Effectiveness of thermomechanical calibration and determination of residual stresses in the shell nose cone of Cyclone-4

User Rating:  / 0
PoorBest 

Authors:

D.G. Sherstiuk, Oles Honchar Dnepropetrovsk National University, postgraduate student, Physics and Engineering Department, Dnipropetrovsk, Ukraine.

A.V. Kulik, Cand. Sci. (Tech.), Oles Honchar Dnepropetrovsk National University, Senior Lecturer of the Physics and Engineering Department, Dnipropetrovsk, Ukraine.

Ye.A. Soshnikov, Public Joint Stock Company “Ukrainian Research Institute of Manufacturing Engineering”, Head of Sector, Dnipropetrovsk, Ukraine.

A.M. May, State Enterprise “Production Association Yuzhny Machine-Building Plant named after A.M. Makarov”, Head of Technology Sector, Dnipropetrovsk, Ukraine.

Abstract:

Purpose. Comparative characteristics of the results of mathematical modeling with experimental data and mathematical treatment of the results of the thermo-mechanical calibration.

The complexity of the design of the fairing shells PH “Cyclone-4”, high cost, large dimensions of articles (diameter of 3000–4000 mm), and typical physico-mechanical characteristics of the materials used require to provide an accurate assessment of the effectiveness of the technologies used in the production process.

Methodology. The paper compares the experimental and calculated parameters of the process of thermomechanical calibration of shells, the large thin-walled structures fairing RN “Cyclone-4”, and assesses its degree of effectiveness depending on the previous technological influences on the product.

The annealing in the fixing device (thermo-mechanical calibration) can be an effective way to deal with the strains in cases where the product is brewed from high-strength material.

Findings. Mathematical treatment of the results of the thermo-mechanical calibration showed sufficient agreement between the experimental and calculated values. The analysis of the experimental data showed the adequacy of the evidence in the process of thermo-mechanical strain gauge calibration.

Determination of the validity of the mathematical model based on an experiment allows us to conclude that the high efficiency method of correction of ellipticity and straightness of oversized shells form depends on the magnitude and distribution of residual stresses produced during the previous production stages.

Analytical calculations and numerical modeling of thermo-mechanical calibration make it clear that the additional annealing treatment is required to relieve residual stresses.

Originality. We have found out that taking into account of all the technological effects during production process improves the efficiency of the thermomechanical calibration and increases the accuracy of the final product.

Practical value. The results can be used for modification of the existing technology of thermomechanical processing of large thin-walled structures, such as shell fairing, RN “Cyclone-4”, and increasing their overall efficiency.

 

References:

 

1. Сварка. Введение в специальность / В.А. Фролов, В.В. Пешков, А.Б. Коломенский, В.А. Казаков. – М., 2004. – 234 с.

 

Frolov, V.A., Peshkov, V.V., Kolomenskiy, A.B. and Kazakov, V.A. (2004), Svarka. Vvedeniye v spetsyalnost [Welding. Specialty Introductory Course], Moscow, Russia.

 

2. Шерстюк Д.Г. Порівняльна характеристика методів забезпечення точності геометричних параметрів вісесиметричних великогабаритних конструкцій / Д.Г. Шерстюк, О.В. Кулик, А.А. Фокін // Вісник Дніпропетровського університету. Серія: ракетно-космічна техніка. –  2012. – Випуск 15. – Том 2. – С. 207–213.

 

Sherstiuk, D.G., Kulik, A.V. and Fokin, A.A. (2012), “Comparison of methods to ensure the accuracy of axisymmetrical geometrical parameters of large structures”, Bulletin of Dnipropetrovsk University, Series: rocket-space technique, Issue 15, Volume 2, DNU, pp. 207–213.

 

3. Головин Г.Ф. Технология термической обработки металлов с применением индукционного нагрева / Головин Г.Ф., Зимин Н.В. – Л.: Машиностроение, 1998. – 87 с.

 

Golovin, G.F. and Zimin, N.V. (1998), Tekhnologiya termicheskoy obrabotki metallov s primeneniyem induktsyonnogo nagreva [Technology of Heat Treatment of Metals with Induction Heating], Mechanical Engineering, St. Petersburg, Russia.

 

4. Залишкові напруги у процесі виготовлення циліндричних та конічних обичайок головного обтічника ракети-носія /
Д.Г. Шерстюк, О.В. Кулик, Є.А. Джур [та ін.] // Системне проектування та аналіз характеристик аерокосмічної техніки: збірних наукових праць, ДНУ ім. О.Гончара. – 2012. – Том XIV. – С. 116–129.

 

Sherstiuk, D.G., Kulik, O.V., Dzhur, Ye.A., Soshnіkov, Ye.A. (2012), “Zalyshkovі napruhy v protsesі vyhotovlennia tsylіndrychnykh ta konіchnykh obychaiok holovnoho obtіchnyka rakety-nosіia” [Residual stresses in the shell nose cone of rocket vehicle production process], System design and performance analysis of aerospace technology: modular scientific papers of
O. Gonchar DNU, Volume XIV, pp. 116–129.

 

5. Махненко О.В. Прогнозирование деформаций при сварке и тепловой правке конструкций на основе методов термопластичности и функции усадки: автореф. диссертация на соискание научной степени доктора технических наук: специальность 05.03.06 „Сварка и родственные технологии“ / О.В. Махненко – К., 2009. –18 с.

 

Makhnenko, O.V. (2009), “Prediction of deformation during welding and thermal straightening designs based on the thermoplastic methods and features of shrinkage”, Abstract of doctor of technical science dissertation, specialty 05.03.06 “Welding and Related Technologies”, Institute of Electric, Paton National Academy of Sciences of Ukraine, Kiev, Ukraine.

 

6. Двуреченский А.Г. Опыт термокалибровки сварных оболочковых конструкций для уменьшения сварочных деформаций и напряжений / А.Г. Двуреченский, В.П. Корнеев, В.А. Казаков // Технология машиностроения. – 2009. – 
№ 12. –  С. 37–44.

 

Dvurechensky, А.G., Korneev, V.P. and Kazakov, V.A. (2009), “Experience of thermal calibration of welded shell structures to reduce the welding deformation and stress”, Manufacturing Engineering, no. 12, pp. 37–44.

 

7. Маршрутно-технологический паспорт: Корпус 94.7300.1220.0340.00.0, цех №87, сверен и откорректирован с эталоном 25.09.12 – Днепропетровск: ПО ГП „Южмаш“ им. А.М. Макарова. – 2012. –15 с.

 

Manufacture-tracking sheet: Site 94.7300.1220.0340. 00.0, workshop No.87, verified and corrected with the standard 25.09.12, Dnepropetrovsk, “Uzmash”, 15 р.

 

8. Маршрутно-технологический паспорт: Корпус 94.7300.1220.0240.00.0, цех №87, сверен и откорректирован с эталоном 07.12.12 – Днепропетровск: ПО ГП „Южмаш“ им. А.М.Макарова. – 2012. – 25 с.

 

Manufacture-tracking sheet [Text]: Site 94.7300.1220.0240.00.0, workshop No.87, verified and corrected with the standard 07.12.12 - Dnepropetrovsk, “Uzmash”, 25 р.

Files:
2014_1_sherstiuk
Date 2014-07-16 Filesize 238.12 KB Download 1158

Visitors

7564954
Today
This Month
All days
4236
87440
7564954

Guest Book

If you have questions, comments or suggestions, you can write them in our "Guest Book"

Registration data

ISSN (print) 2071-2227,
ISSN (online) 2223-2362.
Journal was registered by Ministry of Justice of Ukraine.
Registration number КВ No.17742-6592PR dated April 27, 2011.

Contacts

D.Yavornytskyi ave.,19, pavilion 3, room 24-а, Dnipro, 49005
Tel.: +38 (056) 746 32 79.
e-mail: This email address is being protected from spambots. You need JavaScript enabled to view it.
You are here: Home Archive by issue 2014 Contents No.1 2014 Geotechnical and mining mechanical engineering, machine building Effectiveness of thermomechanical calibration and determination of residual stresses in the shell nose cone of Cyclone-4