CN103522346A - General cutting mould base support - Google Patents
General cutting mould base support Download PDFInfo
- Publication number
- CN103522346A CN103522346A CN201210232910.3A CN201210232910A CN103522346A CN 103522346 A CN103522346 A CN 103522346A CN 201210232910 A CN201210232910 A CN 201210232910A CN 103522346 A CN103522346 A CN 103522346A
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- China
- Prior art keywords
- square steel
- connecting plate
- steel tube
- cross beam
- positioning
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- Legal status (The legal status 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 status listed.)
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Abstract
The invention belongs to the field of airplane equipment, and provides a general cutting mould base support. The general cutting mould base support comprises two supporting seats and a cross beam which are fixedly connected through bolts and nuts. Each supporting seat is formed by welding a positioning plate, a stand column square steel tube, two reinforcing square steel tubes, base boards, reinforcing plates and a connecting cross beam steel tube, wherein the positioning plate is welded to one lateral face of the stand column square steel tube, and two rows of positioning holes are formed in the positioning plate. The cross beam is formed by welding two end connecting plates, a cross beam square steel tube and a connecting plate, wherein the end connecting plates are welded to the two ends of the cross beam square steel tube, two rows of positioning holes are formed in each end connecting plate, the connecting plate is provided with two rows of positioning connecting holes, the two supporting seats and the cross beam are fixedly connected with bolts and nuts through the positioning holes in the connecting plate and the positioning holes in the end connecting plates, and a cutting mould is installed with the positioning holes in a matched mode. The general cutting mould base support is strong in applicability, can position different positioning tools as needed, and meets the requirement for cutting different airplane parts.
Description
Technical field
The invention belongs to aircraft equipment field, relate to a kind of general blanking punch base support.
Background technology
In airplane component manufacture process, the shared ratio of composite material parts increases day by day, for composite material parts on shaping mould after moulding, generally all by cutting tool, carry out the setting that periphery has cut composite products profile, and each cutting tool has independently transporting bracket go-cart, owing to assembling the quantity of technique for aircraft composite, strengthen gradually, the quantity of cutting tool also just increases, will cause like this aircraft manufacturing cost to strengthen, the situation of worker-house usable floor area growing tension, so how to reduce the manufacturing cost of composite cutting tool, there is very large economic worth.
Summary of the invention
The technical problem to be solved in the present invention: a kind of general blanking punch base support is provided, reduces the quantity of composite cutting tool base support, thereby reduce the manufacturing cost of composite cutting tool.
Technical scheme of the present invention: a kind of general blanking punch base support, it is characterized in that, comprising: two bearings, a crossbeam are connected and fixed composition with screw bolt and nut; Bearing is to be welded by location-plate, column square steel tube, two reinforcement square steel tubes, base plate, stiffener, connecting cross beam square steel tubes, and connecting plate is welded on the side of column square steel tube, has two registration holes on connecting plate; Crossbeam is to be welded by two termination connecting plates, crossbeam square steel tube, connecting plate, at crossbeam square steel tube two ends, be welded with termination connecting plate, on the connecting plate of termination with two registration holes, on connecting plate, there are two registration connecting holes, two bearings and crossbeam are to be connected and fixed with bolt and nut by locating hole on locating hole on connecting plate and termination connecting plate, and blanking punch coordinates installation with locating hole.
Beneficial effect of the present invention: applicability of the present invention is strong, can locate different cutting tools as required, has met the needs of different airplane component cuttings.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
Fig. 2 is middle transverse beam structure schematic diagram of the present invention.
Fig. 3 is medium-height trestle structural representation of the present invention.
The specific embodiment
Below the present invention is described in further details.Referring to Fig. 1～3, a kind of general blanking punch base support, comprising: two bearings 1, crossbeam 2 use bolt 3 and nut 4 are connected and fixed composition; Bearing 1 be by location-plate 5, column square steel tube 6, two strengthen square steel tube 7, base plate 8, stiffener 9, connecting cross beam square steel tube 10 and be welded, connecting plate 5 is welded on the side of column square steel tube 6, has two registration holes 11 on connecting plate 5; Crossbeam 2 is to be welded by two termination connecting plates 12, crossbeam square steel tube 13, connecting plate 14, at crossbeam square steel tube 13 two ends, be welded with termination connecting plate 12, on termination connecting plate 12 with two registration holes 16, on connecting plate 14, there are two registration connecting holes 15, two bearings 1 and crossbeam 2 are to be connected and fixed by 16 use bolt 3 nuts 4 of locating hole on locating hole 11 on connecting plate 5 and termination connecting plate 12, and blanking punch coordinates installation with locating hole 15.
Using method of the present invention is: during use, will be that two bearings 1, a crossbeam 2 are adjusted to required installation site first as required, then with bolt 3 and nut 4, be connected and fixed composition diagram 1, on the blanking punch that will install again and crossbeam locating hole 15 interior with bolt and nut, be connected and fixed to install just can use, this general blanking punch base support, solve a difficult problem for support go-carts of cutting tool needs, greatly reduced the manufacturing cost of frock.Improved the service efficiency of frock manufacture efficiency and worker-house area simultaneously.
Claims (1)
1. a general blanking punch base support, is characterized in that, comprising: two bearings, a crossbeam are connected and fixed composition with screw bolt and nut; Bearing is to be welded by location-plate, column square steel tube, two reinforcement square steel tubes, base plate, stiffener, connecting cross beam square steel tubes, and connecting plate is welded on the side of column square steel tube, has two registration holes on connecting plate; Crossbeam is to be welded by two termination connecting plates, crossbeam square steel tube, connecting plate, at crossbeam square steel tube two ends, be welded with termination connecting plate, on the connecting plate of termination with two registration holes, on connecting plate, there are two registration connecting holes, two bearings and crossbeam are to be connected and fixed with bolt and nut by locating hole on locating hole on connecting plate and termination connecting plate, and blanking punch coordinates installation with locating hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210232910.3A CN103522346A (en) | 2012-07-06 | 2012-07-06 | General cutting mould base support |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210232910.3A CN103522346A (en) | 2012-07-06 | 2012-07-06 | General cutting mould base support |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103522346A true CN103522346A (en) | 2014-01-22 |
Family
ID=49924872
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210232910.3A Pending CN103522346A (en) | 2012-07-06 | 2012-07-06 | General cutting mould base support |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103522346A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103878511A (en) * | 2014-04-10 | 2014-06-25 | 太仓斯普宁精密机械有限公司 | Support of precise welding robot |
| CN109052109A (en) * | 2018-08-20 | 2018-12-21 | 宁波宏大电梯有限公司 | A kind of steel structure lift shaft component |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3500770A1 (en) * | 1984-01-13 | 1985-07-25 | Fa. Hans Ehgartner, Wien | Spacer for the blades of a rotatable cutting tool |
| DE19513984A1 (en) * | 1995-04-13 | 1996-10-17 | Karl Grube | Cutting device for manufacture of insulation sheets made from e.g. glass fibre |
| FR2802847A1 (en) * | 1999-12-24 | 2001-06-29 | Lectra Systemes Sa | Safety system for textile cutting table with mobile cross-beam which carries cutter head has bars at each end of beam to detect obstacles at sides of table and which carry light emitters and photoreceptors which detect obstacles on table. |
| CN201484667U (en) * | 2009-09-14 | 2010-05-26 | 哈尔滨飞机工业集团有限责任公司 | Universal combined frame for vertical assembling jig |
| CN201493783U (en) * | 2009-09-14 | 2010-06-02 | 哈尔滨飞机工业集团有限责任公司 | Universal combined horizontal assembly fixture frame |
-
2012
- 2012-07-06 CN CN201210232910.3A patent/CN103522346A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3500770A1 (en) * | 1984-01-13 | 1985-07-25 | Fa. Hans Ehgartner, Wien | Spacer for the blades of a rotatable cutting tool |
| DE19513984A1 (en) * | 1995-04-13 | 1996-10-17 | Karl Grube | Cutting device for manufacture of insulation sheets made from e.g. glass fibre |
| FR2802847A1 (en) * | 1999-12-24 | 2001-06-29 | Lectra Systemes Sa | Safety system for textile cutting table with mobile cross-beam which carries cutter head has bars at each end of beam to detect obstacles at sides of table and which carry light emitters and photoreceptors which detect obstacles on table. |
| CN201484667U (en) * | 2009-09-14 | 2010-05-26 | 哈尔滨飞机工业集团有限责任公司 | Universal combined frame for vertical assembling jig |
| CN201493783U (en) * | 2009-09-14 | 2010-06-02 | 哈尔滨飞机工业集团有限责任公司 | Universal combined horizontal assembly fixture frame |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103878511A (en) * | 2014-04-10 | 2014-06-25 | 太仓斯普宁精密机械有限公司 | Support of precise welding robot |
| CN109052109A (en) * | 2018-08-20 | 2018-12-21 | 宁波宏大电梯有限公司 | A kind of steel structure lift shaft component |
| CN109052109B (en) * | 2018-08-20 | 2024-02-13 | 宁波宏大电梯有限公司 | Steel construction elevator well subassembly |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140122 |