Abstract
Consideration is given to general problems for providing the dynamic strength of monocrystalline gas-turbine blades which are caused by anisotropy of the material and manufacturing deviations of the directions of crystallographic axes, specifically, features of the vibration frequency spectrum of blades and detuning frequencies from resonances, role of the slip system in a crystal on the evaluation of fatigue damage, analysis of data of fatigue tests and strain measurement, and a rational approach to evaluation of the margin of the fatigue strength of blades by maximum tangential stresses.
Similar content being viewed by others
References
Shalin, R.E., Svetlov, I.L., Kachanov, E.B., et al., Monokristally nikelevykh zharoprochnykh splavov, (Single Crystals of Nickel-Based Refractory Alloys), Moscow: Mashinostroenie, 1997.
Shorr, B.F., Mel’nikova, G.V., Magerramova, L.A., et al., Study of Dynamic Characteristics of Turbine with Single Crystalline Blades, in Aviatsionno-kosmicheskaya tekhnika i tekhnologoya (Aerospace Engineering and Technology), Kharkov: Kharkovskii Aviatsionnyi Inst., issue 19, 2000, p. 236.
Kolesnikov, V.I., Pridorozhnyi, R.PP., and Sheremet’ev, A.V., Effect of Crystallographic Orientation on Static Strength and Fatigue Resistance of Monocrystalline Rotor Blades, in Aviatsionno-kosmicheskaya tekhnika i tekhnologoya (Aerospace Engineering and Technology), Kharkov: Kharkovskii Aviatsionnyi Inst., vol. 26, 2001, p. 132.
Mel’nikova, G.V., Shorr, B.F., Magerramova, L.A., et al., Effect of Crystallographic Orientation of Monocrystal and Its Technological Dispersion on Frequency Spectrum of Turbine Blades, in Sb. Nauch. Tr. Aviatsionno-kosmicheskaya tekhnika i tekhnologoya (Aerospace Engineering and Technology), Kharkov: Kharkovskii Aviatsionnyi Inst., vol. 26, 2001, p. 140.
Elenevskii, D.S. and Solyannikov, V.A., Razrabotka metodov i tekhnicheskikh sredstv pouzlovoy dovodki sovremennykh i perspectivnykh aviatsionnykh dvigatelei (Development of Methods and Hardware for Accelerated Nodal Development of Current and Prospective Aviation Engines), Samara: NITs APIDM, 2003.
Makklintok, F. and Aragon, A., Deformatsiya i razrushenie materialov (Deformation and Fracture of Materials), Moscow: Mir, 1970.
Kablov, E.N. and Golubovskii, E.R., Zharoprochnost’ nikelevykh splavov (High-Temperature Strength of Nickel-Based Alloys), Moscow: Mashinostroenie, 1998.
Lukyanov, V.S., Germasheva, O.I., and Tsivirko, E.I., Vestn. Dvigatelestroeniya, 2002, no. 1, p. 68.
Sayyah, M.T. and Schonberg, W.P., New Failure Criterion for Space Shuttle Main Engine Turbine Blades. J. Spacecr. Rockets, 2002, vol. 39, no. 1.
Author information
Authors and Affiliations
Additional information
Original Russian Text © B.F. Shorr, G.V. Mel’nikova, 2010, published in Problemy Mashinostroeniya i Nadezhnosti Mashin, 2010, No. 4, pp. 33–40.
About this article
Cite this article
Shorr, B.F., Mel’nikova, G.V. Some dynamics problems of monocrystalline turbine blades. J. Mach. Manuf. Reliab. 39, 332–337 (2010). https://doi.org/10.3103/S1052618810040059
Received:
Published:
Issue Date:
DOI: https://doi.org/10.3103/S1052618810040059