CN101450533A - Carbon fiber reinforcement resin base composite material lattice structural-component conforming die and method - Google Patents
Carbon fiber reinforcement resin base composite material lattice structural-component conforming die and method Download PDFInfo
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- CN101450533A CN101450533A CNA2007101958291A CN200710195829A CN101450533A CN 101450533 A CN101450533 A CN 101450533A CN A2007101958291 A CNA2007101958291 A CN A2007101958291A CN 200710195829 A CN200710195829 A CN 200710195829A CN 101450533 A CN101450533 A CN 101450533A
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Abstract
The invention relates to a mould and a method for molding a carbon fiber reinforced resin-based composite material grid structural piece. The mould for molding the carbon fiber reinforced resin-based composite material grid structural piece consists of a main body mould, a splitting grid male mould and a splitting grid female mould sequentially from an inner layer to an outer layer; and two end frame pressure loops are arranged on the upper part and the lower part of the main body mould and the splitting grid male mould respectively. The mould can be repeatedly used for a plurality of times; a grid reinforced rib of a molded product has higher dimension precision and position precision; and the quality of the product has good consistency. The method for molding the carbon fiber reinforced resin-based composite material grid structural piece is wholly co-cured and molded, is favorable for ensuring the consistency of the whole performance and quality of the composite material grid structural product so that the structure has good rigidity and bearing capacity.
Description
Technical field
The present invention relates to a kind of Composites Lattice Structure part mould and forming method, be specifically related to a kind of carbon fiber enhancement resin base composite material network part mould and forming method.
Background technology
Along with the development of aerospace industry, improving constantly of space material technological level especially, Composites Lattice Structure obtains using more and more widely.The network that the unidirectional composite material intersection is made can be given full play to the superiority of composite, and constantly improving of design and manufacturing process is expected to reduce as early as possible manufacturing cost, and vast potential for future development and huge potential are arranged.The mould method of the most common moulding grid mainly is following three kinds: the one, and soft mould, this method USAF flies the general laboratory of power (USAF PhillipsLaboratory) and is in the technological precedence status, and is used to produce solar energy pole plate, radome fairing and guided missile adapter.But the method for soft mould also has its shortcoming, and product surface fineness is poor, and rib size instability needs behind the products solidifying soft mode is rived, and cost is higher, will be difficult to the demoulding for the bigger structure of the height/width of rib simultaneously.Another kind of grid forming method is the mould scheme that adopts the rigid foam open channels.Similar to the soft mode method, thereby entering the foam groove, fibre bundle and resin form network.Foam can be stayed in the composite structure, plays the effect of heat preservation and soundproof, also can remove by methods such as machinery, chemistry or heat damages.The major defect of this method is that the grid node fiber volume fraction is up to 60%, thereby to cause the non-position of joints fiber content of rib be 50% of node place, and fiber volume fraction only is 30%.Under this fiber volume fraction, the performance of network is far below shop formable layer composite structure.Another kind method is the die method, as metal pattern.Its shortcoming is that fiber volume fraction is low, and the rib height can not be too high, and labour intensity is big etc.But advantage is also fairly obvious, and promptly the dimensional stability of product is good, the precision height.
Summary of the invention
The object of the present invention is to provide a kind of carbon fiber enhancement resin base composite material network part mould, this mould can be repeatedly used, and the grid reinforcing rib of shaped article has high dimension precision and positional precision, the product quality high conformity; The present invention also provides a kind of carbon fiber enhancement resin base composite material network part forming method, its whole co-curing forms and is beneficial to the overall performance that guarantees the Composites Lattice Structure goods and the uniformity of quality, makes structure have favorable rigidity and bearing capacity.
Carbon fiber enhancement resin base composite material network part mould of the present invention, it is followed successively by main body mould, distinguish grid male, former from the inner to the outer; Two end frame pressure rings are separately positioned on the top and the below of main body mould and distinguish grid male assembly; Described main body mould is made for the steel material; Described distinguish grid male, former are aluminum alloy materials and make; Described distinguish grid male is divided into some lobes at vertical and hoop.
Aforesaid a kind of carbon fiber enhancement resin base composite material network part mould, its described distinguish grid male is provided with expansion slot at place, longitudinal grid reinforcement both ends; Described distinguish grid male is drawn nest in the grid node center, and is provided with chamfering at the place, four angles of grid node; Described stroke of nest diameter of phi is about the grid reinforcing rib width, draws the nest degree of depth at 1.5mm～2mm; The radius R of described chamfering adopts following formula to calculate:
R is the radius of chamfering in the formula;
A is the waling width;
B is a hoop reinforcement width;
Carbon fiber enhancement resin base composite material network part mould of the present invention, it is followed successively by main body mould, silicon rubber grid male, former from the inner to the outer; Two end frame pressure rings are separately positioned on the assembly top and the below of main body mould and silicon rubber grid male; Described main body mould is made for the steel material; Described silicon rubber grid mould is to be made by silastic material; Described former is that aluminum alloy materials is made.
Aforesaid a kind of carbon fiber enhancement resin base composite material network part mould, its described silicon rubber grid male is provided with expansion slot at place, longitudinal grid reinforcement both ends; Described silicon rubber grid male is provided with chamfering at the place, four angles of grid node; The radius R of described chamfering adopts following formula to calculate:
R is the radius of chamfering in the formula;
A is the waling width;
B is a hoop reinforcement width;
Carbon fiber enhancement resin base composite material network part forming method of the present invention, it carries out as follows successively:
(1) at first the distinguish grid male is fixed on the main body mould, then mounting flange on main body mould;
(2) step (1) gained mould is placed on the wrapping machine, twines the carbon fibre initial rinse silk to the grid reinforcing rib place of the outer field distinguish grid male of mould (2); Get one or a few carbon fibre initial rinse silk during winding, earlier twine each longitudinal grid reinforcement successively, and then twine each hoop grid reinforcing rib, twine circulation as one, so circulation is twined until the grid reinforcing rib of distinguish grid male and to be finished;
(3) mould that step (2) gained has been twined the carbon fibre initial rinse silk carries out several times and inhales glue laminated crucial point reason, and described suction glue laminated crucial point reason adopts any one or two kinds in the following method all to adopt;
Described a kind of suction glue laminated crucial point reason method is, the silicon rubber grid that casting is good is in advance embedded step (2) have been twined in each grid reinforcing rib of distinguish grid male of carbon fibre initial rinse silk, with vacuum bag mould is sealed, vacuumize, temperature is at 40～70 ℃, and pressure is at 0.2～0.6Mpa, thereby utilizes silicon rubber that each grid reinforcing rib is transmitted pressure, the unnecessary resin and the fugitive constituent at each grid reinforcing rib place are discharged in realization, and compacting carbon fibre initial rinse silk;
The described another kind of glue laminated crucial point reason method of inhaling is, with vacuum bag step (2) gained mould is sealed, vacuumize, temperature is at 40～70 ℃, pressure is at 0.2～0.6Mpa, thereby utilize silicon rubber that each grid reinforcing rib is transmitted pressure, realize the unnecessary resin and the fugitive constituent at each grid reinforcing rib place are discharged, and compacting carbon fibre initial rinse silk;
(4) to the die surface shop covering of step (3) gained after inhaling glue laminated crucial point reason, the hoop covering adopts the carbon fibre initial rinse silk to twine, and all the other position coverings adopt carbon fiber-free weft fabric shop layer; Then above the mould and below installation end frame pressure ring;
(5) step (4) gained has been spread mould behind the covering and carried out several times and inhale glue and handle, when inhaling glue and handling mould has been sealed with vacuum bag, vacuumized, temperature is at 40～70 ℃, and pressure is at 0.2～0.6Mpa, to get rid of unnecessary resin and fugitive constituent;
(6) outside step (5) gained mould, former is installed, mounting seat under the end frame pressure ring of mould below; Then mould is 100-180 ℃ in temperature, pressure is that 0.3～3.0MPa is cured;
(7) to the mould after the curing of step (6) gained, the former of dismantling successively earlier, base, two end frame pressure rings; Main body mould is upwards extracted, the distinguish grid male is extracted to inside again, obtains fiber-reinforced resin matrix compound material network part at last.
Aforesaid carbon fiber enhancement resin base composite material network part forming method, its described carbon fibre initial rinse silk twine radical and adopt following formula to calculate:
n＝S×ρ×m
f/ρ
f
In the formula, n is a carbon fibre initial rinse silk radical;
S is the grid reinforcing rib sectional area;
ρ is the density of carbon fiber enhancement resin base composite material;
m
fBe carbon fiber weight percentage in the carbon fiber enhancement resin base composite material;
ρ
fBe carbon fibre initial rinse silk thread density.
Aforesaid carbon fiber enhancement resin base composite material network part forming method, it is when each longitudinal grid reinforcement of the described winding of step (2), when the expansion slot place that is wound to longitudinal grid reinforcement both ends, the carbon fibre initial rinse silk evenly scatters, extends to continuously end frame table face to both sides; Described during at place shop, longitudinal grid reinforcement end covering in step (4), carbon fiber-free weft fabric is a thickening degree shop layer, thereby forms a transition region between grid reinforcing rib, covering, end frame.
Carbon fiber enhancement resin base composite material network part forming method of the present invention, it carries out as follows successively:
(1) at first silicon rubber grid mould is fixed on the main body mould, then mounting flange on main body mould;
(2) step (1) gained mould is placed on the wrapping machine, twines the carbon fibre initial rinse silk to the grid reinforcing rib place of the outer field silicon rubber grid of mould mould; Get one or a few carbon fibre initial rinse silk during winding, earlier twine each longitudinal grid reinforcement successively, and then twine each hoop grid reinforcing rib, twine circulation as one, so circulation is twined until the grid reinforcing rib of silicon rubber grid mould and to be finished;
(3) twined the die surface shop covering of carbon fibre initial rinse silk to step (2) gained, the hoop covering adopts the carbon fibre initial rinse silk to twine, and all the other position coverings adopt carbon fiber-free weft fabrics shop layer; Then above the mould and below installation end frame pressure ring;
(4) step (3) gained has been spread mould behind the covering and carried out several times and inhale glue and handle, when inhaling glue and handling mould has been sealed with vacuum bag, vacuumized, temperature is at 40～70 ℃, and pressure is at 0.2～0.6Mpa, to get rid of unnecessary resin and fugitive constituent;
(5) outside step (4) gained mould, former is installed, mounting seat under the end frame pressure ring of mould below; Then mould is 100-180 ℃ in temperature, pressure is that 0.3～3.0MPa is cured;
(6) to the mould after the curing of step (5) gained, the former of dismantling successively earlier, base, two end frame pressure rings; Main body mould is upwards extracted, silicon rubber grid mould is extracted to inside again, obtains fiber-reinforced resin matrix compound material network part at last.
Aforesaid carbon fiber enhancement resin base composite material network part forming method, its described carbon fibre initial rinse silk twine radical and adopt following formula to calculate:
n＝S×ρ×m
f/ρ
f
In the formula, n is a carbon fibre initial rinse silk radical;
S is the grid reinforcing rib sectional area;
ρ is the density of carbon fiber enhancement resin base composite material;
m
fBe carbon fiber weight percentage in the carbon fiber enhancement resin base composite material;
ρ
fBe carbon fibre initial rinse silk thread density.
Aforesaid carbon fiber enhancement resin base composite material network part forming method, it is when each longitudinal grid reinforcement of the described winding of step (2), when the expansion slot place that is wound to longitudinal grid reinforcement both ends, the carbon fibre initial rinse silk evenly scatters, extends to continuously end frame table face to both sides; Described during at place shop, longitudinal grid reinforcement end covering in step (3), carbon fiber-free weft fabric is a thickening degree shop layer, thereby forms a transition region between grid reinforcing rib, covering, end frame.
Effect of the present invention is: carbon fiber enhancement resin base composite material network part mould of the present invention, be applicable to the larger-size network of moulding rib, can effectively solve the problem that large scale reinforcement net lattice structure is difficult for pressurization and demoulding difficulty.Mould of the present invention can be repeatedly used, and the grid reinforcing rib of shaped article has high dimension precision and positional precision, and the product quality high conformity is beneficial to the later stage assembling of product.The distinguish grid male that adopts is applicable to the moulding of high-performance network product; Its distinguish form has solved the problem that network is difficult to the demoulding.The silicon rubber grid mould that adopts utilizes the softness of silicon rubber, easily deformable characteristics, has effectively solved pressure to grid reinforcing rib and has applied problem with the demoulding; Product packing height is difficult for producing defective; Be applicable to complicated network goods such as triangular mesh; Die cost is relatively low.Draw nest and carry out chamfering at grid node place mould, increase volume, solved the problem that grid reinforcing rib intersects continuously.Carbon fiber enhancement resin base composite material network part forming method of the present invention, whole co-curing form and are beneficial to the overall performance that guarantees the Composites Lattice Structure goods and the uniformity of quality, make structure have favorable rigidity and bearing capacity.Forming method of the present invention can be realized the cure under pressure to the Composites Lattice Structure goods, guarantee that finally grid reinforcing rib and covering behind hot-press solidifying have certain fiber volume fraction and lower voidage, guarantee the bonding quality at grid reinforcing rib and covering interface simultaneously.Because covering and grid reinforcing rib bar are Wrapping formed, winding tension can retrain the pressure that silicon rubber produces composite effectively as pretightning force.Utilize silicon rubber mould to transmit pressure and inhale glue, guaranteed the gel content and the density of grid reinforcing rib bar effectively, guaranteed that the complex mesh structure has higher fiber volume fraction and lower porosity; The transition region thickening degree shop layer that covering, grid reinforcing rib, end frame form, the grid reinforcing rib bar extends continuously at the expansion slot place, efficiently solve the transition problem of grid reinforcing rib, covering, end frame, realized the whole co-curing moulding of Composites Lattice Structure product.
Description of drawings
Fig. 1 is embodiment 1 a described carbon fiber enhancement resin base composite material network part forming die structure schematic diagram;
Fig. 2 partly holds frame place enlarged drawing for I among Fig. 1;
Fig. 3 shows cutaway view for distinguish grid male among Fig. 1;
Fig. 4 is the local expanded view of distinguish grid male among Fig. 1;
Fig. 5 is an expansion slot enlarged drawing among Fig. 3;
Fig. 6 is a grid node enlarged drawing among Fig. 3;
Fig. 7 is embodiment 2 described carbon fiber enhancement resin base composite material network part forming die structure schematic diagrames;
Among the figure: 1. main body mould; 2. distinguish grid male; 3. grid product; 4. end frame; 5. base; 6. hold the frame pressure ring; 7. flange; 8. former; 9. silicon rubber grid mould; 10. expansion slot; 11. grid node; 12. draw nest; 13. chamfering; 14. grid reinforcing rib; 15. covering.
The specific embodiment
As shown in Figure 1, carbon fiber enhancement resin base composite material network part mould of the present invention, it is followed successively by main body mould 1, distinguish grid male 2, former 8 from the inner to the outer; Two end frame pressure rings 6 are separately positioned on the top and the below of main body mould 1 and distinguish grid male 2 assemblys; Described main body mould 1 is made for steel; Described distinguish grid male 2, former 8 are aluminium alloy and make.As shown in Figures 3 and 4, distinguish grid male 2 is divided into some lobes at vertical and hoop.
As shown in Figure 5, distinguish grid male 2 is provided with expansion slot 10 at place, longitudinal grid reinforcement both ends.
As shown in Figure 6, distinguish grid male 2 is drawn nest 12 in grid node 11 centers, and is provided with chamfering 13 at the place, four angles of grid node 11; Described stroke of nest diameter of phi is about the grid reinforcing rib width, draws the nest degree of depth at 1.5mm～2mm; The radius R of described chamfering adopts following formula to calculate:
R is the radius of chamfering in the formula;
A is the waling width;
B is a hoop reinforcement width.
Carbon fiber enhancement resin base composite material network part forming method of the present invention, it adopts above-mentioned mould, carries out successively according to following steps:
(1) as shown in Figure 1, at first distinguish grid male 2 is fixed on the main body mould 1, then mounting flange 7 on main body mould 1.
(2) step (1) gained mould is placed on the wrapping machine, twines the carbon fibre initial rinse silk to the grid reinforcing rib place of the outer field distinguish grid male 2 of mould.
The carbon fibre initial rinse silk twines radical and adopts following formula to calculate:
n＝S×ρ×m
f/ρ
f
In the formula, n is a carbon fibre initial rinse silk radical;
S is the grid reinforcing rib sectional area;
ρ is the density of carbon fiber enhancement resin base composite material;
m
fBe carbon fiber weight percentage in the carbon fiber enhancement resin base composite material;
ρ
fBe carbon fibre initial rinse silk thread density;
Get one or a few carbon fibre initial rinse silk during winding, earlier twine each longitudinal grid reinforcement successively, and then twine each hoop grid reinforcing rib, twine circulation as one, so circulation is twined until the grid reinforcing rib of distinguish grid male 2 and to be finished.As shown in Figure 5, when twining each longitudinal grid reinforcement, when expansion slot 10 places that are wound to longitudinal grid reinforcement both ends, the carbon fibre initial rinse silk evenly scatters, extends to continuously end frame table face to both sides.
(3) mould that step (2) gained has been twined the carbon fibre initial rinse silk carries out several times and inhales glue laminated crucial point reason, and described suction glue laminated crucial point reason adopts any one or two kinds in the following method all to adopt.
Described a kind of suction glue laminated crucial point reason method is, the silicon rubber grid that casting is good is in advance embedded step (2) have been twined in each grid reinforcing rib of distinguish grid male 2 of carbon fibre initial rinse silk, with vacuum bag mould is sealed, vacuumize, temperature is at 40～70 ℃, and pressure is at 0.2～0.6Mpa, thereby utilizes silicon rubber that each grid reinforcing rib is transmitted pressure, the unnecessary resin and the fugitive constituent at each grid reinforcing rib place are discharged in realization, and compacting carbon fibre initial rinse silk;
The described another kind of glue laminated crucial point reason method of inhaling is, with vacuum bag step (2) gained mould is sealed, vacuumize, temperature is at 40～70 ℃, pressure is at 0.2～0.6Mpa, thereby utilize silicon rubber that each grid reinforcing rib is transmitted pressure, realize the unnecessary resin and the fugitive constituent at each grid reinforcing rib place are discharged, and compacting carbon fibre initial rinse silk.
(4) to the die surface shop covering of step (3) gained after inhaling glue laminated crucial point reason, the hoop covering adopts the carbon fibre initial rinse silk to twine, and all the other position coverings adopt carbon fiber-free weft fabric shop layer; Then above the mould and below installation end frame pressure ring 6; As shown in Figure 2, when place, longitudinal grid reinforcement end shop covering, carbon fiber-free weft fabric is thickening degree shop layer, thereby forms a transition region between grid reinforcing rib 14, covering 15, end frame 4.
(5) step (4) gained has been spread mould behind the covering and carried out several times and inhale glue and handle, when inhaling glue and handling mould has been sealed with vacuum bag, vacuumized, temperature is at 40～70 ℃, and pressure is at 0.2～0.6Mpa, to get rid of unnecessary resin and fugitive constituent.
(6) outside step (5) gained mould, former 8 is installed, 6 times mounting seat 5 of end frame pressure ring of mould below; Then mould is 100-180 ℃ in temperature, pressure is that 0.3～3.0MPa is cured.
(7) mould after step (6) gained is solidified, the former 8 of dismantling successively earlier, base 5, two end frame pressure rings 6; Main body mould 1 is upwards extracted, distinguish grid male 2 is extracted to inside, obtains fiber-reinforced resin matrix compound material network part at last again.
Embodiment 2
As shown in Figure 7, carbon fiber enhancement resin base composite material network part mould, it is followed successively by main body mould 1, silicon rubber grid male 9, former 8 from the inner to the outer; Two end frame pressure rings 6 are separately positioned on the assembly top and the below of main body mould 1 and silicon rubber grid male 9; Described main body mould 1 is made for steel; Described silicon rubber grid mould is to be made by silastic material; Described former 8 is made for aluminium alloy.
Silicon rubber grid male 9 is provided with expansion slot at place, longitudinal grid reinforcement both ends.Silicon rubber grid male 9 is provided with chamfering at the place, four angles of grid node; The radius R of described chamfering adopts following formula to calculate:
R is the radius of chamfering in the formula;
A is the waling width;
B is a hoop reinforcement width;
Carbon fiber enhancement resin base composite material network part forming method of the present invention, it adopts above-mentioned mould, carries out successively as follows:
(1) at first silicon rubber grid mould 9 is fixed on the main body mould 1, then mounting flange 7 on main body mould 1;
(2) step (1) gained mould is placed on the wrapping machine, twines the carbon fibre initial rinse silk to the grid reinforcing rib place of the outer field silicon rubber grid of mould mould 9.
The carbon fibre initial rinse silk twines radical and adopts following formula to calculate:
n＝S×ρ×m
f/ρ
f
In the formula, n is a carbon fibre initial rinse silk radical;
S is the grid reinforcing rib sectional area;
ρ is the density of carbon fiber enhancement resin base composite material;
m
fBe carbon fiber weight percentage in the carbon fiber enhancement resin base composite material;
ρ
fBe carbon fibre initial rinse silk thread density;
Get one or a few carbon fibre initial rinse silk during winding, earlier twine each longitudinal grid reinforcement successively, and then twine each hoop grid reinforcing rib, twine circulation as one, so circulation is twined until the grid reinforcing rib of silicon rubber grid mould 9 and to be finished; When twining each longitudinal grid reinforcement, when the expansion slot place that is wound to longitudinal grid reinforcement both ends, the carbon fibre initial rinse silk evenly scatters, extends to continuously end frame table face to both sides.
(3) twined the die surface shop covering of carbon fibre initial rinse silk to step (2) gained, the hoop covering adopts the carbon fibre initial rinse silk to twine, and all the other position coverings adopt carbon fiber-free weft fabrics shop layer; Then above the mould and below installation end frame pressure ring 6; When place, longitudinal grid reinforcement end shop covering, carbon fiber-free weft fabric is thickening degree shop layer, thereby forms a transition region between grid reinforcing rib 14, covering 15, end frame 4.
(4) step (3) gained has been spread mould behind the covering and carried out several times and inhale glue and handle, when inhaling glue and handling mould has been sealed with vacuum bag, vacuumized, temperature is at 40～70 ℃, and pressure is at 0.2～0.6Mpa, to get rid of unnecessary resin and fugitive constituent.
(5) outside step (4) gained mould, former 8 is installed, 6 times mounting seat 5 of end frame pressure ring of mould below; Then mould is 100-180 ℃ in temperature, pressure is that 0.3～3.0MPa is cured.
(6) mould after step (5) gained is solidified, the former 8 of dismantling successively earlier, base 5, two end frame pressure rings 6; Main body mould 1 is upwards extracted, silicon rubber grid mould 9 is extracted to inside, obtains fiber-reinforced resin matrix compound material network part at last again.
Claims (10)
1. carbon fiber enhancement resin base composite material network part mould, it is characterized in that: it is followed successively by main body mould (1), distinguish grid male (2), former (8) from the inner to the outer; Two end frame pressure rings (6) are separately positioned on the top and the below of main body mould (1) and distinguish grid male (2) assembly; Described main body mould (1) is made for the steel material; Described distinguish grid male (2), former (8) are aluminum alloy materials and make; Described distinguish grid male (2) is divided into some lobes at vertical and hoop.
2. a kind of carbon fiber enhancement resin base composite material network part mould according to claim 1 is characterized in that: described distinguish grid male (2) is provided with expansion slot (10) at place, longitudinal grid reinforcement both ends; Described distinguish grid male (2) is drawn nest (12) in grid node (11) center, and is provided with chamfering (13) at the place, four angles of grid node (11); Described stroke of nest diameter of phi is about the grid reinforcing rib width, draws the nest degree of depth at 1.5mm～2mm; The radius R of described chamfering adopts following formula to calculate:
R is the radius of chamfering in the formula;
A is the waling width;
B is a hoop reinforcement width;
3. carbon fiber enhancement resin base composite material network part mould, it is characterized in that: it is followed successively by main body mould (1), silicon rubber grid male (9), former (8) from the inner to the outer; Two end frame pressure rings (6) are separately positioned on the assembly top and the below of main body mould (1) and silicon rubber grid male (9); Described main body mould (1) is made for the steel material; Described silicon rubber grid mould is to be made by silastic material; Described former (8) is made for aluminum alloy materials.
4. a kind of carbon fiber enhancement resin base composite material network part mould according to claim 3 is characterized in that: described silicon rubber grid male (9) is provided with expansion slot (10) at place, longitudinal grid reinforcement both ends; Described silicon rubber grid male (9) is provided with chamfering at the place, four angles of grid node; The radius R of described chamfering adopts following formula to calculate:
R is the radius of chamfering in the formula;
A is the waling width;
B is a hoop reinforcement width;
5. carbon fiber enhancement resin base composite material network part forming method, it is characterized in that: this method is carried out as follows successively:
(1) at first distinguish grid male (2) is fixed on the main body mould (1), goes up mounting flange (7) in main body mould (1) then;
(2) step (1) gained mould is placed on the wrapping machine, twines the carbon fibre initial rinse silk to the grid reinforcing rib place of the outer field distinguish grid male of mould (2); Get one or a few carbon fibre initial rinse silk during winding, earlier twine each longitudinal grid reinforcement successively, and then twine each hoop grid reinforcing rib, twine circulation as one, so circulation is twined until the grid reinforcing rib of distinguish grid male (2) and to be finished;
(3) mould that step (2) gained has been twined the carbon fibre initial rinse silk carries out several times and inhales glue laminated crucial point reason, and described suction glue laminated crucial point reason adopts any one or two kinds in the following method all to adopt;
Described a kind of suction glue laminated crucial point reason method is, the silicon rubber grid that casting is good is in advance embedded step (2) have been twined in each grid reinforcing rib of distinguish grid male (2) of carbon fibre initial rinse silk, with vacuum bag mould is sealed, vacuumize, temperature is at 40～70 ℃, and pressure is at 0.2～0.6Mpa, thereby utilizes silicon rubber that each grid reinforcing rib is transmitted pressure, the unnecessary resin and the fugitive constituent at each grid reinforcing rib place are discharged in realization, and compacting carbon fibre initial rinse silk;
The described another kind of glue laminated crucial point reason method of inhaling is, with vacuum bag step (2) gained mould is sealed, vacuumize, temperature is at 40～70 ℃, pressure is at 0.2～0.6Mpa, thereby utilize silicon rubber that each grid reinforcing rib is transmitted pressure, realize the unnecessary resin and the fugitive constituent at each grid reinforcing rib place are discharged, and compacting carbon fibre initial rinse silk;
(4) to the die surface shop covering of step (3) gained after inhaling glue laminated crucial point reason, the hoop covering adopts the carbon fibre initial rinse silk to twine, and all the other position coverings adopt carbon fiber-free weft fabric shop layer; Then above the mould and below installation end frame pressure ring (6);
(5) step (4) gained has been spread mould behind the covering and carried out several times and inhale glue and handle, when inhaling glue and handling mould has been sealed with vacuum bag, vacuumized, temperature is at 40～70 ℃, and pressure is at 0.2～0.6Mpa, to get rid of unnecessary resin and fugitive constituent;
(6) outside step (5) gained mould former (8) is installed, the end frame pressure ring (6) of mould below is mounting seat (5) down; Then mould is 100-180 ℃ in temperature, pressure is that 0.3～3.0MPa is cured;
(7) to the mould after the curing of step (6) gained, the former (8) of dismantling successively earlier, base (5), two end frame pressure rings (6); Main body mould (1) is upwards extracted, distinguish grid male (2) is extracted to inside again, obtains fiber-reinforced resin matrix compound material network part at last.
6. carbon fiber enhancement resin base composite material network part forming method according to claim 5 is characterized in that: described carbon fibre initial rinse silk twines radical and adopts following formula to calculate:
n＝S×ρ×m
f/ρ
f
In the formula, n is a carbon fibre initial rinse silk radical;
S is the grid reinforcing rib sectional area;
ρ is the density of carbon fiber enhancement resin base composite material;
m
fBe carbon fiber weight percentage in the carbon fiber enhancement resin base composite material;
ρ
fBe carbon fibre initial rinse silk thread density.
7. according to claim 5 or 6 described carbon fiber enhancement resin base composite material network part forming methods, it is characterized in that: when each longitudinal grid reinforcement of the described winding of step (2), when the expansion slot that is wound to longitudinal grid reinforcement both ends (10) is located, the carbon fibre initial rinse silk evenly scatters, extends to continuously end frame table face to both sides; Described during at place shop, longitudinal grid reinforcement end covering in step (4), carbon fiber-free weft fabric is a thickening degree shop layer, thereby forms a transition region between grid reinforcing rib (14), covering (15), end frame (4).
8. carbon fiber enhancement resin base composite material network part forming method, it is characterized in that: this method is carried out as follows successively:
(1) at first silicon rubber grid mould (9) is fixed on the main body mould (1), goes up mounting flange (7) in main body mould (1) then;
(2) step (1) gained mould is placed on the wrapping machine, twines the carbon fibre initial rinse silk to the grid reinforcing rib place of the outer field silicon rubber grid of mould mould (9); Get one or a few carbon fibre initial rinse silk during winding, earlier twine each longitudinal grid reinforcement successively, and then twine each hoop grid reinforcing rib, twine circulation as one, so circulation is twined until the grid reinforcing rib of silicon rubber grid mould (9) and to be finished;
(3) twined the die surface shop covering of carbon fibre initial rinse silk to step (2) gained, the hoop covering adopts the carbon fibre initial rinse silk to twine, and all the other position coverings adopt carbon fiber-free weft fabrics shop layer; Then above the mould and below installation end frame pressure ring (6);
(4) step (3) gained has been spread mould behind the covering and carried out several times and inhale glue and handle, when inhaling glue and handling mould has been sealed with vacuum bag, vacuumized, temperature is at 40～70 ℃, and pressure is at 0.2～0.6Mpa, to get rid of unnecessary resin and fugitive constituent;
(5) outside step (4) gained mould former (8) is installed, the end frame pressure ring (6) of mould below is mounting seat (5) down; Then mould is 100-180 ℃ in temperature, pressure is that 0.3～3.0MPa is cured;
(6) to the mould after the curing of step (5) gained, the former (8) of dismantling successively earlier, base (5), two end frame pressure rings (6); Main body mould (1) is upwards extracted, silicon rubber grid mould (9) is extracted to inside again, obtains fiber-reinforced resin matrix compound material network part at last.
9. carbon fiber enhancement resin base composite material network part forming method according to claim 8 is characterized in that: described carbon fibre initial rinse silk twines radical and adopts following formula to calculate:
n＝S×ρ×m
f/ρ
f
In the formula, n is a carbon fibre initial rinse silk radical;
S is the grid reinforcing rib sectional area;
ρ is the density of carbon fiber enhancement resin base composite material;
m
fBe carbon fiber weight percentage in the carbon fiber enhancement resin base composite material;
ρ
fBe carbon fibre initial rinse silk thread density.
10. according to Claim 8 or 9 described carbon fiber enhancement resin base composite material network part forming methods, it is characterized in that: when each longitudinal grid reinforcement of the described winding of step (2), when the expansion slot that is wound to longitudinal grid reinforcement both ends (10) is located, the carbon fibre initial rinse silk evenly scatters, extends to continuously end frame table face to both sides; Described during at place shop, longitudinal grid reinforcement end covering in step (3), carbon fiber-free weft fabric is a thickening degree shop layer, thereby forms a transition region between grid reinforcing rib (14), covering (15), end frame (4).
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