CN106084653B - A kind of method that frame-type raft frame or pedestal are prepared using composite material - Google Patents
A kind of method that frame-type raft frame or pedestal are prepared using composite material Download PDFInfo
- Publication number
- CN106084653B CN106084653B CN201610401799.4A CN201610401799A CN106084653B CN 106084653 B CN106084653 B CN 106084653B CN 201610401799 A CN201610401799 A CN 201610401799A CN 106084653 B CN106084653 B CN 106084653B
- Authority
- CN
- China
- Prior art keywords
- frame
- pedestal
- composite material
- raft frame
- prepared
- 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
- 239000002131 composite material Substances 0.000 title claims abstract description 67
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 title claims abstract description 63
- 238000000034 method Methods 0.000 title claims abstract description 46
- 230000008520 organization Effects 0.000 claims abstract description 35
- 238000012545 processing Methods 0.000 claims abstract description 23
- 238000000465 moulding Methods 0.000 claims abstract description 20
- 230000002787 reinforcement Effects 0.000 claims abstract description 16
- 230000007704 transition Effects 0.000 claims abstract description 16
- 238000007493 shaping process Methods 0.000 claims abstract description 14
- 238000011049 filling Methods 0.000 claims abstract description 10
- 238000000354 decomposition reaction Methods 0.000 claims abstract description 9
- 238000007788 roughening Methods 0.000 claims abstract description 5
- 239000000463 material Substances 0.000 claims description 33
- 239000003822 epoxy resin Substances 0.000 claims description 18
- 229920000647 polyepoxide Polymers 0.000 claims description 18
- 229920005989 resin Polymers 0.000 claims description 17
- 239000011347 resin Substances 0.000 claims description 17
- 239000000853 adhesive Substances 0.000 claims description 16
- 230000001070 adhesive effect Effects 0.000 claims description 16
- 239000003795 chemical substances by application Substances 0.000 claims description 11
- 239000003365 glass fiber Substances 0.000 claims description 11
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 10
- 230000008569 process Effects 0.000 claims description 9
- 239000012779 reinforcing material Substances 0.000 claims description 9
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 claims description 8
- 229910002012 Aerosil® Inorganic materials 0.000 claims description 8
- 239000004593 Epoxy Substances 0.000 claims description 8
- 238000001746 injection moulding Methods 0.000 claims description 8
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 7
- 229920006387 Vinylite Polymers 0.000 claims description 7
- 239000004917 carbon fiber Substances 0.000 claims description 7
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 7
- 229920006337 unsaturated polyester resin Polymers 0.000 claims description 7
- 238000005516 engineering process Methods 0.000 claims description 6
- 239000000203 mixture Substances 0.000 claims description 6
- 238000010276 construction Methods 0.000 claims description 5
- 238000005728 strengthening Methods 0.000 claims description 5
- XMNIXWIUMCBBBL-UHFFFAOYSA-N 2-(2-phenylpropan-2-ylperoxy)propan-2-ylbenzene Chemical compound C=1C=CC=CC=1C(C)(C)OOC(C)(C)C1=CC=CC=C1 XMNIXWIUMCBBBL-UHFFFAOYSA-N 0.000 claims description 4
- 239000004342 Benzoyl peroxide Substances 0.000 claims description 4
- OMPJBNCRMGITSC-UHFFFAOYSA-N Benzoylperoxide Chemical compound C=1C=CC=CC=1C(=O)OOC(=O)C1=CC=CC=C1 OMPJBNCRMGITSC-UHFFFAOYSA-N 0.000 claims description 4
- RPNUMPOLZDHAAY-UHFFFAOYSA-N Diethylenetriamine Chemical compound NCCNCCN RPNUMPOLZDHAAY-UHFFFAOYSA-N 0.000 claims description 4
- 239000004698 Polyethylene Substances 0.000 claims description 4
- 235000019400 benzoyl peroxide Nutrition 0.000 claims description 4
- 230000001680 brushing effect Effects 0.000 claims description 4
- 239000011248 coating agent Substances 0.000 claims description 4
- 238000000576 coating method Methods 0.000 claims description 4
- 150000004985 diamines Chemical group 0.000 claims description 4
- 238000000227 grinding Methods 0.000 claims description 4
- 238000009434 installation Methods 0.000 claims description 4
- 238000003754 machining Methods 0.000 claims description 4
- 229920000768 polyamine Polymers 0.000 claims description 4
- -1 polyethylene Polymers 0.000 claims description 4
- 229920000573 polyethylene Polymers 0.000 claims description 4
- 238000002360 preparation method Methods 0.000 claims description 4
- VILCJCGEZXAXTO-UHFFFAOYSA-N 2,2,2-tetramine Chemical compound NCCNCCNCCN VILCJCGEZXAXTO-UHFFFAOYSA-N 0.000 claims description 3
- WFUGQJXVXHBTEM-UHFFFAOYSA-N 2-hydroperoxy-2-(2-hydroperoxybutan-2-ylperoxy)butane Chemical group CCC(C)(OO)OOC(C)(CC)OO WFUGQJXVXHBTEM-UHFFFAOYSA-N 0.000 claims description 3
- 238000004519 manufacturing process Methods 0.000 claims description 3
- 238000001721 transfer moulding Methods 0.000 claims description 3
- 229960001124 trientine Drugs 0.000 claims description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 2
- 229910052799 carbon Inorganic materials 0.000 claims description 2
- QQZOPKMRPOGIEB-UHFFFAOYSA-N 2-Oxohexane Chemical compound CCCCC(C)=O QQZOPKMRPOGIEB-UHFFFAOYSA-N 0.000 claims 1
- 238000013016 damping Methods 0.000 abstract description 14
- 230000001629 suppression Effects 0.000 abstract description 2
- 239000010410 layer Substances 0.000 description 24
- 239000004744 fabric Substances 0.000 description 16
- 238000005457 optimization Methods 0.000 description 8
- 238000004026 adhesive bonding Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 6
- 238000010586 diagram Methods 0.000 description 4
- 238000001035 drying Methods 0.000 description 4
- 238000002955 isolation Methods 0.000 description 4
- 238000007790 scraping Methods 0.000 description 4
- UICXTANXZJJIBC-UHFFFAOYSA-N 1-(1-hydroperoxycyclohexyl)peroxycyclohexan-1-ol Chemical compound C1CCCCC1(O)OOC1(OO)CCCCC1 UICXTANXZJJIBC-UHFFFAOYSA-N 0.000 description 3
- 230000008859 change Effects 0.000 description 3
- 238000013461 design Methods 0.000 description 3
- 239000000835 fiber Substances 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- 239000000654 additive Substances 0.000 description 2
- 230000000996 additive effect Effects 0.000 description 2
- 238000009411 base construction Methods 0.000 description 2
- 238000009954 braiding Methods 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 238000007667 floating Methods 0.000 description 2
- 238000011900 installation process Methods 0.000 description 2
- 208000020442 loss of weight Diseases 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- FDPIMTJIUBPUKL-UHFFFAOYSA-N pentan-3-one Chemical compound CCC(=O)CC FDPIMTJIUBPUKL-UHFFFAOYSA-N 0.000 description 2
- 238000007665 sagging Methods 0.000 description 2
- VGGSQFUCUMXWEO-UHFFFAOYSA-N Ethene Chemical compound C=C VGGSQFUCUMXWEO-UHFFFAOYSA-N 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 230000002929 anti-fatigue Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 239000011229 interlayer Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 230000010287 polarization Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- AGGKEGLBGGJEBZ-UHFFFAOYSA-N tetramethylenedisulfotetramine Chemical compound C1N(S2(=O)=O)CN3S(=O)(=O)N1CN2C3 AGGKEGLBGGJEBZ-UHFFFAOYSA-N 0.000 description 1
- 230000008719 thickening Effects 0.000 description 1
- 238000009941 weaving Methods 0.000 description 1
- 238000009736 wetting Methods 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
- C08K13/00—Use of mixtures of ingredients not covered by one single of the preceding main groups, each of these compounds being essential
- C08K13/04—Ingredients characterised by their shape and organic or inorganic ingredients
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B17/00—Vessels parts, details, or accessories, not otherwise provided for
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
- C08K3/00—Use of inorganic substances as compounding ingredients
- C08K3/34—Silicon-containing compounds
- C08K3/36—Silica
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
- C08K7/00—Use of ingredients characterised by shape
- C08K7/02—Fibres or whiskers
- C08K7/04—Fibres or whiskers inorganic
- C08K7/06—Elements
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
- C08K7/00—Use of ingredients characterised by shape
- C08K7/02—Fibres or whiskers
- C08K7/04—Fibres or whiskers inorganic
- C08K7/14—Glass
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09J—ADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
- C09J163/00—Adhesives based on epoxy resins; Adhesives based on derivatives of epoxy resins
Landscapes
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Health & Medical Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Medicinal Chemistry (AREA)
- Polymers & Plastics (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Floor Finish (AREA)
Abstract
The present invention discloses a kind of method that frame-type raft frame or pedestal are prepared using composite material, comprises the following steps:Step 1: the STRUCTURE DECOMPOSITION of raft frame or pedestal;Step 2: the shaping of composite material partitioned organization, the demoulding;Step 3: piecemeal molding structure machines;Step 4: partitioned organization pre-assembled;Step 5: bonding plane roughening is handled;Step 6: partitioned organization is bonded;Step 7: the filling of bonding transition region and bonding pad reinforcement formable layer;Step 8: processing perforate and surfacing.It is provided by the invention to prepare that composite material raft frame or base size precision that the method for frame-type raft frame or pedestal prepared using the invention are high, intensity is high, rigidity is high, light-weight, fatigue performance is good, damping capacity is good, effectiveness in vibration suppression is obvious using composite material.
Description
Technical field
The invention belongs to technical field of composite materials, and in particular to one kind prepares frame-type raft frame or base using composite material
The method of seat.
Background technology
Mechanical noise is one of three big noise source of naval vessel, and due to the mechanical equipment huge number on ship, it is each to be distributed in full ship
A cabin, and mechanical noise is the Main Noise Sources of submarine concealment running working condition.Therefore, control machinery noise is vibration damping drop
Make an uproar one of main contents of work.Control machinery noise mainly has by control device vibration level and using vibration isolation technique at present
Both sides measure.Since control low noise equipment potential is limited, it can not meet warship stealth requirement, therefore pipeline shakes
Dynamic control is then most important, and how the development experience of vibration isolation technique single-layer partiting polarization, double-layer vibration isolating, buoyant raft vibration isolation, further carry
The vibration isolating effect of high Floating Raft System is to realize one of key technology of Control of Mechanical Noise.China's naval vessels raft frame or pedestal are equal at present
Prepared using metal material, but metal structure weight weight, vibration damping limited potential, the loss of weight and follow-up vibration damping for being unfavorable for naval vessels are set
Meter.Relative to metal raft frame or pedestal, composite material raft frame or pedestal are light-weight, specific stiffness is high, damping capacity is good, designability
By force, shock resistance is strong, has and preferably subtracts vibration isolating effect.Therefore, composite material raft frame is introduced in large-scale Floating Raft System design
And base construction is one of most effective approach for realizing efficient vibration isolation and loss of weight design.Composite material raft frame or pedestal precision prescribed
Height, intensity is high, and rigidity is high, has good shock resistance and subtracts vibration isolating effect, the current country has no frame-type composite material
Raft frame or the molding related report of pedestal.
The content of the invention
In order to solve the above technical problems, the present invention provides a kind of side that frame-type raft frame or pedestal are prepared using composite material
Method, the composite material raft frame prepared using the invention or base size precision are high, intensity is high, rigidity is high, light-weight, fatigue durability
Energy is good, damping capacity is good, effectiveness in vibration suppression is obvious.
The technical solution adopted in the present invention is:A kind of method that frame-type raft frame or pedestal are prepared using composite material,
Comprise the following steps:
Step 1: the STRUCTURE DECOMPOSITION of raft frame or pedestal
STRUCTURE DECOMPOSITION is carried out according to the overall structure form of raft frame or pedestal, is decomposed into top panel, lower panel and transverse and longitudinal rib
Four part of plate, wherein, transverse and longitudinal floor includes multiple horizontal gussets and longitudinal gusset, between top panel and transverse and longitudinal floor and below
Connection mode between plate and transverse and longitudinal floor is "T"-shaped grafting, and the connection mode between horizontal gusset and longitudinal gusset is
" ten " shape grafting, finally obtains decomposing scheme, and decomposing scheme includes the quantity and ruler of top panel, lower panel and transverse and longitudinal floor
It is very little;
Step 2: the shaping of composite material partitioned organization, the demoulding
The decomposing scheme obtained according to step 1 makes the mould to match, and enterprising in corresponding mould using composite material
Each partitioned organization shaping of row, is demoulded after curing, obtains each piecemeal molding structure, spare;
Step 3: piecemeal molding structure machines
Each piecemeal molding structure demoulded in step 2 is machined out, the decomposing scheme obtained according to step 1 is each
Locating and machining groove or groove is cross-linked on piecemeal molding structure, lower panel machine-shaping fabrication hole, the piecemeal after must processing
Structure, it is spare;
Step 4: partitioned organization pre-assembled
Partitioned organization after the processing obtained to step 3 carries out pre-assembled according to the structure of raft frame or pedestal;
Step 5: bonding plane roughening is handled
To treating that bonding plane carries out grinding process after pre-assembled in step 4, then cleaned out using acetone;
Step 6: partitioned organization is bonded
Preassembly sequence in step 4 is bonded, in partitioned organization bonding plane coating adhesive, first to lower panel
Cemented in place is carried out with transverse and longitudinal floor, is then bonded top panel;
Step 7: the filling of bonding transition region and bonding pad reinforcement formable layer
After the completion of being bonded in step 6, mixed and matched somebody with somebody with aerosil using epoxy construction adhesive or basis material
The putty put carries out transition processing to adhesion zone right angle, then carries out reinforcement formable layer, room to bonding each junction
Temperature placement 24 cures when small;
Step 8: processing perforate and surfacing
Raft frame or pedestal that step 7 obtains are needed into progress perforate according to installation, and top panel and lower panel are put down
Face degree processing, makes upper and lower surface horizontal;Then carry out entirety to surface to polish smooth, and brushing basis material, basis material are solid
The preparation of frame-type raft frame or pedestal is completed after change.
It is described as a kind of further optimization of method that frame-type raft frame or pedestal are prepared using composite material of the present invention
Frame-type composite material be made of the cured dose of curing of reinforcing material and reisn base material, reinforcing material for glass fibre or
Carbon fiber, reisn base material are unsaturated polyester resin, vinylite or epoxy resin.
It is described as a kind of further optimization of method that frame-type raft frame or pedestal are prepared using composite material of the present invention
Reisn base material be unsaturated polyester resin or vinylite, curing agent is methyl ethyl ketone peroxide, cyclohexanone peroxide,
One kind or any mixture in cumyl peroxide, benzoyl peroxide.
It is described as a kind of further optimization of method that frame-type raft frame or pedestal are prepared using composite material of the present invention
Reisn base material be epoxy resin, curing agent is diamine, in diethylenetriamine, triethylene tetramine, polyethylene polyamine
A kind of or any mixture.
As a kind of further optimization of method that frame-type raft frame or pedestal are prepared using composite material of the present invention, step
Composite material partitioned organization forming method described in two is vacuum assisted resin injection moulding process, die press technology for forming or resin
Any of Transfer molding technique.
As a kind of further optimization of method that frame-type raft frame or pedestal are prepared using composite material of the present invention, step
Assemble sequence in four is from top to bottom:Lower panel and in length and breadth floor, top panel and floor in length and breadth.
As a kind of further optimization of method that frame-type raft frame or pedestal are prepared using composite material of the present invention, step
Adhesive described in six is room-temperature curing epoxy structural adhesive.
As a kind of further optimization of method that frame-type raft frame or pedestal are prepared using composite material of the present invention, step
Transition region filling section described in seven is isosceles right triangle or arc-shaped.
As a kind of further optimization of method that frame-type raft frame or pedestal are prepared using composite material of the present invention, step
Bonding pad reinforcement formable layer described in seven uses manual pasting forming process or vacuum assisted resin injection moulding process, bonding pad reinforcement
Layer, as enhancement layer, using epoxy resin as base layer, and is also added with using carbon fiber or glass fibre in epoxy resin
The aerosil of its weight 0.5%-3%.
Compared with prior art, the present invention at least tool has the advantage that and beneficial effect:
1st, the frame-type raft frame or pedestal precision that are prepared using forwarding method of the present invention are high, intensity is high, light-weight, fatigue durability
Energy is good, damping capacity is good, has and significantly subtracts vibration isolating effect.Composite structure specific stiffness is high, damping capacity is good, designability
By force, shock resistance is strong, it is obvious to subtract vibration isolating effect.The composite material frame formula raft frame or pedestal prepared using the present invention, is solved
High accuracy, the high quality formation problems of frame-type composite material raft frame or pedestal, be pushed further into composite material raft frame or
The naval vessels application of pedestal.
2nd, using each structure of partitioned mode forming composite, the Forming Quality of each structure of composite material is improved.
3rd, composite material partitioned organization of the present invention positioning and assembling use inserting mode, improve composite material raft frame or
The formed precision of pedestal.
4th, bonding pad of the present invention improves intensity, the anti-fatigue performance of composite material raft frame or pedestal by thickening reinforcement
And impact strength, while improve composite material raft frame or pedestal subtracts vibration isolating effect.
Brief description of the drawings
Fig. 1 is the structure diagram of raft frame of the present invention or pedestal;
Fig. 2 is the shaping flow diagram of raft frame of the present invention or pedestal;
Fig. 3 is the installation process schematic diagram of T-shape of the present invention connection;
Fig. 4 is the installation process schematic diagram of " ten " type connection of the invention;
Fig. 5 is the front view of raft frame of the present invention or pedestal;
Fig. 6 is the sectional elevation of raft frame of the present invention or pedestal;
Fig. 7 is sectional view of the present invention along A-A directions;
Fig. 8 is sectional view of the present invention along B-B directions;
Reference numeral:1st, top panel, 2, lower panel, 3, transverse and longitudinal floor.
Embodiment
To become apparent present disclosure, below in conjunction with specific embodiment, the present invention will be described in detail.
A kind of method that frame-type raft frame or pedestal are prepared using composite material, is comprised the following steps:
Step 1: the STRUCTURE DECOMPOSITION of raft frame or pedestal
STRUCTURE DECOMPOSITION is carried out according to the overall structure form of raft frame or pedestal, is decomposed into top panel, lower panel and transverse and longitudinal rib
Four part of plate, wherein, transverse and longitudinal floor includes multiple horizontal gussets and longitudinal gusset, between top panel and transverse and longitudinal floor and below
Connection mode between plate and transverse and longitudinal floor is "T"-shaped grafting, and the connection mode between horizontal gusset and longitudinal gusset is
" ten " shape grafting, finally obtains decomposing scheme, and decomposing scheme includes the number and ruler of top panel, lower panel and transverse and longitudinal floor
It is very little;
Step 2: the shaping of composite material partitioned organization, the demoulding
The decomposing scheme obtained according to step 1 makes the mould to match, and enterprising in corresponding mould using composite material
Each partitioned organization shaping of row, forming method is vacuum assisted resin injection moulding process, die press technology for forming or resin transmit mould
Any of moulding process is moulded, damping layer material is also added with when composite material partitioned organization is molded to improve composite material raft
The damping capacity of frame, is demoulded after curing, obtains each piecemeal molding structure, spare;
Step 3: piecemeal molding structure machines
Each piecemeal molding structure demoulded in step 2 is machined out, the decomposing scheme obtained according to step 1 is each
Locating and machining groove or link slot on piecemeal molding structure, lower panel machine-shaping fabrication hole, the partitioned organization after must processing,
It is spare;
Step 4: partitioned organization pre-assembled
Partitioned organization after the processing obtained to step 3 carries out pre-assembled, assemble sequence according to the structure of raft frame or pedestal
For from top to bottom:Lower panel and in length and breadth floor, top panel and floor in length and breadth;
Step 5: bonding plane roughening is handled
To treating that bonding plane carries out grinding process after pre-assembled in step 4, then cleaned out using acetone;
Step 6: partitioned organization is bonded
Preassembly sequence in step 4 is bonded, and in partitioned organization bonding plane coating adhesive, adhesive is room
Warm cured epoxy sqtructural adhesive, uses the scraping blade of one fixed width(Scraping blade width is advisable with being slightly less than groove width)In composite panel
Gluing of surfaces gluing, wherein in raft frame panel slot three faces should all uniform gluing, it is fixed first lower panel and transverse and longitudinal floor be bonded
Position, then carries out cemented in place to lower panel and transverse and longitudinal floor, is then bonded top panel;
Step 7: the filling of bonding transition region and bonding pad reinforcement formable layer
After the completion of being bonded in step 6, mixed and matched somebody with somebody with aerosil using epoxy construction adhesive or basis material
The putty put carries out adhesion zone right angle transition processing, and transition region filling section is isosceles right triangle or arc-shaped, so
Carry out reinforcement formable layer to bonding each junction afterwards, room temperature place 24 it is small when cure, reinforcement formable layer using hand paste into
Type technique or vacuum assisted resin injection moulding process, bonding pad strengthening course using carbon fiber or glass fibre as enhancement layer,
Using epoxy resin as base layer, and its weight 0.5%-3% is also added with epoxy resin sagging epoxy resin in order to prevent
Aerosil;
Step 8: processing perforate and surfacing
Raft frame or pedestal that step 7 obtains are needed into progress perforate according to installation, and top panel and lower panel are put down
Face degree processing, makes upper and lower surface horizontal;Then carry out entirety to surface to polish smooth, and brushing basis material, basis material are solid
The preparation of frame-type raft frame or pedestal is completed after change.
Frame-type composite material of the present invention is made of the cured dose of curing of reinforcing material and reisn base material, increases
Strong material is glass fibre or carbon fiber, and reisn base material is unsaturated polyester resin, vinylite or epoxy resin.When
When reisn base material is unsaturated polyester resin or vinylite, curing agent for methyl ethyl ketone peroxide, cyclohexanone peroxide,
One kind or any mixture in cumyl peroxide, benzoyl peroxide.When reisn base material is epoxy resin, cure
Agent is diamine, diethylenetriamine, triethylene tetramine, one kind or any mixture in polyethylene polyamine.
As preferrred embodiment of the present invention, the carbon fiber that is used as reinforcing material and bonding pad strengthening course army and
Glass fibre, its weaving manner can be in plain weave, twill weave, satin weave, unidirectional braiding, the polyaxial braiding of multilayer
One or more.The reisn base material is unsaturated polyester resin or vinylite, and curing agent is peroxidating first
One or more in ethyl ketone, cyclohexanone peroxide, cumyl peroxide, benzoyl peroxide, and the additive amount of curing agent
For the 1-5% of the weight of basis material.The basis material is epoxy resin, and curing agent is diamine, diethylenetriamine, three
One or more in ethene tetramine, polyethylene polyamine, and the additive amount of curing agent is the 20-100% of the weight of basis material.
Bonding pad strengthening course reinforcing material glass fibre or carbon fibre fabric minimum widith are more than or equal to 30mm in the present invention,
Then 5mm-15mm is successively increased, fabric maximum width must be less than between upper and lower panel highly or bonding pad is away from structural edge width 2
Minimum value again, reinforcement layer thickness is 3mm-5mm.
The present invention is directed to frame-type composite material raft frame or base construction form, and analysis decomposition, its point are carried out to its structure
It is as follows to solve principle:(1)Partitioned organization is as far as possible few, to reduce connection quantity, improves the security of composite material raft frame or pedestal;
(2)Each composite structure decomposed should be easy to shaping, to improve composite material Forming Quality.
The present invention is described in further detail with reference to following embodiments;But following embodiments are only illustration, this hair
It is bright to be not limited to these embodiments.
Step 1: the STRUCTURE DECOMPOSITION of raft frame or pedestal
Decomposed according to the overall structure form of raft frame or pedestal, be decomposed into top panel, lower panel and transverse and longitudinal floor, its
In, transverse and longitudinal floor includes multiple horizontal gussets and longitudinal gusset, between top panel and transverse and longitudinal floor and lower panel and transverse and longitudinal rib
Connection mode between plate is "T"-shaped grafting, and the connection mode between horizontal gusset and longitudinal gusset is " ten " shape grafting,
Decomposing scheme is finally obtained, decomposing scheme includes the number and size of top panel, lower panel and transverse and longitudinal floor;
By taking the frame of composite material raft shown in Fig. 5-8 as an example, length 2500mm, width 2200mm, total height 240mm, cross rib
Plate 7, longitudinal floor 5.
Each panel forming size of table 1
Step 2: the shaping of composite material partitioned organization, the demoulding
The decomposing scheme obtained according to step 1 makes the mould to match, and the shaping of each piecemeal, base are carried out using mould
Body material and curing agent are molded, and forming method is vacuum assisted resin injection moulding process, die press technology for forming or resin
Any of Transfer molding technique, it is also compound to improve added with damping layer material when composite material partitioned organization is molded
The damping capacity of material raft frame, is demoulded after curing, obtains each piecemeal molding structure, spare;
Fabric is using biaxially fabric E-LT450.According to molding plate size carry out respective fiber fabric and
The cutting of damping layer.The fabric cut is put into baking oven and carries out drying and processing, drying temperature is 100 DEG C ± 2 DEG C, is dried
The dry time is 120 ± 5min.
Resin is cured as RIMH137, matching as 100 using the epoxy resin RIM135 of Germany Han Sen companies:30.
The present embodiment panel construction uses vacuum assistant resin infused, and fabric and damping layer are carried out according to Lay up design
Be plated in, be plated in mode and orthogonal be plated in for 0 °/90 °.Release cloth, flow-guiding cloth, injected rubber hose and true are carried out according to vacuum assisted process
The laying of blank pipe, vacuum sealing is carried out using double-ply bag film.The leakproofness of two layers of vacuum bag film is checked respectively.Start true
Sky pump vacuumizes the preform of fabric, and as pressure≤- 0.095MPa of bag film, pressurize 10min, pressure, which reduces, to be no more than
During 0.01MPa.Start vacuum pump, start as vacuum≤- 0.095MPa irrigate resin, when resin complete wetting fabric in advance into
After continuing injecting glue 25min after type body, injected rubber hose is closed with locking pliers.
Step 3: piecemeal molding structure machines
Each piecemeal molding structure demoulded in step 2 is machined out, the decomposing scheme obtained according to step 1 is each
Locating and machining groove or staggeredly groove, the partitioned organization after must processing are spare on piecemeal molding structure;
Step 4: partitioned organization pre-assembled
Partitioned organization after the processing obtained to step 3 carries out pre-assembled, assemble sequence according to the structure of raft frame or pedestal
For from top to bottom:Lower panel and longitudinal gusset, longitudinal gusset and horizontal gusset, top panel and floor in length and breadth;
Step 5: bonding plane roughening is handled
To treating that bonding plane carries out grinding process after pre-assembled in step 4, then cleaned out using acetone;
Step 6: partitioned organization is bonded
Preassembly sequence in step 4 is bonded, and in partitioned organization bonding plane coating adhesive, adhesive is room
Warm cured epoxy sqtructural adhesive, uses the scraping blade of one fixed width(Scraping blade width is advisable with being slightly less than groove width)In composite panel
Gluing of surfaces gluing, wherein in raft frame panel slot three faces should all uniform gluing, it is fixed first lower panel and transverse and longitudinal floor be bonded
Position, then carries out cemented in place to lower panel and transverse and longitudinal floor, is then bonded top panel;
Step 7: the filling of bonding transition region and bonding pad reinforcement formable layer
After the completion of being bonded in step 6, mixed and matched somebody with somebody with aerosil using epoxy construction adhesive or basis material
The putty put carries out adhesion zone right angle transition processing, and transition region filling section is isosceles right triangle or arc-shaped, so
Carry out reinforcement formable layer to bonding each junction afterwards, room temperature place 24 it is small when cure, reinforcement formable layer using hand paste into
Type technique or vacuum assisted resin injection moulding process, bonding pad strengthening course using carbon fiber or glass fibre as enhancement layer,
Using epoxy resin as base layer, and its weight 0.5%-3% is also added with epoxy resin sagging epoxy resin in order to prevent
Aerosil;Configuration ontology putty, resin use RIM135 and RIMH137, ratio 100:30, filler is gas phase two
Silica, putty are preferred with not trickling.After stirring evenly bonding cure after junction filling the section length of side be 10mm etc.
Waist right angled triangle transition region.
Reinforcing material uses high-strength satin weave glass fibre SW220B-90C, the length direction of fabric and the length phase of junction
Together, width is cut according to table 1, and every 15 layers are 1 group.After the completion of fabric cutting in 100 ± 5 DEG C of baking oven at drying
120 ± 10min is managed, seals fabric vacuum bag film after drying process.Using manual pasting forming process, will cut out successively
Glass fibre is placed on joint, and side glue-application-edge makes fiber be close to joint with scraper plate, ensures no starved, shows money or valuables one carries unintentionally, bubble is existing
As.By the fabric width distribution sequence of table, short fabric is cut in lower floor, it is then incremented by successively, make gentle transition at laying.
During laying, ensure that interlayer sticks closely, surfacing, does not have convex-concave fluctuation, after completing laying, then to overall progress
Appropriate finishing.
2 connector reinforcing material width distribution table of table
Step 8: processing perforate and surfacing
Raft frame or pedestal that step 7 obtains are needed into progress perforate according to installation, and top panel and lower panel are put down
Face degree processing, makes upper and lower surface horizontal;Then carry out entirety to surface to polish smooth, and brushing basis material, basis material are solid
The preparation of naval vessels raft frame or pedestal is completed after change.
The raft frame of the present embodiment is tested after shaping, situation is as follows:
The size progress of composite material raft frame or pedestal is shown in Table 3.
3 composite material raft frame dimensional accuracy of table
Claims (9)
- A kind of 1. method that frame-type raft frame or pedestal are prepared using composite material, it is characterised in that:Comprise the following steps:Step 1: the STRUCTURE DECOMPOSITION of raft frame or pedestalSTRUCTURE DECOMPOSITION is carried out according to the overall structure form of raft frame or pedestal, is decomposed into top panel, lower panel and transverse and longitudinal floor altogether Four parts, wherein, transverse and longitudinal floor includes multiple horizontal gussets and longitudinal gusset, between top panel and transverse and longitudinal floor and lower panel Connection mode between transverse and longitudinal floor is "T"-shaped grafting, and the connection mode between horizontal gusset and longitudinal gusset is " ten " Shape grafting, finally obtains decomposing scheme, and decomposing scheme includes the quantity and size of top panel, lower panel and transverse and longitudinal floor;Step 2: the shaping of composite material partitioned organization, the demouldingThe decomposing scheme obtained according to step 1 makes the mould to match, and is carried out using composite material on corresponding mould respectively Partitioned organization is molded, and is demoulded after curing, obtains each piecemeal molding structure, spare;Step 3: piecemeal molding structure machinesEach piecemeal molding structure demoulded in step 2 is machined out, according to the decomposing scheme that step 1 obtains in each piecemeal Locating and machining groove or groove is cross-linked on molding structure, lower panel machine-shaping fabrication hole, the partitioned organization after must processing, It is spare;Step 4: partitioned organization pre-assembledPartitioned organization after the processing obtained to step 3 carries out pre-assembled according to the structure of raft frame or pedestal;Step 5: bonding plane roughening is handledTo treating that bonding plane carries out grinding process after pre-assembled in step 4, then cleaned out using acetone;Step 6: partitioned organization is bondedPreassembly sequence in step 4 is bonded, in partitioned organization bonding plane coating adhesive, first to lower panel and horizontal stroke Longitudinal rib plate carries out cemented in place, is then bonded top panel;Step 7: the filling of bonding transition region and bonding pad reinforcement formable layerAfter the completion of being bonded in step 6, using epoxy construction adhesive or basis material and aerosil mixed configuration Putty carries out transition processing to adhesion zone right angle, then carries out reinforcement formable layer to bonding each junction, and room temperature is put Put 24 it is small when cure;Step 8: processing perforate and surfacingRaft frame or pedestal that step 7 obtains are needed into progress perforate according to installation, and flatness is carried out to top panel and lower panel Processing, makes upper and lower surface horizontal;Then entirety is carried out to surface to polish smooth, and brushing basis material, after basis material cures Complete the preparation of frame-type raft frame or pedestal.
- A kind of 2. method that frame-type raft frame or pedestal are prepared using composite material as claimed in claim 1, it is characterised in that: The composite material is made of the cured dose of curing of reinforcing material and reisn base material, and reinforcing material is fine for glass fibre or carbon Dimension, reisn base material is unsaturated polyester resin, vinylite or epoxy resin.
- A kind of 3. method that frame-type raft frame or pedestal are prepared using composite material as claimed in claim 2, it is characterised in that: The reisn base material is unsaturated polyester resin or vinylite, and curing agent is methyl ethyl ketone peroxide, peroxidating ring One kind or any mixture in hexanone, cumyl peroxide, benzoyl peroxide.
- A kind of 4. method that frame-type raft frame or pedestal are prepared using composite material as claimed in claim 2, it is characterised in that: The reisn base material is epoxy resin, and curing agent is diamine, diethylenetriamine, triethylene tetramine, polyethylene polyamine In one kind or any mixture.
- A kind of 5. method that frame-type raft frame or pedestal are prepared using composite material as claimed in claim 1, it is characterised in that: Composite material partitioned organization forming method is vacuum assisted resin injection moulding process, die press technology for forming or resin in step 2 Any of Transfer molding technique.
- A kind of 6. method that frame-type raft frame or pedestal are prepared using composite material as claimed in claim 1, it is characterised in that: Assemble sequence in step 4 is from top to bottom:Lower panel and in length and breadth floor, top panel and floor in length and breadth.
- A kind of 7. method that frame-type raft frame or pedestal are prepared using composite material as claimed in claim 1, it is characterised in that: Adhesive described in step 6 is room-temperature curing epoxy structural adhesive.
- A kind of 8. method that frame-type raft frame or pedestal are prepared using composite material as claimed in claim 1, it is characterised in that: In step 7 during transition processing, transition region filling section is isosceles right triangle or arc-shaped.
- A kind of 9. method that frame-type raft frame or pedestal are prepared using composite material as claimed in claim 1, it is characterised in that: Bonding pad reinforcement formable layer described in step 7 uses manual pasting forming process or vacuum assisted resin injection moulding process, bonding pad Strengthening course, as enhancement layer, using epoxy resin as base layer, and is also added using carbon fiber or glass fibre in epoxy resin Added with the aerosil of its weight 0.5%-3%.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610401799.4A CN106084653B (en) | 2016-06-08 | 2016-06-08 | A kind of method that frame-type raft frame or pedestal are prepared using composite material |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610401799.4A CN106084653B (en) | 2016-06-08 | 2016-06-08 | A kind of method that frame-type raft frame or pedestal are prepared using composite material |
Publications (2)
Publication Number | Publication Date |
---|---|
CN106084653A CN106084653A (en) | 2016-11-09 |
CN106084653B true CN106084653B (en) | 2018-05-01 |
Family
ID=57228379
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201610401799.4A Active CN106084653B (en) | 2016-06-08 | 2016-06-08 | A kind of method that frame-type raft frame or pedestal are prepared using composite material |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106084653B (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107060371A (en) * | 2017-05-04 | 2017-08-18 | 瞿慧 | One kind building hydraulic pressure steelframe |
CN107323646B (en) * | 2017-06-23 | 2020-05-05 | 武汉理工大学 | A combined carbon fiber composite vibration isolation raft and preparation method thereof |
CN111823616A (en) * | 2020-07-16 | 2020-10-27 | 吉尔博建筑科技(上海)有限公司 | A new type of composite material formwork template and manufacturing process |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103448260B (en) * | 2013-08-27 | 2017-02-15 | 中国船舶重工集团公司第七二五研究所 | Connecting method of shell plate made from composites and metal member |
CN103482014B (en) * | 2013-09-13 | 2015-10-21 | 中国船舶重工集团公司第七一〇研究所 | A kind of composite material pressure shell and forming method thereof |
CN105217007B (en) * | 2015-11-04 | 2018-01-30 | 中国船舶重工集团公司第七○二研究所 | Doubling plate posture composite construction vibro-damping mount |
-
2016
- 2016-06-08 CN CN201610401799.4A patent/CN106084653B/en active Active
Also Published As
Publication number | Publication date |
---|---|
CN106084653A (en) | 2016-11-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US8017054B1 (en) | Systems and methods for fabricating composite fiberglass laminate articles | |
CN110181835B (en) | Forming method of variable-section double-taper aramid fiber honeycomb sandwich structure | |
US6964723B2 (en) | Method for applying pressure to composite laminate areas masked by secondary features | |
US9291151B2 (en) | Wind turbine blade and its producing method | |
EP2903801B1 (en) | Composite structure having a stabilizing element | |
AU2002249955B2 (en) | Forming structural assemblies with 3-D woven joint pre-forms | |
RU2623772C2 (en) | Method for producing three-dimensional object of composite material | |
US7097731B2 (en) | Method of manufacturing a hollow section, grid stiffened panel | |
CN105922703B (en) | A kind of thin-walled foam interlayer structure compound material antenna house preparation method | |
JP2020117215A (en) | Formed composite stringers | |
CN106084653B (en) | A kind of method that frame-type raft frame or pedestal are prepared using composite material | |
CN107521124A (en) | Carbon fiber dual platen reinforced structure part and its manufacture method | |
CN113772076A (en) | Foam sandwich hat-shaped reinforced wall plate structure and integrated forming method | |
CN103171212A (en) | Toughened lamination composite material and preparation method thereof | |
CN104385628A (en) | Vacuum diversion method for preparing novel carbon fiber hovercraft | |
US11760044B2 (en) | Method and apparatus for manufacturing an integrated hull by using three-dimensional structure type fiber clothes and a three-dimensional vacuum infusion process | |
US6726865B2 (en) | Composite material for vehicle hulls and a hull molding process | |
KR102030195B1 (en) | Masterless layup mandrel tool | |
CN109016571B (en) | Preparation method of airfoil | |
CN104428578A (en) | Composite tank having joint with softening strip and method of making the tank | |
US6352609B1 (en) | Composite tooling process for curing materials at elevated temperatures | |
CN114536792B (en) | Connecting structure and connecting method for composite material part and metal part | |
US20240262053A1 (en) | Monolithic molded fan components and method for their manufacture | |
EP0992336A1 (en) | Method of manufacturing a resin impregnated reinforced article | |
US20030051434A1 (en) | Composite structure and method for constructing same |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |