燃气涡轮试验与研究
燃氣渦輪試驗與研究
연기와륜시험여연구
GAS TURBINE EXPERIMENT AND RESEARCH
2013年
4期
8-12,17
,共6页
压气机%叶片造型方法%均匀B样条%激波%Bézier曲线%定制叶型
壓氣機%葉片造型方法%均勻B樣條%激波%Bézier麯線%定製葉型
압기궤%협편조형방법%균균B양조%격파%Bézier곡선%정제협형
compressor%blading method%uniform B-spline%shock wave%Bézier curve%tailored airfoil
应用目前先进的自由曲线理论，开发了一种新的叶片造型方法--B样条控制中线角叶型(BMAA)方法。分别选取准均匀B样条和贝塞尔曲线，实现了对叶型中线和厚度的方便、灵活控制；同时综合考虑方便性与实用性，选取四点控制参数进行设计。分别利用BMAA方法与原有定制叶型、任意中线方法，对某单级压气机进行设计，结果表明：对于超/跨声叶片设计，BMAA方法设计的叶片性能略优于定制叶型；与任意中线叶型达到的性能相当，但叶型控制便捷性和叶型光滑性优于任意中线叶型。
應用目前先進的自由麯線理論，開髮瞭一種新的葉片造型方法--B樣條控製中線角葉型(BMAA)方法。分彆選取準均勻B樣條和貝塞爾麯線，實現瞭對葉型中線和厚度的方便、靈活控製；同時綜閤攷慮方便性與實用性，選取四點控製參數進行設計。分彆利用BMAA方法與原有定製葉型、任意中線方法，對某單級壓氣機進行設計，結果錶明：對于超/跨聲葉片設計，BMAA方法設計的葉片性能略優于定製葉型；與任意中線葉型達到的性能相噹，但葉型控製便捷性和葉型光滑性優于任意中線葉型。
응용목전선진적자유곡선이론，개발료일충신적협편조형방법--B양조공제중선각협형(BMAA)방법。분별선취준균균B양조화패새이곡선，실현료대협형중선화후도적방편、령활공제；동시종합고필방편성여실용성，선취사점공제삼수진행설계。분별이용BMAA방법여원유정제협형、임의중선방법，대모단급압기궤진행설계，결과표명：대우초/과성협편설계，BMAA방법설계적협편성능략우우정제협형；여임의중선협형체도적성능상당，단협형공제편첩성화협형광활성우우임의중선협형。
Using the free-form curve theory, an innovative blading method--BMAA was developed. Uni-form B-spline and Bézier curve were chosen separately to realize the smart control of camber line and thick-ness. Considering the practicability and facility, four points were selected to design the curve of angle. In the end, BMAA, tailored airfoil and arb itrary camber lines methods were adopted to design a single-stage compressor. The results show that the blade designed by new methods is better than tailored airfoil for super-sonic/transonic blading design;and the blading performance is equal to that of arbitrary camber lines. In ad-dition, the convenience of controlling and smoothness of airfoil are superior to that of arbitrary camber lines.
