CN106584886B - The technique for being glued bondline thickness using self-control rubber cover board control - Google Patents
The technique for being glued bondline thickness using self-control rubber cover board control Download PDFInfo
- Publication number
- CN106584886B CN106584886B CN201611235254.7A CN201611235254A CN106584886B CN 106584886 B CN106584886 B CN 106584886B CN 201611235254 A CN201611235254 A CN 201611235254A CN 106584886 B CN106584886 B CN 106584886B
- Authority
- CN
- China
- Prior art keywords
- pressing plate
- stiffening plate
- equal pressing
- glued
- plate
- 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
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
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
- B29C70/342—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
-
- 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
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
- B29L2031/3085—Wings
Abstract
The present invention relates to a kind of techniques for being glued bondline thickness using self-control rubber cover board control, comprising the following steps: 1) makes equal pressing plate;2) glue film is taped against on pre-glued covering, then stiffening plate is placed on glue film and buckles equal pressing plate, removing cloth and the equal pressing plate of surrounding stretching for having hole isolation film;3) pressing plate uses pin to connect positioning with stiffening plate;4) the whole envelope vacuum bag processed by step 2 and 3), and move in autoclave, to pressure is applied at the top of equal pressing plate, heating is solidified, up to the covering bonding layer of uniform thickness after solidification.The equal pressing plate of the technology utilization rubber realizes being uniformly distributed again for hot pressing pressure tank, compared with pressure acts directly in stiffening plate, the influence of positive between stiffening plate and covering to the thickness of glue-line is reduced, to obtain glue-line in homogeneous thickness.It using the easy to operate of the equal pressing plate, accurate positioning and conveniently checks oneself, process and result are visual controllable effect, improve the quality and working efficiency of product.
Description
Technical field
The invention is related to a kind of technique for being glued bondline thickness using self-control rubber cover board control, is used for aircraft skin
The bondline thickness control technique being glued with stiffening plate.
Background technique
Siding due to covering and reinforces template face in Bonding Process in the aircraft tail wing tip horizontal tail stabilization of certain model
Tolerance is big, be easy to cause the cooperation between covering and stiffening plate uneven, so as to cause the covering in Bonding Process and stiffening plate
Between splicing bondline thickness it is widely different, have exceeded code requirement value, cause part to delay to succeed in developing, not only cause
Very huge economic loss, and lead to being discontented with for client.
Summary of the invention
The invention technical problems to be solved are to provide a kind of using self-control rubber cover board control splicing bondline thickness
Technique, the equal pressing plate of the technology utilization rubber realizes being uniformly distributed again for hot pressing pressure tank, acts directly on reinforcement with pressure
It is compared on plate, the influence of positive between stiffening plate and covering to the thickness of glue-line is reduced, so that it is uniform to obtain thickness
Glue-line.It using the easy to operate of the equal pressing plate, accurate positioning and conveniently checks oneself, process and result are visual controllable effect
Fruit improves the quality and working efficiency of product.
In order to solve the above problem, the specific technical solution of the invention is as follows: a kind of to be controlled using self-control rubber cover board
It is glued the technique of bondline thickness, comprising the following steps:
1) it makes equal pressing plate: stiffening plate A being placed at pre-glued covering, in the non-sulphur of stiffening plate upper surface laying several layers
Change rubber, in one layer of dry carbon fibre fabric of bottom first layer upper surface laying of half finished rubber, half finished rubber and carbon fiber
The area for tieing up fabric is greater than the top surface area of stiffening plate A, and surrounding redundance is laid in pre-glued covering upper surface;Whole envelope system
Vacuum bag, and move in autoclave, then pass through curing process, forms equal pressing plate after removing stiffening plate A;
2) glue film is taped against on pre-glued covering, then stiffening plate B is placed on glue film, successively spread on stiffening plate B
Pasting one layer of removing cloth and one layer has hole isolation film, finally buckles equal pressing plate, and removing cloth is pressed with the surrounding for having hole isolation film stretching
Plate;
3) pressing plate uses pin to connect positioning with stiffening plate B;
4) the whole envelope vacuum bag processed by step 2 and 3), and move in autoclave, to application pressure at the top of equal pressing plate, and
Heating is solidified, up to the covering bonding layer of uniform thickness after solidification;
Compared with the stiffening plate B described in the step 2 of stiffening plate A described in step 1), the big 1.5 ~ 2mm of surrounding size, thickness is high
There is stiffening plate to hide slot for 0.3mm, resulting equal pressing plate.
The solidifying pressure of equal pressing plate described in step 1) is 310 ± 30KPa, and solidification temperature is 130 ± 5 DEG C.
Curable adhesive layer pressure described in step 4) is 210 ± 30KPa, and solidification temperature is 121 ± 5 DEG C, the glue-line after solidification
With a thickness of 0.05 ~ 0.5mm.
This is glued the equal pressing plate of technology utilization rubber of bondline thickness to the equal again of pressure using self-control rubber cover board control
Even distribution, it reduces pressure and acts directly in stiffening plate reason and reinforce template face bring pressure and be unevenly distributed, to obtain
Obtained glue-line in homogeneous thickness.The equal pressing plate using easy to operate, be easy to grasp, manufacturing cost is low, convenient for promoting, the technology
A large amount of production cost is saved, while realizing the breakthrough of adhesive bonding technique.
Detailed description of the invention
Fig. 1 is equal platen manufacturing schematic diagram.
Fig. 2 is the equal pressing plate schematic diagram to complete.
Fig. 3 is the process schematic representation for being glued bondline thickness using self-control rubber cover board control.
Specific embodiment
A kind of technique for being glued bondline thickness using self-control rubber cover board control, comprising the following steps:
1) it makes equal pressing plate: stiffening plate A1 is placed at pre-glued covering 2, laying several layers are not in stiffening plate upper surface
Vulcanized rubber 3, in the dry carbon fibre fabric 4 of one layer of the bottom first layer upper surface laying of half finished rubber 3, half finished rubber 3
It is greater than the top surface area of stiffening plate A1 with the area of carbon fibre fabric 4, surrounding redundance is laid in table on pre-glued covering 2
Face;It is whole to seal vacuum bag 5 processed, and move in autoclave, then pass through curing process, solidifying pressure is 310 ± 30KPa, solidification
Temperature is 130 ± 5 DEG C, forms equal pressing plate 6 after removing stiffening plate A1;
2) glue film 7 is taped against on pre-glued covering 2, then stiffening plate B8 is placed on glue film 7, on stiffening plate B8 according to
One layer of removing cloth 9 of secondary paving and one layer have hole isolation film 10, finally buckle equal pressing plate 6, removing cloth 9 and have the four of hole isolation film 10
Week stretches out equal pressing plate 6;
3) pressing plate 6 uses pin to connect positioning with stiffening plate B8;
4) whole by step 2 and 3) seals vacuum bag 5 processed, and moves in autoclave, to applying pressure at the top of equal pressing plate 6,
Pressure value is 210 ± 30KPa, and heats and solidified, and solidification temperature is 121 ± 5 DEG C, and uniform thickness is 0.05 to obtain the final product after solidification
The covering bonding layer of ~ 0.5mm.
Wherein compared with the stiffening plate B8 described in the step 2 of stiffening plate A1 described in step 1), the big 1.5 ~ 2mm of surrounding size,
There is stiffening plate to hide slot, and the cooperation with equal pressing plate and stiffening plate for the high 0.3mm of thickness, resulting equal pressing plate 6.
In hot pressing in-tank-solidification, pressure acts on equal pressing plate first, and equal pressing plate realizes certain buffering and again to pressure
Secondary distribution, so that the pressure acted in stiffening plate is uniform, so that the bondline thickness between stiffening plate and covering is equal
It is even, up to the covering bonding layer of uniform thickness after solidification.
Claims (3)
1. a kind of technique for being glued bondline thickness using self-control rubber cover board control, it is characterised in that the following steps are included:
1) it makes equal pressing plate: stiffening plate A(1) is placed at pre-glued covering (2), laying several layers are not in stiffening plate upper surface
Vulcanized rubber (3), it is unvulcanized in one layer of dry carbon fibre fabric (4) of bottom first layer upper surface laying of half finished rubber (3)
Top surface area of the area of rubber (3) and carbon fibre fabric (4) greater than stiffening plate A(1), surrounding redundance are laid in pre-glued
Covering (2) upper surface;It is whole to seal vacuum bag (5) processed, and move in autoclave, then pass through curing process, removes stiffening plate A
(1) equal pressing plate (6) are formed afterwards;
2) glue film (7) is taped against on pre-glued covering (2), then stiffening plate B(8) is placed on glue film (7), in stiffening plate B
(8) successively one layer of removing cloth (9) of paving and one layer have hole isolation film (10) on, finally buckle equal pressing plate (6), remove cloth (9) and
There is the surrounding of hole isolation film (10) to stretch out equal pressing plate (6);
3) pressing plate (6) uses pin to connect positioning with stiffening plate B(8);
4) the whole envelope vacuum bag (5) processed by step 2 and 3), and move in autoclave, pressure is applied to equal pressing plate (6) top,
And heat and solidified, up to the covering bonding layer of uniform thickness after solidification;
Wherein stiffening plate A(1 described in step 1)) the stiffening plate B(8 described in the step 2) compared with, the big 1.5 ~ 2mm of surrounding size,
There is stiffening plate to hide slot for the high 0.3mm of thickness, resulting equal pressing plate (6).
2. the technique as described in claim 1 for being glued bondline thickness using self-control rubber cover board control, it is characterised in that: step
1) solidifying pressure of the equal pressing plate described in is 310 ± 30KPa, and solidification temperature is 130 ± 5 DEG C.
3. the technique as described in claim 1 for being glued bondline thickness using self-control rubber cover board control, it is characterised in that: step
4) curable adhesive layer pressure described in is 210 ± 30KPa, and solidification temperature is 121 ± 5 DEG C, the bondline thickness after solidification is 0.05 ~
0.5mm。
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201611235254.7A CN106584886B (en) | 2016-12-28 | 2016-12-28 | The technique for being glued bondline thickness using self-control rubber cover board control |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201611235254.7A CN106584886B (en) | 2016-12-28 | 2016-12-28 | The technique for being glued bondline thickness using self-control rubber cover board control |
Publications (2)
Publication Number | Publication Date |
---|---|
CN106584886A CN106584886A (en) | 2017-04-26 |
CN106584886B true CN106584886B (en) | 2019-04-09 |
Family
ID=58603091
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201611235254.7A Active CN106584886B (en) | 2016-12-28 | 2016-12-28 | The technique for being glued bondline thickness using self-control rubber cover board control |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106584886B (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110091519A (en) * | 2018-01-29 | 2019-08-06 | 李璐璐 | A kind of splicing mold |
CN108943761B (en) * | 2018-06-21 | 2020-06-02 | 江西昌河航空工业有限公司 | Curing method for steel mesh and skin of engine nozzle |
CN108973089B (en) * | 2018-07-24 | 2020-05-19 | 中国航空工业集团公司基础技术研究院 | Preparation method of composite material special-shaped skin structure |
CN109466087A (en) * | 2018-12-03 | 2019-03-15 | 江西洪都航空工业集团有限责任公司 | A kind of equal pressing plate manufacturing method of deep camber composite material laminated board |
CN111323276B (en) * | 2018-12-13 | 2023-08-01 | 中国科学院宁波材料技术与工程研究所 | Resin fiber test sample bonding workbench |
CN111002659B (en) * | 2019-12-04 | 2023-06-20 | 江西洪都航空工业集团有限责任公司 | Semi-rigid equalizing plate for molding composite material workpiece and preparation method thereof |
CN112373062B (en) * | 2020-10-19 | 2023-03-24 | 广联航空工业股份有限公司 | Method for realizing skid resistance, sweat releasing and shock absorption of composite material surface |
CN113997601B (en) * | 2021-11-05 | 2024-03-08 | 中航沈飞民用飞机有限责任公司 | Compensation pressurization method for V-shaped composite material part |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102225703A (en) * | 2011-04-12 | 2011-10-26 | 江西洪都航空工业集团有限责任公司 | Manufacturing method of integral glass fiber reinforced plastic unmanned aerial vehicle wing |
CN104401092A (en) * | 2014-11-18 | 2015-03-11 | 江苏恒神纤维材料有限公司 | Method for enabling carbon fiber composite thick laminated structure to uniformly absorb resin and laminated structure |
CN104647765A (en) * | 2013-11-19 | 2015-05-27 | 青岛欧美亚橡胶工业有限公司 | Preparation method of acrylate rubber balance plate |
CN105235237A (en) * | 2015-11-18 | 2016-01-13 | 江西洪都航空工业集团有限责任公司 | Molding technology and molding tool of composite material J-shaped stiffened wallboard |
-
2016
- 2016-12-28 CN CN201611235254.7A patent/CN106584886B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102225703A (en) * | 2011-04-12 | 2011-10-26 | 江西洪都航空工业集团有限责任公司 | Manufacturing method of integral glass fiber reinforced plastic unmanned aerial vehicle wing |
CN104647765A (en) * | 2013-11-19 | 2015-05-27 | 青岛欧美亚橡胶工业有限公司 | Preparation method of acrylate rubber balance plate |
CN104401092A (en) * | 2014-11-18 | 2015-03-11 | 江苏恒神纤维材料有限公司 | Method for enabling carbon fiber composite thick laminated structure to uniformly absorb resin and laminated structure |
CN105235237A (en) * | 2015-11-18 | 2016-01-13 | 江西洪都航空工业集团有限责任公司 | Molding technology and molding tool of composite material J-shaped stiffened wallboard |
Also Published As
Publication number | Publication date |
---|---|
CN106584886A (en) | 2017-04-26 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN106584886B (en) | The technique for being glued bondline thickness using self-control rubber cover board control | |
CN102765198A (en) | Vacuum assisted molding system of composite and molding method of composite | |
CN207224636U (en) | A kind of plastic composites tablet automated tape-laying equipment | |
CN103160214B (en) | The manufacture method of laminating device | |
CN107283868A (en) | A kind of overall localization method of the rib for being molded carbon fibre composite Material Stiffened Panel | |
CN110171183B (en) | Positioning and pressure-equalizing device containing embedded part honeycomb sandwich structure and forming method | |
CN104097329B (en) | A kind of method in composite foam sandwich construction shaping, foamed material being carried out resin infusion pretreatment | |
CN104441693A (en) | Molding process method for novel composite material adhesive film of wind power generation blades | |
CN106573422A (en) | Bonding device and bonding method | |
CN108284623A (en) | The manufacturing process of blade part | |
CN105415700A (en) | Application method for process base plate for curved surface | |
TW201943610A (en) | Thermoplastic film method of three-dimensional surface device | |
CN107214980A (en) | A kind of quick molding method of thermoplastic fiber reinforced composite board | |
CN106769314A (en) | A kind of co-curing is glued the forming frock and its forming method of shearing sample | |
CN110576593B (en) | Film pasting method and application thereof and glass panel | |
JPH04308733A (en) | Method and apparatus for laminating prepreg | |
CN107127982A (en) | A kind of equal pressing plate flexible connecting method being molded for composite product | |
CN109203516A (en) | A kind of manufacturing method of wind electricity blade | |
CN108215241B (en) | Rapid molding method of resin-based composite material | |
KR20190115826A (en) | Combining method of air mattress | |
CN205989548U (en) | A kind of composite foamed body vacuum abutted equipment | |
CN104416918B (en) | Method for producing composite material reinforced part | |
CN103231522A (en) | Vacuum infusion process for forming composite material and composite material | |
CN215242964U (en) | Vacuum bonding solidification forming device | |
TWI611770B (en) | Leather-plastic composite forming method |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |