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一种屏蔽式总温探头设计及其测量误差估计

季念 马朝臣

季念, 马朝臣. 一种屏蔽式总温探头设计及其测量误差估计[J]. 航空动力学报, 2023, 38(7):1749-1761 doi: 10.13224/j.cnki.jasp.20210620
引用本文: 季念, 马朝臣. 一种屏蔽式总温探头设计及其测量误差估计[J]. 航空动力学报, 2023, 38(7):1749-1761 doi: 10.13224/j.cnki.jasp.20210620
JI Nian, MA Chaochen. Design and measurement error estimation of a shielded total temperature probe[J]. Journal of Aerospace Power, 2023, 38(7):1749-1761 doi: 10.13224/j.cnki.jasp.20210620
Citation: JI Nian, MA Chaochen. Design and measurement error estimation of a shielded total temperature probe[J]. Journal of Aerospace Power, 2023, 38(7):1749-1761 doi: 10.13224/j.cnki.jasp.20210620

一种屏蔽式总温探头设计及其测量误差估计

doi: 10.13224/j.cnki.jasp.20210620
详细信息
    作者简介:

    季念(1996-),男,硕士生,主要从事叶轮机械气体动力学方面的研究

    通讯作者:

    马朝臣(1959-),男,教授、博士生导师,博士,主要从事叶轮机械方面的研究。E-mail:mcc1900@bit.edu.cn

  • 中图分类号: V231

Design and measurement error estimation of a shielded total temperature probe

  • 摘要:

    在忽略辐射误差的情况下,使用流固耦合传热数值模拟的方法预测了一种总温探头在不同工况下的速度误差和导热误差。结果表明:在马赫数为0.2~0.6的范围内,导热误差都保持在较小值;总误差的90%以上由速度误差贡献;最大测量误差为1.13 K,比结构A、结构B、结构C以及结构D分别低了331.6%、119.4%、61.6%以及59.5%;速度误差和导热误差存在互相影响的关系,存在最优解可使总误差最小;适用于等温来流和马赫数大于0.5的高速非等温来流的总温测量。最后探讨了热电偶节点位置对测量精度的影响,节点在从设计点远离支持体的过程中,测量误差遵循着先增大后减小的变化规律。

     

  • 图 1  热电偶传热示意图

    Figure 1.  Heat transfer diagram of thermocouple

    图 2  偶丝方向与来流方向的两种关系

    Figure 2.  Two relations between wire direction and incoming flow direction

    图 3  计算域示意图

    Figure 3.  Diagram of computing domaim

    图 4  计算域网格

    Figure 4.  Grid of computational domain

    图 5  Ma=0.5和Ma=0.6时屏蔽罩壁面周围气流流动

    Figure 5.  Airflow around shield wall when Ma=0.5, Ma=0.6

    图 6  Ma=0.6时节点壁面和屏蔽罩壁面的$ {y}^{+} $

    Figure 6.  Wall $ {y}^{+} $ of junction and shield when Ma=0.6

    图 7  数值计算结果与经验公式计算结果对比

    Figure 7.  Comparison between numerical calculation results and empirical formula calculation results

    图 8  不同结构的总温测量设备

    Figure 8.  Total temperature measuring equipment of different structures

    图 9  不同结构总温热电偶测量误差预测结果

    Figure 9.  Prediction results of total temperature thermocouple measurement error of different structures

    图 10  不同落压比和进口温度下出口温度测量误差为1 K时涡轮机绝热效率测量误差

    Figure 10.  Measurement error of turbine adiabatic efficiency when the measurement error of outlet temperature is 1 K under different pressure drop ratios and inlet temperatures

    图 11  裸线式热电偶探头结构简图

    Figure 11.  Structure sketch of bare wire thermocouple probe

    图 12  总温热电偶几何尺寸(单位:mm)

    Figure 12.  Geometric dimensions of total temperature thermocouple (unit: mm)

    图 13  数值计算预测的各类测量误差大小及其百分比

    Figure 13.  Size and percentage of various measurement errors predicted by numerical calculation

    图 14  不同结构总温热电偶测量误差预测结果

    Figure 14.  Prediction results of total temperature thermocouple measurement error of different structures

    图 15  总温探头测量非等温来流示意图

    Figure 15.  Diagram of non-isothermal incoming flow measured by total temperature probe

    图 16  不同温差下总温探头的测量误差

    Figure 16.  Measurement error of total temperature probe under different temperature differences

    图 17  屏蔽罩上5个截面

    Figure 17.  Five sections on the shield

    图 18  Ma=0.3时截面$ {S}_{1} $$ {S}_{2} $$ {S}_{3} $$ {S}_{4} $以及$ {S}_{5} $的流线图

    Figure 18.  Streamlines of sections $ {S}_{1} $, $ {S}_{2} $, $ {S}_{3} $, $ {S}_{4} $ and $ {S}_{5} $ when Ma=0.3

    图 19  Ma=0.6时截面$ {S}_{1} $$ {S}_{2} $$ {S}_{3} $$ {S}_{4} $以及$ {S}_{5} $的流线图

    Figure 19.  Streamlines of sections $ {S}_{1} $, $ {S}_{2} $, $ {S}_{3} $, $ {S}_{4} $ and $ {S}_{5} $ when Ma=0.6

    图 20  Ma=0.5时$ {S_2} $截面上流线图和温度云图

    Figure 20.  Streamlines and temperature contour on section $ {S_2} $ when Ma=0.5

    图 21  Ma=0.5时$ {S_4} $截面上流线图和温度云图

    Figure 21.  Streamlines and temperature contour on section $ {S_4} $ when Ma=0.5

    图 22  型号1、2和3在Ma=0.6时截面$ {S}_{2} $的流线图

    Figure 22.  Streamlines of section $ {S}_{2} $ for models 1, 2 and 3 when Ma=0.6

    图 23  型号1、2和3在Ma=0.6时截面$ {S}_{1} $的流线图

    Figure 23.  Streamlines of section $ {S}_{1} $ for models 1, 2 and 3 when Ma=0.6

    表  1  网格无关性验证

    Table  1.   Verification of grid independence

    网格名称网格数/万Tj/K
    第1套314338.75
    第2套467338.59
    第3套628338.57
    下载: 导出CSV

    表  2  仿真工况

    Table  2.   Simulation conditions

    工况$ {V}_{\mathrm{i}\mathrm{n}} $$ {T}_{\mathrm{s}} $/K$ {p}_{\mathrm{o}\mathrm{u}\mathrm{t}} $/Pa
    AMa=0.2
    BMa=0.3
    CMa=0.4323.15101325
    DMa=0.5
    EMa=0.6
    下载: 导出CSV

    表  3  使用Moffat误差估计公式对裸线式热电偶测量误差进行估计的结果

    Table  3.   Estimation results of measurement error of bare wire thermocouple using Moffat error estimation formula

    Ma${T}_{\mathrm{j} }/{\rm{K}}$$ {T}_{0}/{\rm{K}} $$ {E}_{\mathrm{v}}/{\rm{K}} $$ {E}_{\mathrm{c}}/{\rm{K}} $$ {E}_{\mathrm{r}}/{\rm{K}} $$ E/{\rm{K}} $
    0.2325.1325.7$ 0.65~1.00 $$ 0.38~0.44 $$0.002\;1~0.002\;8$$ 1.03~1.45 $
    0.3327.5329.0$ 1.45~2.68 $$ 0.76~0.89 $$0.003\;7~0.004\;9$$ 2.21~3.16 $
    0.4330.9333.5$ 2.59~4.03 $$ 1.21~1.45 $$0.005\;7~0.007\;6$$ 3.80~5.49 $
    0.5353.3339.3$ 4.04~6.30 $$ 1.72~2.09 $$0.008\;1~0.011\;0$$ 5.77~8.40 $
    0.6340.6346.4$ 5.82~9.07 $$ 2.25~2.78 $$0.011\;0~0.015\;0$$ 8.08~11.86 $
    下载: 导出CSV

    表  4  总温热电偶使用材料[4]

    Table  4.   Materials used for total temperature thermocouple[4]

    名称材料导热系数/
    $(\mathrm{W}/ (\mathrm{m}\cdot \mathrm{K}) )$
    发射率
    屏蔽罩不锈钢150.85
    左偶丝镍硅合金29.710.9
    右偶丝镍硅合金19.250.9
    偶丝节点24.480.9
    支持体尼龙0.20.1
    下载: 导出CSV

    表  5  3种改型偶丝的长度和直径

    Table  5.   Length and diameter of three modified wires

    型号偶丝长/mm偶丝直径/mm长径比
    原型1.70.35.67
    改型12.40.38
    改型22.40.1516
    改型33.10.39.3
    下载: 导出CSV

    表  6  改型后3种屏蔽式总温热电偶在Ma=0.6时的误差组成及增量百分比

    Table  6.   Error composition and increment percentage of three shielded total temperature thermocouples after modification when Ma=0.6

    型号$ {E}_{\mathrm{c}}/{\rm{K}} $${\delta }_{\mathrm{c} }/{\text{%}}$$ {E}_{\mathrm{v}}/{\rm{K}} $${\delta }_{\mathrm{v} }/{\text{%}}$$ E/{\rm{K}} $$\delta /{\text{%}}$
    原型0.1151.0141.129
    10.048−56.51.30628.81.35620.1
    20.077−33.01.22120.41.29815.0
    30.091−20.91.12611.01.035−8.3
    下载: 导出CSV
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  • 收稿日期:  2021-10-31
  • 网络出版日期:  2023-04-25

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