推进技术 ›› 2009, Vol. 30 ›› Issue (6): 656-660.

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超临界RP-3管内换热特性实验

王英杰,徐国强,邓宏武,罗翔   

  1. 北京航空航天大学航空发动机气动热力重点实验室;北京航空航天大学航空发动机气动热力重点实验室;北京航空航天大学航空发动机气动热力重点实验室;北京航空航天大学航空发动机气动热力重点实验室
  • 发布日期:2021-08-15
  • 基金资助:
    国家自然科学基金(50676005)

Experimental investigation on heat transfer of supercritical RP-3

  1. National Key Laboratory of Aircraft Engine, Beijing Univ.of Aeronautics and Astronautics, Beijing 100191, China;National Key Laboratory of Aircraft Engine, Beijing Univ.of Aeronautics and Astronautics, Beijing 100191, China;National Key Laboratory of Aircraft Engine, Beijing Univ.of Aeronautics and Astronautics, Beijing 100191, China;National Key Laboratory of Aircraft Engine, Beijing Univ.of Aeronautics and Astronautics, Beijing 100191, China
  • Published:2021-08-15

摘要: 实验研究了超临界RP-3管内换热特性。实验段为2100mm长、外径2.2mm,内径1.8mm不锈钢管(材质:1Cr18Ni9Ti)。RP-3在5MPa压力下流经该实验管,采用近似等热流加热方式将其从127℃加热至427℃。通过测量0min,20min,30min,45min和60min时管外壁和流体温度得到管内对流换热系数hin沿流向分布、结焦对管内传热系数Kin影响。研究结果表明:在远离临界点的亚临界区域,hin随着RP-3温度上升逐渐增大;在近临界区管内对流换热系数迅速增加;而进入超临界区域后,hin保持在1.8×104W/(m·℃)附近;结焦对管内传热影响显著,Kin随结焦增多逐渐降低,而降幅逐渐减小。

关键词: 燃气轮机;超临界;加热;对流;传热系数;结焦

Abstract: Experiments are performed to investigate heat transfer characteristics of supercritical RP-3. The test section is a 2 100 mm long, 2.2 mm O.D., 1.8 mm I.D., stainless steel tube (manufactured with 1Cr18Ni9Ti). RP-3 is heated electrically up to 427℃ from 127℃ as it flows through the test tube. The variation of convective heat transfer coefficient(hin) along the tube is achieved by measuring outer tube and fuel temperature at 0 min, 20 min, 30 min, 45 min and 60 min. The influence of coke deposition on heat transfer is also studied. The experimental results reveal that hin increases gradually as RP-3 temperature rises up in subcritical state, hin maintains at a constant value as it reaches to approximately 1.8×104 W/(m2·℃) for supercritical RP-3. The heat transfer is enhanced significantly at near-critical zone. The coke deposition has great effects on RP-3 heat transfer, which decreases as coke accumulated on tube surface.

Key words: Gas turbine;Supercriticality;Heating;Convection;Heat transfer coefficient;Coke deposition+