CN100512992C - Combination beam type tension force stretching method - Google Patents
Combination beam type tension force stretching method Download PDFInfo
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- CN100512992C CN100512992C CNB2007103065296A CN200710306529A CN100512992C CN 100512992 C CN100512992 C CN 100512992C CN B2007103065296 A CNB2007103065296 A CN B2007103065296A CN 200710306529 A CN200710306529 A CN 200710306529A CN 100512992 C CN100512992 C CN 100512992C
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Abstract
The invention belongs to the processing field of nonferrous metal and ferrous metal, in particular to a compound beam tension drawing method. The invention is characterized in that an upper beam (1), a lower beam (2), an upper clamping incline (6) and a lower clamping incline are beveloid with the same angle. The upper beam (1) is connected with the upper clamping incline (6) to form an upper clamping jaw. The lower beam (2) is connected with the lower clamping incline (7) to form a lower clamping jaw. An upper stiffening beam (3) is arranged above the upper clamping jaw. A lower stiffening beam (4) is arranged below the lower clamping jaw. The upper stiffening beam (3) is connected with the lower stiffening beam (4) by a pull pier. The upper stiffening beam (3) and the lower stiffening beam (4) are used for reducing the vertical bending deflection of the beam caused by the component of pulling force. The upper clamping jaw and the lower clamping jaw form a jaw. Stretching sheet material (10) is stretched by the jaw of the upper clamping jaw and the lower clamping jaw. The whole machine head of the invention is easy to be casted, processed, transported, installed and repaired. The machine head has strong rigidity under load operation.
Description
Technical field
The invention belongs to the coloured and ferrous metal manufacture field of metallurgical equipment, particularly a kind of novel combination beam type tension force stretching method.
Background technology
The tension force stretching machine is used for coloured or black strip, tube, rod section material etc. are stretched.By making the stretching of the certain percentage elongation of material production, on the one hand metal is carried out intensive treatment, play aligning, leveling effect on the other hand, be widely used in metallurgy industry, aluminium and aluminium alloy processing industry.
Tension force stretching machine version is more, the head that traditional tension force stretching machine is used to clamp stretching adopts whole forge piece, though good rigidly, but because of enclosed construction restriction makes the head processing difficulties, precision is difficult to guarantee when especially processing the clamping inclined-plane of head, the mobile guide the when clamping claw that this inclined-plane is used for the jaw assembly clamps or opens.For large-tonnage, Wide and Thick Slab, heavy tension force stretching machine, the conspicuous contradiction that the head overall structure is brought is that single part weight is overweight, and casting, processing all can't be finished.
Summary of the invention
The purpose of this invention is to provide a kind of novel combination beam type tension force stretching method, the device that this method adopted not only makes body clamp the inclined-plane and is easy to processing, and whole head casting, processing transportation, an installation and maintenance difficult technologies difficult problem under the situation that guarantees equipment performance, have been solved for large-tonnage, Wide and Thick Slab, heavy tension force stretching machine from structure.
For achieving the above object, the technical scheme of the object of the invention is, design a kind of combination beam type tension force stretching method, it is characterized in that: the device that this method adopted comprises buttress brace 3 at least, following buttress brace 4, entablature 1, sill 2, last clamping inclined-plane 6 reaches and clamps inclined-plane 7 down, entablature 1, sill 2, last clamping inclined-plane 6 reaches and clamps inclined-plane 7 down is the clinohedral of equal angular, entablature 1 and 6 inclined-planes, last clamping inclined-plane connect and compose clamping clip, sill 2 and following 7 inclined-planes, inclined-plane that clamp connect and compose down clamping clip, there is last buttress brace 3 last clamping clip upper end, there is following buttress brace 4 following clamping clip lower end, last buttress brace 3 is connected by pulling force post 5 with following buttress brace 4, and last buttress brace 3 and following buttress brace 4 are used to reduce the flexural deformation that tensile force component causes that crossbeam vertically produces; Last clamping clip and following clamping clip jaw form jaw; Stretching sheet material 10 stretches by the jaw between last clamping clip and the following clamping clip.
Described entablature 1 and go up to clamp between 6 inclined-planes, inclined-plane and sill 2 and clamp down adjusted plate 8 and following adjustable plate 9 are arranged between 7 inclined-planes, inclined-plane.
The described clamping inclined-plane 6 of going up has upper jaw securing member 11 and lower jaw securing member 12 to be used to regulate jaw size with following inclined-plane 7 one sides that clamp.
Described adjusted plate 8 and following adjustable plate 9 are the secured adjusted jaw size.
Described upper jaw securing member 11 and lower jaw securing member 12 are used to finely tune jaw size.
Characteristics of the present invention are: the device that the present invention does employing belongs to finishing equipment, the heavy tension force stretching machine that is used for big tensile force is because whole subdivision, the combination beam type structure up and down of adopting of tension force stretching machine head, the whole head that is used to clamp stretching is divided into several parts, it is open that body clamps the inclined-plane, be easy to processing, thereby raising machining accuracy, and each parts installation, processing, easy to maintenance; Upper and lower crossbeam and upper and lower buttress brace adopt and draw column (beam) to connect, and draw column (beam) to bear the component that tensile force vertically produces, and guarantee the rigidity of whole head under load condition.
Description of drawings
Below in conjunction with the embodiment accompanying drawing content of the present invention is illustrated.
Fig. 1 is a structural representation of the present invention;
Fig. 2 is a cutaway view of the present invention.
Among the figure: 1, entablature; 2, sill; 3, go up buttress brace; 4, following buttress brace; 5, pulling force post; 6, clamp the inclined-plane on; 7, clamp the inclined-plane down; 8, adjusted plate; 9, following adjustable plate; 10, stretching sheet material; 11, upper jaw securing member; 12, lower jaw securing member.
The specific embodiment
As depicted in figs. 1 and 2, the stretching-machine that this method adopts comprises buttress brace 3, following buttress brace 4, entablature 1, sill 2, last clamping inclined-plane 6 reaches and clamps inclined-plane 7 down, entablature 1, sill 2, last clamping inclined-plane 6 reaches and clamps inclined-plane 7 down is the clinohedral of equal angular, entablature 1 and 6 inclined-planes, last clamping inclined-plane connect and compose clamping clip, sill 2 and following 7 inclined-planes, inclined-plane that clamp connect and compose down clamping clip, there is last buttress brace 3 last clamping clip upper end, there is following buttress brace 4 following clamping clip lower end, last buttress brace 3 is connected by pulling force post 5 with following buttress brace 4, makes clamping clip and following clamping clip jaw form jaw; Stretching sheet material 10 stretches by the jaw between last clamping clip and the following clamping clip.In order to regulate jaw size, entablature 1 and go up to clamp between 6 inclined-planes, inclined-plane and sill 2 and clamp down adjusted plate 8 and following adjustable plate 9 are arranged between 7 inclined-planes, inclined-plane, last clamping inclined-plane 6 and following inclined-plane 7 one sides that clamp have upper jaw securing member 11 and lower jaw securing member 12 to be used to regulate jaw size, the former is the secured adjusted jaw size, and the latter finely tunes jaw size.
Claims (1)
1, a kind of combination beam type tension force stretching method, it is characterized in that: the device that this method adopted comprises buttress brace (3) at least, following buttress brace (4), entablature (1), sill (2), last clamping inclined-plane (6) reaches and clamps inclined-plane (7) down, entablature (1), sill (2), last clamping inclined-plane (6) reaches and clamps inclined-plane (7) down is the clinohedral of equal angular, entablature (1) and inclined-plane, last clamping inclined-plane (6) connect and compose clamping clip, sill (2) and the following inclined-plane, inclined-plane (7) that clamps connect and compose down clamping clip, there is last buttress brace (3) last clamping clip upper end, there is following buttress brace (4) following clamping clip lower end, last buttress brace (3) is connected by pulling force post (5) with following buttress brace (4), and last buttress brace (3) and following buttress brace (4) are used to reduce the flexural deformation that tensile force component causes that crossbeam vertically produces; Last clamping clip and following clamping clip jaw form jaw; Stretching sheet material (10) stretches by the jaw between last clamping clip and the following clamping clip; There are adjusted plate (8) and following adjustable plate (9), upper jaw securing member (11) and lower jaw securing member (12) to be used to regulate jaw size between entablature (1) and the inclined-plane, last clamping inclined-plane (6) and between sill (2) and the following clamping inclined-plane, inclined-plane (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2007103065296A CN100512992C (en) | 2007-12-29 | 2007-12-29 | Combination beam type tension force stretching method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2007103065296A CN100512992C (en) | 2007-12-29 | 2007-12-29 | Combination beam type tension force stretching method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN101214507A CN101214507A (en) | 2008-07-09 |
| CN100512992C true CN100512992C (en) | 2009-07-15 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB2007103065296A Active CN100512992C (en) | 2007-12-29 | 2007-12-29 | Combination beam type tension force stretching method |
Country Status (1)
| Country | Link |
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| CN (1) | CN100512992C (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106585068A (en) * | 2016-10-27 | 2017-04-26 | 苏州仓旻电子科技有限公司 | Leveling detection device suitable for metal composite plate |
| CN109530463B (en) * | 2019-01-15 | 2024-09-17 | 中国重型机械研究院股份公司 | Bolt combination beam |
| CN109530464B (en) * | 2019-01-15 | 2024-10-01 | 中国重型机械研究院股份公司 | Connecting piece composite beam |
| CN109530465B (en) * | 2019-01-15 | 2024-10-01 | 中国重型机械研究院股份公司 | Load-bearing surface composite beam |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4148210A (en) * | 1976-08-17 | 1979-04-10 | Ab Nike Hydraulik | Self-tightening pull clamp for attaching to sheet metal flanges and the like |
| DE3539618A1 (en) * | 1985-11-08 | 1987-05-14 | Schloemann Siemag Ag | Clamping device with wedge drive |
| CN1223178A (en) * | 1997-11-13 | 1999-07-21 | 米什兰构思与开发公司 | Machining of sheet without removal material |
| CN1704183A (en) * | 2004-06-03 | 2005-12-07 | 中国科学院金属研究所 | Aluminum alloy tubing straightening method and special fixture thereof |
| CN200974082Y (en) * | 2006-09-27 | 2007-11-14 | 宝山钢铁股份有限公司 | Hydraulic clamp tool |
| CN200974081Y (en) * | 2006-09-27 | 2007-11-14 | 宝山钢铁股份有限公司 | Mechanical clamp apparatus |
-
2007
- 2007-12-29 CN CNB2007103065296A patent/CN100512992C/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4148210A (en) * | 1976-08-17 | 1979-04-10 | Ab Nike Hydraulik | Self-tightening pull clamp for attaching to sheet metal flanges and the like |
| DE3539618A1 (en) * | 1985-11-08 | 1987-05-14 | Schloemann Siemag Ag | Clamping device with wedge drive |
| CN1223178A (en) * | 1997-11-13 | 1999-07-21 | 米什兰构思与开发公司 | Machining of sheet without removal material |
| CN1704183A (en) * | 2004-06-03 | 2005-12-07 | 中国科学院金属研究所 | Aluminum alloy tubing straightening method and special fixture thereof |
| CN200974082Y (en) * | 2006-09-27 | 2007-11-14 | 宝山钢铁股份有限公司 | Hydraulic clamp tool |
| CN200974081Y (en) * | 2006-09-27 | 2007-11-14 | 宝山钢铁股份有限公司 | Mechanical clamp apparatus |
Also Published As
| Publication number | Publication date |
|---|---|
| CN101214507A (en) | 2008-07-09 |
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Owner name: CHINA NATIONAL HEAVY MACHINERY RESEARCH INSTITUTE Free format text: FORMER NAME: CHINA HEAVY MACHINERY INSTITUTE |
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| CP01 | Change in the name or title of a patent holder |
Address after: 710032 Shaanxi city in Xi'an province Xin Jiamiao Xi'an Heavy Machinery Research Institute Patentee after: CHINA NATIONAL HEAVY MACHINERY RESEARCH INSTITUTE Co.,Ltd. Address before: 710032 Shaanxi city in Xi'an province Xin Jiamiao Xi'an Heavy Machinery Research Institute Patentee before: China National Heavy Machinery Research Institute Co.,Ltd. Address after: 710032 Shaanxi city in Xi'an province Xin Jiamiao Xi'an Heavy Machinery Research Institute Patentee after: China National Heavy Machinery Research Institute Co.,Ltd. Address before: 710032 Shaanxi city in Xi'an province Xin Jiamiao Xi'an Heavy Machinery Research Institute Patentee before: China National Heavy Machinery Research Institute Co.,Ltd. |