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Article(id=1261262689964273997, tenantId=1146029695717560320, journalId=1146123166801305609, issueId=1261262687258985194, articleNumber=null, orderNo=null, doi=10.12404/j.issn.1671-1815.2405473, pmid=null, cstr=null, oa=null, hot=null, price=null, onlineType=0, articleFormat=0, articleType=null, articleTypeStr=research-article, receivedDate=1721491200000, receivedDateStr=2024-07-21, revisedDate=1744646400000, revisedDateStr=2025-04-15, acceptedDate=null, acceptedDateStr=null, onlineDate=1778638058414, onlineDateStr=2026-05-13, pubDate=1752768000000, pubDateStr=2025-07-18, doiRegisterDate=null, doiRegisterDateStr=null, onlineIssueDate=1778638058414, onlineIssueDateStr=2026-05-13, onlineJustAcceptDate=null, onlineJustAcceptDateStr=null, onlineFirstDate=null, onlineFirstDateStr=null, sourceXml=null, magXml=null, createTime=1778638058414, creator=13701087609, updateTime=1778638058414, updator=13701087609, issue=Issue{id=1261262687258985194, tenantId=1146029695717560320, journalId=1146123166801305609, year='2025', volume='25', issue='20', pageStart='8317', pageEnd='8759', issueExtLink='null', onlineDate='null', pubDate='null', beforeIssueId=null, nextIssueId=null, price=null, status=1, issueComplete=1, articleOrder=1, issueType=-1, specialIssue=null, createTime=1778638057769, creator=13701087609, updateTime=1778753106634, updator=13701087609, preIssue=null, nextIssue=null, ext={EN=IssueExt(id=1261745237240722095, tenantId=1146029695717560320, journalId=1146123166801305609, issueId=1261262687258985194, language=EN, specialIssueTitle=, coverIllustrator=null, specialIssueEditor=, specialIssueAbout=), CN=IssueExt(id=1261745237240722096, tenantId=1146029695717560320, journalId=1146123166801305609, issueId=1261262687258985194, language=CN, specialIssueTitle=, coverIllustrator=null, specialIssueEditor=, specialIssueAbout=)}, issueFiles=null}, startPage=8364, endPage=8370, ext={EN=ArticleExt(id=1261262691780407638, articleId=1261262689964273997, tenantId=1146029695717560320, journalId=1146123166801305609, language=EN, title=Experimental Device and Method of Annular Perturbation Detonation, columnId=1156264149949735860, journalTitle=Science Technology and Engineering, columnName=Papers·Mechanics, runingTitle=null, highlight=null, articleAbstract=

Due to the high calorific value of energetic materials combined with their flammable and explosive nature. The propagation in the tube will affect the shape and geometric dimensions of the tube, resulting in the propagation of detonations is affected. In order to deeply investigate the influence of annular perturbation on the propagation of detonation waves, accurately and clearly observe the propagation dynamics of the detonation wave in annular tube, and better reflect the influence of boundary layer effect and curvature tube wall on detonation waves.An annular disturbance detonation experimental device was built up. Annular disturbance was realized by adding disturbance tubes with different diameters to the end of the smooth circular tube. The detonation wave velocity, triple-point trajectory, and cell structure were observed by using a data acquisition system composed of pressure sensors and smoke films. The experimental system of annular disturbance detonation was constructed successfully. It was able to obtain the ideal propagation data with remarkable regularity and high reliability. After verification, the detonation experimental device built has excellent data acquisition capabilities, and the obtained data confirms that the device is scientific and effective. The experimental system built contributes to providing theoretical support for accident prevention and control, allowing scientific instruments to play a more significant role in supporting technological innovation and societal development.

, correspAuthors=Huan-juan ZHAO, authorNote=null, correspAuthorsNote=null, copyrightStatement=null, copyrightOwner=null, extLink=null, articleAbsUrl=null, sourceXml=null, magXml=null, pdfUrl=null, pdf=null, pdfFileSize=null, pdfExtLink=null, richHtmlUrl=null, mobilePdfUrl=null, reviewReport=null, pdfFirstPage=null, abstractGraph=null, abstractGraphContent=null, abstractVideo=null, citation=null, cebUrl=null, magXmlContent=null, mapNumber=null, authorCompany=null, fund=null, authors=null, authorsList=Yu-kun GAO, Ying-xin BAO, Yu-xuan LU, Jing LIU, Yi-fu YANG, Huan-juan ZHAO), CN=ArticleExt(id=1261262702324887979, articleId=1261262689964273997, tenantId=1146029695717560320, journalId=1146123166801305609, language=CN, title=环形扰动爆轰实验装置及方法, columnId=1156264150092342198, journalTitle=科学技术与工程, columnName=论文·力学, runingTitle=null, highlight=null, articleAbstract=

由于含能材料的高热值及其伴随着易燃易爆的特性,在管道中传播时会影响管道的形状及几何尺寸,导致爆轰的传播受到影响。为了深入探究环形扰动对爆轰波传播的影响,精确、清晰观察环形管道中爆轰波的传播动力学过程,更好地体现边界层效应和曲率管壁对爆轰波传播的影响。搭建环形扰动爆轰实验装置,在光滑圆管末段加入不同直径尺寸的扰动管实现环形扰动,利用压力传感器、烟膜组成的数据采集系统得到爆轰波速度、三波点轨迹、胞格结构等数据。成功搭建了环形扰动爆轰实验系统,并且获得了较为理想的传播数据,数据具有显著的规律性和高度的可靠性。经过验证,所搭建的爆轰实验装置具有良好的数据采集能力,所获得的数据证实了装置具备科学性与有效性。所搭建的实验系统有助于为事故防控提供理论支持,使科研仪器充分发挥支撑科技创新、社会发展的作用。

, correspAuthors=赵焕娟, authorNote=null, correspAuthorsNote=
* 赵焕娟(1985—),女,汉族,山东日照人,博士,教授。研究方向:爆轰机理、冲击动力学。E-mail:。
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高玉坤(1983—),男,汉族,山东胶州人,博士,高级工程师。研究方向:实验室安全与管理。E-mail:。

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高玉坤(1983—),男,汉族,山东胶州人,博士,高级工程师。研究方向:实验室安全与管理。E-mail:。

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高玉坤(1983—),男,汉族,山东胶州人,博士,高级工程师。研究方向:实验室安全与管理。E-mail:。

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A Detonation pipeline group visually displaying the transverse and longitudinal wave structure of spiral detonation: CN108831275B[P]. 2020-07-31., articleTitle=null, refAbstract=null)], funds=[Fund(id=1261262746486715222, tenantId=1146029695717560320, journalId=1146123166801305609, articleId=1261262689964273997, awardId=SKLCS-2024023, language=CN, fundingSource=化学品安全全国重点实验室开放课题项目(SKLCS-2024023), fundOrder=null, country=null)], companyList=[AuthorCompany(id=1261262705365758415, tenantId=1146029695717560320, journalId=1146123166801305609, articleId=1261262689964273997, xref=1, ext=[AuthorCompanyExt(id=1261262705453838800, tenantId=1146029695717560320, journalId=1146123166801305609, articleId=1261262689964273997, companyId=1261262705365758415, language=EN, country=null, province=null, city=null, postcode=null, companyName=null, departmentName=null, remark=1 School of Resources and Safety Engineering, University of Science and Technology Beijing, Beijing 100083, China), AuthorCompanyExt(id=1261262705785188820, tenantId=1146029695717560320, journalId=1146123166801305609, articleId=1261262689964273997, companyId=1261262705365758415, language=CN, country=null, province=null, city=null, postcode=null, companyName=null, departmentName=null, remark=1 北京科技大学土资源与安全工程学院, 北京 100083)]), AuthorCompany(id=1261262706422723044, tenantId=1146029695717560320, journalId=1146123166801305609, articleId=1261262689964273997, xref=2, ext=[AuthorCompanyExt(id=1261262706514997735, tenantId=1146029695717560320, journalId=1146123166801305609, articleId=1261262689964273997, companyId=1261262706422723044, language=EN, country=null, province=null, city=null, postcode=null, companyName=null, departmentName=null, remark=2 School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China), AuthorCompanyExt(id=1261262706586300906, tenantId=1146029695717560320, journalId=1146123166801305609, articleId=1261262689964273997, companyId=1261262706422723044, language=CN, country=null, province=null, city=null, postcode=null, companyName=null, departmentName=null, remark=2 北京理工大学宇航学院, 北京 100081)])], figs=[ArticleFig(id=1261262736630100711, tenantId=1146029695717560320, journalId=1146123166801305609, articleId=1261262689964273997, language=EN, label=Fig.1, caption=Ring disturbance detonation experiment platform, figureFileSmall=mSAe0sOXmHSHWbX4Xdkm8A==, figureFileBig=CPXH+IJLWbzf0nO0rtSVvw==, tableContent=null), ArticleFig(id=1261262736835621612, tenantId=1146029695717560320, journalId=1146123166801305609, articleId=1261262689964273997, language=CN, label=图1, caption=环形扰动爆轰实验平台

w为环形管道宽度

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V为实验中测得爆轰波传播速度;VCJ为理论CJ速度;D为圆形管道直径;P0为管道内初始压力

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PCB113B27 pressure sensor parameters

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传感器型号 PCB113B27
测量范围/kPa 689.4
灵敏度/(mV·kPa-1) 7.25
分辨率/kPa 0.007
共振频率/kHz ≥500
响应时间/☐s ≤1.0
), ArticleFig(id=1261262746230862669, tenantId=1146029695717560320, journalId=1146123166801305609, articleId=1261262689964273997, language=CN, label=表1, caption=

PCB113B27压力传感器参数

, figureFileSmall=null, figureFileBig=null, tableContent=
传感器型号 PCB113B27
测量范围/kPa 689.4
灵敏度/(mV·kPa-1) 7.25
分辨率/kPa 0.007
共振频率/kHz ≥500
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环形扰动爆轰实验装置及方法
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高玉坤 1 , 包颖昕 1 , 卢宇轩 1 , 刘婧 2 , 杨轶芙 1 , 赵焕娟 1, *
科学技术与工程 | 论文·力学 2025,25(20): 8364-8370
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科学技术与工程 | 论文·力学 2025, 25(20): 8364-8370
环形扰动爆轰实验装置及方法
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高玉坤1 , 包颖昕1, 卢宇轩1, 刘婧2, 杨轶芙1, 赵焕娟1, *
作者信息
  • 1 北京科技大学土资源与安全工程学院, 北京 100083
  • 2 北京理工大学宇航学院, 北京 100081

    • 高玉坤(1983—),男,汉族,山东胶州人,博士,高级工程师。研究方向:实验室安全与管理。E-mail:。

通讯作者:

* 赵焕娟(1985—),女,汉族,山东日照人,博士,教授。研究方向:爆轰机理、冲击动力学。E-mail:。
Experimental Device and Method of Annular Perturbation Detonation
Yu-kun GAO1 , Ying-xin BAO1, Yu-xuan LU1, Jing LIU2, Yi-fu YANG1, Huan-juan ZHAO1, *
Affiliations
  • 1 School of Resources and Safety Engineering, University of Science and Technology Beijing, Beijing 100083, China
  • 2 School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
出版时间: 2025-07-18 doi: 10.12404/j.issn.1671-1815.2405473
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摘要
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由于含能材料的高热值及其伴随着易燃易爆的特性,在管道中传播时会影响管道的形状及几何尺寸,导致爆轰的传播受到影响。为了深入探究环形扰动对爆轰波传播的影响,精确、清晰观察环形管道中爆轰波的传播动力学过程,更好地体现边界层效应和曲率管壁对爆轰波传播的影响。搭建环形扰动爆轰实验装置,在光滑圆管末段加入不同直径尺寸的扰动管实现环形扰动,利用压力传感器、烟膜组成的数据采集系统得到爆轰波速度、三波点轨迹、胞格结构等数据。成功搭建了环形扰动爆轰实验系统,并且获得了较为理想的传播数据,数据具有显著的规律性和高度的可靠性。经过验证,所搭建的爆轰实验装置具有良好的数据采集能力,所获得的数据证实了装置具备科学性与有效性。所搭建的实验系统有助于为事故防控提供理论支持,使科研仪器充分发挥支撑科技创新、社会发展的作用。

爆轰实验  /  环形扰动  /  胞格结构  /  三波点轨迹

Due to the high calorific value of energetic materials combined with their flammable and explosive nature. The propagation in the tube will affect the shape and geometric dimensions of the tube, resulting in the propagation of detonations is affected. In order to deeply investigate the influence of annular perturbation on the propagation of detonation waves, accurately and clearly observe the propagation dynamics of the detonation wave in annular tube, and better reflect the influence of boundary layer effect and curvature tube wall on detonation waves.An annular disturbance detonation experimental device was built up. Annular disturbance was realized by adding disturbance tubes with different diameters to the end of the smooth circular tube. The detonation wave velocity, triple-point trajectory, and cell structure were observed by using a data acquisition system composed of pressure sensors and smoke films. The experimental system of annular disturbance detonation was constructed successfully. It was able to obtain the ideal propagation data with remarkable regularity and high reliability. After verification, the detonation experimental device built has excellent data acquisition capabilities, and the obtained data confirms that the device is scientific and effective. The experimental system built contributes to providing theoretical support for accident prevention and control, allowing scientific instruments to play a more significant role in supporting technological innovation and societal development.

detonation experiment  /  annular perturbation  /  cellular structure  /  triple point trajectory
高玉坤, 包颖昕, 卢宇轩, 刘婧, 杨轶芙, 赵焕娟. 环形扰动爆轰实验装置及方法. 科学技术与工程, 2025 , 25 (20) : 8364 -8370 . DOI: 10.12404/j.issn.1671-1815.2405473
Yu-kun GAO, Ying-xin BAO, Yu-xuan LU, Jing LIU, Yi-fu YANG, Huan-juan ZHAO. Experimental Device and Method of Annular Perturbation Detonation[J]. Science Technology and Engineering, 2025 , 25 (20) : 8364 -8370 . DOI: 10.12404/j.issn.1671-1815.2405473
正文
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科学发展和科技创新离不开科研仪器的支撑。与发达国家相比,中国科研仪器的利用率还有很大差距,共享水平仍有待提高,对外服务率和跨区域共享水平更是有待提升。中国科研仪器充分发挥支撑科技创新、社会发展的作用还没有实现[1]。
含能材料由于其热值高被广泛应用于工业生产,如发动机工业[2-4]、太阳能电池[5]、火炸药[6]等。但是含能材料作为易燃易爆物,具有爆炸性和爆燃性,在追求高能化的过程中,会部分牺牲掉热安全性,也存在巨大的安全隐患[7-8]。因此,学者们对含能材料的爆轰特性进行研究,测量其爆轰传播过程中的速度波动[9],并用烟膜技术捕捉测量了爆轰波的胞格结构。胞格结构是实验结果分析的重要参数[10],胞格尺寸是描述爆轰传播的重要参数[11]。在爆轰波传播过程中,横波、马赫杆和前导激波的交点轨迹构成了鱼鳞形的胞格结构[12],胞格尺寸的大小与爆轰化学反应强弱程度有关,胞格的分布规律一定程度上也可以反映出可燃气体的性质[11,13-14]。
边界条件是爆轰传播的重要影响因素[15],在以往实验研究中发现,使用粗糙壁[16]、吸声壁[17]、多孔壁[18]和多孔材料[19-20]等会导致爆轰波传播出现较大的速度损失,甚至爆轰失效的情况。管道的形状及几何尺寸也会对爆轰有影响,相较于方形管道,圆形管道截面积大于方形,可以输送更多的流体且受力更加均匀。在普通圆形管道中加入扰动管形成环形管道,具有结构紧凑、传热面积大、流动性好、传热系数高等显著优点,可以更好地体现边界层效应和曲率管壁对爆轰波传播的影响[21-23],近年来在诸如石油化工[24]、电力[25]、航天推进[26]等技术行业已受到关注,如旋转爆轰发动机环形构造的燃烧室等。
在环形扰动爆轰研究方面,贺顺江等[27]研究了不同含量氩气稀释过的乙炔-氧气爆轰波经直管道沿切向进入环形通道中的传播过程和模式,发现环形通道的宽度会使高浓度或低浓度气体爆轰波的临界管径趋近于经典衍射问题中不稳定爆轰波的临界管径。孟豪龙等[28]使用OpenFOAM软件对环形燃烧室中凹腔对旋转爆轰流畅的影响进行研究,发现相较于同轴圆环形旋转爆轰燃烧室,凹腔基环形旋转爆轰燃烧室具有更大的速度亏损。褚驰等[29]采用OpenFOAM软件对爆轰波进入发动机环形燃烧室传播过程进行数值模拟研究,发现爆轰波在进入环形燃烧室后衰减为燃烧波,并存在“初始爆轰波解耦-爆燃转爆轰-触发旋转爆轰波”的过程。杨怀远等[30]对火焰在环形通道内的形态演变过程进行实验研究,发现环形通道几何效应对火焰传播影响并产生一系列火模式,其舌形火焰在爆轰起爆过程中发挥了重要作用。Yao等[31]对环形通道中爆轰波传播的胞格结构特征进行研究,发现环形通道对胞格结构的影响取决于内半径和通道宽度。由此可见,环形扰动对爆轰波及火焰传播、爆轰波胞格结构都产生了巨大的影响。因此,展开环形扰动对爆轰波传播动力学影响的研究具有极大的重要性。
鉴于此,搭建环形扰动爆轰实验装置,在光滑圆管末段加入不同直径尺寸的扰动管实现环形扰动,利用压力传感器记录爆轰波到达时间并通过距离时间计算爆轰传播速度,分析速度波动。同时,使用烟膜记录爆轰过程在环形管壁面、扰动管内外壁面、管道端面留下的三波点轨迹,观察环管中爆轰波的传播动力学过程,研究环形扰动对爆轰波传播的作用,有助于为事故防控提供理论支持。
1 气相爆轰实验技术
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1.1 实验装置系统
基于真实输运管道特征自主搭建了环形扰动爆轰实验装置,如图1所示。整个环形管道实验系统是由管道系统、数据采集系统、充配气系统、点火系统和气体监测系统组成。
1.2 管道系统
为充分研究和分析爆轰波传播过程中的特性,管道管径需胞格尺寸大小,爆轰传播机理可以量化为$\frac{d}{\lambda }$=1,其中,$\lambda $为一个胞格尺寸的大小,d为爆轰管道管径大小。管径应大于一个爆轰波胞格尺寸,才能够使爆轰波正常、稳定传播。因此,设计环形扰动爆轰实验装置的管道系统为内径80 mm。管道长度由过驱和稳定传播长度的总长度决定,包含驱动段和实验段,因此设计两段管道长度均为2 m,使数据采集系统能够完整记录爆轰波的起爆及传播过程。
管道共有4节,每节长1 000 mm、厚度5 mm,各节管道首尾端部为开槽的法兰,相邻法兰之间使用螺丝进行连接,并加入橡胶垫片以保证实验的密闭性,每次实验前必须对爆轰管道进行气密性检查。
管道系统由驱动段和实验段组成,分别为2 000 mm。驱动段内部设有直径为80 mm的铜制Shchelkin螺旋线来促进稳定爆轰的形成。实验段分为实验段前段和后段。在实验段后段中分别插入3种内径d=20、40、60 mm的扰动管构成3种尺寸的环形管道,扰动管长度均为1 000 mm,厚度均为5 mm,得到宽度w=25、15、5 mm的环形通道。扰动管实物图如图2所示。
1.3 数据采集系统
1.3.1 烟膜系统
爆轰波实际上是三维结构,横波、马赫杆和前导激波碰撞形成三波点并在该点局部区域产生高温高压区,从而在烟熏薄膜上擦除烟尘留下三波点轨迹,左旋和右旋三波点轨迹交叉构成了菱形的胞格结构。采用厚度为1 mm,长度1 000 mm的PVC薄膜作为烟迹载体[32],具体宽度根据实验管道内壁周长进行剪裁。在对薄膜烟熏之前需先使用酒精湿巾擦拭,去除薄膜表面残留的灰尘等颗粒杂物,有利于后续烟尘颗粒的吸附。本实验烟膜使用煤油燃料进行熏制,熏制过程中在煤油灯罩出烟口处放置铁丝网片,可以吸附过滤煤油燃烧过程中较大的烟尘颗粒,保证烟熏膜上烟尘的均匀性。此外在熏制过程中应时刻注意调整PVC薄膜和火焰之间的距离,确保烟尘颗粒分布均匀,颗粒堆积厚度一致。
如图3所示,烟膜制作完成后将其放置于合适方式记录管道中不同位置的横波结构与纵波结构[33],如在内部管内壁和外壁、外管内壁、端面处放置烟膜,直观显示管道中距管道中心线不同极径处的横波与纵波结构。烟膜背面需与管道内壁面紧贴无缝隙,需在两端贴置双面胶,同时烟膜在管道内应留出一定空隙确保不会遮挡压力传感器探头。为防止人为操作等原因带来的偶然性实验结果,通常在实验中对每组条件进行三次实验。通过记录不同极径处螺旋爆轰横波结构,并与对应的纵向波结构对比分析,有助于几何体现爆轰波在不同截面处的三维结构,对于爆轰结构研究与探索具有重要的意义。
1.3.2 压力传感器系统
爆轰波传播过程是瞬时行为,传播速度约为2 000 m/s,因此捕捉爆轰波的瞬时压力对于传感器的采样频率有较高要求。本实验装置系统中采用压电式压力传感器,型号为PCB113B27。表1为PCB113B27压力传感器的参数。压力传感器系统主要由压力传感器、482C信号调节器和DS1104示波器组成。图4为PCB113B27压力传感器、482C信号调节器和DS1104示波器的实物图。压力传感器将采集到的压力信号转变为电信号,经过调节器输入至示波器从而将电信号转变为可视化的波形图像,爆轰波抵达压力传感器处时传感器电信号发生突跃,在示波器上显示为出现电压波峰,之后可以将波形图保存在电脑。
1.4 充配气系统
图5为本实验装置系统中的充配气系统示意图,主要包括控制面板、真空泵、压力表、混气瓶、燃料气瓶、氧气瓶、氩气瓶、爆轰管道。配气流程为首先通过塑胶软管连接各控制面板、气瓶和真空泵,检查整个气体通路的气密性。气密性满足要求后打开真空泵和混气瓶之间的阀门,将混气瓶抽至真空后关闭真空泵和阀门。之后采用道尔顿分压法依次将燃料气、氩气、氧气充入混气瓶中,每次充入新的气体之前需先将塑胶软管中的残留气体排出,抽至真空状态。混合后的气体需在混气瓶中静置24 h确保预混气体的均匀性。充气流程为每组实验之前,通过控制面板将真空泵和爆轰管道连通,使用真空泵将管道内部抽为真空,之后关闭阀门,通过压力表监测管道内压力变化,若管道内压力可维持稳定数值5 min即可视为爆轰管道气密性合格。再次使用真空泵对管道抽真空,之后通过控制面板关闭真空泵阀门,打开混气瓶管道阀门和混气瓶阀门将预混气缓慢充入爆轰管道,当爆轰管道内压力达到实验压力时关闭所有阀门,利用真空泵将塑胶管道中的残留预混气抽出排至室外。
1.5 点火系统
本实验装置中的点火系统所采用的点火方式为高压电火花点火,图6为电火花点火系统示意图。高压点火系统主要由高压电源、电容组、触发器和火花塞组成。在点火之前,首先连接电容组和高压电源,对电容组进行充电,当达到15 kV时关闭高压电源,然后按下触发器,电容组可以对火花塞放电从而引爆管道内的可燃预混气体。
1.6 气体监测系统
本实验涉及的危险因素较多,可燃预混气一旦在实验过程中发生泄漏遇到电火花或其他火源非常容易引发火灾爆炸事故。因此需要设置气体监测装置对整个实验环境进行监测,针对实验气体选用了气体检测器,如图7所示。
2 爆轰实验系统数据获取与分析
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爆轰实验数据通过数据采集系统收集。而后,经由专业的数据处理方法,能够从中提取出具有重要研究价值的爆轰波特性数据,涵盖爆轰波传播速度、胞格尺寸以及结构等关键参数。
爆轰波速度可通过压力传感器系统获得。根据数据采集系统中将电信号转变为的可视化波形图像,爆轰波抵达压力传感器处时传感器电信号发生突跃,在示波器上显示为出现电压波峰,如图8所示。通过电压波峰判断每个探针监测数据的时间,可以用来预估推进剂点火起爆的时间。通过管道两个相邻电探针之间的距离除以波峰出现的时间差,可以得到爆轰波的传播速度。
胞格尺寸及其结构能够借助烟膜系统予以获取。为了更为清晰地描绘甲烷-氧预混气的爆轰波传播结构,可对烟膜进行扫描操作,并运用 PS 处理技术剔除烟膜的背景层,采用50%灰度的图层作为背景,进而获取仅包含三波点轨迹线的图片。
所设计的实验装置已进行多组实验,得到的实验数据结果近似。通过本装备可以得到爆轰波速度和胞格结构数据如图9所示。实验装置得到的结果较为理想,能够明确看出,爆轰波速度的衰减,胞格结构清晰可见,满足装置设计要求。
结果(图9)显示,本装置所得数据具有明显的规律性,并且能够在不同的初始条件下进行实验,具有实验可靠性。这充分证明了本实验装置的科学性,能为研究提供更可靠的数据支持。
3 结论
收起
(1)搭建环形扰动爆轰实验平台,实物为管径80 mm,长度为4 000 mm的高强度不锈钢光滑圆管。爆轰实验装置系统由管道系统、数据采集系统、充配气系统、点火系统及气体检测系统组成。通过在圆管中设置不同的环形管道(w = 25、15、5 mm),并利用压力传感器、烟膜构成的数据采集系统获得爆轰波速度、三波点轨迹、胞格结构等,观察环管中爆轰波的传播动力学过程,研究环形扰动对爆轰波传播的作用。
(2)本实验装置能够完整记录爆轰波的传播过程,并可以清晰地观察和记录胞格结构、爆轰波速度等数据,数据较为理想。由此可见,环形扰动爆轰实验平台拓宽了传统实验管道的初始条件,提出了横波及纵波结构的测试方法,有助于几何体现爆轰波在不同截面处的三维结构。
基金
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  • 化学品安全全国重点实验室开放课题项目(SKLCS-2024023)
文献
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2025年第25卷第20期
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doi: 10.12404/j.issn.1671-1815.2405473
  • 接收时间：2024-07-21
  • 首发时间：2026-05-13
  • 出版时间：2025-07-18
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  • 收稿日期：2024-07-21
  • 修回日期：2025-04-15
基金
化学品安全全国重点实验室开放课题项目(SKLCS-2024023)
作者信息
    1 北京科技大学土资源与安全工程学院, 北京 100083
    2 北京理工大学宇航学院, 北京 100081

通讯作者:

* 赵焕娟(1985—),女,汉族,山东日照人,博士,教授。研究方向:爆轰机理、冲击动力学。E-mail:。
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