Non-Axisymmetric Flows and Rotordynamic Forces in an Eccentric Shrouded Centrifugal Compressor—Part 1: Measurement

Author:

Song Jieun1,Kim Suyong1,Park Tae Choon2,Cha Bong-Jun2,Lim Dong Hun3,Hong Joo Sung3,Lee Tae Wook3,Song Seung Jin1

Affiliation:

1. Department of Mechanical and Aerospace Engineering, Seoul National University, Seoul 08826, South Korea

2. Korea Aerospace Research Institute, Daejeon 34133, South Korea

3. Hanwha Power Systems, Seongnam-si, Gyeonggi-do 13488, South Korea

Abstract

Abstract Centrifugal compressors can suffer from rotordynamic instability. While individual components (e.g., seals, shrouds) have been previously investigated, an integrated experimental or analytical study at the compressor system level is scarce. For the first time, non-axisymmetric pressure distributions in a statically eccentric shrouded centrifugal compressor with eye-labyrinth seals have been measured for various eccentricities. From the pressure measurements, direct and cross-coupled stiffness coefficients have been determined. Thus, the contributions of the pressure perturbations in the shroud cavity and labyrinth seals have been simultaneously investigated. The cross-coupled stiffness coefficients in the shroud and labyrinth seals are both positive and one order of magnitude larger than the direct stiffness coefficients. Furthermore, in the tested compressor, contrary to the common assumption, the cross-coupled stiffness in the shroud is 2.5 times larger than that in the labyrinth seals. Thus, not only eye-labyrinth seals but also shrouds need to be considered in rotordynamic analysis.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference24 articles.

1. Flow Induced Spring Coefficients of Labyrinth Seals for Application in Rotor Dynamics,1980

2. Rotordynamic Forces Due to Turbine Tip Leakage—Part II: Radius Scale Effects and Experimental Verification;ASME J. Turbomach.,1997

3. Unsteady Flow and Whirl-Inducing Forces in Axial-Flow Compressors—Part I: Experiment;ASME J. Turbomach.,2000

4. Experimental Rotordynamic Coefficient Results for Teeth-on-Rotor and Teeth-on-Stator Labyrinth Gas Seals;ASME J. Eng. Gas Turbines Power,1986

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