Cyclic compression of a multi-layer multi-span corrugated package with plastic deformation of its tapes


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Abstract

In this article we present our solution of the problem of cyclic compression of a single-layer and multi-layer corrugation, as well as of a single-layer multi-span corrugation by the FEM method using Ansys. This problem can be considered as the first part of the general complex nonlinear problem of cyclic compression of a multi-layer multi-span corrugated package with dry friction on the contact surfaces. We conducted an analysis of the known published solutions to this problem, and we discovered inaccuracy of some of them and the physical reason resulting in this unacceptable error. A very large number of published solutions to this problem are generally explained by the presence of successful examples of their practical application in the field of aircraft and rocket engine manufacturing, by the wide possibilities of their use as damping devices in both of these areas, and, for example, in the automotive industry, by their high elastic-friction, strength and performance characteristics. All the known published solutions to this problem were obtained for cyclic compression of a multilayer multi-span package in the region of its elastic deformations and for the same geometric shape of the corrugation. The task of improving the mass characteristics of an engineering unit is quite relevant for the development of shock-proof single-shot damping devices that increase the passive safety of the car – bumper protective devices. This can be solved by using single-layer or two-layer, multi-span packages with an optimally selected geometric shape of the corrugation, deformable in the elastic-plastic region. Therefore, the above-mentioned problems are solved taking into account the elastic-plastic deformation of the corrugations for any of their geometric shapes. The obtained solutions make it possible to construct any loading processes in the field of elastic-hysteresis package loops. We also investigated the influence of the parameters of the corrugated package on its elastic-friction characteristics (including the shape of the corrugation and the presence of gaps between the tapes of the package at the tops of their corrugations).

About the authors

R. I. Alkeev

Samara National Research University

Author for correspondence.
Email: wild_cat_ruru@mail.ru

Senior Lecturer, Department of Engineering Graphics

Russian Federation

V. I. Suslikov

Samara National Research University

Email: suslikov_v_i@yandex.ru

Candidate of Science (Engineering),
Associate Professor of the Department of Aircraft Engine Design and Construction

Russian Federation

I. D. Eskin

Samara National Research University

Email: Izold.eskinid@mail.ru

Candidate of Science (Engineering),
Associate Professor of the Department of Aircraft Engine Design and Construction

Russian Federation

References

  1. Ivashchenko V.I., Eskin I.D. Metodika rascheta razgruzochnogo ustroystva dlya dempferov opor rotorov. V sb.: «Vibratsionnaya prochnost' i nadezhnost' dvigateley i sistem letatel'nykh apparatov». Kuybyshev: Kuybyshev Aviation Institute Publ., 1985. P. 39-45. (In Russ.)
  2. Mal'teev M.A., Ponomarev Yu.K. Metodologiya opredeleniya uprugodissipativnykh kharakteristik opor truboprovodov s mnogosloynymi paketami. V sb.: «Nadezhnost' mekhanicheskikh sistem». Samara: Samara State Technical University Publ., 1995. P. 146. (In Russ.)
  3. Eskin I.D., Ermakov A.I., Garshin E.A. Rotor kompressora aviatsionnogo gazoturbinnogo dvigatelya so sparkoy bliskov i sparkoy bliska s «klassicheskim» rabochim kolesom i so sparkoy «klassicheskogo» rabochego kolesa s rabochim kolesom s chetvertoy po shestuyu stupen' s ustroystvami dempfirovaniya kolebaniy rabochikh lopatok etikh bliskov i rabochikh koles, rotor ventilyatora i rotor bustera s ustroystvom dempfirovaniya kolebaniy rabochikh shirokokhordnykh lopatok ventilyatora, sposob sborki sparki s dempfiruyushchim ustroystvom [Rotor of aircraft gas-turbine engine compressor with twin of blisks and twin of blisk with classic impeller and with twin of classic impeller with impeller with fourth-to-sixth stage with devices for damping vibrations of workers of these clips and impellers, fan rotor and booster rotor with device for damping of vibrations ofworkingwidechord blades of fan, twin assembly methodwith damper device]. Patent RF, no. 2665789, 2018. (Publ. 04.09.2018, bull. no. 25)
  4. Eskin I.D., Ermakov A.I. Dlinnaya pustotelaya shirokokhordnaya lopatka ventilyatora i sposob ee izgotovleniya [Long hollow wide chord fan blade and method of its manufacture]. Patent RF, no. 2626523, 2017. (Publ. 28.07.2017, bull. no. 22)
  5. Eskin I.D., Suslikov V.I., Alkeev R.I. Bampernoe ustroystvo avtomobilya [Car protective bumper]. Patent RF, no. 2506177, 2014. (Publ. 10.02.2014, bull. no. 4)
  6. Eskin I.D., Alkeev R.I., Suslikov V.I. Bampernoe zashchitnoe ustroystvo dlya legkovykh avtomobiley i sposob izgotovleniya ego uprugogisterezisnogo elementa [Car bumper and method of its strain hysteresis element fabrication]. Patent RF, no. 2559675, 2015. (Publ. 10.08.2015, bull. no. 22)
  7. Eskin I.D., Khramova A.A., Suslikov V.I. Bampernoe zashchitnoe ustroystvo avtomobilya [Car protective bumper]. Patent RF, no. 2478052, 2013. (Publ. 27.03.2013, bull. no. 9)
  8. Eskin I.D., Alkeev R.I. Zashchitnoe ustroystvo, povyshayushchee bezopasnost' voditelya i passazhirov pri avarii avtomobilya [Protective device improving the safety of the driver and passengers in the event of a car accident]. Patent RF, no. 78463, 2008. (Publ. 27.11.2008)
  9. Eskin I.D., Alkeev R.I. Penal'noe zashchitnoe ustroystvo dlya povysheniya bezopasnosti voditelya i passazhirov pri avarii avtomobilya [Protective device improving the safety of the driver and passengers in the event of a car accident]. Patent RF, no. 82171, 2009. (Publ. 20.04.2009)
  10. Eskin I.D., Ermakov A.I. Pustotelaya shirokokhordaya lopatka ventilyatora. Sposob ee izgotovleniya [Hollow wide-chord blade of the fan and method of its manufacture]. Patent RF, no. 2622682, 2017. (Publ. 19.06.2017, bull. no. 17)
  11. Eskin I.D. Issledovanie obobshchennykh uprugofriktsionnykh kharakteristik dempferov i amortizatorov aviatsionnykh dvigateley. Dis. … kand. tekh. nauk [Analysis of generalized elastic-friction characteristics of dampers and shock absorbers of aircraft engines: Candidate of Science (Engineering) Dissertation]. Kuybyshev, 1973. 315 p.
  12. Kondrashov N.S. Uprugofriktsionnye kharakteristiki dempferov s gofrirovannymi lentami. V sb.: «Vibratsionnaya prochnost' i nadezhnost' dvigateley i sistem letatel'nykh apparatov». Vyp. 51. Kuybyshev: Kuybyshev Aviation Institute Publ., 1972. P. 45-62. (In Russ.)
  13. Eskin I.D., Alkeev R.I., Ivaschenko V.I. Cyclic compression of a multilayer multispan laminated package of corrugated sheets. Vestnik of the Samara State Aerospace University. 2013. No. 1 (39). P. 178-191. (In Russ.). doi: 10.18287/1998-6629-2013-0-1(39)-178-191
  14. Eskin I.D., Alkeev R.I., Ivashchenko V.I. Experimental and design analysis of models of cyclic compression for a multilayer multispan package of corrugated sheets. Vestnik of the Samara State Aerospace University. 2013. No. 1 (39). P. 192-200. (In Russ.). doi: 10.18287/1998-6629-2013-0-1(39)-192-200

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