A Feasibility Analysis to Use Topological Optimization in Gear Design
https://doi.org/10.24108/aplts.0317.0000072
Abstract
The paper conducts a feasibility analysis for using a topology optimization (TO) when designing the gears for advanced engines.
The goal of TO is to find an optimal material distribution in designing area for given loads with constraints consideration. This study performs 3D computations using a finite-element analysis.
Optimization of the certain statements of the problem has been provided. In case 1 an increasing rigidity of diaphragm of the helical gear with decreasing mass was specified, as a criterion. As a result of optimization there were two conical sections getting into one thin wall, connected at the face where the axial force is applied. Some aviation engine and helicopter transmission schemes have a similar embodiment of a diaphragm of the helical gear. In case 2 the frequency detuning was carried out. The result is a complicated design, containing closed cavities, so it is hard to manufacture it by traditional manufacturing methods. Case 3 solves a problem of increasing torsional rigidity with mass restrictions. The optimized design has a splitting diaphragm and a closed cavity.
The final calculation is carried out for case 1. As a result, maximum displacements for initial and optimized designs are obtained. The analysis and comparing results have shown that the optimized design has over 2 times increased diaphragm rigidity as compared to the initial design, with mass being 10 % less and equivalent stresses reduced by 13%.
The analysis of the results has shown that TO can be used in designing gears taking into account the requirements for mass, rigidity, natural frequencies. It is advisable to refine a design of components using parametric optimization after TO and engineering study of results.About the Authors
B. E. VasilyevCentral Institute of Aviation Motors n.a. P.I. Baranov, Moscow; Bauman Moscow State Technical University, Moscow
Russian Federation
D. V. Kalinin
Russian Federation
M. S. Svinareva
Russian Federation
N. A. Gudkov
Russian Federation
References
1. Seppälä J., Hupfer A. Topology optimization in structural design of a LP turbine guide vane: potential of additive manufacturing for weight reduction // ASME Turbo Expo 2014: Turbine technical conf. and exposition (Dusseldorf, Germany, June 16-20, 2014): Proc. N.Y.: ASME, 2014. 10 p. DOI: 10.1115/GT2014-25637
2. Rozvany G.I.N. A critical review of established methods of structural topology optimization. Structural and Multidisciplinary Optimization, 2009, vol. 37, no. 3, pp. 217-237. DOI: 10.1007/s00158-007-0217-0
3. Vasil’ev B.E., Magerramova L.A. Analysis of the possibility of using topology optimization in the design of uncooled turbine rotor blades. Vestnik Saratovskogo universiteta. Aerokosmicheskaia tekhnika, tekhnologii i mashinostroenie [Vestnik of Samara Univ. Aerospace and Mechanical Engineering], 2015, vol. 14, no. 3, pt.1: spec. iss., pp. 139-147. DOI: 10.18287/2412-7329-2015-14-3-139-147 (in Russian)
4. Browne P.A. Topology optimization of linear elastic structures: doct. diss. … 2013. 180 p.
5. Sysoeva V.V., Chedrik V.V. Algorithms for optimizing the topology of power structures. Uchenye zapiski TSAGI [Proc. of the TSAGI], 2011, vol. 42, no. 2, pp. 91-102 (in Russian).
6. Stolpe M. On some fundamental properties of structural topology optimization problems. Structural and Multidisciplinary Optimization, 2010, vol. 41, no. 5, pp. 661-670. DOI: 10.1007/s00158-009-0476-z
7. Rozvany G.I.N. On symmetry and non-uniqueness in exact topology optimization. Structural and Multidisciplinary Optimization, 2011, vol. 43, no. 3, pp. 297-317. DOI: 10.1007/s00158-010-0564-0
8. Ryo Watada, Makoto Ohsaki, Yoshihiro Kanno. Non-uniqueness and symmetry of optimal topology of a shell for minimum compliance. Structural and Multidisciplinary Optimization, 2011, vol. 43, no. 4, pp. 459-471. DOI: 10.1007/s00158-010-0587-6
9. Salnikov A.V. Strength reliability of turbine rotor ensuring based on multidisciplinary optimization. 29th Congress of the Intern. Council of the Aeronautical Sciences: ICAS 2014 (St. Petersburg, Russia, Sept. 7-12, 2014): Proc. Vol. 3. Red Hook, 2014. Pp. 2669-2675.
10. Magerramova L.A., Nozhnitskij Yu.A., Vasil’ev B.E., Kinzburskij V.S. The use of additive technologies for production of advanced gas-turbine engine components. Tekhnologiia legkikh splavov [Technology of Light Alloys], 2015, no. 4, pp. 7-13 (in Russian).
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Review
For citations:
Vasilyev B.E., Kalinin D.V., Svinareva M.S., Gudkov N.A. A Feasibility Analysis to Use Topological Optimization in Gear Design. Machines and Plants: Design and Exploiting. 2017;(3):35-45. (In Russ.) https://doi.org/10.24108/aplts.0317.0000072