红外与激光工程
紅外與激光工程
홍외여격광공정
INFRARED AND LASER ENGINEERING
2014年
6期
1750-1754
,共5页
苏铁%陈爽%杨富荣%陈力%郑尧邦
囌鐵%陳爽%楊富榮%陳力%鄭堯邦
소철%진상%양부영%진력%정요방
平面激光诱导荧光(PLIF)%OH%瞬态燃烧场%二维温度场
平麵激光誘導熒光(PLIF)%OH%瞬態燃燒場%二維溫度場
평면격광유도형광(PLIF)%OH%순태연소장%이유온도장
PLIF%OH%transient combustion%two dimensional temperature field
在复杂的燃烧流场等试验研究中,平面激光诱导荧光技术(PLIF)被用于特定气体分子浓度分布、火焰构造和温度分布的测量。基于双色激光诱导荧光测温原理,设计了双激发PLIF系统,选取两条合适的OH自由基激励线,定量测量了甲烷-空气预混火焰的二维瞬态温度场分布。实验中,通过对两个激光脉冲功率和激光轮廓分布监控以及双ICCD成像的空间位置校正,提高了测量的精细程度。给出了测量结果,并与稳态燃烧场火焰的热电偶测量结果进行了对比,不确定度优于5%,这种二维瞬态测温技术能够满足超声速燃烧诊断中的应用。
在複雜的燃燒流場等試驗研究中,平麵激光誘導熒光技術(PLIF)被用于特定氣體分子濃度分佈、火燄構造和溫度分佈的測量。基于雙色激光誘導熒光測溫原理,設計瞭雙激髮PLIF繫統,選取兩條閤適的OH自由基激勵線,定量測量瞭甲烷-空氣預混火燄的二維瞬態溫度場分佈。實驗中,通過對兩箇激光脈遲功率和激光輪廓分佈鑑控以及雙ICCD成像的空間位置校正,提高瞭測量的精細程度。給齣瞭測量結果,併與穩態燃燒場火燄的熱電偶測量結果進行瞭對比,不確定度優于5%,這種二維瞬態測溫技術能夠滿足超聲速燃燒診斷中的應用。
재복잡적연소류장등시험연구중,평면격광유도형광기술(PLIF)피용우특정기체분자농도분포、화염구조화온도분포적측량。기우쌍색격광유도형광측온원리,설계료쌍격발PLIF계통,선취량조합괄적OH자유기격려선,정량측량료갑완-공기예혼화염적이유순태온도장분포。실험중,통과대량개격광맥충공솔화격광륜곽분포감공이급쌍ICCD성상적공간위치교정,제고료측량적정세정도。급출료측량결과,병여은태연소장화염적열전우측량결과진행료대비,불학정도우우5%,저충이유순태측온기술능구만족초성속연소진단중적응용。
Planar laser induced fluorescence (PLIF) is the most intuitive and effective measurement technology, which shows a broad application prospects in the complex combustion flow field diagnostics because of its abundant information, non-contact, high spatial and temporal resolutions, visualization and other advantages. PLIF technology can provide a two-dimensional imaging and many parameters such as temperature, velocity, component concentration and pressure of some special cross-section in the flame and other flows. A two-excitation planar laser-induced fluorescence (PLIF) system was set up based on the two line PLIF technology. Two dimensional instantaneous temperature distribution of premixed CH4/air flame was measured quantitative by picking two proper spectrum lines. In experiments, by acquiring the power of laser pulses and the profile distribution and revising the spatial positions of the ICCD imaging, the precision was elevated. The measurement results are more precise compared with the results of thermoelectric couple and the uncertainty is less than 5%, which can suffice with the applications in supersonic combustion diagnostics.