航空发动机
航空髮動機
항공발동궤
AERO ENGINE
2011年
4期
24-28,32
,共6页
处理机匣%风扇%数值模拟%稳定性%航空发动机
處理機匣%風扇%數值模擬%穩定性%航空髮動機
처리궤갑%풍선%수치모의%은정성%항공발동궤
casing treatment%fan%numerical simulation%stability%aeroengine
在对驻室式处理机匣内部流动及扩稳机理进行数值研究叫基础上,采用数值模拟方法进一步分析处理机匣对风扇性能的影响。通过取消处理槽上方的驻室,提高了处理机匣对设计转速的扩稳能力。根据叶尖间隙内的相对速度分布和处理机匣内的回流量,分析了处理机匣的扩稳特性。研究结果表明:处理机匣产生扩稳作用的原因在于处理机匣能使转子叶尖进口气流加速,增加流体能量,从而抑制由叶尖泄漏流发展成泄漏涡.讲而改善流动环境。
在對駐室式處理機匣內部流動及擴穩機理進行數值研究叫基礎上,採用數值模擬方法進一步分析處理機匣對風扇性能的影響。通過取消處理槽上方的駐室,提高瞭處理機匣對設計轉速的擴穩能力。根據葉尖間隙內的相對速度分佈和處理機匣內的迴流量,分析瞭處理機匣的擴穩特性。研究結果錶明:處理機匣產生擴穩作用的原因在于處理機匣能使轉子葉尖進口氣流加速,增加流體能量,從而抑製由葉尖洩漏流髮展成洩漏渦.講而改善流動環境。
재대주실식처리궤갑내부류동급확은궤리진행수치연구규기출상,채용수치모의방법진일보분석처리궤갑대풍선성능적영향。통과취소처리조상방적주실,제고료처리궤갑대설계전속적확은능력。근거협첨간극내적상대속도분포화처리궤갑내적회류량,분석료처리궤갑적확은특성。연구결과표명:처리궤갑산생확은작용적원인재우처리궤갑능사전자협첨진구기류가속,증가류체능량,종이억제유협첨설루류발전성설루와.강이개선류동배경。
Based on the numerical study of internal flow and steady expansion mechanism in the chamber casing treatment, a further analysis of the influence of the casing treatment on the performance of a fan had been carried out by numerical simulation. The improvement of the stability was enhanced at design speed without the plenum chamber above the slots. According to the relative velocity in the tip clearance and the mass flow rate in the casing treatment, the steady expansion characteristics of the casing treatment were analyzed. The results indicate that the casing treatment forms a path through which the blockage flow is sucked in and then blown out with high velocity at the front of the casing treatment. This process will suppress the tip leakage flow and the related vortex, and then improve the stability of the compressor.