Research of restrained bending of aircraft parts with curved sides


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Abstract

In the article the authors present a method of restrained elastomer bending of aircraft sheet parts with curved sides. Manufacturing of a part is carried out in two transitions; as a result of the first transition a part with thinning in the radial part is obtained, the second transition is carried out on the mold block of reduced height, as a result of which the resulting wave of excess material deforms along the radius of the bending mandrel. In the finished part, we can observe an increase in the thickness of the workpiece in the zone of the bend radius. Numerical studies of the process were conducted using the ANSYS/LS-DYNA software complex. As part of the study, the process flow model was worked out, the distribution of thickness of the material of the part over the entire surface under consideration was obtained, and graphs were plotted showing the elastomer pressure distributions and the deformation of the material of the part at characteristic points.

About the authors

E. G. Gromova

Samara National Research University

Author for correspondence.
Email: pla.gromova@ya.ru

Candidate of Science (Engineering), Associate Professor, Department of Aircraft Production and Quality Control in Mechanical Engineering

Russian Federation

V. K. Moiseev

Samara National Research University

Email: moiseevvk@mail.ru

Doctor of Science (Engineering), Professor, Department of Aircraft Production and Quality Control in Mechanical Engineering

Russian Federation

A. A. Sharov

Samara National Research University

Email: aa.sharov@ya.ru

Candidate of Science (Engineering), Associate Professor, Department of Aircraft Production and Quality Control in Mechanical Engineering

Russian Federation

O. V. Lomovskoi

Samara National Research University

Email: oleg.lomovskoi@ya.ru

Candidate of Science (Engineering), Associate Professor, Department of Aircraft Production and Quality Control in Mechanical Engineering

Russian Federation

М. N. Mantusov

Ulyanovsk branch of Tupolev Design Bureau

Email: mishaufkb@ya.ru

Leading Engineer

Russian Federation

A. N. Plotnikov

Samara National Research University

Email: anplotnikov@ya.ru

Candidate of Science (Engineering), Associate Professor, Department of Aircraft Production and Quality Control in Mechanical Engineering

Russian Federation

References

  1. Mosieev V.K., Mantusov М.N., Plotnikov A.N., Lomovskoi O.V., Sharov A.A. Improving the technology of bending curved sides of aircraft parts. Izvestiya Samarskogo Nauchnogo Tsentra RAN. 2018. V. 20, no. 4 (3). P. 441-444. (In Russ.)
  2. Mantusov M.N., Moiseev V.K., Sharov A.A., Gromova E.G., Ryzhakov S.G. Stamping of sheet details with curvilinear sides by elastic material. Izvestiya Samarskogo Nauchnogo Tsentra RAN. 2018. V. 20, no. 4 (3). P. 332-336. (In Russ.)
  3. Grechnikov F.V., Moiseev V.K., Lomovskoy O.V., Sharov A.A., Mantusov M.N. Stamping with tangential compression of high-precision sheet metal parts. Forging and Stamping Production. Material Working by Pressure. 2019. No. 7. P. 3-9. (In Russ.)
  4. Moiseyev V.K., Sharov A.A., Gromova E.G., Mantusov M.N. Results of the sheet parts curved edges constrained bending with elastomer. Key Engineering Materials. 2017. V. 746. P. 285-289. doi: 10.4028/ href='www.scientific.net/kem.746.285' target='_blank'>www.scientific.net/kem.746.285
  5. Kravchuk A.S., Kravchuk A.I. Elektronnaya biblioteka mekhaniki i fiziki. Lektsii po ANSYS/LS-DYNA i osnovam LS-PREPOST. Ch. 3. Osnovnye elementy graficheskogo interfeysa LS-PREPOST. Reshenie zadach s pomoshch'yu LS-DYNA Solver [Electronic library of Mechanics and Physics. Lectures on ANSYS/LS-DYNA and the basics of LS-PREPOST. The basic elements of the graphical interface of LS-PREPOST. Solving problems with LS-DYNA Solver]. Minsk: Belarusian State University Publ., 2013. 74 p.

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