论文信息 - Developing a Procedure for Technical Status Control of a Turbine Compressor Package Blades

Developing a Procedure for Technical Status Control of a Turbine Compressor Package Blades

The article discusses the models of repair process of a turbine compressor package blades. The author determines the boundaries of the assured quality area considering mathematical model analysis and defect detection of rotor blades based on the results of natural vibration frequency measurements.

Yury Klochkov | Albina Gazizulina | Ljubisa Papic | Irina Vasilieva

[1] K. M. Eveker,et al. Control-Oriented High-Frequency Turbomachinery Modeling: General 1D Model Development , 1993 .

[2] P. Kundur,et al. Experience with testing and modeling of gas turbines , 2001, 2001 IEEE Power Engineering Society Winter Meeting. Conference Proceedings (Cat. No.01CH37194).

[3] K. M. Eveker,et al. Aircraft Engine Committee Best 1993 Paper Award: Control-Oriented High-Frequency Turbomachinery Modeling: General One-Dimensional Model Development , 1995 .

[4] K. M. Eveker,et al. Control-Oriented High-Frequency Turbomachinery Modeling: Single-Stage Compression System One-Dimensional Model , 1995 .

[5] R.M. Murray,et al. Control of rotating stall in a low-speed axial flow compressor using pulsed air injection: modeling, simulations, and experimental validation , 1995, Proceedings of 1995 34th IEEE Conference on Decision and Control.

[6] Jan Tommy Gravdahl,et al. Compressor Surge and Rotating Stall: Modeling and Control , 1998 .