journal article·2017-07-25Open access

Vibration Characteristics and Damping Analysis of the Blisk-Deposited Hard Coating Using the Rayleigh-Ritz Method

Feng Gao, Wei Sun

Coatings· Volume 7· Issue 8

Abstract

For the purpose of improving the working reliability of the blisk (integrally-bladed disk) under severe environment, a passive vibration reduction method by depositing a hard coating on both sides of blades is developed and then investigated systematically. Firstly, an analytical model of the blisk-deposited hard coating is taken into account. Secondly, by using the Oberst beam theory and axial symmetry property, the composite hard-coated blade is equivalent to a special homogeneous blade possessing the equivalent material parameters. Then, energy equations of the blisk with hard-coated blades are derived by using the complex-valued modulus, and then substituted into the Lagrange equations. Additionally, eigenvalue equations of the blisk with hard-coated blades are acquired by taking advantage of Rayleigh-Ritz method, and its natural characteristics are obtained subsequently. Further, the frequency response functions of the blisk with hard-coated blades are formulated by using proportional damping to achieve its damping matrix. Finally, a stainless-steel blisk with deposited NiCoCrAlY + YSZ hard coating on both sides of the blades is chosen as the study case to conduct numerical calculations, and the results are compared with those obtained by experimental tests in terms of natural frequencies and mode shapes. The variation of natural frequencies, modal loss factors and frequency response functions of the blisk generated by hard coating are studied, respectively, and the influence of the coating thickness on the damping capacity are further discussed.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Bladed Disk Vibration Dynamics · Composite Structure Analysis and Optimization · Electromagnetic Launch and Propulsion Technology

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

School of Mechanical Engineering & Automation, Northeastern University, Shenyang 110819, China

Key Laboratory of Vibration and Control of Aero-Propulsion System Ministry of Education, Northeastern University, Shenyang 110819, China

References (52)

Show source-provided references
1. On high-speed turning of a third-generation gamma titanium aluminide10.1007/s00170-012-4157-5 ↗
2. Milling of gamma titanium-aluminum alloys10.1007/s00170-011-3812-6 ↗
3. Grinding of gamma TiAl intermetallic alloys10.1016/j.proeng.2013.08.182 ↗
4. Turn-milling of blades in turning centres and multitasking machines controlling tool tilt angle10.1177/0954405414535589 ↗
5. Optimised methodology for aircraft engine IBRs five-axis machining process
6. Kosing, O.E., Scharl, R., and Schmuhl, H.J. (2001, January 4–7). Design Improvements of the EJ 200 HP Compressor: From Design Verification Engine to a Future All Blisk Version. Proceedings of the ASME Turbo Expo 2001 Power for Land, Sea, and Air, New Orleans, LA, USA.10.1115/2001-GT-0283 ↗
7. Klinger, H., Lazik, W., and Wunderlich, T. (2008, January 9–13). The engine 3E core engine. Proceedings of the ASME Turbo Expo 2008: Power for Land, Sea, and Air, Berlin, Germany.10.1115/GT2008-50679 ↗
8. Younossi, O., Arena, M.V., Moore, R.M., Lorell, M., and Mason, J. (2002). Military jet Engine Acquisition: Technology Basics and Cost-Estimating Methodology, RAND Corp.
9. Numerical investigations of localized vibrations of mistuned blade integrated disks (blisks)10.1115/1.2985074 ↗
10. Experimental and numerical investigation of rotating bladed disk forced response using underplatform friction dampers10.1115/1.2903845 ↗
11. Robust analysis of design in vibration of turbomachines10.1115/1.4007442 ↗
12. A new reduced order modeling for stability and forced response analysis of aero-coupled blades considering various mode families10.1115/1.4003830 ↗
13. Computation of the statistics of forced response of a mistuned bladed disk assembly via polynomial chaos10.1115/1.2215620 ↗
14. Dissipated energy and boundary condition effects associated to dry friction on the dynamics of vibrating structures10.1016/j.mechmachtheory.2010.11.014 ↗
15. Experimental study of dynamic characteristics of dry friction damping of turbine blade steel10.4028/www.scientific.net/AMR.690-693.1979 ↗
16. Li, G., Zhang, Q., Zhao, W., Zhou, Q., and Xie, Y.H. (2015, January 15–16). Dynamic response analysis of blades with damping structures of shroud and snubber. Proceedings of the First International Conference on Information Sciences, Machinery, Materials and Energy, Jinan, China.10.2991/icismme-15.2015.55 ↗
17. Underplatform dampers for turbine blades: Theoretical modelling, analysis and comparison with experimental data10.1115/1.1385830 ↗
18. Advanced modeling of underplatform friction dampers for analysis of bladed disk vibration10.1115/1.2372775 ↗
19. Modelling the nonlinear behaviour of an underplatform damper test rig for turbine applications10.1016/j.ymssp.2016.09.007 ↗
20. Qualitative analysis of forced response of blisks with friction ring dampers10.1016/j.euromechsol.2006.10.002 ↗
21. Laxalde, D., Thouverez, F., and Lombard, J.P. (2007, January 14–17). Vibration control for integrally bladed disks using friction ring dampers. Proceedings of the ASME Turbo Expo 2007: Power for Land, Sea, and Air, Montreal, QC, Canada.10.1115/GT2007-27087 ↗
22. Laxalde, D., Gibert, C., and Thouverez, F. (2008, January 9–13). Experimental and numerical investigations of friction rings damping of blisks. Proceedings of the ASME Turbo Expo 2008: Power for Land, Sea, and Air, Berlin, Germany.10.1115/GT2008-50862 ↗
23. Forced response analysis of integrally bladed disks with friction ring dampers10.1115/1.4000763 ↗
24. Wear resistance and anti-friction of expansion cone with hard coating10.1016/S1876-3804(16)30038-6 ↗
25. Shubin, A.Y., Potekaev, A.I., Savostikov, V.M., Galsanov, S.V., Dmitriev, V.S., Stepanov, I.B., Kashkarov, E.B., and Dammer, V.H. (2017, January 20–21). Comparative physical-tribological properties of anti-friction ion-plasma Ti-C-Mo-S coating on VT6 alloy or 20X13 and 40X steels. Proceedings of the IOP Conference Series: Materials Science and Engineering, Bangkok, Thailand.10.1088/1757-899X/168/1/012038 ↗
26. Design of functionally graded multilayer thermal barrier coatings for gas turbine application10.1016/j.surfcoat.2015.11.054 ↗
27. Modeling and simulation of the temperature and stress fields in a 3D turbine blade coated with thermal barrier coatings10.1016/j.surfcoat.2017.03.012 ↗
28. Anti-corrosive properties of silane coatings deposited on anodised aluminium10.1016/j.electacta.2016.10.080 ↗
29. Anti-corrosive performance of electropolymerized phosphomolybdic acid doped PANI coating on 304SS10.1016/j.apsusc.2015.11.029 ↗
30. Yen, H.Y. (2000). New Analysis and Design Procedures for Ensuring Gas Turbine Blades and Adhesive Bonded Joints Structural Integrity and Durability. [Ph.D. Thesis, Ohio State University].
31. Li, H., Ying, L., and Sun, W. (2014). Analysis of nonlinear vibration of hard coating thin plate by finite element iteration method. Shock Vib., 2014.10.1155/2014/941709 ↗
32. Solution of natural characteristics of a hard-coating plate based on Lindstedt-Poincaré perturbation method and its valedictions by FEM and measurement10.1007/s11071-015-2063-8 ↗
33. Torvik, P.J., and Langley, B. (2015, January 27–29). Material properties of hard coatings developed for high damping. Proceedings of the 51st AIAA/SAE/ASEE Joint Propulsion Conference, Orlando, FL, USA.10.2514/6.2015-4195 ↗
34. Hysteretic damping of structures vibrating at resonance: An iterative complex eigensolution method based on damping-stress relation10.1016/j.compstruc.2007.02.026 ↗
35. Vibro-acoustic study of a viscoelastic sandwich ring immersed in water10.1016/j.jsv.2011.10.004 ↗
36. Complex modal analysis of rods with viscous damping devices10.1016/j.jsv.2013.11.030 ↗
37. Vibration analysis of composite sandwich beams with viscoelastic core by using differential transform method10.1016/j.compstruct.2010.05.022 ↗
38. Identification of mechanical parameters of hard-coating materials with strain-dependence10.1007/s12206-013-0939-4 ↗
39. Sun, W., Liu, Y., and Du, G. (2015). Analytical modeling of hard-coating cantilever composite plate considering the material nonlinearity of hard coating. Math. Probl. Eng., 2015.10.1155/2015/978392 ↗
40. Free vibration of non-uniform nanobeams using Rayleigh-Ritz method10.1016/j.physe.2014.10.039 ↗
41. Post-buckling analysis of cracked multilayered composite plates by pb-2 Rayleigh-Ritz method10.1016/j.compstruct.2015.05.007 ↗
42. Free vibration of functionally graded porous cylindrical shell using a sinusoidal shear deformation theory10.1016/j.ast.2017.03.003 ↗
43. Analysis of free vibration of rotating disk-blade coupled systems by using artificial springs and orthogonal polynomials10.1006/jsvi.1996.0106 ↗
44. Traveling wave analysis of rotating cross-ply laminated cylindrical shells with arbitrary boundaries conditions via Rayleigh-Ritz method10.1016/j.compstruct.2015.08.015 ↗
45. Vibration analysis of rotating pretwisted tapered blades made of functionally graded materials10.1016/j.ijmecsci.2016.10.002 ↗
46. Dynamic response of coupled shaft torsion and blade bending in rotor blade system10.1007/s12206-013-0702-x ↗
47. Wave based method for vibration analysis of elastically coupled annular plate and cylindrical shell structures10.1016/j.apacoust.2017.03.012 ↗
48. Vibration and damping analysis of the bladed disk with damping hard coating on blades10.1016/j.ast.2016.08.016 ↗
49. Development and validation of a composite finite element with damping capability10.1016/j.compstruct.2012.10.020 ↗
50. Vibration studies of rotating cylindrical shells with arbitrary edges using characteristic orthogonal polynomials in the Rayleigh-Ritz method10.1016/j.ijmecsci.2013.01.013 ↗
51. Vibration and damping analysis of sandwich viscoelastic-core beam using Reddy’s higher-order theory10.1016/j.compstruct.2016.01.017 ↗
52. Dynamic particle difference method for the analysis of proportionally damped system and cracked concrete beam