RU2001126560A - Method and device for manufacturing a metal honeycomb element - Google Patents

Method and device for manufacturing a metal honeycomb element

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Publication number
RU2001126560A
RU2001126560A RU2001126560/02A RU2001126560A RU2001126560A RU 2001126560 A RU2001126560 A RU 2001126560A RU 2001126560/02 A RU2001126560/02 A RU 2001126560/02A RU 2001126560 A RU2001126560 A RU 2001126560A RU 2001126560 A RU2001126560 A RU 2001126560A
Authority
RU
Russia
Prior art keywords
crimp elements
crimp
tubular casing
elements
plate
Prior art date
Application number
RU2001126560/02A
Other languages
Russian (ru)
Other versions
RU2233207C2 (en
Inventor
Лудвиг ВИРЕС
Original Assignee
Эмитек Гезельшафт Фюр Эмиссионстехнологи Мбх
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from DE19912871A external-priority patent/DE19912871A1/en
Application filed by Эмитек Гезельшафт Фюр Эмиссионстехнологи Мбх filed Critical Эмитек Гезельшафт Фюр Эмиссионстехнологи Мбх
Publication of RU2001126560A publication Critical patent/RU2001126560A/en
Application granted granted Critical
Publication of RU2233207C2 publication Critical patent/RU2233207C2/en

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Claims (16)

1. Способ изготовления металлического сотового элемента, при осуществлении которого, по меньшей мере, один, по крайней мере, частично структурированный или профилированный металлический лист (1, 2) свертывают в рулон или скручивают либо из него формируют слоистую структуру с получением основы, которую помещают в трубчатый кожух (5), после чего к наружной поверхности трубчатого кожуха (5) последовательно, если смотреть в окружном направлении этого трубчатого кожуха (5), прикладывают в основном линейно действующее и направленное в основном радиально внутрь усилие, под действием которого происходит упругая деформация по крайней мере указанного трубчатого кожуха (5).1. A method of manufacturing a metal honeycomb element, in the implementation of which at least one at least partially structured or profiled metal sheet (1, 2) is rolled up or twisted or a layered structure is formed from it to obtain a base, which is placed into the tubular casing (5), after which, to the outer surface of the tubular casing (5), in succession, when viewed in the circumferential direction of this tubular casing (5), a linearly acting and directed mainly for the sake of the force inside which causes elastic deformation of at least the specified tubular casing (5). 2. Способ по п.1, в котором сотовый элемент помещают, по крайней мере, между двумя отстоящими друг от друга обжимными элементами (6, 7, 8, 13, 14, 15, 16) и, по меньшей мере, один из этих обжимных элементов (6, 7, 8, 13, 14, 15, 15 16) приводят в движение, при этом предусмотрена возможность изменения относительного расстояния между по меньшей мере двумя из числа указанных по меньшей мере двух обжимных элементов (6, 7, 8, 13, 14, 15, 16).2. The method according to claim 1, in which the honeycomb element is placed at least between two spaced apart crimp elements (6, 7, 8, 13, 14, 15, 16) and at least one of these crimp elements (6, 7, 8, 13, 14, 15, 15 16) are set in motion, while it is possible to change the relative distance between at least two of the at least two crimp elements (6, 7, 8, 13, 14, 15, 16). 3. Способ по п.2, в котором по крайней мере один из обжимных элементов (13, 14, 15) приводят в поступательное, движение.3. The method according to claim 2, in which at least one of the crimp elements (13, 14, 15) is brought into translational motion. 4. Способ по п.3, в котором сотовый элемент помещают между двумя пластинчатыми обжимными элементами (13, 14), при этом указанные пластинчатые обжимные элементы (13, 14) перемещают друг относительно друга навстречу друг другу и в основном параллельно друг другу.4. The method according to claim 3, in which the honeycomb element is placed between two plate crimp elements (13, 14), while said plate crimp elements (13, 14) are moved relative to each other towards each other and basically parallel to each other. 5. Способ по п.4, в котором один из пластинчатых обжимных элементов установлен неподвижно, а другой пластинчатый обжимной элемент приводят в движение.5. The method according to claim 4, in which one of the plate crimp elements is fixed, and the other plate crimp element is set in motion. 6. Способ по п.4, в котором пластинчатые обжимные элементы (13, 14) перемещают во взаимно противоположных направлениях.6. The method according to claim 4, in which the plate crimp elements (13, 14) are moved in mutually opposite directions. 7. Способ по п.2 или 3, в котором, по крайней мере, один из обжимных элементов (6, 7, 8, 16) приводят во вращение.7. The method according to claim 2 or 3, in which at least one of the crimp elements (6, 7, 8, 16) is rotated. 8. Способ по п.7, в котором сотовый элемент помещают, по крайней мере, между тремя цилиндрическими обжимными элементами (6, 7, 8), каждый из которых имеет возможность вращения вокруг своей оси (9, 10, 11).8. The method according to claim 7, in which the honeycomb element is placed between at least three cylindrical crimp elements (6, 7, 8), each of which has the ability to rotate around its axis (9, 10, 11). 9. Устройство для изготовления металлического сотового элемента, состоящего из основы, полученной свертыванием в рулон или скручиванием, по меньшей мере, одного, по крайней мере, частично структурированного или профилированного металлического листа (1, 2) либо формированием из него слоистой структуры, и из трубчатого кожуха (5), в котором расположена указанная основа, отличающееся наличием, по меньшей мере, двух подвижных друг относительно друга обжимных элементов (6, 7, 8, 13, 14, 15, 16) и возможностью изменения относительного расстояния между, по меньшей мере, двумя из числа указанных, по меньшей мере, двух обжимных элементов (6, 7, 8, 13, 14, 15, 16), при этом предусмотрена возможность такого расположения сотового элемента между обжимными элементами (6, 7, 8, 13, 14, 15, 16), чтобы обеспечивался контакт этих обжимных элементов (6, 7, 8, 13, 14, 15, 16) с наружной поверхностью трубчатого кожуха (5) и обеспечивалась последовательная передача от них, по крайней мере, на часть окружности трубчатого кожуха (5) направленного в основном радиально внутрь усилия, обусловливающего упругую деформацию, по крайней мере, указанного трубчатого кожуха (5).9. A device for manufacturing a metal honeycomb element consisting of a base obtained by rolling or twisting at least one at least partially structured or profiled metal sheet (1, 2) or forming a layered structure therefrom, and from a tubular casing (5), in which the specified base is located, characterized by the presence of at least two crimp elements (6, 7, 8, 13, 14, 15, 16) movable relative to each other and the possibility of changing the relative distance between, in m at least two of the specified at least two crimp elements (6, 7, 8, 13, 14, 15, 16), while the possibility of such an arrangement of the honeycomb element between the crimp elements (6, 7, 8, 13 , 14, 15, 16), in order to ensure contact of these crimp elements (6, 7, 8, 13, 14, 15, 16) with the outer surface of the tubular casing (5) and ensure sequential transmission from them, at least to part the circumference of the tubular casing (5) directed mainly radially inward to the force causing elastic deformation, at least tubular casing (5). 10. Устройство по п.9, отличающееся тем, что, по меньшей мере, один из обжимных элементов (6, 7, 8, 13, 14, 15, 16) кинематически связан с приводом.10. The device according to claim 9, characterized in that at least one of the crimp elements (6, 7, 8, 13, 14, 15, 16) is kinematically connected to the drive. 11. Устройство по п.9 или 10, отличающееся тем, что, по крайней мере, один из обжимных элементов (13, 14, 15) выполнен с возможностью поступательного движения.11. The device according to claim 9 or 10, characterized in that at least one of the crimp elements (13, 14, 15) is made with the possibility of translational motion. 12. Устройство по п.11, отличающееся тем, что обжимные элементы (13, 14) имеют пластинчатую форму и выполнены с возможностью параллельного перемещения друг относительно друга.12. The device according to claim 11, characterized in that the crimp elements (13, 14) have a plate shape and are made with the possibility of parallel movement relative to each other. 13. Устройство по п.12, отличающееся тем, что один из пластинчатых обжимных элементов выполнен неподвижным, а другой обжимной элемент выполнен подвижным.13. The device according to p. 12, characterized in that one of the plate crimp elements is stationary, and the other crimp element is movable. 14. Устройство по п.12, отличающееся тем, что предусмотрена возможность перемещения пластинчатых обжимных элементов (13, 14) во взаимно противоположных направлениях.14. The device according to claim 12, characterized in that it is possible to move the plate crimp elements (13, 14) in mutually opposite directions. 15. Устройство по п.9, 10 или 11, отличающееся тем, что, по крайней мере, один из обжимных элементов (6, 7, 8,16) выполнен с возможностью вращения.15. The device according to claim 9, 10 or 11, characterized in that at least one of the crimp elements (6, 7, 8.16) is rotatable. 16. Устройство по п.15, отличающееся наличием, по крайней мере, трех цилиндрических обжимных элементов (6, 7, 8), каждый из которых выполнен с возможностью вращения вокруг своей оси (9, 10, 11).16. The device according to p. 15, characterized by the presence of at least three cylindrical crimp elements (6, 7, 8), each of which is rotatable around its axis (9, 10, 11).
RU2001126560/02A 1999-03-22 2000-02-09 Method for making honeycomb metallic member and apparatus for performing the same RU2233207C2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19912871.5 1999-03-22
DE19912871A DE19912871A1 (en) 1999-03-22 1999-03-22 Method and device for producing a metallic honeycomb body

Publications (2)

Publication Number Publication Date
RU2001126560A true RU2001126560A (en) 2003-08-10
RU2233207C2 RU2233207C2 (en) 2004-07-27

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Country Status (11)

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US (1) US6751864B2 (en)
EP (1) EP1163433A1 (en)
JP (1) JP2002539952A (en)
KR (1) KR20020000864A (en)
CN (1) CN1133802C (en)
AU (1) AU2671200A (en)
DE (1) DE19912871A1 (en)
PL (1) PL349954A1 (en)
RU (1) RU2233207C2 (en)
TW (1) TW467789B (en)
WO (1) WO2000057039A1 (en)

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