Название |
Development and investigation of large-sized lagging aluminium sheets of the 1163 RDTV (РДТВ) grade with regulated solid cladding and improved service characteristics compared with similar parameters of serial sheets |
Информация об авторе |
All-Russian Scientific Research Institute of Aviation Materials “VIAM”, Moscow, Russia
V. V. Antipov, Deputy Chief Executive Officer, e-mail: antipovvv@viam.ru E. A. Tkachenko, Head of Department
“Stupino Metallurgical Company” JSC, Stupino, Moscow Oblast, Russia
V. M. Chertovikov, Chief Executive Officer
V. P. Gorokhov, Head of Bureau |
Реферат |
There is developed and introduced a process of manufacturing of large-size lagging sheets from 1163 alloy (1163 RDTV (РДТВ) and 1163 RDMV (РДМВ) grades) with regulated solid cladding made of AD35P (АД35П) alloy. Mechanical properties and fatigue characteristics of this alloy are increased, in comparison with commercially available sheets of 1163 ATV (АТВ) grade, which crack resistance (Kсapp) is equal to the Al cladding sheets of 2524 T351 grade. This is confirmed by complex broad investigations and tests. The 6.5 mm thick plates made of AD35P and AD1pl (АД1пл) alloys with low content of titanium, iron and silicon, were used for obtaining of cladding (solid regulated with technological). Investigated sheets of 1163 RDTV grade have high technological plasticity indices both in the annealed state and in hardened conditions. These indices are identical to similar characteristics of serial-produced sheets. Corrosion properties of the 1163 RDTV alloy sheets are identical to the parameters of serial sheets of 1163 ATV and 1163 RDTV grades. Special normative documentation was developed and issued according to the results of carried out researches and tests. This documentation is necessary for serial production of large-sized lagging sheets of 1163 RDTV and 1163 RDMV grades with improved service characteristics (thickness of 1.0–4.0 mm, width of less than 2200 mm and length of less than 9500 mm (according to the Technical Conditions TU 1-801-006–2011)) and mechanical properties (σВ (UTS) 425 MPa, σ0,2 (YTS) 275 MPa, (El) 15% (for the sheets with thickness of 1.5–4.0 mm) and σВ (UTS) 405 MPa, σ0,2 (YTS) 270 MPa, (El) 15% (for the sheets with thickness of 1.0–1.4 mm)). There is also issued the technological instruction for manufacturing of sheets (including large-sized sheets) from 1163 alloy with solid regulated cladding, in production conditions of Stupino Metallurgical Company. |
Библиографический список |
1. OST 1-90070–92. Listy obshivochnye iz alyuminievykh splavov. Tekhnicheskie usloviya (Industrial Standard 1-90070–92. Lagging sheets made of aluminium alloys. Technical conditions). Introduced : 1992-10-01. Moscow : Publishing House of Standards, 1992. 2. TU 1811-003-50193719–03. Listy iz alyuminievogo splava marki 1163, plakirovannye alyuminievym splavom marki AD35P (Technical conditions 1811-003-50193719–03. Sheets made of aluminium alloy of 1163 grade, cladded by aluminium alloy of AD35P (АД35П) grade). Moscow, 2003. 3. AIMS 03-04-020. Aluminium alloy (2524). Solution treated, controlled stretched and naturally aged (T351). High damage tolerant properties. Blagnac (France), 1998 4. Sertifikat 1.2.3.0053–85. Alyuminievye listy 1163RDTV tolshchinoy 2–4 mm (Certificate 1.2.3.0053–85. Aluminium sheets of 1163RDTV (1163 РДТВ) grade with 2–4 mm thickness). Moscow: Central aerohydrodynamic institute, VIAM, 1985. 5. Kablov E. N. Strategicheskie napravleniya razvitiya materialov i tekhnologiy ikh pererabotki na period do 2030 goda (Strategic directions of development of materials and technologies of their processing for the period till 2030). Aviatsionnye materialy i tekhnologii : nauchno-tekhnicheskiy sbornik (Aviation materials and technologies : scientific and technical collection). Moscow : VIAM, 2012. No. 5. pp. 7–17. 6. Antipov V. V. Strategiya razvitiya titanovykh, magnievykh, berillievykh i alyuminievykh splavov (Strategy of development of titanium, magnesium, berillium and aluminium alloys). Aviatsionnye materialy i tekhnologii : nauchno-tekhnicheskiy sbornik (Aviation materials and technologies : scientific and technical collection). Moscow : VIAM, 2012. No. 5. pp. 160–166. 7. Tarasov Yu. M., Antipov V. V. Novye materialy VIAM dlya perspektivnoy aviatsionnoy tekhniki proizvodstva Otkrytogo aktsionernogo obshchestva “OAK” (New materials of VIAM for prospective aviation machinery, manufactured by “United Aircraft Corporation” JSC). Aviatsionnye materialy i tekhnologii : nauchnotekhnicheskiy sbornik (Aviation materials and technologies : scientific and technical collection). Moscow : VIAM, 2012. No. 2. pp. 10–17. 8. Antipov V. V., Senatorova O. G., Tkachenko E. A., Vakhromov R. O. Alyuminievye deformiruemye splavy (Aluminium wrought alloys). Aviatsionnye materialy i tekhnologii : yubileynyy nauchnotekhnicheskiy sbornik (Aviation materials and technologies : anniversary scientific and technical collection). Moscow : VIAM, 2012. pp. 167–182. 9. Kvasov F. I., Fridlyander I. N. Alyuminievye splavy tipa duralyumin (Aluminium alloys of duralumin type). Moscow : Metallurgiya, 1984. 240 p. 10. OST 1-90048–90. Splavy alyuminievye deformiruemye. Marki (Industrial Standard 1-90048–90. Aluminium wrought alloys. Grades). Introduced : 1991-02-01. 11. International Alloy Designations and Chemical Composition Limits. The Aluminum Association for Wrought Aluminium and Wrought Aluminium Alloys. February, 2009. 12. Turchenkov V. A., Baranov D. E., Gagarin M. V., Shishkin M. D. Metodicheskiy podkhod k provedeniyu ekspertizy materialov (Methodical approach to materials expertise). Aviatsionnye materialy i tekhnologii : nauchno-tekhnicheskiy sbornik (Aviation materials and technologies : scientific and technical collection). Moscow : VIAM, 2012. No. 1. pp. 47–53. 13. Erasov V. S., Grinevich A. V., Sennik V. Ya., Konovalov V. V. et al. Raschetnye znacheniya kharakteristik prochnosti aviatsionnykh materialov (Design values of characteristics of durability of aviation materials). Aviatsionnye materialy i tekhnologii : nauchno-tekhnicheskiy sbornik (Aviation materials and technologies : scientific and technical collection). Moscow : VIAM, 2012. No. 2. pp. 14–16. 14. Erasov V. S., Nuzhnyy G. A. Zhestkiy tsikl nagruzheniya pri ustalostnykh ispytaniyakh (Tough loading cycle in the time of fatigue tests). Aviatsionnye materialy i tekhnologii : nauchnotekhnicheskiy sbornik (Aviation materials and technologies : scientific and technical collection). Moscow : VIAM, 2011. No. 4. pp. 35–40. 15. GOST 1497–84. Metally. Metody ispytaniy na rastyazhenie (State Standard 1497–84. Metals. Methods of pull tests). Introduced : 1986-01-01. Moscow : Publishing House of Standards, 2008. 16. GOST 25.502–79. Raschety i ispytaniya na prochnost v mashinostroenii. Metody mekhanicheskikh ispytaniy metallov. Metody ispytaniy na ustalost (State Standard 25.502–79. Calculations and strength tests in mechanical engineering. Methods of mechanical tests of metals. Methods of fatigue tests). Introduced : 1981-01-01. Moscow : Publishing House of Standards, 2005. 17. GOST 25.506–85. Raschety i ispytaniya na prochnost. Metody mekhanicheskikh ispytaniy metallov. Opredelenie kharakteristik treshchinostoykosti (vyazkosti razrusheniya) pri staticheskom nagruzhenii (State Standard 25.506–85. Calculations and strength tests. Methods of mechanical tests of metals. Definition of characteristics of crack resistance (fracture toughness) in the time of static loading). Introduced : 1986-01-01. Moscow : Publishing House of Standards, 2005. 18. OST 1-90268–78. Metally. Metod opredeleniya skorosti rosta ustalostnoy treshchiny (Industrial Standard 1-90268–78. Metals. Method of definition of growth rate of fatigue crack). Introduced : 1979-01-01. Moscow : Publishing House of Standards, 1979. 19. Stepnov M. N. Statisticheskie metody obrabotki rezultatov mekhanicheskikh ispytaniy : spravochnik (Statistic methods of processing of results of mechanical testings : reference book). Moscow : Mashinostroenie, 1985. 232 p. 20. GOST R ISO 21747–2010. Statisticheskie metody. Statistiki prigodnosti i vosproizvodimosti protsessa dlya kolichestvennykh kharakteristik kachestva (State Standard R ISO 21747–2010. Statistic methods. Statistics of appropriateness and repeatability of process for quantitative characteristic of quality). Introduced : 2011-12-01. Moscow : Publishing House of Standards, 2012. 21. TU 1-801-006–2011. Oblitsovochnye listy tolshchinoy ot 1.0 do 4.0 mm iz alyuminievogo splava marki 1163 s tverdoy reglamentirovannoy plakirovkoy (Technical conditions 1-801-006–2011. Facing sheets with thickness from 1.0 to 4.0 mm from aluminium alloy of 1163 grade with solid regulated cladding). Stupino (Moscow Oblast), 2011. |