The purpose of this study was to analyze the impact of blades with slots in a rotary compressor. The equations for contact forces were derived from Newton’s law. Updated moving Lagrangian descriptions with the hybrid technique and the Newark time integration method were used to determine the nodal displacement vectors. The finite element method was used to analyze the contact forces and the stresses of blades. The maximum blade contact force of 2.3 KN was larger than the maximum static force of 1 KN. The maximum blade impact Von Mises stress of 12.3 Mpa that occurred at the contact point was greater than the previous calculated static stress of 5.15 Mpa. Hence, the impact effect was significant. Experimental modal analysis was also used to determine the first and second natural frequencies of blades.
Issue Section:
Technical Papers
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, 1994
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Fukuta
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, Yanagisawa
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, Shimizu
, T.
, and Suzuki
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, 1995
, “Mathematical-Model of Van-Compressors for Computer-Simulation of Automotive Air-Conditioning Cycle
,” JSME Int. J., Ser. B
, 38
, No. 2
, pp. 199
–205
.3.
Gorrepati
, K. M.
, 1996
, “Analysis of Modal Parameters of Adhesively Bonded Double-Strap Joints by The Modal Strain Energy Method
,” ASME J. Vibr. Acoust.
, 118
, No. 1
, pp. 28
–35
.4.
Ooi
, K. T.
, and Wong
, T. N.
, 1997
, “A Computer Simulation of a Rotary Compressor for Household Refrigerators
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, 17
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, pp. 65
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.5.
Huang, Yuan Mao, and Chiu, Y. F. 1998, “Performance and Dynamics of a Rotary Compressor with a Composite Stator Inner Contour,” ASME FEDSM 98-4856, pp. 1–8.
6.
Padovan
, J.
, Tovichakchaikul
, S.
, and Zeid
, I.
, 1984
, “Finite Element Analysis of Steadily Moving Contact Fields
,” Comput. Struct.
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, No. 2
, pp. 191
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Fukuta
, M.
, 1993
, “Vane Behavior in Vane Compressors under Start-up Operation,” (1st Report, Force Acting on Vane), Nippon Kikai Gakkai Ronbunshu, B Hen
, Trans. Jpn. Soc. Mech. Eng., Ser. B
, 59
, No. 567
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–3492
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Amirouche
, F. M. L.
, 1993
, “Finite Element Modeling of Contact Conditions in Multibody System Dynamics
,” Nonlinear Dyn.
, 4
, No. 1
, pp. 83
–102
.9.
Sisir, K. P., 1993, “On the Dynamics of a Rotary Compressor: Part 1-Mathematical Modeling,” ASME Advances in Design Automation, DE-Vol. 65-1, 1, pp. 207–216.
10.
Malone
, J. G.
, 1994
, “Parallel Finite Element Contact/Impact Algorithm for Non-linear Explicit Transient Analysis: Part 1-The Search Algorithm And Contact
,” Int. J. Numer. Methods Eng.
, 37
, No. 4
, pp. 559
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Choi
, Chang-Koon
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, “Gap Element for Three-Dimensional Elasto-Plastic Contact Problems
,” Comput. Struct.
, 61
, No. 6
, pp. 1155
–1167
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Huang
, Yuan Mao
, and Chang
, Chii-how
, 1997
, “The Stress and Deflection Analysis for the Radial Blades of the RCAC System
,” Int. J. Refrig.
, 20
, No. 1
, pp. 55
–62
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, J. C.
, Wriggers
, P.
, Schweizerhof
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, 1986
, “Finite Deformation Post-Buckling Analysis Involving Inelasticity and Contact Problems
,” Int. J. Numer. Methods Eng.
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, and Wriggers
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, “A Two-Level Iteration Method for Solution of Contact Problems
,” Comput. Methods Appl. Mech. Eng.
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, pp. 131
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Auricchio
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, 1996
, “Augmented Lagrangian Finite-Element for Plate Contact Problems
,” Int. J. Numer. Methods Eng.
, 39
, No. 24
, pp. 4141
–4158
.16.
Kahyai
, S.
, Niazy
, A-S. M.
, and Weingarten
, V. I.
, 1993
, “A Hybrid Technique for Generalized Contact Problems
,” Cosmos/m Advanced Modules
, 4
, Part 1
, pp. 73
–86
.17.
Huang
, Yuan Mao
, 1995
, “Analysis of the Rotor-Cooler Air-Conditioning System
,” Int. J. Refrig.
, 18
, No. 6
, pp. 367
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.18.
Huebner, K. H., 1995, “Basic Equation from Linear Elasticity Theory, The Finite Element Method for Engineers,” John Wiley & Sons, Inc., Appendix C, pp. 561–577.
19.
Morfey
, C. L.
, and Koopmann
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, 1982
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,” Noise and Vibration
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.20.
Knothe
, K. L.
, 1993
, “Modeling of Railway Track and Vehicle/Track Interaction at High Frequencies
,” Veh. Syst. Dyn.
, 22
, No. 3–4
, pp. 209
–262
.Copyright © 2001
by ASME
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