原子能科学技术
原子能科學技術
원자능과학기술
ATOMIC ENERGY SCIENCE AND TECHNOLOGY
2014年
3期
447-452
,共6页
卫光仁%柴宝华%魏国锋%毕可明%冯波%韩冶%龙俞伊
衛光仁%柴寶華%魏國鋒%畢可明%馮波%韓冶%龍俞伊
위광인%시보화%위국봉%필가명%풍파%한야%룡유이
干道%高温热管%极限传热功率%重力
榦道%高溫熱管%極限傳熱功率%重力
간도%고온열관%겁한전열공솔%중력
artery%high temperature heat pipe%limit heat transfer power%gravity
干道式高温热管传热性能试验主要是为了获得干道式热管在不同温度范围的传热极限及重力场对传热极限的影响。在真空条件下启动热管,调节水套气隙氩气和氦气比例来测量声速极限,建立可调角度台架得到不同倾角下热管的极限传热性能。试验得到400~650℃工作温度下热管的极限传热功率曲线及不同倾角下热管的极限传热功率。此类热管510℃以下传热极限为声速限;±10°范围内重力对传热极限无影响;极限传热功率为2.8 kW。
榦道式高溫熱管傳熱性能試驗主要是為瞭穫得榦道式熱管在不同溫度範圍的傳熱極限及重力場對傳熱極限的影響。在真空條件下啟動熱管,調節水套氣隙氬氣和氦氣比例來測量聲速極限,建立可調角度檯架得到不同傾角下熱管的極限傳熱性能。試驗得到400~650℃工作溫度下熱管的極限傳熱功率麯線及不同傾角下熱管的極限傳熱功率。此類熱管510℃以下傳熱極限為聲速限;±10°範圍內重力對傳熱極限無影響;極限傳熱功率為2.8 kW。
간도식고온열관전열성능시험주요시위료획득간도식열관재불동온도범위적전열겁한급중력장대전열겁한적영향。재진공조건하계동열관,조절수투기극아기화양기비례래측량성속겁한,건립가조각도태가득도불동경각하열관적겁한전열성능。시험득도400~650℃공작온도하열관적겁한전열공솔곡선급불동경각하열관적겁한전열공솔。차류열관510℃이하전열겁한위성속한;±10°범위내중력대전열겁한무영향;겁한전열공솔위2.8 kW。
Heat transfer experiments to obtain heat transfer limit at different tempera-tures and the effect of gravity on heat transfer limit for heat pipe with arteries were per-formed .The heat pipe was started up under vacuum condition ,and the angle adjustable bench was built to obtain properties of heat transfer limit at different angles . The profiles of the limit heat transfer power for heat pipe were got at the working temperature from 400 ℃ to 650 ℃ and at different angles .Under the temperature of 510 ℃ ,the limit of heat transfer for this type heat pipe is sound velocity limit .Gravity has little effect on heat transfer limit under the angle zone ± 10° .The limit heat transfer power of this type heat pipe is 2.8 kW .