The objective of the present study is to develop an efficient design algorithm for minimum weight design of a rotor bearing system under the requirements of operational speed range, i.e., multiple frequency constraints, to increase the performance of an existent rotor system. The system is modeled as an assemblage of rigid disks, shaft elements with distributed mass and stiffness, and discrete bearings. The system design variables are the inner radius of shaft elements and the stiffnesses of bearings. The optimization techniques employed to compare the results are method of exterior penalty function, method of feasible directions, and method of modified feasible directions. The parameter sensitivity analysis of the system is also presented. Three examples are used to demonstrate the merits of the design algorithm. The results indicate that the weight of the rotor bearing system can be significantly reduced at the optimum stage.
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October 1988
Research Papers
Minimum Weight Design of a Rotor Bearing System With Multiple Frequency Constraints
Ting Nung Shiau,
Ting Nung Shiau
National Cheng Kung University, Institute of Aeronautics and Astronautics, Tainan, Taiwan
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Jon Li Hwang
Jon Li Hwang
National Cheng Kung University, Institute of Aeronautics and Astronautics, Tainan, Taiwan
Search for other works by this author on:
Ting Nung Shiau
National Cheng Kung University, Institute of Aeronautics and Astronautics, Tainan, Taiwan
Jon Li Hwang
National Cheng Kung University, Institute of Aeronautics and Astronautics, Tainan, Taiwan
J. Eng. Gas Turbines Power. Oct 1988, 110(4): 592-599 (8 pages)
Published Online: October 1, 1988
Article history
Received:
December 21, 1987
Online:
October 15, 2009
Citation
Shiau, T. N., and Hwang, J. L. (October 1, 1988). "Minimum Weight Design of a Rotor Bearing System With Multiple Frequency Constraints." ASME. J. Eng. Gas Turbines Power. October 1988; 110(4): 592–599. https://doi.org/10.1115/1.3240176
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