CN114837908B - Ignition circuit of semiconductor spark plug for micro electric thruster - Google Patents
Ignition circuit of semiconductor spark plug for micro electric thruster Download PDFInfo
- Publication number
- CN114837908B CN114837908B CN202210479341.6A CN202210479341A CN114837908B CN 114837908 B CN114837908 B CN 114837908B CN 202210479341 A CN202210479341 A CN 202210479341A CN 114837908 B CN114837908 B CN 114837908B
- Authority
- CN
- China
- Prior art keywords
- network
- voltage
- igbt
- output
- ignition
- 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.)
- Active
Links
- 239000004065 semiconductor Substances 0.000 title claims abstract description 21
- 239000003990 capacitor Substances 0.000 claims abstract description 46
- 238000004146 energy storage Methods 0.000 claims description 32
- 230000001052 transient effect Effects 0.000 claims description 14
- 238000006243 chemical reaction Methods 0.000 claims description 13
- 230000001629 suppression Effects 0.000 claims description 13
- 230000001105 regulatory effect Effects 0.000 claims description 12
- 239000013307 optical fiber Substances 0.000 claims description 7
- 230000000630 rising effect Effects 0.000 claims description 6
- 230000003068 static effect Effects 0.000 claims description 4
- 230000000295 complement effect Effects 0.000 claims description 3
- 230000000087 stabilizing effect Effects 0.000 claims 1
- 238000013461 design Methods 0.000 abstract description 14
- 108091092878 Microsatellite Proteins 0.000 abstract description 3
- 230000004044 response Effects 0.000 abstract description 3
- 230000009977 dual effect Effects 0.000 abstract description 2
- 230000015556 catabolic process Effects 0.000 description 6
- 238000010438 heat treatment Methods 0.000 description 5
- 230000002457 bidirectional effect Effects 0.000 description 4
- 230000033228 biological regulation Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 238000002474 experimental method Methods 0.000 description 4
- 238000005457 optimization Methods 0.000 description 4
- 238000009834 vaporization Methods 0.000 description 4
- 230000008016 vaporization Effects 0.000 description 4
- 230000008859 change Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000011160 research Methods 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 230000001276 controlling effect Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000005265 energy consumption Methods 0.000 description 2
- 238000001914 filtration Methods 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 101001121408 Homo sapiens L-amino-acid oxidase Proteins 0.000 description 1
- 101000827703 Homo sapiens Polyphosphoinositide phosphatase Proteins 0.000 description 1
- 102100026388 L-amino-acid oxidase Human genes 0.000 description 1
- 102100023591 Polyphosphoinositide phosphatase Human genes 0.000 description 1
- 101100012902 Saccharomyces cerevisiae (strain ATCC 204508 / S288c) FIG2 gene Proteins 0.000 description 1
- 101100233916 Saccharomyces cerevisiae (strain ATCC 204508 / S288c) KAR5 gene Proteins 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H1/00—Using plasma to produce a reactive propulsive thrust
- F03H1/0087—Electro-dynamic thrusters, e.g. pulsed plasma thrusters
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H1/00—Using plasma to produce a reactive propulsive thrust
- F03H1/0006—Details applicable to different types of plasma thrusters
-
- H—ELECTRICITY
- H03—ELECTRONIC CIRCUITRY
- H03K—PULSE TECHNIQUE
- H03K17/00—Electronic switching or gating, i.e. not by contact-making and –breaking
- H03K17/51—Electronic switching or gating, i.e. not by contact-making and –breaking characterised by the components used
- H03K17/56—Electronic switching or gating, i.e. not by contact-making and –breaking characterised by the components used by the use, as active elements, of semiconductor devices
- H03K17/567—Circuits characterised by the use of more than one type of semiconductor device, e.g. BIMOS, composite devices such as IGBT
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B70/00—Technologies for an efficient end-user side electric power management and consumption
- Y02B70/10—Technologies improving the efficiency by using switched-mode power supplies [SMPS], i.e. efficient power electronics conversion e.g. power factor correction or reduction of losses in power supplies or efficient standby modes
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Dc-Dc Converters (AREA)
- Ignition Installations For Internal Combustion Engines (AREA)
Abstract
本发明属于微小卫星电推进技术领域,具体为一种微型电推进器半导体火花塞的点火电路。本发明的点火电路采用电容直接输出设计,无输出变压器,能有效提高点火能量效率。实施例的实验结果显示,相同工况下,本发明的点火电路比变压器点火电路的点火能量效率增加数倍。输出网络的简化使得点火电路体积减小,重量减轻。采用双闭环控制系统和PID控制器,提高了电源的稳态电压精度和电压响应速率,使输出电压更加精密,提升了负载调整能力;采用输出电压上升速率控制设计,可优化火花塞点火电路能量效率。
The present invention belongs to the technical field of micro-satellite electric propulsion, and specifically is an ignition circuit for a semiconductor spark plug of a micro electric thruster. The ignition circuit of the present invention adopts a capacitor direct output design without an output transformer, which can effectively improve the ignition energy efficiency. The experimental results of the embodiment show that under the same working conditions, the ignition energy efficiency of the ignition circuit of the present invention is several times higher than that of the transformer ignition circuit. The simplification of the output network reduces the size and weight of the ignition circuit. The use of a dual closed-loop control system and a PID controller improves the steady-state voltage accuracy and voltage response rate of the power supply, makes the output voltage more precise, and enhances the load adjustment capability; the output voltage rise rate control design can optimize the energy efficiency of the spark plug ignition circuit.
Description
技术领域Technical Field
本发明属于微小卫星电推进技术领域,具体为一种微型电推进器半导体火花塞的点火电路。The invention belongs to the technical field of micro-satellite electric propulsion, and in particular relates to an ignition circuit of a semiconductor spark plug of a micro electric propulsion device.
背景技术Background Art
脉冲等离子体推进器(Pulsed Plasma Thruster,PPT)因其结构简单、体积小、重量轻、功率低、高比冲、推力小等特点,已成功应用于卫星姿态与轨道控制以及微小卫星主推进系统中,用以执行控制精度较高的空间推进任务。其中,半导体火花塞用作PPT放电的点火器,具有结构简单、可控性强、成本低等优点,目前已成为PPT的首选启动方式。火花塞的点火电路是PPT的关键组成部分,直接决定火花塞的点火稳定性及寿命,进而影响PPT的性能稳定性与寿命。Pulsed Plasma Thruster (PPT) has been successfully applied to satellite attitude and orbit control and microsatellite main propulsion system due to its simple structure, small size, light weight, low power, high specific impulse and low thrust, to perform space propulsion tasks with high control accuracy. Among them, semiconductor spark plug is used as the igniter of PPT discharge, which has the advantages of simple structure, strong controllability and low cost, and has become the preferred starting method of PPT. The ignition circuit of the spark plug is a key component of PPT, which directly determines the ignition stability and life of the spark plug, and thus affects the performance stability and life of PPT.
目前,PPT系统的火花塞点火多采脉冲变压器输出驱动[鲁文涛.基于脉冲等离子体源的航天器表面电位主动控制的研究[D].中国科学院研究生院(空间科学与应用研究中心),2010]和复合驱动[胡宗森.40J脉冲等离子体推力器(PPT)性能研究[D];中国发明专利CN 107725297 A]等技术路线。其中,脉冲变压器输出驱动点火是利用脉冲变压器实现输出的二次升压,将电容能量释放到火花塞上,使火花塞击穿完成点火;复合驱动点火是利用二极管单向导通特性,在脉冲变压器输出驱动点火的基础上增加续流电容,用以提高火花塞点火能量。上述两种点火电路设计虽然均能有效点火,但是存在一些共同的缺陷:At present, the spark plug ignition of the PPT system mainly adopts pulse transformer output drive [Lu Wentao. Research on active control of spacecraft surface potential based on pulse plasma source [D]. Graduate School of the Chinese Academy of Sciences (Space Science and Application Research Center), 2010] and composite drive [Hu Zongsen. Research on the performance of 40J pulsed plasma thruster (PPT) [D]; Chinese invention patent CN 107725297 A] and other technical routes. Among them, pulse transformer output drive ignition uses the pulse transformer to achieve secondary boost of the output, release the capacitor energy to the spark plug, and make the spark plug breakdown to complete ignition; composite drive ignition uses the unidirectional conduction characteristics of the diode to add a freewheeling capacitor on the basis of the pulse transformer output drive ignition to increase the spark plug ignition energy. Although the above two ignition circuit designs can effectively ignite, they have some common defects:
1、能量转换效率低。上述两种设计均采用两组变压器,第一组变压器用于将星载直流低压变换为直流高压为电容充电,第二组变压器用于二次升压,将电容能量释放到火花塞上,由于变压器存在漏磁和磁饱和问题,使用变压器越多,能量转换效率越低,并且体积和重量难以轻小化,不利于星载应用。1. Low energy conversion efficiency. Both designs above use two sets of transformers. The first set of transformers is used to convert the satellite-borne DC low voltage into DC high voltage to charge the capacitor, and the second set of transformers is used for secondary boosting to release the capacitor energy to the spark plug. Due to the leakage and magnetic saturation problems of transformers, the more transformers are used, the lower the energy conversion efficiency, and the volume and weight are difficult to be minimized, which is not conducive to satellite-borne applications.
2、输出电压脉冲的上升速率不可控。火花塞的放电包括两个阶段:半导体膜加热气化和气化团的击穿导通。电压上升速率影响火花塞注入能量在气化和击穿阶段之间的分配,不合理分配会降低火花塞能量效率。如果电压上升速率不可控,制约火花塞能量效率的进一步优化。2. The rising rate of the output voltage pulse is uncontrollable. The discharge of the spark plug includes two stages: heating and vaporization of the semiconductor film and breakdown and conduction of the vaporized group. The voltage rising rate affects the distribution of the spark plug injected energy between the vaporization and breakdown stages. Unreasonable distribution will reduce the energy efficiency of the spark plug. If the voltage rising rate is uncontrollable, it will restrict the further optimization of the spark plug energy efficiency.
3、输出稳态精度和负载调整能力不足。火花塞作为驱动电源的负载,放电较复杂,要求驱动电源具备很强的负载调整能力且输出电压稳定。现有设计中采用电压负反馈设计应对此要求,即单闭环电压负反馈,反馈量取自输出电压,但是火花塞电流变化比电压变化迅速,电压负反馈对负载变动响应慢,不如电流反馈及时迅速,导致电源输出稳态精度和负载调整能力不足。另外,电路的电压噪声分量会引起系统增益和相位的变化,若没有相应补偿网络,会导致电路振荡,所以点火电路的抗干扰性不理想。3. Insufficient output steady-state accuracy and load adjustment capability. As the load of the driving power supply, the spark plug has a complex discharge, which requires the driving power supply to have a strong load adjustment capability and a stable output voltage. The existing design adopts a voltage negative feedback design to meet this requirement, that is, a single closed-loop voltage negative feedback, and the feedback amount is taken from the output voltage. However, the spark plug current changes faster than the voltage change, and the voltage negative feedback responds slowly to load changes, which is not as timely and rapid as the current feedback, resulting in insufficient steady-state accuracy and load adjustment capability of the power supply output. In addition, the voltage noise component of the circuit will cause changes in the system gain and phase. If there is no corresponding compensation network, it will cause circuit oscillation, so the anti-interference performance of the ignition circuit is not ideal.
发明内容Summary of the invention
本发明目的是针对上述三个方面的设计缺陷,设计了一种重量轻、点火能量转换效率可优化、负载调整率低的高能效精密半导体火花塞点火电路。The purpose of the present invention is to design a high-efficiency precision semiconductor spark plug ignition circuit with light weight, optimized ignition energy conversion efficiency and low load regulation rate in response to the design defects in the above three aspects.
本发明采用如下技术方案:The present invention adopts the following technical solution:
一种微型电推进器半导体火花塞的点火电路,包括:升压单元1、调节控制单元2、点火输出单元3、IGBT驱动及控制单元4和低压供电单元5;升压单元1将星载直流低压VS转换为直流高压,对点火输出单元3中的储能电容充电;调节控制单元2实现精确调节和快速稳定储能电容的充电电压,并且具有过压、过流和短路保护功能;点火输出单元3使半导体火花塞SP的储能电容容量可调;IGBT驱动及控制单元4根据外触发信号ET控制点火输出单元3中IGBT导通与关断以及输出电压脉冲的上升速率;低压供电单元5为整个电路低压供电。An ignition circuit for a semiconductor spark plug of a micro electric thruster comprises: a boost unit 1, a regulating control unit 2, an ignition output unit 3, an IGBT drive and control unit 4 and a low-voltage power supply unit 5; the boost unit 1 converts a satellite-borne DC low voltage VS into a DC high voltage to charge an energy storage capacitor in the ignition output unit 3; the regulating control unit 2 realizes accurate regulation and rapid stabilization of the charging voltage of the energy storage capacitor, and has overvoltage, overcurrent and short-circuit protection functions; the ignition output unit 3 makes the energy storage capacitor capacity of the semiconductor spark plug SP adjustable; the IGBT drive and control unit 4 controls the on and off of the IGBT in the ignition output unit 3 and the rising rate of the output voltage pulse according to an external trigger signal ET; the low-voltage power supply unit 5 supplies low-voltage power to the entire circuit.
所述升压单元1,包括输入滤波与保护网络11、推挽式逆变网络12和全波倍压整流滤波网络13。其中,所述输入滤波与保护网络11的输入端连接星载直流低压VS,输出端连接推挽式逆变网络12,防止输入端故障时对其他单元造成损坏;所述推挽式逆变网络12的输入端与输入滤波与保护网络11以及PWM控制网络21连接,输出端与全波倍压整流滤波网络13和电流反馈网络22连接,通过功率管的不断交替导通与关断,将星载直流低压VS逆变为方波交流电压,经高频变压器升为高频交流方波;所述全波倍压整流滤波网络13输出端连接储能电容调节网络31,将高频交流方波变为可调直流高压输出。The boost unit 1 includes an input filter and protection network 11, a push-pull inverter network 12 and a full-wave voltage doubler rectifier filter network 13. The input end of the input filter and protection network 11 is connected to the satellite-borne DC low voltage VS, and the output end is connected to the push-pull inverter network 12 to prevent damage to other units when the input end fails; the input end of the push-pull inverter network 12 is connected to the input filter and protection network 11 and the PWM control network 21, and the output end is connected to the full-wave voltage doubler rectifier filter network 13 and the current feedback network 22. Through the continuous alternating conduction and shutdown of the power tube, the satellite-borne DC low voltage VS is inverted into a square wave AC voltage, which is then boosted to a high-frequency AC square wave through a high-frequency transformer; the output end of the full-wave voltage doubler rectifier filter network 13 is connected to the energy storage capacitor adjustment network 31 to convert the high-frequency AC square wave into an adjustable DC high-voltage output.
所述调节控制单元2,包括PWM控制网络21、电流反馈网络22、电压反馈网络23和过流保护网络24。其中,所述PWM控制网络21的输入端与电流反馈网络22、电压反馈网络23、过流保护网络24以及低压供电单元5连接,输出端与推挽式逆变网络12连接;所述PWM控制网络21将所述电流反馈网络22和所述电压反馈网络23的反馈信号与设定电压值进行比较调制,输出互补对称的PWM脉冲信号,驱动并控制所述推挽式逆变网络12中功率管的导通与关断,使升压单元1输出稳定的直流高压。所述电压反馈网络23的输入端连接储能电容调节网络31,所述电流反馈网络22的输入端连接推挽式逆变网络12。所述电流反馈网络22与所述电压反馈网络23构成双闭环控制系统,其中,所述推挽式逆变网络12、所述电流反馈网络22与所述PWM控制网络21形成第一闭合回路,作为双闭环控制系统的内环,使系统能够快速调整负载扰动的影响;所述推挽式逆变网络12、所述全波倍压整流滤波网络13、所述电压反馈网络23与所述PWM控制网络21形成第二闭合回路,作为双闭环控制系统的外环,提高输出电压的稳定性。并且所述电流反馈网络22和所述电压反馈网络23均采用PID控制器对电压误差进行调节补偿,用以提高电路抗干扰性;所述过流保护网络24输入端连接全波倍压整流滤波网络13,当检测电流超过设定值时,封锁所述PWM控制网络21的脉冲输出,使电路停止工作,对电路起到过流保护作用。The regulating control unit 2 includes a PWM control network 21, a current feedback network 22, a voltage feedback network 23 and an overcurrent protection network 24. The input end of the PWM control network 21 is connected to the current feedback network 22, the voltage feedback network 23, the overcurrent protection network 24 and the low-voltage power supply unit 5, and the output end is connected to the push-pull inverter network 12; the PWM control network 21 compares and modulates the feedback signals of the current feedback network 22 and the voltage feedback network 23 with the set voltage value, outputs a complementary and symmetrical PWM pulse signal, drives and controls the conduction and shutdown of the power tube in the push-pull inverter network 12, so that the boost unit 1 outputs a stable DC high voltage. The input end of the voltage feedback network 23 is connected to the energy storage capacitor regulating network 31, and the input end of the current feedback network 22 is connected to the push-pull inverter network 12. The current feedback network 22 and the voltage feedback network 23 constitute a double closed-loop control system, wherein the push-pull inverter network 12, the current feedback network 22 and the PWM control network 21 form a first closed loop, which serves as the inner loop of the double closed-loop control system, so that the system can quickly adjust the influence of load disturbance; the push-pull inverter network 12, the full-wave voltage doubler rectifier filter network 13, the voltage feedback network 23 and the PWM control network 21 form a second closed loop, which serves as the outer loop of the double closed-loop control system, so as to improve the stability of the output voltage. In addition, the current feedback network 22 and the voltage feedback network 23 both use PID controllers to adjust and compensate the voltage error, so as to improve the anti-interference performance of the circuit; the input end of the overcurrent protection network 24 is connected to the full-wave voltage doubler rectifier filter network 13, and when the detected current exceeds the set value, the pulse output of the PWM control network 21 is blocked, so that the circuit stops working, and the circuit plays an overcurrent protection role.
所述点火输出单元3,包括储能电容调节网络31、IGBT串联网络32、IGBT均压网络33和瞬态干扰抑制网络34。其中,所述储能电容调节网络31的输入端连接全波倍压整流滤波网络13,输出端连接IGBT串联网络32,使储能电容容量可调;所述IGBT串联网络32的输入端与储能电容调节网络31、IGBT均压网络33和电压上升速率控制网络43连接,输出端与瞬态干扰抑制网络34,通过接收IGBT驱动及控制单元4中的外触发信号ET来控制火花塞点火;所述IGBT串联网络32中采用双管IGBT串联来实现单管IGBT功能;所述IGBT均压网络33用于解决双管IGBT串联中静态和动态均压问题;所述瞬态干扰抑制网络34的输出端连接火花塞,用于抑制火花塞点火反向电压,并吸收过电压浪涌。The ignition output unit 3 includes an energy storage capacitor adjustment network 31, an IGBT series network 32, an IGBT voltage balancing network 33 and a transient interference suppression network 34. The input end of the energy storage capacitor adjustment network 31 is connected to the full-wave voltage doubler rectifier filter network 13, and the output end is connected to the IGBT series network 32, so that the energy storage capacitor capacity is adjustable; the input end of the IGBT series network 32 is connected to the energy storage capacitor adjustment network 31, the IGBT voltage balancing network 33 and the voltage rise rate control network 43, and the output end is connected to the transient interference suppression network 34, and the spark plug ignition is controlled by receiving the external trigger signal ET in the IGBT drive and control unit 4; the IGBT series network 32 adopts a double-tube IGBT series connection to realize the single-tube IGBT function; the IGBT voltage balancing network 33 is used to solve the static and dynamic voltage balancing problems in the double-tube IGBT series connection; the output end of the transient interference suppression network 34 is connected to the spark plug, which is used to suppress the spark plug ignition reverse voltage and absorb overvoltage surges.
所述IGBT驱动及控制单元4,包括光纤输入网络41、IGBT驱动及保护网络42和电压上升速率调节网络43。其中,光纤输入网络41的输入端连接外触发信号ET,输出端连接IGBT驱动及保护网络42;IGBT驱动及保护网络42的输出端连接电压上升速率控制网络43,对IGBT串联网络32中的IGBT进行驱动与保护;电压上升速率控制网络43的输出端连接IGBT串联网络32,通过改变IGBT串联网络32中IGBT的导通速率来控制输出电压脉冲上升速率,实现火花塞点火能量转换效率的优化。The IGBT drive and control unit 4 includes an optical fiber input network 41, an IGBT drive and protection network 42, and a voltage rise rate adjustment network 43. The input end of the optical fiber input network 41 is connected to the external trigger signal ET, and the output end is connected to the IGBT drive and protection network 42; the output end of the IGBT drive and protection network 42 is connected to the voltage rise rate control network 43 to drive and protect the IGBT in the IGBT series network 32; the output end of the voltage rise rate control network 43 is connected to the IGBT series network 32, and the output voltage pulse rise rate is controlled by changing the conduction rate of the IGBT in the IGBT series network 32, so as to optimize the spark plug ignition energy conversion efficiency.
所述低压供电单元5的输入端连接星载直流低压VS,输出端分别与PWM控制网络21和IGBT驱动及保护网络42连接,为火花塞点火电路低压供电。The input end of the low-voltage power supply unit 5 is connected to the satellite-borne DC low voltage VS, and the output end is respectively connected to the PWM control network 21 and the IGBT drive and protection network 42 to provide low-voltage power to the spark plug ignition circuit.
与现有技术相比,本发明有益效果:Compared with the prior art, the present invention has the following beneficial effects:
本发明的点火电路采用电容直接输出设计,无输出变压器,能有效提高点火能量效率。实施例的实验结果显示,相同工况下,本发明的点火电路比变压器点火电路的点火能量效率增加数倍。输出网络的简化使得点火电路体积减小,重量减轻。采用双闭环控制系统和PID控制器,提高了电源的稳态电压精度和电压响应速率,使输出电压更加精密,提升了负载调整能力;采用输出电压上升速率控制设计,可优化火花塞点火电路能量效率。The ignition circuit of the present invention adopts a capacitor direct output design without an output transformer, which can effectively improve the ignition energy efficiency. The experimental results of the embodiment show that under the same working conditions, the ignition energy efficiency of the ignition circuit of the present invention is several times higher than that of the transformer ignition circuit. The simplification of the output network reduces the volume and weight of the ignition circuit. The use of a dual closed-loop control system and a PID controller improves the steady-state voltage accuracy and voltage response rate of the power supply, makes the output voltage more precise, and enhances the load adjustment capability; the output voltage rise rate control design can optimize the energy efficiency of the spark plug ignition circuit.
附图说明BRIEF DESCRIPTION OF THE DRAWINGS
图1是本发明的高能效精密半导体火花塞点火电路的结构框图;FIG1 is a block diagram of a high energy efficiency precision semiconductor spark plug ignition circuit of the present invention;
图2是本发明实施例的IGBT串联网络和电压上升速率控制网络的电路图;2 is a circuit diagram of an IGBT series network and a voltage rise rate control network according to an embodiment of the present invention;
图3是本发明实施例的能量效率与变压器点火电路的能量效率对比;FIG3 is a comparison of the energy efficiency of an embodiment of the present invention and the energy efficiency of a transformer ignition circuit;
图4是本发明实施例点火能量效率随输出电压上升速率的优化特性。FIG. 4 is an optimization characteristic of the ignition energy efficiency with the output voltage rising rate according to an embodiment of the present invention.
图中:In the figure:
1升压单元、2调节控制单元、3点火输出单元、4IGBT驱动及控制单元、5低压供电单元;1 boost unit, 2 regulation control unit, 3 ignition output unit, 4 IGBT drive and control unit, 5 low voltage power supply unit;
11滤波与保护网络、12推挽式逆变网络、13全波倍压整流滤波网络;11 filtering and protection network, 12 push-pull inverter network, 13 full-wave voltage doubler rectifier filtering network;
21PWM控制网络、22电流反馈网络、23电压反馈网络、24过流保护网络;21PWM control network, 22 current feedback network, 23 voltage feedback network, 24 overcurrent protection network;
31储能电容调节网络、32IGBT串联网络、33IGBT均压网络、34瞬态干扰抑制网络;31 energy storage capacitor regulation network, 32 IGBT series network, 33 IGBT voltage balancing network, 34 transient interference suppression network;
41光纤输入网络、42IGBT驱动及保护网络、43电压上升速率控制网络;41 optical fiber input network, 42 IGBT drive and protection network, 43 voltage rise rate control network;
VS星载直流低压、SP半导体火花塞、ET外触发信号。VS onboard DC low voltage, SP semiconductor spark plug, ET external trigger signal.
具体实施方式DETAILED DESCRIPTION
以下结合附图和技术方案,进一步说明本发明的具体实施方式。The specific implementation of the present invention is further described below in conjunction with the accompanying drawings and technical solutions.
本发明具体方案的实施例结构框图如图1所示。本发明的一种微型电推进器半导体火花塞的点火电路主要由升压单元1、调节控制单元2、点火输出单元3、IGBT驱动及控制单元4和低压供电单元5组成。星载直流低压VS(通常为28V)经升压单元1转换为2kV可调直流高压,对点火输出单元3中储能电容充电;外触发信号ET经IGBT驱动控制单元4,控制并驱动点火输出单元3中IGBT的通断,将储能电容能量释放给火花塞,使火花塞点火;其中,调节控制单元2根据电流反馈信号和电压反馈信号与设定电压值进行比较调制,使升压单元1输出稳定直流高压;低压供电单元5为火花塞点火电路低压供电。The structural block diagram of the embodiment of the specific scheme of the present invention is shown in Figure 1. The ignition circuit of a semiconductor spark plug of a micro electric thruster of the present invention is mainly composed of a boost unit 1, a regulating control unit 2, an ignition output unit 3, an IGBT drive and control unit 4 and a low-voltage power supply unit 5. The satellite-borne DC low voltage VS (usually 28V) is converted into a 2kV adjustable DC high voltage by the boost unit 1 to charge the energy storage capacitor in the ignition output unit 3; the external trigger signal ET controls and drives the on and off of the IGBT in the ignition output unit 3 through the IGBT drive control unit 4, releases the energy of the energy storage capacitor to the spark plug, and ignites the spark plug; wherein, the regulating control unit 2 compares and modulates the current feedback signal and the voltage feedback signal with the set voltage value, so that the boost unit 1 outputs a stable DC high voltage; the low-voltage power supply unit 5 supplies low-voltage power to the spark plug ignition circuit.
本实施例的工作原理及功能详细如下:The working principle and functions of this embodiment are as follows:
上述升压单元1,包括输入滤波与保护网络11、推挽式逆变网络12、全波倍压整流滤波网络13。其中,输入滤波与保护网络11输入端连接星载直流低压VS,输出端连接推挽式逆变网络12,用于防止输入端故障时对其他单元造成损坏;推挽式逆变网络12的输入端分别和输入滤波与保护网络11、PWM控制网络21连接,输出端分别与全波倍压整流滤波网络13和电流反馈网络22连接,通过PWM控制网络21的输出信号来控制功率管的不断交替导通与关断,将星载直流低压VS逆变为方波交流电压,经高频变压器升为幅值500V的高频交流方波,再经全波倍压整流滤波网络13变为2kV可调直流高压输出;全波倍压整流滤波网络13输出端连接储能电容调节网络31,为储能电容调节网络31中储能电容提供稳定的直流高压。本发明采用全波倍压整流,相较于中国发明专利CN 107769582B中的对称倍压整流,减小了关键整流器件的电应力和绝缘防护难度,提高了电路的可靠性,降低了输出电压纹波。The boost unit 1 includes an input filter and protection network 11, a push-pull inverter network 12, and a full-wave voltage doubler rectifier filter network 13. The input end of the input filter and protection network 11 is connected to the satellite-borne DC low voltage VS, and the output end is connected to the push-pull inverter network 12, so as to prevent damage to other units when the input end fails; the input end of the push-pull inverter network 12 is respectively connected to the input filter and protection network 11 and the PWM control network 21, and the output end is respectively connected to the full-wave voltage doubler rectifier filter network 13 and the current feedback network 22, and the output signal of the PWM control network 21 is used to control the continuous alternating conduction and shutdown of the power tube, and the satellite-borne DC low voltage VS is inverted into a square wave AC voltage, which is then increased to a high-frequency AC square wave with an amplitude of 500V by a high-frequency transformer, and then converted into a 2kV adjustable DC high voltage output by the full-wave voltage doubler rectifier filter network 13; the output end of the full-wave voltage doubler rectifier filter network 13 is connected to the energy storage capacitor adjustment network 31, and a stable DC high voltage is provided for the energy storage capacitor in the energy storage capacitor adjustment network 31. The present invention adopts full-wave voltage doubler rectification, which reduces the electrical stress and insulation protection difficulty of key rectifying components, improves the reliability of the circuit, and reduces the output voltage ripple compared to the symmetrical voltage doubler rectification in the Chinese invention patent CN 107769582B.
上述调节控制单元2,包括PWM控制网络21,电流反馈网络22、电压反馈网络23和过流保护网络24。其中,PWM控制网络21的输入端分别与电流反馈网络22、电压反馈网络23、过流保护网络24以及低压供电单元5连接,输出端与推挽式逆变网络12连接,将电流反馈网络22与电压反馈网络23的反馈信号与设定电压值进行比较调制,输出互补对称的PWM脉冲信号,通过调节功率管驱动信号的占空比来调节推挽式逆变网络12中功率管的导通与关断,使升压单元1输出稳定的直流高压;电流反馈网络22的输入端连接推挽式逆变网络12,电压反馈网络23的输入端连接储能电容调节网络31,电流反馈网络22与电压反馈网络23构成双闭环控制系统,其中,所述推挽式逆变网络12、所述电流反馈网络22与PWM控制网络21形成第一闭合回路,作为双闭环控制系统的内环;所述推挽式逆变网络12、所述全波倍压整流网络13、所述电压反馈网络23与所述PWM控制网络21形成第二闭合回路,作为双闭环控制系统的外环。工作原理为:取样电阻对电压取样,与设定电压进行比较得到电压误差,电压反馈外环PID控制器对电压误差进行调节补偿,作为电流反馈内环的基准信号,将该基准信号与电流反馈内环检测到的电流相比较,得到输出电流误差,再由电流反馈内环PID控制器对电流误差调节补偿,进而输出相应的PWM脉冲信号。因火花塞点火电流的变化比电压变化快,电流反馈内环使得系统能够快速调整负载扰动的影响,电压反馈外环则提高了输出电压的稳定性。本发明采用双闭环反馈设计使系统能够快速调整负载扰动的影响,提高了输出电压的稳定性,同时采用PID控制器可有效补偿电路中由于电压噪声分量引起的增益和相位变化,提高电路抗干扰性,使半导体火花塞点火电路输出更加精密。相较于中国发明专利CN101943148A和CN107725297A中的单闭环电压反馈,双闭环反馈设计可以克服单环反馈对负载扰动调整能力不足的问题。过流保护网络24的输入端连接全波倍压整流滤波网络13,当检测电流超过设定值时,封锁PWM控制网络21的脉冲输出,使电路停止工作,对电路起到过流保护作用。The above-mentioned regulating and controlling unit 2 includes a PWM control network 21, a current feedback network 22, a voltage feedback network 23 and an overcurrent protection network 24. The input end of the PWM control network 21 is respectively connected to the current feedback network 22, the voltage feedback network 23, the overcurrent protection network 24 and the low-voltage power supply unit 5, and the output end is connected to the push-pull inverter network 12, and the feedback signals of the current feedback network 22 and the voltage feedback network 23 are compared and modulated with the set voltage value, and a complementary and symmetrical PWM pulse signal is output, and the conduction and shutdown of the power tube in the push-pull inverter network 12 are adjusted by adjusting the duty cycle of the power tube drive signal, so that the boost unit 1 outputs a stable DC high voltage; the input end of the current feedback network 22 The push-pull inverter network 12 is connected, the input end of the voltage feedback network 23 is connected to the energy storage capacitor adjustment network 31, and the current feedback network 22 and the voltage feedback network 23 form a double closed-loop control system, wherein the push-pull inverter network 12, the current feedback network 22 and the PWM control network 21 form a first closed loop as the inner loop of the double closed-loop control system; the push-pull inverter network 12, the full-wave voltage doubler rectifier network 13, the voltage feedback network 23 and the PWM control network 21 form a second closed loop as the outer loop of the double closed-loop control system. The working principle is: the sampling resistor samples the voltage, compares it with the set voltage to obtain the voltage error, and the voltage feedback outer loop PID controller adjusts and compensates the voltage error as the reference signal of the current feedback inner loop, compares the reference signal with the current detected by the current feedback inner loop, and obtains the output current error, and then the current feedback inner loop PID controller adjusts and compensates the current error, and then outputs the corresponding PWM pulse signal. Because the change of spark plug ignition current is faster than that of voltage, the current feedback inner loop enables the system to quickly adjust the influence of load disturbance, and the voltage feedback outer loop improves the stability of the output voltage. The present invention adopts a double closed-loop feedback design to enable the system to quickly adjust the influence of load disturbance, improve the stability of the output voltage, and at the same time, the PID controller can effectively compensate for the gain and phase changes caused by the voltage noise component in the circuit, improve the anti-interference of the circuit, and make the output of the semiconductor spark plug ignition circuit more precise. Compared with the single closed-loop voltage feedback in Chinese invention patents CN101943148A and CN107725297A, the double closed-loop feedback design can overcome the problem of insufficient adjustment ability of single-loop feedback to load disturbance. The input end of the overcurrent protection network 24 is connected to the full-wave voltage doubler rectifier filter network 13. When the detected current exceeds the set value, the pulse output of the PWM control network 21 is blocked, the circuit stops working, and the circuit is protected from overcurrent.
上述点火输出单元3,包括储能电容调节网络31、IGBT串联网络32、IGBT均压网络33、瞬态干扰抑制网络34。其中,储能电容调节网络31的输入端连接全波倍压整流滤波网络13,输出端连接IGBT串联网络32,用于实现储能电容容量可调;IGBT串联网络32的输入端分别与储能电容调节网络31、IGBT均压网络33和电压上升速率控制网络43连接,输出端连接瞬态干扰抑制网络34,通过接收单元4中的外触发信号ET来控制火花塞点火。为了降低点火电路体积,IGBT串联网络32中采用双管IGBT串联来实现单管IGBT功能,本实施例根据实验所用火花塞的标称性能:额定电压1200V,峰值电流200A,点火电路输出电压设计为2000V可调,波动5%、保险系数10%,所需耐压值2400V、电流容量300A的单管IGBT,而300A/2400V的双管IGBT比单管IGBT体积小一倍左右。通过IGBT均压网络33来解决串联IGBT的静态和动态均压问题;瞬态干扰抑制网络34的输出端连接火花塞,用于抑制火花塞点火反向电压,并吸收过电压浪涌。该单元无输出脉冲变压器,而是电容直接放电设计,减少了由于变压器磁饱和漏磁等问题带来的约40%的能量损耗,提升了电路能量转换效率,并且可减小约25%的体积和35%的重量。本发明以推挽式逆变与倍压整流结合方案替代变压器升压方案,采用电容直接放电设计,将电容储能直接释放于火花塞,相较于《鲁文涛:基于脉冲等离子体源的航天器表面电位主动控制的研究》的点火电路和中国发明专利CN 107725297A的点火电路,取消了二次升压变压器,可减少由于变压器的磁饱和、漏磁等问题带来的能耗,显著提升电路的能量转换效率,同时减小电源体积和重量,有益于星载应用。The above-mentioned ignition output unit 3 includes an energy storage capacitor adjustment network 31, an IGBT series network 32, an IGBT voltage balancing network 33, and a transient interference suppression network 34. Among them, the input end of the energy storage capacitor adjustment network 31 is connected to the full-wave voltage doubler rectifier filter network 13, and the output end is connected to the IGBT series network 32, which is used to realize the adjustable capacity of the energy storage capacitor; the input end of the IGBT series network 32 is respectively connected to the energy storage capacitor adjustment network 31, the IGBT voltage balancing network 33 and the voltage rise rate control network 43, and the output end is connected to the transient interference suppression network 34, and the spark plug ignition is controlled by the external trigger signal ET in the receiving unit 4. In order to reduce the volume of the ignition circuit, the IGBT series network 32 uses a double-tube IGBT in series to realize the function of a single-tube IGBT. This embodiment is based on the nominal performance of the spark plug used in the experiment: rated voltage 1200V, peak current 200A, the ignition circuit output voltage is designed to be 2000V adjustable, fluctuation 5%, insurance factor 10%, the required withstand voltage value is 2400V, the current capacity is 300A, and the double-tube IGBT of 300A/2400V is about half the size of the single-tube IGBT. The static and dynamic voltage equalization problems of the series IGBT are solved by the IGBT voltage equalization network 33; the output end of the transient interference suppression network 34 is connected to the spark plug to suppress the spark plug ignition reverse voltage and absorb overvoltage surges. The unit has no output pulse transformer, but a capacitor direct discharge design, which reduces about 40% of the energy loss caused by problems such as transformer magnetic saturation leakage, improves the circuit energy conversion efficiency, and can reduce about 25% of the volume and 35% of the weight. The present invention replaces the transformer boosting scheme with a push-pull inverter combined with a voltage doubling rectifier scheme, and adopts a capacitor direct discharge design to release the capacitor energy directly to the spark plug. Compared with the ignition circuit of "Lu Wentao: Research on Active Control of Spacecraft Surface Potential Based on Pulsed Plasma Source" and the ignition circuit of Chinese invention patent CN 107725297A, the secondary boosting transformer is cancelled, which can reduce the energy consumption caused by the magnetic saturation and leakage of the transformer, significantly improve the energy conversion efficiency of the circuit, and reduce the size and weight of the power supply at the same time, which is beneficial to spaceborne applications.
上述IGBT驱动控制单元4,包括光纤输入网络41、IGBT驱动及保护网络42、电压上升速率控制网络43。其中,光纤输入网络41的输入端与外部触发信号ET连接,输出端与IGBT驱动及保护网络42连接,用来实现外触发信号的隔离与传输;IGBT驱动及保护网络42的输出端连接电压上升速率控制网络43,对IGBT串联网络32中的IGBT进行驱动与保护;电压上升速率控制网络43的输出端连接IGBT串联网络32,通过改变IGBT串联网络32中IGBT的导通速率来控制输出电压脉冲上升速率,实现火花塞点火能量转换效率的优化。The above-mentioned IGBT drive control unit 4 includes an optical fiber input network 41, an IGBT drive and protection network 42, and a voltage rise rate control network 43. Among them, the input end of the optical fiber input network 41 is connected to the external trigger signal ET, and the output end is connected to the IGBT drive and protection network 42, so as to realize the isolation and transmission of the external trigger signal; the output end of the IGBT drive and protection network 42 is connected to the voltage rise rate control network 43, so as to drive and protect the IGBT in the IGBT series network 32; the output end of the voltage rise rate control network 43 is connected to the IGBT series network 32, and the output voltage pulse rise rate is controlled by changing the conduction rate of the IGBT in the IGBT series network 32, so as to realize the optimization of the spark plug ignition energy conversion efficiency.
在其中一个具体实施例中,IGBT串联网络32和电压上升速率控制网络43的电路图如图2所示。第一IGBT1和第二IGBT2串联组成所述IGBT串联网络32。所述电压上升速率控制网络43包括第一至第二驱动接口(J1、J2)、第一至第四电阻(R1、R2、R4、R5)、第一至第六二极管(D1、D2、D3、D4、D5、D6)、第一至第二可变栅极电阻(VR1、VR2)、第一至第二栅射极电容(CG1、CG2)、第一至第二栅极泄放电阻(R3、R6)、第一至第二双向瞬态电压抑制二极管(TVS1、TVS2)。In one specific embodiment, the circuit diagram of the IGBT series network 32 and the voltage rise rate control network 43 is shown in FIG2 . The first IGBT1 and the second IGBT2 are connected in series to form the IGBT series network 32. The voltage rise rate control network 43 includes the first to second drive interfaces (J1, J2), the first to fourth resistors (R1, R2, R4, R5), the first to sixth diodes (D1, D2, D3, D4, D5, D6), the first to second variable gate resistors (VR1, VR2), the first to second gate emitter capacitors (CG1, CG2), the first to second gate discharge resistors (R3, R6), and the first to second bidirectional transient voltage suppressor diodes (TVS1, TVS2).
其中,第一驱动接口J1的C接口依次与第一电阻R1、第一二极管D1、第二二极管D2串联,再与第一IGBT1的集电极端连接,第一二极管D1和第二二极管D2的方向均指向第一IGBT1集电极端;第一驱动接口J1的G接口依次与第一可变栅极电阻VR1和第二电阻R2串联,再与第一IGBT1的栅极端连接,第三二极管D3并联在第二电阻R2两端,方向指向第一IGBT1的栅极端;第一驱动接口J1的E接口与第一IGBT1的发射极端连接,在靠近第一IGBT1栅极和发射极之间依次并联第一双向瞬态电压抑制二极管TVS1、第一栅极泄放电阻R3、第一栅射极电容CG1。第二驱动接口J2的C接口依次与第三电阻R4、第四二极管D4、第五二极管D5串联,再与第二IGBT2的集电极端连接,第四二极管D4和第五二极管D5的方向均指向第二IGBT2集电极端;第二驱动接口J2的G接口依次与第二可变栅极电阻VR2和第四电阻R5串联,再与第二IGBT2的栅极端连接,第六二极管D6并联在第四电阻R5两端,方向指向第二IGBT2的栅极端;第二驱动接口J2的E接口与第二IGBT2的发射极端连接,在靠近第二IGBT2栅极和发射极之间依次并联第二双向瞬态电压抑制二极管TVS2、第二栅极泄放电阻R6、第二栅射极电容CG2。其中,第一电阻R1和第四电阻R4分别用于减小第一二极管D1、第二二极管D2和第四二极管D4、第五二极管D5上的反向峰值电流,而第一二极管D1、第二二极管(D2)和第四二极管D4、第五二极管D5分别用于抑制第一IGBT1和第二IGBT2集电极上的高压尖峰脉冲;第一和第二双向瞬态电压抑制二极管TVS1、TVS2分别用于抑制第一IGBT1和第二IGBT2正反向峰值电压,防止IGBT电压过冲;第一可变栅极电阻VR2、第一栅射极电容CG1和第二可变栅极电阻VR2、第二栅射极电容CG2分别用于调整第一IGBT1和第二IGBT2的导通速率;第一和第二栅极泄放电阻(R3、R6)分别用于防止第一IGBT1和第二IGBT2栅极被静电击穿;第一驱动接口J1和第二驱动接口J2与所述IGBT驱动保护网络42中IGBT的驱动芯片连接。Among them, the C interface of the first drive interface J1 is connected in series with the first resistor R1, the first diode D1, and the second diode D2 in sequence, and then connected to the collector end of the first IGBT1, and the directions of the first diode D1 and the second diode D2 both point to the collector end of the first IGBT1; the G interface of the first drive interface J1 is connected in series with the first variable gate resistor VR1 and the second resistor R2 in sequence, and then connected to the gate end of the first IGBT1, and the third diode D3 is connected in parallel at both ends of the second resistor R2, and the direction points to the gate end of the first IGBT1; the E interface of the first drive interface J1 is connected to the emitter end of the first IGBT1, and the first bidirectional transient voltage suppression diode TVS1, the first gate discharge resistor R3, and the first gate-emitter capacitor CG1 are connected in parallel in sequence between the gate and emitter of the first IGBT1. The C interface of the second drive interface J2 is connected in series with the third resistor R4, the fourth diode D4, and the fifth diode D5 in sequence, and then connected to the collector end of the second IGBT2. The directions of the fourth diode D4 and the fifth diode D5 both point to the collector end of the second IGBT2; the G interface of the second drive interface J2 is connected in series with the second variable gate resistor VR2 and the fourth resistor R5 in sequence, and then connected to the gate end of the second IGBT2. The sixth diode D6 is connected in parallel at both ends of the fourth resistor R5, and its direction points to the gate end of the second IGBT2; the E interface of the second drive interface J2 is connected to the emitter end of the second IGBT2, and the second bidirectional transient voltage suppression diode TVS2, the second gate discharge resistor R6, and the second gate-emitter capacitor CG2 are connected in parallel in sequence between the gate and emitter of the second IGBT2. Among them, the first resistor R1 and the fourth resistor R4 are respectively used to reduce the reverse peak current on the first diode D1, the second diode D2, the fourth diode D4, and the fifth diode D5, while the first diode D1, the second diode (D2), the fourth diode D4, and the fifth diode D5 are respectively used to suppress the high-voltage spike pulses on the collectors of the first IGBT1 and the second IGBT2; the first and second bidirectional transient voltage suppression diodes TVS1 and TVS2 are respectively used to suppress the forward and reverse peak voltages of the first IGBT1 and the second IGBT2 to prevent IGBT voltage overshoot; the first variable gate resistor VR2, the first gate-emitter capacitor CG1 and the second variable gate resistor VR2 and the second gate-emitter capacitor CG2 are respectively used to adjust the conduction rate of the first IGBT1 and the second IGBT2; the first and second gate discharge resistors (R3, R6) are respectively used to prevent the gates of the first IGBT1 and the second IGBT2 from being broken down by static electricity; the first drive interface J1 and the second drive interface J2 are connected to the IGBT drive chip in the IGBT drive protection network 42.
在IGBT电压上升速率控制网络43中,当第一IGBT1开通时,驱动电流经第一可变栅极电阻VR1和第三二极管D3流向IGBT1的栅极,即栅极电阻Rg=VR1,当第一IGBT1关闭时,由于第三二极管D3的单向导电性,IGBT栅极经第一可变栅极电阻VR1和第二电阻R2放电,即栅极电阻Rg=VR1+R2,这样可以分别控制IGBT1开通和关断的电压变化速率dv/dt,减少IGBT集电极电压的尖脉冲值,从而改善开关过程,减少开关损耗。In the IGBT voltage rise rate control network 43, when the first IGBT1 is turned on, the driving current flows to the gate of IGBT1 through the first variable gate resistor VR1 and the third diode D3, that is, the gate resistor Rg=VR1. When the first IGBT1 is turned off, due to the unidirectional conductivity of the third diode D3, the IGBT gate is discharged through the first variable gate resistor VR1 and the second resistor R2, that is, the gate resistor Rg=VR1+R2. In this way, the voltage change rate dv/dt of the IGBT1 turning on and off can be controlled respectively, and the spike pulse value of the IGBT collector voltage can be reduced, thereby improving the switching process and reducing the switching loss.
通过调节0~20Ω的可变栅极电阻(VR1、VR2)和0~30nF的可变栅射极电容(CG1、CG2),来改变IGBT的导通速率,使火花塞点火电路输出电压脉冲的上升速率在3000~8000V/μs可控。控制输出电压脉冲上升速率对能量转化效率的优化原理是:火花塞的点火过程包括半导体膜的加热气化和气化团的击穿导通两个阶段,施加于火花塞的电压脉冲驱动两个阶段的完成。电压上升速率决定半导体膜的加热气化时长,如果上升速率过快,虽然半导体膜温升速率快,但是由于持续时间短,形成的气化团密度太低,导致击穿困难以及带电粒子不足;如果电压上升速率过慢,会延长加热阶段,过多的加热耗能和散热损耗,降低击穿阶段能量,同样导致带电粒子不足。优化电压上升速率,不仅可以提高点火电路能量转换效率,而且可以提高火花塞点火质量。在IGBT安全的工作区内,选择合适的栅极电阻和栅射极电容,可减小IGBT米勒效应,优化火花塞点火能量转换效率。By adjusting the variable gate resistor (VR1, VR2) of 0-20Ω and the variable gate-emitter capacitor (CG1, CG2) of 0-30nF, the conduction rate of the IGBT is changed, so that the rise rate of the output voltage pulse of the spark plug ignition circuit can be controlled at 3000-8000V/μs. The optimization principle of controlling the rise rate of the output voltage pulse for energy conversion efficiency is: the ignition process of the spark plug includes two stages: heating and vaporization of the semiconductor film and breakdown and conduction of the vaporized group. The voltage pulse applied to the spark plug drives the completion of the two stages. The voltage rise rate determines the heating and vaporization time of the semiconductor film. If the rise rate is too fast, although the semiconductor film temperature rise rate is fast, due to the short duration, the density of the vaporized group formed is too low, resulting in difficulty in breakdown and insufficient charged particles; if the voltage rise rate is too slow, the heating stage will be extended, and excessive heating energy consumption and heat dissipation loss will reduce the energy of the breakdown stage, which will also lead to insufficient charged particles. Optimizing the voltage rise rate can not only improve the energy conversion efficiency of the ignition circuit, but also improve the ignition quality of the spark plug. In the safe working area of IGBT, selecting appropriate gate resistance and gate-emitter capacitance can reduce the IGBT Miller effect and optimize the spark plug ignition energy conversion efficiency.
上述低压供电单元5输入端连接星载电源,输出端分别与上述PWM控制网络21和IGBT驱动保护网络42连接,将星载直流低压VS 28V转换为直流15V和±5V,为火花塞点火电路低压供电。The input end of the low-voltage power supply unit 5 is connected to the satellite power supply, and the output end is connected to the PWM control network 21 and the IGBT drive protection network 42 respectively, converting the satellite DC low voltage VS 28V into DC 15V and ±5V to provide low-voltage power for the spark plug ignition circuit.
实验experiment
实验1,为了测试本发明的半导体火花塞点火电路能量效率,根据变压器输出驱动点火电路和本发明制作了两个应用例。在储能电容0.1μF和较低真空度工况下,使用同一个半导体火花塞对两种点火电路进行对比试验,得到的点火能量随电压的变化曲线如图3所示。Experiment 1, in order to test the energy efficiency of the semiconductor spark plug ignition circuit of the present invention, two application examples were made according to the transformer output drive ignition circuit and the present invention. Under the conditions of energy storage capacitor 0.1μF and lower vacuum degree, the same semiconductor spark plug was used to conduct a comparative test on the two ignition circuits, and the obtained ignition energy versus voltage curve is shown in Figure 3.
由图3可知,相同工况下,本发明点火电路相比于变压器输出驱动点火电路,火花塞点火能量可增加1.6~2.6倍。本发明的点火电路大幅度提高了火花塞的能量转换效率。As shown in Figure 3, under the same working conditions, the ignition circuit of the present invention can increase the spark plug ignition energy by 1.6 to 2.6 times compared with the transformer output drive ignition circuit. The ignition circuit of the present invention greatly improves the energy conversion efficiency of the spark plug.
实验2,为了测试本发明的点火电路对输出电压脉冲上升速率的可控性,在储能电容0.1μF和较低真空度工况下,对点火能量效率随输出电压上升速率的变化进行了测试。Experiment 2, in order to test the controllability of the ignition circuit of the present invention on the output voltage pulse rise rate, the ignition energy efficiency was tested as a function of the output voltage rise rate under the conditions of a 0.1 μF energy storage capacitor and a relatively low vacuum degree.
改变电压上升速率控制网络43中可变栅极电阻值来控制输出电压上升速率。在保障火花塞有效点火前提下,控制栅射极电容不变,调节可变栅极电阻,得到的能量效率随输出电压脉冲上升速率的优化特性曲线如图4所示。The output voltage rise rate is controlled by changing the variable gate resistance value in the voltage rise rate control network 43. Under the premise of ensuring effective ignition of the spark plug, the gate-emitter capacitance is controlled unchanged, and the variable gate resistance is adjusted. The optimized characteristic curve of energy efficiency versus output voltage pulse rise rate is shown in FIG4 .
由图4可知,在相同储能电容量,不同充电电压工况下,半导体火花塞均在栅极电阻Rg=2Ω时实现点火能量最高。可见,电压上升速率控制网络可以优化火花塞的能量分配,使点火电路能量转换效率提高。As shown in Figure 4, under the same energy storage capacity and different charging voltage conditions, the semiconductor spark plug achieves the highest ignition energy when the gate resistance Rg = 2Ω. It can be seen that the voltage rise rate control network can optimize the energy distribution of the spark plug and improve the energy conversion efficiency of the ignition circuit.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210479341.6A CN114837908B (en) | 2022-05-05 | 2022-05-05 | Ignition circuit of semiconductor spark plug for micro electric thruster |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210479341.6A CN114837908B (en) | 2022-05-05 | 2022-05-05 | Ignition circuit of semiconductor spark plug for micro electric thruster |
Publications (2)
Publication Number | Publication Date |
---|---|
CN114837908A CN114837908A (en) | 2022-08-02 |
CN114837908B true CN114837908B (en) | 2024-08-09 |
Family
ID=82568156
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202210479341.6A Active CN114837908B (en) | 2022-05-05 | 2022-05-05 | Ignition circuit of semiconductor spark plug for micro electric thruster |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN114837908B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115383261B (en) * | 2022-09-14 | 2025-03-28 | 新疆大学 | A high-efficiency, low-voltage, micro-arc processing power supply and control method |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102177334A (en) * | 2008-09-09 | 2011-09-07 | 雷诺股份公司 | Device for measuring ionization current in radio frequency ignition systems of internal combustion engines |
CN107725297A (en) * | 2017-11-30 | 2018-02-23 | 中国人民解放军国防科技大学 | Ignition circuit for micro pulse plasma thruster |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5754011A (en) * | 1995-07-14 | 1998-05-19 | Unison Industries Limited Partnership | Method and apparatus for controllably generating sparks in an ignition system or the like |
EP1155485B1 (en) * | 1998-12-23 | 2007-05-09 | Champion Aerospace Inc. | Inductive ignition circuit |
CN108005869B (en) * | 2017-11-30 | 2019-05-03 | 中国人民解放军国防科技大学 | An ignition circuit for semiconductor spark plugs of miniature pulsed plasma thrusters |
-
2022
- 2022-05-05 CN CN202210479341.6A patent/CN114837908B/en active Active
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102177334A (en) * | 2008-09-09 | 2011-09-07 | 雷诺股份公司 | Device for measuring ionization current in radio frequency ignition systems of internal combustion engines |
CN107725297A (en) * | 2017-11-30 | 2018-02-23 | 中国人民解放军国防科技大学 | Ignition circuit for micro pulse plasma thruster |
Also Published As
Publication number | Publication date |
---|---|
CN114837908A (en) | 2022-08-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN109194113B (en) | Power factor corrector with active power decoupling function and control method thereof | |
CN110957922B (en) | Single-stage high-frequency isolated bidirectional DC converter and grid-connected energy storage system | |
CN108183603B (en) | A kind of single-stage is without bridge Sofe Switch resonance isolated form circuit of power factor correction | |
CN112468011B (en) | Voltage-limiting shaping circuit applied to high-voltage microsecond pulse power supply | |
CN114285286B (en) | A single-stage zero-current switching full-bridge step-up DC converter and its control method | |
CN210412978U (en) | High-stability high-current arc welding power supply based on inverter technology | |
CN114583951A (en) | A high-gain converter for photovoltaic DC module and its control method | |
CN114837908B (en) | Ignition circuit of semiconductor spark plug for micro electric thruster | |
CN113884959B (en) | A flat-top wave pulse strong magnetic field generating device and method | |
CN112968451A (en) | Full-power conversion wind turbine generator control system and method with energy storage function | |
CN107681896A (en) | Dual-duty cycle control device for current-mode bridge photovoltaic converter | |
CN110492727A (en) | A kind of driving circuit for IGBT series average-voltage | |
CN113251395A (en) | Steam generator's controlling means based on electromagnetic induction heating technique | |
CN108880263A (en) | The double active bridge inverter control methods of cascade connection type for having soft start function | |
CN110581641B (en) | Device and method for reducing power consumption of linear adjusting tube of parallel linear filter | |
CN109494841B (en) | Main circuit structure of storage battery charging device | |
Luewisuthichat et al. | Analysis and implement DC-DC integrated boost-flyback converter with LED street light stand-by application | |
CN112467983B (en) | A control circuit based on a buck-boost synchronous regulator | |
CN107846156A (en) | A kind of repetition square-topped pulse electric current-producing device of multistage composite structure | |
CN216751538U (en) | A soft switching boost chopper circuit | |
CN108566091B (en) | DC/DC converter and control method thereof | |
CN106026717B (en) | Three-phase rectifier and its control method for high frequency high voltage dc power source | |
CN103269160B (en) | Three-state direct current-direct current converter and control method thereof | |
CN115224923A (en) | Short circuit cut-off control method and device of LLC converter | |
CN207304385U (en) | A kind of single-phase X-type misplacement three-level AC stream regulating circuit |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |