CN206633449U - It is molded the Wound Dies of inside grid reinforced cylindrical shell structure product - Google Patents
It is molded the Wound Dies of inside grid reinforced cylindrical shell structure product Download PDFInfo
- Publication number
- CN206633449U CN206633449U CN201720365881.6U CN201720365881U CN206633449U CN 206633449 U CN206633449 U CN 206633449U CN 201720365881 U CN201720365881 U CN 201720365881U CN 206633449 U CN206633449 U CN 206633449U
- Authority
- CN
- China
- Prior art keywords
- main body
- core
- mould
- body mould
- product
- Prior art date
- 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.)
- Active
Links
Landscapes
- Moulding By Coating Moulds (AREA)
Abstract
The utility model is a kind of Wound Dies for being molded inside grid reinforced cylindrical shell structure product, including main body mould, core and external mold, uniform T-slot is set respectively in main body mould both sides, core is assembled by T-shaped piece with main body mould, external mold is arranged on the outside of core, for limiting the profile of molded article, the end frame flange beneficial to molded article flange is set respectively at the both ends of main body mould, end socket is provided with the outside of the frame flange of end.The utility model mould can repeatedly use, and the grid reinforcing rib of shaped article has higher dimensional accuracy and positional precision, and product quality uniformity is good, be assembled beneficial to the later stage of product.
Description
Technical field
The utility model designs a kind of mould, specifically a kind of to be molded twining for inside grid reinforced cylindrical shell structure product
Around mould.
Background technology
With the continuous improvement of the development of aerospace industry, especially space material technological level, Composites Lattice Structure
More and more it is widely applied.Network made of unidirectional composite material intersection can give full play to the superior of composite
Property, design and the constantly improve of manufacturing process is expected to reduce manufacturing cost as early as possible, there is vast potential for future development and huge potential;
The die method of most commonly seen shaping grid is mainly following three kinds:First, soft mould, it is general that this method USAF flies power
Laboratory(USAF Phillips Laboratory)In technological precedence status, and for producing solar energy pole plate, radome fairing
With guided missile adapter, but the method for soft mould also has its shortcoming, and product surface finish is poor, and rib size is unstable, production
Need to rive soft mode after product solidification, cost is higher, will be difficult to take off simultaneously for the bigger structure of the height/width of rib
Mould;Another grid forming method is the mould program using rigid foam open channels.It is similar to soft mode method, fibre bundle and
Resin enters foam groove so as to form network, and foam can be stayed in composite structure;Play the work of heat preservation and soundproof
With can also remove by machinery, chemistry or the methods of heat damage, the major defect of this method is, grid node fiber
Volume content is up to 60%, thus causes rib not a node position fiber content to be 50% at node, and fiber volume fraction is only
For 30%;Under this fiber volume fraction, the performance of network is far below laying forming composite structure;The third side
Method is die method, such as metal pattern, and its shortcoming is that fiber volume fraction is low, and rib height can not be too high, and labor intensity is big etc., but
Advantage is also fairly obvious, i.e. the good stability of the dimension of product, and precision is high.
The content of the invention
In order to solve the above problems, the utility model provides a kind of carbon fiber enhancement resin base composite material network
Part mould, the mould can repeatedly use, and the grid reinforcing rib of shaped article has higher dimensional accuracy and position
Precision, product quality uniformity are good.
In order to achieve the above object, the utility model is achieved through the following technical solutions:
The utility model is a kind of Wound Dies for being molded inside grid reinforced cylindrical shell structure product, including main body mould, core
Mould and external mold, uniform T-slot is set respectively in main body mould both sides, core is assembled by T-shaped piece with main body mould, and external mold is set
Put in the outside of core, for limiting the profile of molded article, set respectively beneficial to molded article flange at the both ends of main body mould
End frame flange, end frame flange on the outside of be provided with end socket.
Further improvement of the utility model is:Positioned at the both ends of the core by locating ring.
The beneficial effects of the utility model are:This kind is molded the Wound Dies of inside grid reinforced cylindrical shell structure product, fits
For being molded the larger-size network of rib, can effectively solve large scale reinforcement network and be not easy to pressurize and be stripped
The problem of difficult.The utility model mould can repeatedly use, and the grid reinforcing rib of shaped article has higher size essence
Degree and positional precision, product quality uniformity is good, is assembled beneficial to the later stage of product.What is used divides valve grid male, suitable for height
The shaping of performance network product;Its point of lobed formula solves the problems, such as that network is difficult to be stripped.The mould at grid node
Tool draws nest and carries out chamfering, increases volume, solves the problems, such as that grid reinforcing rib continuously intersects.
Brief description of the drawings
Fig. 1 is the structural representation of the utility model product.
Fig. 2 is the structural representation for the Wound Dies that the utility model is molded inside grid reinforced cylindrical shell structure product.
Fig. 3 is the decomposition texture signal for the Wound Dies that the utility model is molded inside grid reinforced cylindrical shell structure product
Figure.
Fig. 4 is the utility model T-slot and the structural representation of T-shaped block.
Embodiment
In order to deepen to understanding of the present utility model, the utility model is done further below in conjunction with drawings and examples
It is described in detail, the embodiment is only used for explaining the utility model, and the scope of protection of the utility model is not formed and limited.
As Figure 1-4, the utility model is a kind of Wound Dies for being molded inside grid reinforced cylindrical shell structure product, is wrapped
Main body mould 3, core 7 and external mold 4 are included, uniform T-slot 9 is set respectively in the both sides of main body mould 3, the core 7 is by can
Adjust T-shaped piece 10 to be assembled with main body mould 3, the external mold 4 is arranged on the outside of the core 7, for limiting molded article 1
Profile, the end frame flange 5 beneficial to molded article flange is set respectively at the both ends of the main body mould 3, in the end frame flange 5
Outside be provided with end socket 8, load onto end socket servicing unit by both ends and realize 10 ° of windings, and rise and be compacted during winding laying
Effect, positioned at the both ends of the core 7 by locating ring 6.
The use step of the Wound Dies includes:
(1)Mould is cleared up, assembles mould;
(2)Then the prepreg tape winding of reinforcement is carried out on the muscle groove of core 7 by wrapping machine, and is put close to reinforcement
Upper airfelt beats vacuum bag and carries out pre-compacted;Aforesaid operations so are repeated, until rib winding finishes;
(3)The paving of covering prepreg is carried out close to the outer surface of core 7 again, after mould moved into baking oven consolidated
Change, curing and demolding;
(4)The demoulding order be:External mold 4 is first dismantled, then dismantles both ends end frame flange 5, the surplus processing of product is carried out, adds
Work is complete to dismantle both ends locating ring 6, by remaining part move to winding arbor extraction press take off main body mould 3, finally by core 7 out of product 1 side draw
Go out, obtain product.
Embodiment one
The utility model is a kind of Wound Dies for being molded inside grid reinforced cylindrical shell structure product, such as Fig. 2, Fig. 3, including
Main body mould 3, core 7, locating ring 6, end frame flange 5, end socket 8 and external mold 4, above-described main body mould 3 are punching block, and core 7 is
Aluminum dipping form, remaining is punching block, as shown in figure 4, core 7 is being longitudinally divided into some valves, as shown in figure 4, being provided with sliced core 7
T-shaped piece, assembled by the T-slot 9 with being provided with main body mould 3.
The mold use process is as follows:Mould is first cleared up, assembles mould, the pre- of reinforcement is then carried out by wrapping machine
Leaching band winding, put airfelt etc. and beat vacuum bag progress pre-compacted;Aforesaid operations so are repeated, until rib has been wound
Finish;Carry out the paving of covering prepreg again, after mould moved into baking oven solidified, curing and demolding;The demoulding order be:
External mold 4 is first dismantled, then dismantles both ends end frame flange 5, the surplus processing of product is carried out, processes and dismantle both ends locating ring 6,
Remaining part is moved into winding arbor extraction press and takes off main body mould 3, finally core 7 is taken out from the inner side of product 1, obtains product 1.The structure of product 1
As shown in Figure 1.
Such Wound Dies, main body mould 3 and core 7 are split structures, can individually be dismantled, and during the demoulding, main body mould 3 can
Extracted out from centre, then carry out the demoulding of core 7, greatly reduce the demoulding difficulty with the product 1 of grid reinforcing rib 2, external mold 4 is steel
Mould, the appearance and size of product 1 can be accurately controlled, the exterior skin of product 1 made is without post processing.
Mould, which uses, in embodiment first dismantles external mold 4, end frame flange 5 and locating ring 6, then main body mould 3 is extracted out, finally
The stripping means that core is taken out from the inner chamber of product 1 are stripped, the T-slot that main body mould 3 and core 7 connect be provided with it is appropriate between
Gap;The part of core 7 is provided with draft angle, greatly reduces demoulding difficulty, and embodiment core mould 7 passes through T-slot and locating ring and master
Body mould 3 is fixed, and can be accurately positioned.The size of embodiment product 1 ensures by mould, the accurate size of product 1 worked it out without
Post-process, it is time saving and energy saving.
Claims (2)
1. a kind of Wound Dies for being molded inside grid reinforced cylindrical shell structure product, including main body mould(3), core(7)And external mold
(4), it is characterised in that:In the main body mould(3)Both sides set uniform T-slot respectively(9), the core(7)Pass through T-shaped piece
(10)With main body mould(3)Assembled, the external mold(4)It is arranged on the core(7)Outside, for limiting molded article
(1)Profile, in the main body mould(3)Both ends end frame flange beneficial to molded article flange is set respectively(5), at the end
Frame flange(5)Outside be provided with end socket(8).
2. the Wound Dies of inside grid reinforced cylindrical shell structure product are molded according to claim 1, it is characterised in that:Institute
State core(7)Both ends pass through locating ring(6)Positioned.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201720365881.6U CN206633449U (en) | 2017-04-10 | 2017-04-10 | It is molded the Wound Dies of inside grid reinforced cylindrical shell structure product |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201720365881.6U CN206633449U (en) | 2017-04-10 | 2017-04-10 | It is molded the Wound Dies of inside grid reinforced cylindrical shell structure product |
Publications (1)
Publication Number | Publication Date |
---|---|
CN206633449U true CN206633449U (en) | 2017-11-14 |
Family
ID=60247579
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201720365881.6U Active CN206633449U (en) | 2017-04-10 | 2017-04-10 | It is molded the Wound Dies of inside grid reinforced cylindrical shell structure product |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN206633449U (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106976250A (en) * | 2017-04-10 | 2017-07-25 | 江苏恒神股份有限公司 | It is molded the Wound Dies of inside grid reinforced cylindrical shell structure product and uses step |
CN110591356A (en) * | 2019-09-11 | 2019-12-20 | 长春长光宇航复合材料有限公司 | Wave-transparent composite material half cover and preparation method thereof |
CN113844078A (en) * | 2021-07-20 | 2021-12-28 | 航天材料及工艺研究所 | Preparation method of ultra-light multi-feature skin-free framework type composite shell |
-
2017
- 2017-04-10 CN CN201720365881.6U patent/CN206633449U/en active Active
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106976250A (en) * | 2017-04-10 | 2017-07-25 | 江苏恒神股份有限公司 | It is molded the Wound Dies of inside grid reinforced cylindrical shell structure product and uses step |
CN110591356A (en) * | 2019-09-11 | 2019-12-20 | 长春长光宇航复合材料有限公司 | Wave-transparent composite material half cover and preparation method thereof |
CN110591356B (en) * | 2019-09-11 | 2022-02-22 | 长春长光宇航复合材料有限公司 | Wave-transparent composite material half cover and preparation method thereof |
CN113844078A (en) * | 2021-07-20 | 2021-12-28 | 航天材料及工艺研究所 | Preparation method of ultra-light multi-feature skin-free framework type composite shell |
CN113844078B (en) * | 2021-07-20 | 2023-07-28 | 航天材料及工艺研究所 | Preparation method of ultra-light multi-feature skin-free skeleton type composite shell |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN106976250A (en) | It is molded the Wound Dies of inside grid reinforced cylindrical shell structure product and uses step | |
CN101450533B (en) | Carbon fiber reinforcement resin base composite material lattice structural-component conforming die and method | |
CN206633449U (en) | It is molded the Wound Dies of inside grid reinforced cylindrical shell structure product | |
CN103341987B (en) | Ω long purlin orthogonal stiffeners composites wallboard co-curing reaction | |
CN108162430A (en) | A kind of abnormity composite material grid covering bay section forming method | |
CN108995250B (en) | RTM forming die of composite material part with segmented rotary structure | |
CN105058820A (en) | Forming tool and forming method for large-sized T-shaped composite material stringer | |
CN209191346U (en) | Manufacture the molding die of large-scale unmanned plane rib | |
CN106515045B (en) | Composite material joint skirt automatic placement molding method | |
CN108407332A (en) | A kind of composite material grid stressed-skin construction part compression-moulding methods | |
CN104494166A (en) | Air bag forming method of composite material part with T-shaped reinforced web structure | |
CN108638538A (en) | A kind of simple composite material grid product forming method | |
CN105619828A (en) | Twisted carbon filling method for gaps of R corners of I-shaped beam | |
CN101992265A (en) | Method for manufacturing resin casting die used for modeling sodium silicate self-hardening sand | |
CN104690985A (en) | Fan blade manufacturing technology based on die pressing method | |
CN217777845U (en) | VARI mould for forming inner grid reinforced shell structure workpiece | |
CN103950205B (en) | A kind of T-shaped cross section ring-type rotary structure composite product forming method | |
CN216099959U (en) | Reinforced cylinder winding forming tool | |
CN113844078B (en) | Preparation method of ultra-light multi-feature skin-free skeleton type composite shell | |
CN102248685A (en) | Forming method of glass fiber reinforced plastic (GFRP) | |
CN213056088U (en) | Molding tool for square beam-like structural parts made of composite materials | |
CN103551524B (en) | Casting method for multislot belt wheel, core making mold used in casting method and casting mold | |
CN207240916U (en) | High-pressure resin Transfer molding mould | |
CN220428726U (en) | Thermal insulation block mould box | |
CN218463022U (en) | Mould of jumbo size tube-shape cabin section |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant |