CAJ | 학술논문

本文介绍一高性能单级跨音速风扇的设计与试验结果。该风扇设计压比2.3，设计效率0.88，具有高切线速度510 m/s(相对马赫数达1.72)和低展弦比。在气动设计过程中，为了改善级效率，使用了前缘掠型和任意空间积迭曲线新技术。为了提高气动设计的可靠性，对风扇进行了三维有粘流动计算分析和气动的优化。试验结果表明：这台风扇性能达到了它的设计目标。设计点压比(2.3)效率为89.5%，峰值效率达90.8%，最高压比达2.491，喘振裕度超过11.5%。这台风扇显示了当今国际上先进风扇水平。高水平性能的取得归功于在高速和高负荷风扇气动设计中准三维和三维粘性设计系统的应用。
본문개소일고성능단급과음속풍선적설계여시험결과。해풍선설계압비2.3，설계효솔0.88，구유고절선속도510 m/s(상대마혁수체1.72)화저전현비。 재기동설계과정중，위료개선급효솔，사용료전연략형화임의공간적질곡선신기술。위료제고기동설계적가고성，대풍선진행료삼유유점류동계산분석화기동적우화。 시험결과표명：저태풍선성능체도료타적설계목표。설계점압비(2.3)효솔위89.5%，봉치효솔체90.8%，최고압비체2.491，천진유도초과11.5%。 저태풍선현시료당금국제상선진풍선수평。고수평성능적취득귀공우재고속화고부하풍선기동설계중준삼유화삼유점성설계계통적응용。
This paper presents design and experimental resultsfor a high performance single stage transonic fan with design pressureratio 2.3 and design efficiency 0.88 at high tip speed 510m/s (relativeMach number reaches 1.72) and low aspect ratio. 　　New techniques of leadingedge sweep and any spatial stack curve have been applied to aerodynamicdesign of both rotor and stator in order to improve stage efficiency.A three dimensional viscous flow analysis and aero-optimization wereused to enhance reliability of aerodynamic design. 　　Test results prove that performance of this fan achieves its design goal.Efficiency of design pressure ratio point (2.3) is 89.5%, peak efficiencyis 90.8%, maximum pressure ratio reaches 2.491, surge margin is higherthan 11.5%. 　　This single stage fan has demonstrated performance for thecurrent world level. Outstanding performance is attribute to use ofQuasi-two dimensional and three dimensional viscous design system inaerodynamic design of the high speed and highly loaded fan stage。