大氣低壓模擬艙研制與初步應(yīng)用
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公益性(氣象)行業(yè)專項(xiàng)(GYHY201106041)資助


Development and Preliminary Application of Hypobaric Chamber
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    摘要:

    本文介紹了自主研制大氣低壓模擬艙基本參數(shù)及其性能測(cè)試和初步應(yīng)用結(jié)果。艙體尺寸為550~600 mm,長(zhǎng)600 mm,具備自動(dòng)和手動(dòng)兩種氣壓控制方式,艙內(nèi)極限低壓可達(dá)21 hPa。測(cè)試表明:在抽氣時(shí)艙內(nèi)氣壓變化率平均41 hPa/s,艙內(nèi)氣壓對(duì)數(shù)與抽氣時(shí)間在量程范圍內(nèi)基本呈線性變化,壓力響應(yīng)特性曲線隨著氣壓的降低而降低;放氣時(shí)艙內(nèi)氣壓變化率平均66 hPa/s,值在100 hPa附近達(dá)到最大且向氣壓的高、低兩個(gè)方向減小。艙內(nèi)壓力響應(yīng)靜態(tài)點(diǎn)測(cè)試在10 s到1 min內(nèi)為22% ~ 36%,1 ~ 10 min為36±18%。漏氣率在10 min內(nèi)為04 Pa/min, 實(shí)際壓力控制偏差在10、20、40 min和1 h內(nèi)分別為004、01、019和025 hPa。應(yīng)用低壓模擬艙對(duì)美國(guó)SPC 6A型臭氧探空儀在100 hPa以下泵效訂正系數(shù)測(cè)量的結(jié)果與廠家提供的校準(zhǔn)曲線對(duì)比顯示結(jié)果較好,偏差在70 hPa以上泵效小于25%、35~70 hPa小于5%、20~35 hPa小于6%、20 hPa以下小于5%。低壓模擬艙滿足氣象探空儀器檢測(cè)的低壓環(huán)境需求。

    Abstract:

    A self developed hypobaric chamber and its technological parameters, as well as the performance tests and preliminary application, are introduced. The chamber is cylindrical shaped with the dimension of 600 mm in length and 550〖CD*2〗600 mm in diameter. The internal pressure of chamber can be reduced in an automatic or manual mode, and the lowest value can be 21 hPa. Performance testing results show that the average pumping rate of the chamber is 41 hPa/s. The logarithm of pressure in chamber varies linearly with suction time within effective pressure range. The chamber pressure response curve decreases with decreasing pressure, and the average deflation rate of the chamber pressure is 66 hPa/s. The deflation efficiency maximum value is around 100 hPa, with the efficiency reducing from 100 hPa in the higher or lower direction. The static response tests show that the chamber air pressure variability is 22% to 36% in 10〖CD*2〗60 s, and 36±18% in 1〖CD*2〗10 min. The average air leak rate of the chamber is 04 Pa/min in 10 min, and the actual pressure deviations in 10, 20, 40 min and 1 hour is 004, 01, 019, and 025 hPa, respectively. The hypobaric chamber is used for testing the SPC 6A ozonesonde pump efficiency in a low pressure environment. The results show that the deviation of pump efficiency correction factor is <25%, <5%, <6%, and <5%, 〖JP2〗respectively, when the corresponding air pressure is >70 hPa, 70〖CD*2〗35 hPa, 35〖CD*2〗20 hPa, and <20 hPa. These measured pump efficiency correction factors are consist with the original values provided by the manufacture. The hypobaric chamber is expected to provide a low pressure environment for correlative meteorological instrument performance testing.

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田宏民,鄭向東,湯潔,林偉立,楊文.大氣低壓模擬艙研制與初步應(yīng)用[J].氣象科技,2015,43(1):30~35

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  • 收稿日期:2014-01-20
  • 定稿日期:2014-03-05
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  • 在線發(fā)布日期: 2015-02-13
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