, firing cable 2 and partly lead Body sparking plug 3, the igniter are connect with one end of the firing cable, the other end of the firing cable with it is described Semiconductor discharge plug connection, the igniter DHZ-72A low pressure point firearm, the semiconductor discharge plug be BDZ-53F electricity Mouth.
Embodiment 2:
According to Gas Turbine Generating Units high energy ignition unit described in embodiment 1, it is arranged in the semiconductor discharge plug Combuster has light diesel fuel in the combustion chamber, and the ignition end of the semiconductor discharge plug connects with insulator Place is to be wrapped up central electrode with semiconductor material, and the semiconductor material is filled between central electrode and shell.
Embodiment 3:
The Gas Turbine Generating Units high energy ignition unit according to embodiment 1 or 2, the semiconductor discharge plug material For titanium dioxide.
Embodiment 4:
Ignition system matches low pressure point firearm using semiconductor discharge plug.The reason of selecting semiconductor discharge plug is semiconductor The breakdown voltage of sparking plug is lower, is usually no more than 1000V, and breakdown voltage is unrelated with air pressure, spark energy is not with air pressure Change and change.Semiconductor discharge plug does not have spark gap, and ignition end and insulator joint are with semiconductor material (two Titanium oxide TiO2) central electrode is encased, electric discharge is carried out along semiconductor surface.Semiconductor material is filled in central electrode and shell It is very close to each other for sealing between body, between them.Since semiconductor adulterates more, electricity close to sparking plug ignition end surface portion Subnumber amount is big, and when two electrodes of sparking plug add voltage, semiconductor surface will have larger current to flow through, to make sparking plug table Face fever, heat decline the resistivity of semiconductor, further increase electric current, and sparking plug surface temperature further increases, thus So that semiconductor surface is generated hot dissociation, generates arcing events, this electric discharge along semiconductor surface between final electrode Phenomenon is formed in the steam ionosphere by semiconductor surface, is not the punch-through of the air gap.Semiconductor discharge plug is hit It is very low to wear voltage, without specific rated value.The experiment proved that: it is existing that 55V can just make the surface of semiconductor discharge plug generate electric discharge As.If applied voltage reaches 800~2000V, semiconductor discharge plug electric discharge is exceedingly fast.

Claims (3)

1. a kind of Gas Turbine Generating Units high energy ignition unit, composition includes: igniter, firing cable and semi-conductor electricity Mouth, it is characterized in that: the igniter is connect with one end of the firing cable, the other end of the firing cable with The semiconductor discharge plug connection, the igniter DHZ-72A are low pressure point firearm, and the semiconductor discharge plug is BDZ- 53F sparking plug.
2. Gas Turbine Generating Units high energy ignition unit according to claim 1, it is characterized in that: the semi-conductor electricity Combuster is set in mouth, there is light diesel fuel in the combustion chamber, the ignition end of the semiconductor discharge plug with it is exhausted Edge body joint is to be wrapped up central electrode with semiconductor material, the semiconductor material be filled in central electrode and shell it Between.
3. Gas Turbine Generating Units high energy ignition unit according to claim 1, it is characterized in that: the semi-conductor electricity Mouth material is titanium dioxide.
CN201822152182.0U 2018-12-18 2018-12-18 A kind of Gas Turbine Generating Units high energy ignition unit Expired - Fee Related CN209340039U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201822152182.0U CN209340039U (en) 2018-12-18 2018-12-18 A kind of Gas Turbine Generating Units high energy ignition unit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201822152182.0U CN209340039U (en) 2018-12-18 2018-12-18 A kind of Gas Turbine Generating Units high energy ignition unit

Publications (1)

Publication Number Publication Date
CN209340039U true CN209340039U (en) 2019-09-03

Family

ID=67758024

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201822152182.0U Expired - Fee Related CN209340039U (en) 2018-12-18 2018-12-18 A kind of Gas Turbine Generating Units high energy ignition unit

Country Status (1)

Country Link
CN (1) CN209340039U (en)

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20190903

Termination date: 20201218

CF01 Termination of patent right due to non-payment of annual fee