CN105619662B - A kind of extractor of aviation composite solidification product - Google Patents
A kind of extractor of aviation composite solidification product Download PDFInfo
- Publication number
- CN105619662B CN105619662B CN201610165759.4A CN201610165759A CN105619662B CN 105619662 B CN105619662 B CN 105619662B CN 201610165759 A CN201610165759 A CN 201610165759A CN 105619662 B CN105619662 B CN 105619662B
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- CN
- China
- Prior art keywords
- top plate
- product
- jacking block
- sliding block
- face
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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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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Moulds, Cores, Or Mandrels (AREA)
Abstract
The invention discloses a kind of extractor of aviation composite solidification product, including top plate, grab, jacking block, connecting rod with fulcrum, handwheel, screw rod, sliding block, the top plate is connected by the grab with forming frock end face, the jacking block acts on the binding face of product and forming frock through the top plate, the connecting rod is connected by fulcrum its described with the top plate, one end of the connecting rod acts on the jacking block, the other end is fixed with the sliding block, the sliding block is connected with the screw rod, the handwheel is fixed with the sliding block, the screw acting withstands forming frock end face in the top plate.It is an advantage of the invention that：Steady thrust is applied to product using mechanical transmission structure, it is taken off from forming frock, is not easily caused the layering of product product, rapid operation, conveniently, clamping is quick.
Description
Technical field
The present invention relates to a kind of extractor.
Background technology
After aviation composite product curing molding, the product of solidification need to be taken off from frock.Due to product and frock
Fitting is close, and is limited by product shape and structure, larger for the C-shaped beam product 1-1 stripping operation difficulty shown in accompanying drawing 1,
The web 1-3 of forming frock 1-2 both sides slopes inwardly, and can only along its length exert a force during the demoulding and be taken out by arrow in figure
Go out.
It is stripped at present by the way of being tapped from product one end end face to the other end, because product thickness is small, taps operation
Inconvenience, and easily cause composite product lamination defect occur and scrap.
The content of the invention
Goal of the invention：In view of the above-mentioned problems, it is an object of the invention to provide a kind of extractor, solves stripping operation inconvenience
Aviation composite is caused to solidify the problem of product product is layered with the demoulding is tapped.
Technical scheme：A kind of extractor of aviation composite solidification product, including top plate, grab, jacking block, there is branch
Connecting rod, handwheel, screw rod, the sliding block of point, the top plate are connected by the grab with forming frock end face, and the jacking block passes through institute
The binding face that top plate acts on product and forming frock is stated, the connecting rod is connected by fulcrum its described with the top plate, described
One end of connecting rod acts on the jacking block, and the other end is fixed with the sliding block, and the sliding block is connected with the screw rod, the handwheel
Fixed with the sliding block, the screw acting withstands forming frock end face in the top plate.
Also include spring leaf, the spring leaf is fixed with the top plate and suppressing action is in the jacking block, ensures that jacking block is made
For product and the binding face of forming frock, jacking block is prevented to be upturned.
The jacking block is flat, applies steady thrust to the binding face of product and forming frock.
The position that the connecting rod acts on the jacking block offers arc groove face, and connecting rod is moved with fulcrum under lever principle
Make, arc groove face can be with jacking block reliable contacts.
The screw head is sphere, is contacted with forming frock end face point.
Beneficial effect：Compared with prior art, it is an advantage of the invention that：Product is applied using mechanical transmission structure steady
Thrust, it is taken off from forming frock, be not easily caused the layering of product product, rapid operation, conveniently, clamping is quick.
Brief description of the drawings
Fig. 1 is product and forming frock combination schematic diagram；
Fig. 2 is schematic structural view of the invention.
Embodiment
Below in conjunction with the accompanying drawings and specific embodiment, the present invention is furture elucidated, it should be understood that these embodiments are merely to illustrate
The present invention rather than limitation the scope of the present invention, after the present invention has been read, those skilled in the art are each to the present invention's
The modification of the kind equivalent form of value falls within the application appended claims limited range.
As shown in Figure 2, the extractor of a kind of aviation composite solidification product, including top plate 1, grab 2, jacking block 3,
Connecting rod 5, handwheel 6, screw rod 7, sliding block 8, spring leaf 9 with fulcrum 4.
Top plate 1 is connected by grab 2 with the end face of forming frock 11, and jacking block 3 is flat, and jacking block 3 acts on through top plate 1
The binding face 12 of product and forming frock.Connecting rod 5 is connected by its fulcrum 4 with top plate 1, and connecting rod 5 can be swung around fulcrum 4, even
One end of bar 5 acts on jacking block 3, and the corresponding contact site with both offers arc groove face 10 on connecting rod 5, connecting rod 5 it is another
End is fixed with sliding block 8.Sliding block 8 is threadedly coupled with screw rod 7, and handwheel 6 is fixed with sliding block 8, and screw rod 7 acts on top plate 1 and withstands shaping
Frock end face, the head of screw rod 7 are sphere, are contacted with forming frock end face point.Spring leaf 9 and top plate 1 fix and suppressing action in
Jacking block 3.
Handwheel is rotated, sliding block is moved right along screw rod, the lower end of drivening rod is tilted to the right, and according to lever principle, connects
The upper end of bar is tilted to the left, and acts on jacking block, forces in the binding face of product and forming frock, makes between product and forming frock
Loosen or the product other end is stretched out outside frock, its product can be removed from forming frock afterwards.
Claims (2)
- A kind of 1. extractor of aviation composite solidification product, it is characterised in that：Including top plate (1), grab (2), jacking block (3), have fulcrum (4) connecting rod (5), handwheel (6), screw rod (7), sliding block (8), the top plate (1) by the grab (2) with Forming frock end face connects, and the jacking block (3) acts on the binding face of product and forming frock through the top plate (1), described Connecting rod (5) is connected by fulcrum its described (4) with the top plate (1), and one end of the connecting rod (5) acts on the jacking block (3), The other end is fixed with the sliding block (8), and the sliding block (8) is connected with the screw rod (7), the handwheel (6) and the sliding block (8) Fixed, the screw rod (7) acts on the top plate (1) and withstands forming frock end face；Also include spring leaf (9), the spring leaf (9) is fixed with the top plate (1) and suppressing action is in the jacking block (3)；Institute It is flat to state jacking block (3)；The position that the connecting rod (5) acts on the jacking block (3) offers arc groove face (10).
- A kind of 2. extractor of aviation composite solidification product according to claim 1, it is characterised in that：The spiral shell Bar (7) head is sphere, is contacted with forming frock end face point.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610165759.4A CN105619662B (en) | 2016-03-22 | 2016-03-22 | A kind of extractor of aviation composite solidification product |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610165759.4A CN105619662B (en) | 2016-03-22 | 2016-03-22 | A kind of extractor of aviation composite solidification product |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105619662A CN105619662A (en) | 2016-06-01 |
| CN105619662B true CN105619662B (en) | 2018-03-06 |
Family
ID=56035186
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610165759.4A Active CN105619662B (en) | 2016-03-22 | 2016-03-22 | A kind of extractor of aviation composite solidification product |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105619662B (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105619662B (en) * | 2016-03-22 | 2018-03-06 | 菲舍尔航空部件（镇江）有限公司 | A kind of extractor of aviation composite solidification product |
| CN109834958B (en) * | 2017-11-29 | 2021-05-07 | 中国航空工业集团公司济南特种结构研究所 | Demoulding device for cured composite material |
| CN111267273A (en) * | 2020-03-16 | 2020-06-12 | 沈阳飞机工业（集团）有限公司 | Demoulding method based on L-shaped tool |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE961395C (en) * | 1944-01-21 | 1957-04-04 | Guenther Langlotz | Ejection device on injection molding machines |
| CN2277121Y (en) * | 1996-12-30 | 1998-03-25 | 鸿海精密工业股份有限公司 | Liftout device |
| CN201147991Y (en) * | 2007-11-29 | 2008-11-12 | 昌河飞机工业（集团）有限责任公司 | Big length to diameter ratio composite material equal diameter pipe fitting mould emptier |
| CN203391370U (en) * | 2013-07-03 | 2014-01-15 | 金坛市威克压片机械制造有限公司 | Mold core ejection device in tablet press |
| CN203557586U (en) * | 2013-11-29 | 2014-04-23 | 哈尔滨复合材料设备开发公司 | Demoulding device for composite pipe |
| CN204149471U (en) * | 2014-06-04 | 2015-02-11 | 嘉兴职业技术学院 | A kind of stripper apparatus of rubber axle sleeve |
| CN204414613U (en) * | 2014-12-17 | 2015-06-24 | 连云港东鼎实业有限公司 | GRP pipe core die assembly |
| CN204975098U (en) * | 2015-08-11 | 2016-01-20 | 郑州派斯汽车车身工程有限公司 | Mould is crow bar mechanism for liftout |
| CN105619662A (en) * | 2016-03-22 | 2016-06-01 | 菲舍尔航空部件（镇江）有限公司 | Demolding tool for aviation composite cured product |
-
2016
- 2016-03-22 CN CN201610165759.4A patent/CN105619662B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE961395C (en) * | 1944-01-21 | 1957-04-04 | Guenther Langlotz | Ejection device on injection molding machines |
| CN2277121Y (en) * | 1996-12-30 | 1998-03-25 | 鸿海精密工业股份有限公司 | Liftout device |
| CN201147991Y (en) * | 2007-11-29 | 2008-11-12 | 昌河飞机工业（集团）有限责任公司 | Big length to diameter ratio composite material equal diameter pipe fitting mould emptier |
| CN203391370U (en) * | 2013-07-03 | 2014-01-15 | 金坛市威克压片机械制造有限公司 | Mold core ejection device in tablet press |
| CN203557586U (en) * | 2013-11-29 | 2014-04-23 | 哈尔滨复合材料设备开发公司 | Demoulding device for composite pipe |
| CN204149471U (en) * | 2014-06-04 | 2015-02-11 | 嘉兴职业技术学院 | A kind of stripper apparatus of rubber axle sleeve |
| CN204414613U (en) * | 2014-12-17 | 2015-06-24 | 连云港东鼎实业有限公司 | GRP pipe core die assembly |
| CN204975098U (en) * | 2015-08-11 | 2016-01-20 | 郑州派斯汽车车身工程有限公司 | Mould is crow bar mechanism for liftout |
| CN105619662A (en) * | 2016-03-22 | 2016-06-01 | 菲舍尔航空部件（镇江）有限公司 | Demolding tool for aviation composite cured product |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105619662A (en) | 2016-06-01 |
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