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DOI | 10.3390/aerospace6120132 |
Determination of Serviceability Limits of a Turboshaft Engine by the Criterion of Blade Natural Frequency and Stall Margin | |
Dvirnyk, Yaroslav; Pavlenko, Dmytro; Przysowa, Radoslaw | |
通讯作者 | Przysowa, R (corresponding author), Inst Tech Wojsk Lotniczych, Ul Ksiecia Boleslawa 6, PL-01494 Warsaw, Poland. ; Przysowa, R (corresponding author), Technol Partners Fdn, Ul Pawinskiego 5A, PL-02106 Warsaw, Poland. |
来源期刊 | AEROSPACE |
EISSN | 2226-4310 |
出版年 | 2019 |
卷号 | 6期号:12 |
英文摘要 | This paper analyzes the health and performance of the 12-stage axial compressor of the TV3-117VM/VMA turboshaft operated in a desert environment. The results of the dimensional control of 4800 worn blades are analyzed to model the wear process. Operational experience and two-phase flow simulations are used to assess the effectiveness of an inlet particle separator. Numerical modal analysis is performed to generate the Campbell diagram of the worn blades and identify resonant blade vibrations which can lead to high cycle fatigue (HCF): mode 7 engine order 30 in the first stage and mode 8 engine order 60 in the fourth. It is also shown that the gradual loss of the stall margin over time determines the serviceability limits of compressor blades. In particular, the chord wear of sixth-stage blades as high as 6.19 mm results in a reduction of the stall margin by 15-17% and a permanent stall at 770-790 flight hours. In addition, recommendations setting out go/no-go criteria are made to maintenance and repair organizations. |
英文关键词 | gas-turbine performance turboshaft axial compressor blade FEM CFD erosion wear stall margin compressor surge brownout |
类型 | Article |
语种 | 英语 |
开放获取类型 | gold, Green Published |
收录类别 | SCI-E |
WOS记录号 | WOS:000505768100006 |
WOS关键词 | EROSION |
WOS类目 | Engineering, Aerospace |
WOS研究方向 | Engineering |
资源类型 | 期刊论文 |
条目标识符 | http://119.78.100.177/qdio/handle/2XILL650/369770 |
作者单位 | [Dvirnyk, Yaroslav] Motor Sich JSC, 15 Motorostroiteley Ave, UA-69068 Zaporizhzhia, Ukraine; [Dvirnyk, Yaroslav; Pavlenko, Dmytro] Natl Univ Zaporizhzhia Polytech, Dept Mech Engn, 64 Zhukovskogo St, UA-69061 Zaporizhzhia, Ukraine; [Pavlenko, Dmytro] Zaporizhzhia Machine Bldg Design Bur Progress Sta, 2 Ivanova St, UA-69068 Zaporizhzhia, Ukraine; [Przysowa, Radoslaw] Inst Tech Wojsk Lotniczych, Ul Ksiecia Boleslawa 6, PL-01494 Warsaw, Poland; [Przysowa, Radoslaw] Technol Partners Fdn, Ul Pawinskiego 5A, PL-02106 Warsaw, Poland |
推荐引用方式 GB/T 7714 | Dvirnyk, Yaroslav,Pavlenko, Dmytro,Przysowa, Radoslaw. Determination of Serviceability Limits of a Turboshaft Engine by the Criterion of Blade Natural Frequency and Stall Margin[J],2019,6(12). |
APA | Dvirnyk, Yaroslav,Pavlenko, Dmytro,&Przysowa, Radoslaw.(2019).Determination of Serviceability Limits of a Turboshaft Engine by the Criterion of Blade Natural Frequency and Stall Margin.AEROSPACE,6(12). |
MLA | Dvirnyk, Yaroslav,et al."Determination of Serviceability Limits of a Turboshaft Engine by the Criterion of Blade Natural Frequency and Stall Margin".AEROSPACE 6.12(2019). |
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