RU2007135701A - METHOD FOR MANUFACTURING THIN-WALLED SHELLS - Google Patents
METHOD FOR MANUFACTURING THIN-WALLED SHELLS Download PDFInfo
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- RU2007135701A RU2007135701A RU2007135701/02A RU2007135701A RU2007135701A RU 2007135701 A RU2007135701 A RU 2007135701A RU 2007135701/02 A RU2007135701/02 A RU 2007135701/02A RU 2007135701 A RU2007135701 A RU 2007135701A RU 2007135701 A RU2007135701 A RU 2007135701A
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- tensile strength
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Abstract
Способ изготовления тонкостенных крупногабаритных оболочек оживальной формы из заготовки конусной формы из малопластичных труднодеформируемых сталей путем однопереходной штамповкой в штампе, выполненном с зазором между матрицей и пуансоном, с предварительным нагревом заготовки, отличающийся тем, что перед штамповкой со стороны большего диаметра заготовки формируют фланец для зажима ее в матрице, а нагрев заготовки производят до температуры, определяемой по пределу прочности, найденному из соотношения: ! ! где σBt - предел прочности нагретой заготовки; ! σB - предел прочности обрабатываемого материала при t=20°; ! mB - коэффициент вытяжки при t=20° в точке максимального прогиба; ! mBt - коэффициент вытяжки в точке максимального прогиба при нагреве; ! К - коэффициент пропорциональности, выведенный опытным путем, зависящий от механических свойств обрабатываемого материала.A method of manufacturing thin-walled large-sized shells of a lively shape from a cone-shaped blank from low-plastic hardly deformed steels by single-pass stamping in a stamp made with a gap between the die and the punch, with pre-heating the blank, characterized in that a flange is formed before stamping from the side of the larger diameter of the blank to clamp it in the matrix, and the workpiece is heated to a temperature determined by the tensile strength found from the relation:! ! where σBt is the tensile strength of the heated billet; ! σB is the tensile strength of the processed material at t = 20 °; ! mB is the drawing coefficient at t = 20 ° at the point of maximum deflection; ! mBt is the drawing coefficient at the point of maximum deflection during heating; ! K is the coefficient of proportionality, derived empirically, depending on the mechanical properties of the processed material.
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Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2007135701/02A RU2365454C2 (en) | 2007-09-26 | 2007-09-26 | Method for one-pass die forging thin-walled large-dimensioned ogival-shaped shells of cone-shaped blank parts made of low-ductility difficult-to-form steel of "bhc-16" grade |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2007135701/02A RU2365454C2 (en) | 2007-09-26 | 2007-09-26 | Method for one-pass die forging thin-walled large-dimensioned ogival-shaped shells of cone-shaped blank parts made of low-ductility difficult-to-form steel of "bhc-16" grade |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2007135701A true RU2007135701A (en) | 2009-04-10 |
RU2365454C2 RU2365454C2 (en) | 2009-08-27 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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RU2007135701/02A RU2365454C2 (en) | 2007-09-26 | 2007-09-26 | Method for one-pass die forging thin-walled large-dimensioned ogival-shaped shells of cone-shaped blank parts made of low-ductility difficult-to-form steel of "bhc-16" grade |
Country Status (1)
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RU (1) | RU2365454C2 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2466815C2 (en) * | 2010-12-30 | 2012-11-20 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" (ФГУП "ГКНПЦ им. М.В. Хруничева") | Method of forming ogival-shape equidistant shell stack |
RU2638605C2 (en) * | 2015-05-25 | 2017-12-14 | Общество с ограниченной ответственностью научно-производственное предприятие "Технологический центр" | Method for manufacturing thin-walled shells of complex form |
RU2635990C2 (en) * | 2015-12-08 | 2017-11-17 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" (ФГУП "ГКНПЦ им. М.В. Хруничева") | Method to form part of semispherical shape from hard-deformable titanium alloy bt6-c in one die |
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2007
- 2007-09-26 RU RU2007135701/02A patent/RU2365454C2/en active IP Right Revival
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Publication number | Publication date |
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RU2365454C2 (en) | 2009-08-27 |
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