CN115241738B - Gravity-type high-voltage pulse discharge switch for coaxial cylindrical deflagration drive - Google Patents
Gravity-type high-voltage pulse discharge switch for coaxial cylindrical deflagration drive Download PDFInfo
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Abstract
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技术领域technical field
本发明涉及高温高速气体动力学、高速飞行器等实验研究的技术领域,更具体地,涉及一种用于同轴柱面爆燃驱动装置的重力式高压脉冲放电开关。The invention relates to the technical field of high-temperature high-speed gas dynamics, high-speed aircraft and other experimental research, and more specifically, relates to a gravity-type high-voltage pulse discharge switch for a coaxial cylindrical deflagration drive device.
背景技术Background technique
激波管/风洞是一种广泛用于高温高速气体动力学、高速飞行器等领域的实验设备,基本原理是:高压驱动气体通过激波压缩低压试验气体,使之达到所需的试验状态。如图1所示,典型的激波管/风洞包括驱动段1’、被驱动段2’、喷管3’和试验段4’;试验前,驱动段1’与被驱动段2’以膜片5’隔开,在驱动段1’中充入高压的驱动气体,在被驱动段2’中充入低压的试验气体;试验时,膜片5’破裂,高压气体膨胀、进入被驱动段2’,同时在被驱动段2’中产生一道快速运动的激波;若直接采用激波后的气体开展试验,则设备以激波管模式运行;若利用经喷管3’加速后的试验气体开展试验,则设备以激波风洞模式运行。The shock tube/wind tunnel is a kind of experimental equipment widely used in the fields of high-temperature and high-speed aerodynamics, high-speed aircraft, etc. The basic principle is: the high-pressure driving gas compresses the low-pressure test gas through the shock wave to make it reach the required test state. As shown in Figure 1, a typical shock tube/wind tunnel includes a driving section 1', a driven section 2', a nozzle 3' and a test section 4'; before the test, the driving section 1' and the driven section 2' are The diaphragm 5' is separated, and the driving section 1' is filled with high-pressure driving gas, and the driven section 2' is filled with low-pressure test gas; during the test, the diaphragm 5' ruptures, and the high-pressure gas expands and enters the driven section 2'. At the same time, a fast-moving shock wave is generated in the driven section 2'; if the gas after the shock wave is directly used to carry out the test, the equipment operates in the shock tube mode; if the gas accelerated by the nozzle 3' is used The test gas is used to carry out the test, and the equipment operates in the shock tunnel mode.
试验气体的总温、总压范围是衡量设备能力的主要指标,二者取决于高压驱动气体的驱动能力。常温高压气体已无法满足日益苛刻的试验需求,为此,国内外已发展出三种高性能的驱动技术:活塞驱动、加热轻气体驱动以及爆轰驱动。其中,爆轰驱动技术具有成本低、结构简单而且较为安全等特点,是目前国内的主流技术。The total temperature and total pressure range of the test gas are the main indicators to measure the capability of the equipment, both of which depend on the driving ability of the high-pressure driving gas. Normal temperature and high pressure gas can no longer meet the increasingly demanding test requirements. Therefore, three high-performance drive technologies have been developed at home and abroad: piston drive, heated light gas drive and detonation drive. Among them, the detonation drive technology has the characteristics of low cost, simple structure and relatively safe, and is currently the mainstream technology in China.
爆轰驱动激波管是由Bird在1957年首先提出的。中国科学院力学研究所的俞鸿儒先生在1981年建造了一个13.3m长的爆轰驱动激波管,1983年投入使用。中国科学院力学研究所于1994年研制了JF-10爆轰驱动高焓激波风洞【参见俞鸿儒、赵伟、袁生学的氢氧爆轰驱动激波风洞的性能-气动试验与测量控制,1993,7(3):38-42】。在俞鸿儒先生的帮助下Gronig等人于1993年在德国亚琛工业大学建造了应用反向爆轰驱动的高焓激波风洞(TH2-D)。1994年,NASA修改原来的自由活塞驱动的设计方案,在GASL建成建设了正向爆轰驱动高焓激波风洞(HYPULSE),该风洞同时可以工作于反射激波风洞模式和膨胀管模式【参见ChueRSM,Tsai C-Y,Bakos RJ,Erdos JI,Rogers RC(2002)NASA’s HYPULSE Facility atGASL-ADual Mode,Dual Driver Reflected-Shock/Expansion Tunnel.In:Lu F,Marren D(eds),Advanced Hypersonic Test Facilities,Progress in Astronautics andAeronautics,Vol.198,AIAA,Chapter 3,pp29-71】。The detonation-driven shock tube was first proposed by Bird in 1957. Mr. Yu Hongru from the Institute of Mechanics, Chinese Academy of Sciences built a 13.3m long detonation-driven shock tube in 1981 and put it into use in 1983. The Institute of Mechanics of the Chinese Academy of Sciences developed the JF-10 detonation-driven high-enthalpy shock tunnel in 1994 [see Yu Hongru, Zhao Wei, Yuan Shengxue, Performance of Hydrogen-Oxygen Detonation-Driven Shock Tunnel - Aerodynamic Test and Measurement Control, 1993, 7(3):38-42]. With the help of Mr. Yu Hongru, Gronig and others built a high-enthalpy shock tunnel (TH2-D) driven by reverse detonation at RWTH Aachen University in Germany in 1993. In 1994, NASA modified the original free-piston-driven design, and built a forward detonation-driven high-enthalpy shock tunnel (HYPULSE) in GASL. The wind tunnel can work in both reflection shock tunnel mode and expansion tube Mode [see ChueRSM, Tsai C-Y, Bakos RJ, Erdos JI, Rogers RC (2002) NASA's HYPULSE Facility at GASL-ADual Mode, Dual Driver Reflected-Shock/Expansion Tunnel. In: Lu F, Marren D (eds), Advanced Hypersonic Test Facilities, Progress in Astronautics and Aeronautics, Vol.198, AIAA,
爆轰驱动需要在驱动段内形成沿轴向传播的爆轰波,爆轰波后的不均匀的流场导致该驱动技术存在以下问题:第一,可爆轰的气体混合比例范围比可爆燃的范围窄的多,驱动气体的温度和声速范围也相应更窄,因此限制了爆轰驱动能够提供的试验气体总温范围;第二,爆轰驱动提供的有效驱动压力不超过设备承压极限的40%,限制了试验气体的总压范围。The detonation drive needs to form a detonation wave propagating in the axial direction in the driving section, and the uneven flow field behind the detonation wave causes the following problems in this drive technology: First, the gas mixing ratio range that can be detonated is lower than that of the gas that can be detonated. The range of the test gas is much narrower, and the range of temperature and sound velocity of the driving gas is correspondingly narrower, thus limiting the total temperature range of the test gas that the detonation drive can provide; second, the effective driving pressure provided by the detonation drive does not exceed the pressure limit of the equipment 40% limits the total pressure range of the test gas.
由于爆轰驱动存在上述问题,需要克服上述问题,需要引入同轴柱面爆燃驱动技术,但同轴柱面爆燃驱动技术需要在驱动段两端分别插接高压电极,在两个高压电极之间布置一条沿驱动段轴中心线方向的点火丝,利用放电系统给点火丝供电,其中,所需的高压脉冲电源以高压电容作为储能元件,高压电容中的电荷完全释放所需的时间比燃烧持续时间(10ms量级)长,燃烧产物中含有大量离子和水,极易发生击穿。为了保证设备和人员安全,需要将通电持续时间控制在毫秒量级,且需要良好的重复性;普通的机械式继电器难以满足要求,而基于半导体技术的固态继电器价格昂贵,且容易损坏。Due to the above-mentioned problems in the detonation drive, the above-mentioned problems need to be overcome, and the coaxial cylindrical deflagration drive technology needs to be introduced. Arrange an ignition wire along the center line of the driving section axis, and use the discharge system to supply power to the ignition wire. Among them, the required high-voltage pulse power supply uses a high-voltage capacitor as an energy storage element, and the time required for the charge in the high-voltage capacitor to be completely released The duration (on the order of 10 ms) is long, and the combustion products contain a large amount of ions and water, which is very prone to breakdown. In order to ensure the safety of equipment and personnel, the power-on duration needs to be controlled in milliseconds and requires good repeatability; ordinary mechanical relays are difficult to meet the requirements, and solid-state relays based on semiconductor technology are expensive and easily damaged.
现有文献1(CN201911027930.5)公开了一种井下作业脉冲放电开关结构,包括固定电极部分、可调电极部分、绝缘层;所述固定电极部分包括上部接线端、固定电极、内六角紧定螺钉。所述可调电极部分包括下部接线端、可调电极、固定螺母、紧定螺钉和紧定螺母。所述绝缘层包括上端绝缘层、中部绝缘层和下端绝缘层,但该方案仍未满足上述需求。Existing document 1 (CN201911027930.5) discloses a pulse discharge switch structure for downhole operations, including a fixed electrode part, an adjustable electrode part, and an insulating layer; the fixed electrode part includes an upper terminal, a fixed electrode, an inner hexagonal clamp screw. The adjustable electrode part includes a lower terminal, an adjustable electrode, a fixing nut, a set screw and a set nut. The insulating layer includes an upper insulating layer, a middle insulating layer and a lower insulating layer, but this solution still does not meet the above requirements.
现有文献2(CN102407947A)公开了激波风洞爆轰双驱装置,包括:激波风洞,该激波风洞具爆轰驱动段,该爆轰驱动段的一端设置有卸爆段,另一端设置有被驱动段;在所述卸爆段和爆轰驱动段之间设有第一膜片,在所述被驱动段和爆轰驱动段之间设有第二膜片;在所述爆轰驱动段的靠近所述卸爆段的一段设置有正向爆轰驱动点火装置,在所述爆轰驱动段的靠近所述被驱动段的一段设置有反向爆轰驱动点火装置;在所述正向爆轰驱动点火装置和反向爆轰驱动点火装置之间连接有可控延时触发装置,其方法如下:1)在激波风洞爆轰驱动段的靠近卸爆段的一端设置正向爆轰点火装置,在爆轰驱动段的靠近被驱动段的一端设置反向爆轰驱动点火装置;2)通过正向爆轰点火装置进行点火,形成正向驱动爆轰波;3)当正向爆轰波沿爆轰驱动段传播预定时间后,通过反向爆轰驱动点火装置进行点火,形成反向驱动爆轰波;4)反向驱动爆轰波将设置在被驱动段和爆轰驱动段之间的膜片撕裂,正向爆轰波与反向爆轰波相交后形成运动激波,该运动激波进入被驱动段,以对被驱动段的试验气体进行压缩。Existing document 2 (CN102407947A) discloses a shock tunnel detonation dual-drive device, comprising: a shock tunnel, the shock tunnel has a detonation driving section, and one end of the detonation driving section is provided with a detonation section, The other end is provided with a driven section; a first diaphragm is arranged between the detonation unloading section and the detonation driving section, and a second diaphragm is arranged between the driven section and the detonation driving section; A section of the detonation drive section close to the detonation section is provided with a forward detonation drive ignition device, and a section of the detonation drive section close to the driven section is provided with a reverse detonation drive ignition device; A controllable delay trigger device is connected between the forward detonation driven ignition device and the reverse detonation driven ignition device, and the method is as follows: 1) near the detonation unloading section of the shock wave wind tunnel detonation drive section A positive detonation ignition device is arranged at one end, and a reverse detonation driving ignition device is arranged at the end of the detonation driving section close to the driven section; 2) ignition is carried out by the forward detonation ignition device to form a forward driving detonation wave; 3) After the forward detonation wave propagates along the detonation driving section for a predetermined time, the ignition device is driven by the reverse detonation to ignite to form a reverse drive detonation wave; 4) The reverse drive detonation wave will be set at the driven The diaphragm between the detonation driving section and the detonation driving section is torn, and the forward detonation wave intersects with the reverse detonation wave to form a moving shock wave, which enters the driven section to conduct a compression.
为了满足同轴柱面爆燃驱动技术,本发明提出一种用于同轴柱面爆燃驱动装置的重力式高压脉冲放电开关,并且该用于同轴柱面爆燃驱动装置的重力式高压脉冲放电开关是本领域技术人员不容易想到的。In order to meet the coaxial cylinder deflagration drive technology, the present invention proposes a gravity type high voltage pulse discharge switch for coaxial cylinder deflagration drive device, and the gravity type high voltage pulse discharge switch for coaxial cylinder deflagration drive device It is not easy for those skilled in the art to think of.
发明内容Contents of the invention
有鉴于此,本发明提供了一种用于同轴柱面爆燃驱动装置的重力式高压脉冲放电开关,包括绝缘筒、绝缘滑块、第一电源正极接线柱、第二电源正极接线柱、点火丝极接线柱和电源负极接线柱;In view of this, the present invention provides a gravity-type high-voltage pulse discharge switch for a coaxial cylindrical deflagration drive device, including an insulating cylinder, an insulating slider, a positive terminal of the first power supply, a positive terminal of the second power supply, an ignition Filament terminal and power supply negative terminal;
所述绝缘筒内的底端设置有缓冲垫;The bottom end of the insulating cylinder is provided with a buffer pad;
所述绝缘筒内设置有绝缘滑块,所述绝缘滑块靠近所缓冲垫一侧设置有导电端子;An insulating slider is arranged in the insulating cylinder, and a conductive terminal is arranged on the side of the insulating slider near the buffer pad;
所述第一电源正极接线柱和所述电源负极接线柱分别安装于所述绝缘筒靠近所述缓冲垫一侧,所述第一电源正极接线柱和所述电源负极接线柱相对应;The positive terminal of the first power supply and the negative terminal of the power supply are respectively installed on the side of the insulating cylinder close to the buffer pad, and the positive terminal of the first power supply corresponds to the negative terminal of the power supply;
所述第二电源正极接线柱安装于所述绝缘筒靠近所述第一电源正极接线柱远离所述缓冲垫一侧,所述点火丝极接线柱安装于所述绝缘筒靠近所述电源负极接线柱远离所述缓冲垫一侧,其中,所述第二电源正极接线柱与所述点火丝极接线柱相对应;The positive terminal of the second power supply is installed on the side of the insulating cylinder close to the positive terminal of the first power supply and away from the buffer pad, and the terminal of the ignition wire is installed on the negative terminal of the insulating cylinder close to the negative terminal of the power supply. The post is far away from the side of the buffer pad, wherein the positive terminal of the second power supply corresponds to the terminal of the ignition filament;
所述第一电源正极接线柱和所述电源负极接线柱均设置有与所述导电端子相接触的第一滑动触点,所述第一电源正极接线柱的第一滑动触点通过所述导电端子与所述电源负极接线柱的第一滑动触点电连接;Both the positive terminal of the first power supply and the negative terminal of the power supply are provided with a first sliding contact in contact with the conductive terminal, and the first sliding contact of the positive terminal of the first power supply passes through the conductive terminal. The terminal is electrically connected to the first sliding contact of the negative terminal of the power supply;
所述第二电源正极接线柱和所述点火丝极接线柱均设置有与所述导电端子相接触的第二滑动触点,所述第二电源正极接线柱的第二滑动触点通过导电端子与所述点火丝极接线柱的第二滑动触点电连接;Both the positive terminal of the second power supply and the terminal of the ignition wire are provided with a second sliding contact in contact with the conductive terminal, and the second sliding contact of the positive terminal of the second power supply passes through the conductive terminal electrically connected to the second sliding contact of the ignition wire terminal;
所述第一电源正极接线柱和所述第二电源正极接线柱并联,所述第一电源正极接线柱、所述第二电源正极接线柱和所述电源负极接线柱分别与高压电容电连接;The positive terminal of the first power supply and the positive terminal of the second power supply are connected in parallel, and the positive terminal of the first power supply, the positive terminal of the second power supply and the negative terminal of the power supply are respectively electrically connected to a high-voltage capacitor;
所述绝缘筒和绝缘滑块的形状分别为柱体,所述柱体沿所述第一方向的截面为圆形或方形;The shapes of the insulating cylinder and the insulating slider are cylinders respectively, and the cross-section of the cylinders along the first direction is circular or square;
所述绝缘滑块沿第一方向上的长度大于所述绝缘滑块的直径,所述第一方向为由所述绝缘滑块指向所述缓冲垫的方向;The length of the insulating slider along a first direction is greater than the diameter of the insulating slider, and the first direction is a direction from the insulating slider to the buffer pad;
所述导电端子沿所述第一方向的高度为d1,所述第一滑动触点与所述第二滑动触点之间沿所述第一方向的长度为d2,所述第一滑动触点与所述缓冲垫之间沿所述第一方向的长度为d3,其中,d2>d1>d3。The height of the conductive terminal along the first direction is d1, the length between the first sliding contact and the second sliding contact along the first direction is d2, and the first sliding contact The length along the first direction between the buffer pad and the buffer pad is d3, wherein, d2>d1>d3.
可选地,所述第一滑动触点包括与所述第一电源正极接线柱相连接的第一子滑动触点和与所述电源负极接线柱相连接的第二子滑动触点;Optionally, the first sliding contact includes a first sub-sliding contact connected to the positive terminal of the first power supply and a second sub-sliding contact connected to the negative terminal of the power supply;
所述第一子滑动触点包括第一触头段和与所述第一触头段相连接的第一触点段,所述第一触头段位于第一子滑动触点靠近第一电源正极接线柱一侧,所述第一触点段位于第一子滑动触点远离第一电源正极接线柱一侧,所述第一触头段与所述第一触点段之间的夹角为θ1,180°>θ1>90°;The first sub-sliding contact includes a first contact segment and a first contact segment connected to the first contact segment, and the first contact segment is located at the first sub-sliding contact close to the first power supply On the side of the positive terminal, the first contact segment is located on the side of the first sub-sliding contact away from the positive terminal of the first power supply, the angle between the first contact segment and the first contact segment θ1, 180°>θ1>90°;
所述第二子滑动触点包括第二触头段和与所述第二触头段相连接的第二触点段,所述第二触头段位于第二子滑动触点靠近所述电源负极接线柱一侧,所述第二触点段位于第二子滑动触点远离所述电源负极接线柱一侧,所述第二触头段与所述第二触点段之间的夹角为θ2,180°>θ2>90°;The second sub-sliding contact includes a second contact segment and a second contact segment connected to the second contact segment, and the second contact segment is located at the second sub-sliding contact close to the power supply On the side of the negative terminal, the second contact segment is located on the side of the second sub-sliding contact away from the negative terminal of the power supply, the angle between the second contact segment and the second contact segment θ2, 180°>θ2>90°;
其中,θ1=θ2。Among them, θ1=θ2.
可选地,所述第一触点段与所述第二触头段之间沿第二方向上的长度略小于所述导电端子的直径,其中,所述略小于的范围为0.5~1㎝,所述第二方向与所述第一方向相交。Optionally, the length between the first contact segment and the second contact segment along the second direction is slightly smaller than the diameter of the conductive terminal, wherein the slightly smaller range is 0.5-1 cm , the second direction intersects the first direction.
可选地,所述第二滑动触点包括与所述第二电源正极接线柱相连接的第三子滑动触点和与所述点火丝极接线柱相连接的第四子滑动触点;Optionally, the second sliding contact includes a third sub-sliding contact connected to the positive terminal of the second power supply and a fourth sub-sliding contact connected to the ignition filament terminal;
所述第三子滑动触点包括第三触头段和与所述第三触头段相连接的第三触点段,所述第三触头段位于第三子滑动触点靠近第二电源正极接线柱一侧,所述第三触点段位于第三子滑动触点远离第二电源正极接线柱一侧,所述第三触头段与所述第三触点段之间的夹角为θ3,180°>θ3>90°;The third sub-sliding contact includes a third contact segment and a third contact segment connected to the third contact segment, and the third contact segment is located at the third sub-sliding contact close to the second power supply On the side of the positive terminal, the third contact segment is located on the side of the third sub-sliding contact away from the positive terminal of the second power supply, the angle between the third contact segment and the third contact segment θ3, 180°>θ3>90°;
所述第四子滑动触点包括第四触头段和与所述第四触头段相连接的第四触点段,所述第四触头段位于第四子滑动触点靠近所述点火丝极接线柱一侧,所述第四触点段位于第四子滑动触点远离所述点火丝极接线柱一侧,所述第四触头段与所述第四触点段之间的夹角为θ4,180°>θ4>90°;其中,θ3=θ4。The fourth sub-sliding contact includes a fourth contact segment and a fourth contact segment connected to the fourth contact segment, and the fourth contact segment is located at the fourth sub-sliding contact close to the ignition On the side of the filament terminal, the fourth contact segment is located on the side of the fourth sub-sliding contact away from the ignition filament terminal, and between the fourth contact segment and the fourth contact segment The included angle is θ4, 180°>θ4>90°; wherein, θ3=θ4.
可选地,所述第一触点段与所述第二触点段之间沿第二方向上的长度略小于所述导电端子的直径;所述第三触点段与所述第四触点段之间沿第二方向上的长度略小于所述导电端子的直径,其中,所述略小于的范围均为0.5~1㎝,所述第二方向与所述第一方向相交。Optionally, the length between the first contact segment and the second contact segment along the second direction is slightly smaller than the diameter of the conductive terminal; the third contact segment and the fourth contact The length between point segments along the second direction is slightly smaller than the diameter of the conductive terminal, wherein the slightly smaller range is 0.5-1 cm, and the second direction intersects the first direction.
可选地,所述绝缘滑块沿第一方向上的长度为5-10cm,所述绝缘滑块的直径为3-4cm。Optionally, the length of the insulating slider along the first direction is 5-10 cm, and the diameter of the insulating slider is 3-4 cm.
可选地,d1=2-3cm,d2=4-5cm,d3=1-2cm。Optionally, d1=2-3cm, d2=4-5cm, d3=1-2cm.
可选地,所述缓冲垫为泡沫垫、橡胶垫或充气垫。Optionally, the buffer pad is a foam pad, a rubber pad or an inflatable pad.
可选地,所述绝缘滑块的材质为塑料、橡胶或木材。Optionally, the insulating slider is made of plastic, rubber or wood.
与现有技术相比,本发明提供的用于同轴柱面爆燃驱动装置的重力式高压脉冲放电开关,至少实现了如下的有益效果:Compared with the prior art, the gravity-type high-voltage pulse discharge switch for the coaxial cylindrical deflagration driving device provided by the present invention at least achieves the following beneficial effects:
第一,通过高压电容正极、第二电源正极接线柱、第二滑动触点、导电端子与点火丝极接线柱串联实现对点火丝供电,能够保证毫秒级的时间精度,实现精确控制通电时间,以及通过高压电容正极、第一电源正极接线柱、第一滑动触点、导电端子与电源负极接线柱、高压电容负极串联,同时第一电源正极接线柱与第二电源正极接线柱并联,使高压电容内的剩余电荷直接中和,从而保证设备和人员的安全;First, the power supply to the ignition wire is realized by connecting the positive pole of the high-voltage capacitor, the positive terminal of the second power supply, the second sliding contact, the conductive terminal and the terminal of the ignition wire in series, which can ensure the time accuracy of milliseconds and realize precise control of the power-on time. And through the positive pole of the high-voltage capacitor, the positive pole of the first power supply, the first sliding contact, the conductive terminal, the negative pole of the power supply, and the negative pole of the high-voltage capacitor in series, and at the same time, the positive pole of the first power supply is connected in parallel with the positive pole of the second power supply, so that the high voltage The residual charge in the capacitor is directly neutralized to ensure the safety of equipment and personnel;
第二,通过缓冲垫,防止导电端子反弹造成第二滑动触点再次导通,避免意外击穿;Second, the buffer pad is used to prevent the rebound of the conductive terminal from causing the second sliding contact to be turned on again, so as to avoid accidental breakdown;
第三,通过绝缘筒和绝缘滑块的配合,能够承受数万伏特的高电压,结构强壮,安全可靠;Third, through the cooperation of the insulating cylinder and the insulating slider, it can withstand high voltage of tens of thousands of volts, and the structure is strong, safe and reliable;
第四,所用材料和工艺均较便宜,成本比相同电压、电流等级的固态继电器低得多。Fourth, the materials and processes used are relatively cheap, and the cost is much lower than that of solid state relays with the same voltage and current level.
当然,实施本发明的任一产品必不特定需要同时达到以上所述的所有技术效果。Of course, any product implementing the present invention does not necessarily need to achieve all the above-mentioned technical effects at the same time.
通过以下参照附图对本发明的示例性实施例的详细描述,本发明的其它特征及其优点将会变得清楚。Other features of the present invention and advantages thereof will become apparent from the following detailed description of exemplary embodiments of the present invention with reference to the accompanying drawings.
附图说明Description of drawings
被结合在说明书中并构成说明书的一部分的附图示出了本发明的实施例,并且连同其说明一起用于解释本发明的原理。The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention.
图1是现有技术中提供的一种激波管/风洞的结构示意图;Fig. 1 is a structural schematic diagram of a shock tube/wind tunnel provided in the prior art;
图2是本发明实施例提供的用于同轴柱面爆燃驱动装置的重力式高压脉冲放电开关的结构示意图;Fig. 2 is a schematic structural diagram of a gravity-type high-voltage pulse discharge switch for a coaxial cylindrical deflagration drive device provided by an embodiment of the present invention;
图3是图2中A处放大图;Figure 3 is an enlarged view of A in Figure 2;
图4是本发明实施例提供的一种用于激波管/风洞的同轴柱面爆燃驱动装置的结构示意图;Fig. 4 is a schematic structural diagram of a coaxial cylindrical deflagration driving device for a shock tube/wind tunnel provided by an embodiment of the present invention;
图5是图4中B处结构放大图;Figure 5 is an enlarged view of the structure at B in Figure 4;
图6是本发明实施例提供的一种激波管/风洞的结构示意图;Fig. 6 is a schematic structural diagram of a shock tube/wind tunnel provided by an embodiment of the present invention;
具体实施方式detailed description
现在将参照附图来详细描述本发明的各种示例性实施例。应注意到:除非另外具体说明,否则在这些实施例中阐述的部件和步骤的相对布置、数字表达式和数值不限制本发明的范围。Various exemplary embodiments of the present invention will now be described in detail with reference to the accompanying drawings. It should be noted that the relative arrangements of components and steps, numerical expressions and numerical values set forth in these embodiments do not limit the scope of the present invention unless specifically stated otherwise.
以下对至少一个示例性实施例的描述实际上仅仅是说明性的,决不作为对本发明及其应用或使用的任何限制。The following description of at least one exemplary embodiment is merely illustrative in nature and in no way taken as limiting the invention, its application or uses.
对于相关领域普通技术人员已知的技术、方法和设备可能不作详细讨论,但在适当情况下,所述技术、方法和设备应当被视为说明书的一部分。Techniques, methods and devices known to those of ordinary skill in the relevant art may not be discussed in detail, but where appropriate, such techniques, methods and devices should be considered part of the description.
在这里示出和讨论的所有例子中,任何具体值应被解释为仅仅是示例性的,而不是作为限制。因此,示例性实施例的其它例子可以具有不同的值。In all examples shown and discussed herein, any specific values should be construed as exemplary only, and not as limitations. Therefore, other instances of the exemplary embodiment may have different values.
应注意到:相似的标号和字母在下面的附图中表示类似项,因此,一旦某一项在一个附图中被定义,则在随后的附图中不需要对其进行进一步讨论。It should be noted that like numerals and letters denote like items in the following figures, therefore, once an item is defined in one figure, it does not require further discussion in subsequent figures.
图2是本发明实施例提供的用于同轴柱面爆燃驱动装置的重力式高压脉冲放电开关的结构示意图;图3是图2中A处放大图;参见图2和图3所示,本实施例提供一种用于同轴柱面爆燃驱动装置的重力式高压脉冲放电开关1000,包括绝缘筒100、绝缘滑块200、第一电源正极接线柱300、第二电源正极接线柱400、点火丝极接线柱500和电源负极接线柱600;Fig. 2 is a schematic structural diagram of a gravity-type high-voltage pulse discharge switch used in a coaxial cylindrical deflagration drive device provided by an embodiment of the present invention; Fig. 3 is an enlarged view of A in Fig. 2; see Fig. 2 and Fig. 3, this The embodiment provides a gravity-type high-voltage
绝缘筒100内的底端设置有缓冲垫101;The bottom end of the insulating
绝缘筒100内设置有绝缘滑块200,绝缘滑块200靠近所缓冲垫101一侧设置有导电端子201;An insulating
第一电源正极接线柱300和电源负极接线柱600分别安装于绝缘筒100靠近缓冲垫101一侧,第一电源正极接线柱300和电源负极接线柱600相对应;The first
第二电源正极接线柱400安装于绝缘筒100靠近第一电源正极接线柱300远离缓冲垫101一侧,点火丝极接线柱500安装于绝缘筒100靠近电源负极接线柱600远离缓冲垫101一侧,其中,第二电源正极接线柱400与点火丝极接线柱500相对应;The second power
第一电源正极接线柱300和电源负极接线柱600均设置有与导电端子201相接触的第一滑动触点301,第一电源正极接线柱300的第一滑动触点301通过导电端子201与电源负极接线柱600的第一滑动触点301电连接;The first
第二电源正极接线柱400和点火丝极接线柱500均设置有与导电端子201相接触的第二滑动触点401,第二电源正极接线柱400的第二滑动触点401通过导电端子201与点火丝极接线柱500的第二滑动触点401电连接;The second
第一电源正极接线柱300和第二电源正极接线柱400并联,一同连接到高压电容71的正极;电源负极接线柱600则与高压电容71的负极连接;The
绝缘筒100和绝缘滑块200的形状分别为柱体,柱体沿第一方向的截面可以是圆形或方形;The shapes of the insulating
绝缘滑块200沿第一方向E上的长度大于绝缘滑块200的直径,第一方向E为由绝缘滑块200指向缓冲垫101的方向;The length of the insulating
导电端子201沿第一方向E的长度为d1,第一滑动触点301与第二滑动触点401之间沿第一方向E的长度为d2,第一滑动触点301与缓冲垫101之间沿第一方向E的长度为d3,其中,d2>d1>d3。The length of the
具体的,该用于同轴柱面爆燃驱动装置的重力式高压脉冲放电开关1000包括绝缘筒100、绝缘滑块200、第一电源正极接线柱300、第二电源正极接线柱400、点火丝极接线柱500和电源负极接线柱600,其中,使用时可以将绝缘筒100竖直放置,也可以将绝缘筒100倾斜放置;Specifically, the gravity-type high-voltage
为了使第一电源正极接线柱300与电源负极接线柱600的正负极导通的时间足够长,在绝缘筒100的底端设置有缓冲垫101,缓冲垫101位于绝缘筒100内,缓冲垫101可以为泡沫垫、橡胶垫或充气垫;In order to make the positive and negative conduction time of the first power
在绝缘筒100内设置有绝缘滑块200,绝缘滑块200可以将绝缘滑块200从顶部滑落,在重力作用下在绝缘筒100内加速下落,在绝缘滑块200靠近所缓冲垫101一侧设置有导电端子201,导电端子201可以为一段金属柱,绝缘滑块200的材质为塑料、橡胶或木材;An insulating
第一电源正极接线柱300和电源负极接线柱600分别安装在绝缘筒100靠近缓冲垫101一侧,也就是说,第一电源正极接线柱300和电源负极接线柱600位于绝缘筒100的底部,其中,第一电源正极接线柱300与电源负极接线柱600相对应;The first
第二电源正极接线柱400安装在绝缘筒100靠近第一电源正极接线柱300远离缓冲垫101一侧,点火丝极接线柱500安装绝缘筒100靠近电源负极接线柱600远离缓冲垫101一侧,其中,第二电源正极接线柱400与点火丝极接线柱500相对应,也就是说,第二电源正极接线柱400与点火丝极接线柱500也位于绝缘筒100的底部;The second power supply
在第一电源正极接线柱300和电源负极接线柱600上均设置有与导电端子201相接触的第一滑动触点301,第一电源正极接线柱300的第一滑动触点301通过导电端子201与电源负极接线柱600的第一滑动触点301电连接,也就是说:第一电源正极接线柱300的第一滑动触点301、导电端子201与电源负极接线柱600的第一滑动触点301之间为串联;The first sliding
在第二电源正极接线柱400和点火丝极接线柱500均设置有与导电端子201相接触的第二滑动触点401,第二电源正极接线柱400的第二滑动触点401通过导电端子201与点火丝极接线柱500的第二滑动触点401电连接,也就是说:第二电源正极接线柱400的第二滑动触点401、导电端子201与点火丝极接线柱500的第二滑动触点401之间为串联;Both the
第一电源正极接线柱300和第二电源正极接线柱400并联,具体使用时,将第一电源正极接线柱300和第二电源正极接线柱400与高压电容71正极电连接,点火丝极接线柱500与点火丝13的正极电连接,电源负极接线柱600与高压电容71负极电连接,高压电容71用于存储高压电,并向点火丝放电;The first
绝缘筒100和绝缘滑块200的形状分别为柱体,柱体沿第一方向的截面可以是圆形或方形,其截面也可以采用其它形状,本示例中绝缘筒100和绝缘滑块200均为圆柱体;The shapes of the insulating
为了防止导电端子201在下落过程中翻转,将绝缘滑块200沿第一方向E上的长度大于绝缘滑块200的直径,第一方向E为由绝缘滑块200指向缓冲垫101的方向,如绝缘滑块200沿第一方向E上的长度可以为5-10cm,绝缘滑块200的直径可以为3-4cm;In order to prevent the conductive terminal 201 from turning over during the falling process, the length of the insulating
将导电端子201沿第一方向E的高度为d1,第一滑动触点301与第二滑动触点401之间沿第一方向E的长度为d2,第一滑动触点301与缓冲垫101之间沿第一方向E的长度为d3,其中,d2>d1>d3,也就是说,第一滑动触点301与第二滑动触点401之间的间距最大,第一滑动触点301与缓冲垫101之间沿第一方向E的间距略小于导电端子201的高度d1,如d1=2-3cm,d2=4-5cm,d3=1-2cm,具体的,如d1=3,d2=5,d3=2,或者,d1=2,d2=5,d3=1,可以根据实际情况,调整d1、d2和d3的数值,从而使导电端子201在几乎不反弹的情况下直接停留在电源负极接线柱600的第一滑动触点301上,进而使第一电源正极接线柱300与电源负极接线柱600的正负极导通的时间足够长。The height of the conductive terminal 201 along the first direction E is d1, the length between the first sliding contact 301 and the second sliding contact 401 along the first direction E is d2, and the distance between the first sliding contact 301 and the buffer pad 101 is The length along the first direction E is d3, wherein, d2>d1>d3, that is to say, the distance between the first sliding contact 301 and the second sliding contact 401 is the largest, and the distance between the first sliding contact 301 and the buffer The distance between the pads 101 along the first direction E is slightly smaller than the height d1 of the conductive terminal 201, such as d1=2-3cm, d2=4-5cm, d3=1-2cm, specifically, such as d1=3, d2=5 , d3=2, or d1=2, d2=5, d3=1, the values of d1, d2 and d3 can be adjusted according to the actual situation, so that the conductive terminal 201 stays directly at the negative pole of the power supply without rebounding On the first sliding contact 301 of the binding post 600 , and then the positive and negative terminals of the first power supply positive terminal 300 and the power supply negative terminal 600 are conducted for a long enough time.
具体使用时,绝缘筒100可以竖直放置,也可以倾斜放置;先将第一电源正极接线柱300和第二电源正极接线柱400分别与高压电容71正极电连接,点火丝极接线柱500与点火丝13的正极电连接,电源负极接线柱600与高压电容71负极电连接;将绝缘滑块200从顶部抛落,让绝缘滑块200在重力作用下加速下落;当导电端子201与第二电源正极接线柱400和点火丝极接线柱500上的第二滑动触点401接触时,高压电容正极与点火丝13的正极导通,电源对点火丝13供电;随着导电端子201继续下落,导电端子201与第二滑动触点401脱离,停止对点火丝13供电;稍后,导电端子201与第一电源正极接线柱300和电源负极接线柱600上的第一滑动触点301接触,此时电源正负极连通,电容内的剩余电荷直接中和,由于在绝缘筒100底部设置有缓冲垫101,从而使导电端子201在几乎不反弹的情况下直接停留在第一滑动触点301上,进而使第一电源正极接线柱300与电源负极接线柱600的正负极导通的时间足够长;若将绝缘筒100采用倾斜放置时,通过调节倾斜角度来精确调节点火丝13的供电持续时间。During specific use, the insulating
与现有技术相比,本发明提供的用于同轴柱面爆燃驱动装置的重力式高压脉冲放电开关,至少实现了如下的有益效果:Compared with the prior art, the gravity-type high-voltage pulse discharge switch for the coaxial cylindrical deflagration driving device provided by the present invention at least achieves the following beneficial effects:
第一,通过高压电容71正极、第二电源正极接线柱400、第二滑动触点401、导电端子201与点火丝极接线柱500串联实现对点火丝供电,能够保证毫秒级的时间精度,实现精确控制通电时间,以及通过高压电容71正极、第一电源正极接线柱300、第一滑动触点301、导电端子201与电源负极接线柱600、高压电容负极串联,同时第一电源正极接线柱300与第二电源正极接线柱400并联,使高压电容71内的剩余电荷直接中和,从而保证设备和人员的安全;First, the ignition wire is powered by connecting the positive pole of the high-
第二,通过缓冲垫101,防止导电端子201反弹造成第二滑动触点401再次导通,避免意外击穿;Second, the
第三,通过绝缘筒100和绝缘滑块的配合,能够承受数万伏特的高电压,结构强壮,安全可靠;Third, through the cooperation of the insulating
第四,所用材料和工艺均较便宜,成本比相同电压、电流等级的固态继电器低得多。Fourth, the materials and processes used are relatively cheap, and the cost is much lower than that of solid state relays with the same voltage and current level.
在本发明的一种可选实施例中,第一滑动触点301包括与第一电源正极接线柱300相连接的第一子滑动触点302和与电源负极接线柱600相连接的第二子滑动触点303;In an optional embodiment of the present invention, the first sliding
第一子滑动触点302包括第一触头段304和与第一触头段304相连接的第一触点段305,第一触头段304位于第一子滑动触点302靠近第一电源正极接线柱300一侧,第一触点段305位于第一子滑动触点302远离第一电源正极接线柱300一侧,第一触头段304与第一触点段305之间的夹角为θ1,180°>θ1>90°;The first
第二子滑动触点303包括第二触头段306和与第二触头段306相连接的第二触点段307,第二触头段306位于第二子滑动触点303靠近电源负极接线柱600一侧,第二触点段307位于第二子滑动触点303远离电源负极接线柱600一侧,第二触头段306与第二触点段307之间的夹角为θ2,180°>θ2>90°;The second sub-sliding contact 303 includes a second contact segment 306 and a second contact segment 307 connected to the second contact segment 306. The second contact segment 306 is located at the second sub-sliding contact 303 and is close to the negative pole of the power supply. On the side of the
其中,θ1=θ2。Among them, θ1=θ2.
具体的,第一滑动触点301包括第一子滑动触点302和第二子滑动触点303,第一子滑动触点302与第一电源正极接线柱300相连接,第二子滑动触点303与电源负极接线柱600相连接;Specifically, the first sliding
第一子滑动触点302包括第一触头段304和第一触点段305,第一触点段305与第一触头段304相连接,第一触头段304位于第一子滑动触点302靠近第一电源正极接线柱300一侧,第一触点段305位于第一子滑动触点302远离第一电源正极接线柱300一侧,第一触头段304与第一触点段305之间的夹角为θ1,180°>θ1>90°,也就是说,第一触点段305与导电端子201直接接触,第一触头段304与第一触点段305之间为钝角,第一触点段305为倾斜向下,夹角θ1朝向缓冲垫101;The first
第二子滑动触点303包括第二触头段306和第二触点段307,第二触头段306与第二触点段307相连接,第二触头段306位于第二子滑动触点303靠近电源负极接线柱600一侧,第二触点段307位于第二子滑动触点303远离电源负极接线柱600一侧,第二触头段306与第二触点段307之间的夹角为θ1,180°>θ2>90°;也就是说:第二触点段307与导电端子201直接接触,第二触头段306与第二触点段307之间为钝角,第二触点段307为倾斜向下,夹角θ2朝向缓冲垫101,第一触点段305和第二触点段307为镜像对称设置;其中,θ1=θ2,采用该方案,可以使带导电端子201的绝缘滑块200顺畅滑落。The second sub-sliding contact 303 includes a second contact segment 306 and a second contact segment 307, the second contact segment 306 is connected to the second contact segment 307, and the second contact segment 306 is located at the second sub-sliding contact. The point 303 is close to the side of the
在本发明的一种可选实施例中,第二滑动触点401包括与第二电源正极接线柱400相连接的第三子滑动触点402和与点火丝极接线柱500相连接的第四子滑动触点403;In an optional embodiment of the present invention, the second sliding
第三子滑动触点402包括第三触头段404和与第三触头段404相连接的第三触点段405,第三触头段404位于第三子滑动触点402靠近第二电源正极接线柱400一侧,第三触点段405位于第三子滑动触点402远离第二电源正极接线柱400一侧,第三触头段404与第三触点段405之间的夹角为θ3,180°>θ3>90°;The third sub-sliding contact 402 includes a third contact segment 404 and a third contact segment 405 connected to the third contact segment 404, the third contact segment 404 is located at the third sub-sliding contact 402 close to the second power supply On the
第四子滑动触点403包括第四触头段406和与第四触头段406相连接的第四触点段407,第四触头段406位于第四子滑动触点403靠近点火丝极接线柱500一侧,第四触点段407位于第四子滑动触点403远离点火丝极接线柱500一侧,第四触头段406与第四触点段407之间的夹角为θ4,180°>θ4>90°;其中,θ3=θ4。The fourth sub-sliding contact 403 includes a fourth contact segment 406 and a fourth contact segment 407 connected to the fourth contact segment 406, the fourth contact segment 406 is located at the fourth sub-sliding contact 403 close to the ignition wire On the side of the terminal 500, the fourth contact segment 407 is located on the side of the fourth sub-sliding contact 403 away from the
具体的,第二滑动触点401包括第三子滑动触点402和第三子滑动触点403,第三子滑动触点402与第二电源正极接线柱400相连接,第四子滑动触点403与点火丝极接线柱500相连接;Specifically, the second sliding
第三子滑动触点402包括第三触头段404和第三触点段405,第三触头段404与第三触点段405相连接,第三触头段404位于第三子滑动触点402靠近第二电源正极接线柱400一侧,第三触点段405位于第三子滑动触点402远离第二电源正极接线柱400一侧,第三触头段404与第三触点段405之间的夹角为θ3,180°>θ3>90°,也就是说,第三触点段405与导电端子201直接接触,第三触头段404与第三触点段405之间为钝角,第三触点段405为倾斜向下,夹角θ3朝向缓冲垫101;The third sub-sliding contact 402 includes a third contact segment 404 and a third contact segment 405, the third contact segment 404 is connected to the third contact segment 405, and the third contact segment 404 is located at the third sub-sliding contact The point 402 is close to the side of the
第四子滑动触点403包括第四触头段406和第四触点段407,第四触头段406和第四触点段407相连接,第四触头段406位于第四子滑动触点403靠近点火丝极接线柱500一侧,第四触点段407位于第四子滑动触点403远离点火丝极接线柱500一侧,第四触头段406与第四触点段407之间的夹角为θ4,180°>θ4>90°;也就是说:第四触点段407与导电端子201直接接触,第四触头段406与第四触点段407之间为钝角,第四触点段407为倾斜向下,夹角θ4朝向缓冲垫101;其中,θ3=θ4,第四触点段407和第四触点段407为镜像对称设置,采用该方案,可以使带导电端子201的绝缘滑块200顺畅滑落,由于在绝缘筒100底部设置有缓冲垫101,可以使第一电源正极接线柱300与电源负极接线柱600的正负极导通时间足够长,从而使导电端子201停滞在第二滑动触点401处,进而更好的中和电容内的剩余电荷。The fourth sub-sliding contact 403 includes a fourth contact segment 406 and a fourth contact segment 407, the fourth contact segment 406 and the fourth contact segment 407 are connected, and the fourth contact segment 406 is located at the fourth sub-sliding contact The point 403 is close to the side of the
在本发明的一种可选实施例中,第三触点段405与第四触点段407之间沿第二方向F上的长度d4略小于导电端子201的直径,其中,略小于的范围为0.5-1cm;若低于0.5cm,则第三触点段405和第四触点段407与导电端子201接触的不充分,若大于1cm,则导电端子201无法顺利滑落;因此,将略小于的范围限定在0.5-1cm,第二方向F与第一方向E相交,当然第一触点段305与第二触点段307沿第二方向F上的长度d5也略小于导电端子201的直径,略小于的范围可以为0.5~1㎝,若低于0.5cm,则第一触点段305与第二触点段307与导电端子201接触的不充分,若大于1cm,则导电端子201无法顺利滑落;因此,将略小于的范围限定在0.5-1cm,可以使第一触点段305和第二触点段307与导电端子201更充分地接触,从而使电源正负极连通,将电容内的剩余电荷直接中和;使第三触点段405和第四触点段407与导电端子201更充分地接触,使高压电容正极与点火丝13的正极导通,电源对点火丝13供电。In an optional embodiment of the present invention, the length d4 along the second direction F between the third contact segment 405 and the fourth contact segment 407 is slightly smaller than the diameter of the conductive terminal 201, wherein the range of slightly smaller than is 0.5-1cm; if it is less than 0.5cm, the third contact segment 405 and the fourth contact segment 407 are not in sufficient contact with the conductive terminal 201, and if it is greater than 1cm, the conductive terminal 201 cannot slide down smoothly; The range of less than 0.5-1cm, the second direction F intersects the first direction E, of course, the length d5 of the first contact segment 305 and the second contact segment 307 along the second direction F is also slightly smaller than that of the conductive terminal 201 The diameter, which is slightly smaller than 0.5-1cm, if it is less than 0.5cm, then the contact between the first contact segment 305 and the second contact segment 307 and the conductive terminal 201 is insufficient; if it is larger than 1cm, the conductive terminal 201 It cannot slide down smoothly; therefore, limiting the range slightly smaller than 0.5-1cm can make the first contact segment 305 and the second contact segment 307 more fully contact with the conductive terminal 201, so that the positive and negative poles of the power supply can be connected. The remaining charge in the capacitor is directly neutralized; the third contact segment 405 and the fourth contact segment 407 are more fully in contact with the
图4是本发明实施例提供的一种用于激波管/风洞的同轴柱面爆燃驱动装置的结构示意图;图5是图4中B处结构放大图;如图4-图5所示,本实施例提供一种用于激波管/风洞的同轴柱面爆燃驱动装置,包括爆燃驱动段1、被驱动段2、用于将爆燃驱动段1和被驱动段2隔开的膜片5、盲板14和放电系统7,其中,爆燃驱动段1一端连通被驱动段2,另一端连接盲板14;Fig. 4 is a schematic structural view of a coaxial cylindrical deflagration driving device for a shock tube/wind tunnel provided by an embodiment of the present invention; Fig. 5 is an enlarged view of the structure at B in Fig. 4; as shown in Fig. 4-Fig. 5 As shown, this embodiment provides a coaxial cylindrical deflagration driving device for a shock tube/wind tunnel, including a deflagration driving section 1, a driven
爆燃驱动段1为等截面直管,爆燃驱动段1上插接有沿径向Y延伸的第一电极11和第二电极12,第一电极11位于爆燃驱动段靠近盲板14一侧,第二电极12位于爆燃驱动段1靠近被驱动段2一侧,第一电极11与第二电极12之间电连接有沿轴向X延伸的点火丝13,轴向X为由爆燃驱动段1指向被驱动段2的轴中心线的方向,径向Y与轴向X相交;The deflagration driving section 1 is a straight tube with equal cross-section. The
沿轴向X上,第一电极11与盲板14之间的长度为L1,第二电极12与膜片5之间的长度为L2,L1和L2的长度限定为0.5cm-20cm;Along the axis X, the length between the
爆燃驱动段1上开设有与第一电极11和第二电极12相配合的开孔8,第一电极11和第二电极12与开孔8的接触面设置有密封圈81;The deflagration driving section 1 is provided with an
爆燃驱动段1内充有可燃混气;The deflagration driving section 1 is filled with combustible gas mixture;
放电系统7包括重力式高压脉冲放电开关1000和高压电容71,重力式高压脉冲放电开关1000包括绝缘筒100、绝缘滑块200、第一电源正极接线柱300、第二电源正极接线柱400、点火丝极接线柱500和电源负极接线柱600,该重力式高压脉冲放电开关1000为上述用于同轴柱面爆燃驱动装置的重力式高压脉冲放电开关1000;The
由高压电容71正极、第二电源正极接线柱400、第二滑动触点401、导电端子201、点火丝极接线柱500、第一电极11、点火丝13、第二电极12、高压电容71负极构成点火回路;由高压电容71正极、第一电源正极接线柱300、第一滑动触点301、导电端子201、电源负极接线柱600、高压电容71负极构成卸荷回路,第一电源正极接线柱300和第二电源正极接线柱400并联,高压电容71用于存储高压电,并向点火丝放电,其中,高压电容71可产生2000V的高压。The positive pole of the high-
具体的,该用于激波管/风洞的同轴柱面爆燃驱动装置包括爆燃驱动段1、被驱动段2,爆燃驱动段1一端连通被驱动段2,另一端连接盲板14,爆燃驱动段1与被驱动段2之间设置膜片5,被驱动段2通过喷管3连通试验段4,盲板14为法兰盖,利用盲板14堵上爆燃驱动段1的端头,无需再使用传统的卸爆段以及在卸爆段与爆燃驱动段之间设置膜片,不仅有利于降低占用空间面积,还可以降低成本;Specifically, the coaxial cylindrical deflagration driving device for a shock tube/wind tunnel includes a deflagration driving section 1 and a driven
在爆燃驱动段1插接有沿径向Y延伸的第一电极11和第二电极12,第一电极11位于爆燃驱动段1靠近盲板14一侧,第二电极12位于爆燃驱动段1靠近被驱动段2一侧,也就是说将第一电极11和第二电极12插接于爆燃驱动段1的两端;在第一电极11与第二电极12之间电连接有沿轴向延伸的点火丝13,轴向X为由盲板14指向被驱动段2的轴中心线的方向,径向Y与轴向X相交,可选地,点火丝13可以为铜、银、镍铬、钨和合金中任一种金属材质,点火丝13的长度根据爆燃驱动段1的长度进行调整;A
第一电极11到盲板14的轴向距离为L1,第二电极12与膜片5的轴向距离为L2,若L1和L2的长度小于0.5cm,有可能发生击穿,导致设备损坏或危害人员安全;若L1和L2的长度大于20cm,则有可能导致爆燃驱动段1内可燃混气燃烧不稳定,因此,将L1和L2的长度限定为0.5cm-20cm,不仅尽可能将点火丝13在爆燃驱动段内沿轴向布置的更长一些,能够进一步使爆燃驱动段1内可燃混气燃烧的更充分,而且可以避免第一电极11与爆燃驱动段端头之间以及第二电极12与膜片5之间的距离过近,从而避免发生击穿,保证设备以及人员的安全;The axial distance between the
在爆燃驱动段1上开设有与第一电极11和第二电极12相配合的开孔8,图5中为了在图上显示开孔8,将开孔8的孔径画的比实际大些,开孔8与第一电极11相配合,第二电极12与开孔8相配合,通过开孔8便于将第一电极11和第二电极12插接于燃烧驱动段1,为了保证爆燃驱动段1内的密封性,在第一电极11插接至爆燃驱动段1后,在第一电极1与开孔8相接触的爆燃驱动段1的接触面设置密封圈81,在第二电极12与开孔8相接触的爆燃驱动段1的接触面设置密封圈81;On the deflagration driving section 1, there is an
爆燃驱动段1内充有可燃混气,可燃混气可以包括燃料、氧化剂和惰性气体,其中,燃料为氢、一氧化碳或烷烯炔烃,也可以为其它可燃气体;氧化剂为氧或一氧化二氮,也可以为其它氧化性气体,惰性气体为氮气、稀有气体或二氧化碳,也可以为其它不参与燃烧反应的气体;燃料:氧化剂:惰性气体之间的比例可以为1:1:1,燃料:氧化剂:惰性气体之间的比例也可以为2:1:1,燃料:氧化剂:惰性气体之间的比例还可以为2:1:7,燃料、氧化剂和惰性气体三者的比例关系根据实验要求确定;The deflagration driving section 1 is filled with a combustible gas mixture, which can include fuel, oxidant and inert gas, wherein the fuel is hydrogen, carbon monoxide or alkenyne, and can also be other combustible gases; the oxidant is oxygen or dioxide Nitrogen can also be other oxidizing gases, and inert gases can be nitrogen, rare gases or carbon dioxide, or other gases that do not participate in combustion reactions; the ratio of fuel: oxidant: inert gas can be 1:1:1, fuel : The ratio between oxidant: inert gas can also be 2:1:1, the ratio between fuel: oxidant: inert gas can also be 2:1:7, and the ratio of fuel, oxidant and inert gas is based on experiments require determination;
放电系统7包括重力式高压脉冲放电开关1000和高压电容71,重力式高压脉冲放电开关1000包括绝缘筒100、绝缘滑块200、第一电源正极接线柱300、第二电源正极接线柱400、点火丝极接线柱500和电源负极接线柱600,该重力式高压脉冲放电开关1000为上述用于同轴柱面爆燃驱动装置的重力式高压脉冲放电开关1000;The
具体的,绝缘筒100内的底端设置有缓冲垫101;绝缘筒100内设置有绝缘滑块200,绝缘滑块200靠近所缓冲垫101一侧设置有导电端子201;第一电源正极接线柱300和电源负极接线柱600分别安装于绝缘筒100靠近缓冲垫101一侧,第一电源正极接线柱300和电源负极接线柱600相对应;第二电源正极接线柱400安装于绝缘筒100靠近第一电源正极接线柱300远离缓冲垫101一侧,点火丝极接线柱500安装于绝缘筒100靠近电源负极接线柱600远离缓冲垫101一侧,其中,第二电源正极接线柱400与点火丝极接线柱500相对应;第一电源正极接线柱300和电源负极接线柱600均设置有与导电端子201相接触的第一滑动触点301,第一电源正极接线柱300的第一滑动触点301通过导电端子201与电源负极接线柱600的第一滑动触点301电连接;第二电源正极接线柱400和点火丝极接线柱500均设置有与导电端子201相接触的第二滑动触点401,第二电源正极接线柱400的第二滑动触点401通过导电端子201与点火丝极接线柱500的第二滑动触点401电连接;Specifically, the bottom end of the insulating
由高压电容71正极、第二电源正极接线柱400、第二滑动触点401、导电端子201、点火丝极接线柱500、第一电极11、点火丝13、第二电极12、高压电容71负极构成点火回路;由高压电容71正极、第一电源正极接线柱300、第一滑动触点301、导电端子201、电源负极接线柱600、高压电容71负极构成卸荷回路,第一电源正极接线柱300和第二电源正极接线柱400并联,也就是说,点火回路与卸荷回路并联;高压电容71用于存储高压电,并向点火丝放电。The positive pole of the high-
高压电容71充电后,导电端子201与第二电源正极接线柱400和点火丝极接线柱500上的第二滑动触点401接触时,高压电容71正极与第一电极11导通,高压电容71对点火丝13供电;随着导电端子201继续下落,导电端子201与第二滑动触点401脱离,停止对点火丝13供电;持续预定时间后,导电端子201与第一电源正极接线柱300和电源负极接线柱600上的第一滑动触点301接触,此时电源正负极连通,电容内的剩余电荷直接中和,完成卸荷,上述预定时间可以为5-30毫秒。After the high-
该用于激波管/风洞的同轴柱面爆燃驱动装置的组装顺序如下:The assembly sequence for this Coaxial Cylindrical Deflagration Drive for Shock Tube/Wind Tunnel is as follows:
提供爆燃驱动段1;Provide deflagration driving section 1;
首先,在爆燃驱动段1上开设有放置第一电极11和第二电极12的开孔8;其次,在第一电极11和第二电极12与开孔8的接触面安装密封圈81,然后在开孔8内插接第一电极11和第二电极12,第一电极11位于爆燃驱动段靠近盲板14一侧,第二电极12位于爆燃驱动段1靠近被驱动段2一侧,插接好第一电极11和第二电极12之后;再在第一电极11与第二电极12之间连接沿轴向X延伸的点火丝13;Firstly, the
在爆燃驱动段1与被驱动段2之间安装膜片,在爆燃驱动段1靠近膜片5一端连接被驱动段2,另一端连接有盲板14;A diaphragm is installed between the deflagration driving section 1 and the driven
在爆燃驱动段1内充有可燃混气;The deflagration driving section 1 is filled with combustible gas mixture;
组装放电系统7,将第一电源正极接线柱300和第二电源正极接线柱400分别与高压电容71正极电连接,点火丝极接线柱500与第一电极11电连接,第二电极12与高压电容71负极电连接,第一电源正极接线柱300和第二电源正极接线柱400并联,其中,将高压电容71正极、第二电源正极接线柱400、第二滑动触点401、导电端子201、点火丝极接线柱500、第一电极11、点火丝13、第二电极12、高压电容71负极构成点火回路;将高压电容71正极、第一电源正极接线柱300、第一滑动触点301、导电端子201、电源负极接线柱600、高压电容71负极构成卸荷回路。Assemble the
按照上述组装顺序对用于激波管/风洞的同轴柱面爆燃驱动装置进行组装,不仅可以更好地插接第一电极以及第二电极,使点火丝13的位置布设的更精确,而且可以避免可燃混气漏气,保证人身安全,同时便于操作。Assembling the coaxial cylindrical deflagration driving device for the shock tube/wind tunnel according to the above assembly sequence can not only better insert the first electrode and the second electrode, but also make the position of the
当然,在不考虑高压电容向点火丝放电的情况下,上述组装顺序可以做出适当调整,可以在安装完被驱动段2或盲板14之后,先组装放电系统7,再向爆燃驱动段1内充有可燃混气,具体如下:Of course, without considering the discharge of the high-voltage capacitor to the ignition wire, the above-mentioned assembly sequence can be adjusted appropriately. After the driven
第一,提供爆燃驱动段1;First, provide a deflagration driving section 1;
第二,首先,在爆燃驱动段1上开设有放置第一电极11和第二电极12的开孔8;其次,在第一电极11和第二电极12与开孔8的接触面安装密封圈81,然后在开孔8内插接第一电极11和第二电极12,第一电极11位于爆燃驱动段靠近盲板14一侧,第二电极12位于爆燃驱动段1靠近被驱动段2一侧,插接好第一电极11和第二电极12之后;再在第一电极11与第二电极12之间连接沿轴向X延伸的点火丝13;Second, at first, on the deflagration driving section 1, there are
第三,在爆燃驱动段1与被驱动段2之间安装膜片,在爆燃驱动段1靠近膜片5一端连接被驱动段2,另一端连接有盲板14;Thirdly, a diaphragm is installed between the deflagration driving section 1 and the driven
第四,组装放电系统7,将第一电源正极接线柱300和第二电源正极接线柱400分别与高压电容71正极电连接,点火丝极接线柱500与第一电极11电连接,第二电极12与高压电容71负极电连接,第一电源正极接线柱300和第二电源正极接线柱400并联,其中,将高压电容71正极、第二电源正极接线柱400、第二滑动触点401、导电端子201、点火丝极接线柱500、第一电极11、点火丝13、第二电极12、高压电容71负极构成点火回路;将高压电容71正极、第一电源正极接线柱300、第一滑动触点301、导电端子201、电源负极接线柱600、高压电容71负极构成卸荷回路;Fourth, assemble the
第五,在爆燃驱动段1内充有可燃混气。Fifth, the deflagration driving section 1 is filled with combustible gas mixture.
需要说明的是:第一,提供爆燃驱动段1;第二,首先,在爆燃驱动段1上开设有放置第一电极11和第二电极12的开孔8;其次,在第一电极11和第二电极12与开孔8的接触面安装密封圈81,然后在开孔8内插接第一电极11和第二电极12,第一电极11位于爆燃驱动段靠近盲板14一侧,第二电极12位于爆燃驱动段1靠近被驱动段2一侧,插接好第一电极11和第二电极12之后;再在第一电极11与第二电极12之间连接沿轴向X延伸的点火丝13;第三,在爆燃驱动段1与被驱动段2之间安装膜片,在爆燃驱动段1靠近膜片5一端连接被驱动段2,另一端连接有盲板14;上述三个步骤组装顺序是不可逆的,也就是上述组装顺序无法颠倒的,颠倒后则无法实施。It should be noted that: first, a deflagration driving section 1 is provided; secondly, firstly,
工作原理如下:在爆燃驱动段1内有一根沿轴向X布置的点火丝13,高压电容71充电后,先闭合点火回路,高压电容71通过第一电极11和第二电极12与点火丝13导通,点火丝13两端施加数千至数万伏特的高电压,在点火回路通电瞬间,点火丝13剧烈发热,在微秒量级的时间内点燃点火丝13附近的可燃混气,点燃后形成柱状火焰面,并沿径向扩大;通过使点火丝13与爆燃驱动段1的管道严格同轴,保证沿轴向各处同时燃尽;由于高压电容71的放电过程比燃烧过程更长,需要在燃烧结束前将高压电容71中剩余的电荷卸掉,因此当持续预定时间后,闭合卸荷回路,将高压电容71正负极短路,高压电容71中的电荷即经由卸荷回路瞬间返回高压电容71,完成卸荷,从而防止高压电容71正极附近击穿燃烧产物,产生安全事故。The working principle is as follows: in the deflagration driving section 1 there is an
需要说明的是:爆轰驱动需要在驱动段管道内形成沿轴向传播的爆轰波,而爆燃驱动则是使爆燃驱动段1的管道内的气体沿轴向同时点火,以爆燃而非爆轰的方式完成燃烧,并沿轴向X同时结束燃烧。It should be noted that the detonation drive needs to form a detonation wave propagating axially in the pipeline of the driving section, while the deflagration drive is to ignite the gas in the pipeline of the deflagration driving section 1 simultaneously in the axial direction, so as to detonate instead of detonate. The combustion is completed in a bombing manner, and the combustion is simultaneously completed along the axis X.
通常激波管/风洞的有效工作时间大致在几毫秒至100毫秒量级,为了提供精确的试验条件,必须严格保证爆燃驱动段中的可燃混气同时点火,同时燃尽。Generally, the effective working time of the shock tube/wind tunnel is on the order of a few milliseconds to 100 milliseconds. In order to provide accurate test conditions, it is necessary to strictly ensure that the combustible gas mixture in the deflagration driving section is ignited and burned out at the same time.
通过上述实施例可知,本发明提供的用于激波管/风洞的同轴柱面爆燃驱动装置,至少实现了如下的有益效果:It can be seen from the above embodiments that the coaxial cylindrical deflagration driving device for shock tube/wind tunnel provided by the present invention at least achieves the following beneficial effects:
第一,现有技术中由爆轰驱动在驱动段管道内形成沿轴向传播的爆轰波,由于爆轰波极高的压力峰不能全部用来驱动,爆轰驱动提供的有效压力大大低于设备的承压极限,而本发明中以爆燃取代爆轰,不存在爆轰中的压力峰,燃烧压力可以100%用于压缩试验气体,因此提高了试验气体的压力;First, in the prior art, the detonation drive forms a detonation wave propagating axially in the pipeline of the driving section. Since the extremely high pressure peak of the detonation wave cannot be used for driving, the effective pressure provided by the detonation drive is much lower. Due to the pressure limit of the equipment, detonation is replaced by detonation in the present invention, there is no pressure peak in detonation, and the combustion pressure can be 100% used to compress the test gas, thus increasing the pressure of the test gas;
第二,爆燃的混气比例极限比爆轰宽得多,驱动气体的温度和声速范围更大,对应的试验气体总温范围也因此比爆轰驱动更大。Second, the mixture ratio limit of deflagration is much wider than that of detonation, and the range of temperature and sound velocity of the driving gas is larger, and the corresponding total temperature range of the test gas is therefore larger than that of detonation driving.
第三,通过高压电容正极、第二电源正极接线柱、第二滑动触点、导电端子与点火丝极接线柱串联实现对点火丝供电,能够保证毫秒级的时间精度,实现精确控制通电时间,以及通过高压电容正极、第一电源正极接线柱、第一滑动触点、导电端子与电源负极接线柱、高压电容负极串联,同时第一电源正极接线柱与第二电源正极接线柱并联,使高压电容内的剩余电荷直接中和,从而保证设备和人员的安全;Third, the power supply to the ignition wire is realized through the positive pole of the high-voltage capacitor, the positive terminal of the second power supply, the second sliding contact, the conductive terminal and the terminal of the ignition wire in series, which can ensure the time accuracy of milliseconds and realize precise control of the power-on time. And through the positive pole of the high-voltage capacitor, the positive pole of the first power supply, the first sliding contact, the conductive terminal, the negative pole of the power supply, and the negative pole of the high-voltage capacitor in series, and at the same time, the positive pole of the first power supply is connected in parallel with the positive pole of the second power supply, so that the high voltage The residual charge in the capacitor is directly neutralized to ensure the safety of equipment and personnel;
第四,通过缓冲垫使导电端子在几乎不反弹的情况下直接停留在第一滑动触点上,避免了导电端子再次将点火回路导通引发意外击穿。Fourth, the conductive terminal stays directly on the first sliding contact with almost no rebound through the buffer pad, which avoids accidental breakdown caused by the conductive terminal turning on the ignition circuit again.
图6是本发明实施例提供的一种激波管/风洞的结构示意图;本发明实施例还有一种激波管/风洞,包括本发明实施例提供的用于激波管/风洞的同轴柱面爆燃驱动装置。Fig. 6 is a schematic structural diagram of a shock tube/wind tunnel provided by an embodiment of the present invention; an embodiment of the present invention also has a shock tube/wind tunnel, including a shock tube/wind tunnel provided by an embodiment of the present invention The coaxial cylindrical deflagration drive device.
虽然已经通过例子对本发明的一些特定实施例进行了详细说明,但是本领域的技术人员应该理解,以上例子仅是为了进行说明,而不是为了限制本发明的范围。本领域的技术人员应该理解,可在不脱离本发明的范围和精神的情况下,对以上实施例进行修改。本发明的范围由所附权利要求来限定。Although some specific embodiments of the present invention have been described in detail through examples, those skilled in the art should understand that the above examples are for illustration only and not intended to limit the scope of the present invention. Those skilled in the art will appreciate that modifications can be made to the above embodiments without departing from the scope and spirit of the invention. The scope of the invention is defined by the appended claims.
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