A compressor blade of low aspect ratio is a typical shell-type structure and its natural frequency and vibratory stress are sensitive to a manufacturing tolerance. In designing a blade, the designer should take the variation of the vibration characteristics into account, and evaluate the mechanical strength of the blade. This paper, first, proposes an analysis method for predicting the resonant stress due to the interaction force between the vane and blade, using 3-D CFD and the modal analysis method based on 3-D FEM. Rig tests of the compressor are carried out, and the measured frequencies and vibratory stresses are compared to predicted values, and the validity of the proposed method is verified. In the second place, a practical analysis method for predicting the variation of the natural frequency and vibratory stress of the blade is proposed, where the variation of the vibration characteristics such as a natural frequency and a resonant stress is evaluated by the first order second moment method in addition to 3-D CTD and 3-D EEM. The calculated results are compared with measured ones. From the results, it is confirmed that the variation of the vibration characteristics can be predicted by the simple method proposed in this paper.
Skip Nav Destination
ASME Turbo Expo 2006: Power for Land, Sea, and Air
May 8–11, 2006
Barcelona, Spain
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
0-7918-4240-1
PROCEEDINGS PAPER
Analysis of Variation of Natural Frequency and Resonant Stress of Blade
Yasutomo Kaneko,
Yasutomo Kaneko
Mitsubishi Heavy Industries, Ltd., Takasago, Hyogo, Japan
Search for other works by this author on:
Kazushi Mori,
Kazushi Mori
Mitsubishi Heavy Industries, Ltd., Takasago, Hyogo, Japan
Search for other works by this author on:
Hiroyuki Yamashita,
Hiroyuki Yamashita
Mitsubishi Heavy Industries, Ltd., Takasago, Hyogo, Japan
Search for other works by this author on:
Kenji Sato
Kenji Sato
Mitsubishi Heavy Industries, Ltd., Takasago, Hyogo, Japan
Search for other works by this author on:
Yasutomo Kaneko
Mitsubishi Heavy Industries, Ltd., Takasago, Hyogo, Japan
Kazushi Mori
Mitsubishi Heavy Industries, Ltd., Takasago, Hyogo, Japan
Hiroyuki Yamashita
Mitsubishi Heavy Industries, Ltd., Takasago, Hyogo, Japan
Kenji Sato
Mitsubishi Heavy Industries, Ltd., Takasago, Hyogo, Japan
Paper No:
GT2006-90176, pp. 801-807; 7 pages
Published Online:
September 19, 2008
Citation
Kaneko, Y, Mori, K, Yamashita, H, & Sato, K. "Analysis of Variation of Natural Frequency and Resonant Stress of Blade." Proceedings of the ASME Turbo Expo 2006: Power for Land, Sea, and Air. Volume 5: Marine; Microturbines and Small Turbomachinery; Oil and Gas Applications; Structures and Dynamics, Parts A and B. Barcelona, Spain. May 8–11, 2006. pp. 801-807. ASME. https://doi.org/10.1115/GT2006-90176
Download citation file:
12
Views
Related Proceedings Papers
Related Articles
Forced Response Analysis of a Mistuned, Compressor Blisk Comparing Three Different Reduced Order Model Approaches
J. Eng. Gas Turbines Power (June,2017)
Approach to Unidirectional Coupled CFD–FEM Analysis of Axial Turbocharger Turbine Blades
J. Turbomach (January,2002)
Method for Predicting Unsteady Vibration of Gas Turbine Compressor Blades Under Subsonic Near-Stall Conditions
J. Eng. Gas Turbines Power (December,2014)
Related Chapters
List of Commercial Codes
Introduction to Finite Element, Boundary Element, and Meshless Methods: With Applications to Heat Transfer and Fluid Flow
Subsection NF—Supports
Companion Guide to the ASME Boiler and Pressure Vessel Codes, Volume 1, Fifth Edition
Subsection NF—Supports
Online Companion Guide to the ASME Boiler & Pressure Vessel Codes