CN106945311A - A kind of many beam box section co-curing shapings of composite make frock and manufacture craft with enhancement layer - Google Patents
A kind of many beam box section co-curing shapings of composite make frock and manufacture craft with enhancement layer Download PDFInfo
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- CN106945311A CN106945311A CN201710296952.6A CN201710296952A CN106945311A CN 106945311 A CN106945311 A CN 106945311A CN 201710296952 A CN201710296952 A CN 201710296952A CN 106945311 A CN106945311 A CN 106945311A
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- enhancement layer
- frock
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- 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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/545—Perforating, cutting or machining during or after moulding
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- 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
- B29C70/443—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 and impregnating by vacuum or injection
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
The invention belongs to composite autoclave forming process technical field, the making frock of specifically related to a kind of many beam box section co-curing shaping enhancement layers of composite, frock upper die body is made including enhancement layer and enhancement layer makes frock lower mold body, both include coplanar side, and it is on-right angle that the side is angled with enhancement layer institute.The making frock of above-mentioned enhancement layer is further related to utilize to the manufacture craft of enhancement layer.The enhancement layer makes frock and manufacture craft on the basis of existing multiple solidification reassembles technique, improves the intensity of part, can ensure Forming Quality.In summary, by adopting the above-described technical solution, the present invention is relative to the beneficial effect of prior art：The present invention has ensured the shaping strength of part central sill and covering junction, further ensures the Forming Quality of part.Present invention process is simple to operate, and repeatability is strong.
Description
Technical field
The invention belongs to composite autoclave forming process technical field, in particular it relates to a kind of many beams of composite
Box section co-curing shaping makes frock with enhancement layer, and using the technique of the making frock making enhancement layer.
Background technology
Autoclave (Hot Air Autoelave write a Chinese character in simplified form Atitoelave) be it is a kind of for polymer matrix composite into
The process equipment of type process characteristic, the method for moulding process is carried out autoclave molding method using this equipment.Autoclave molding
Method is the main method for manufacturing continuous lod same with thermosetting compound material product, is now widely used for advanced composite material knot
The shaping of structure, honeycomb sandwich construction and metal or adhesive bonding of composites structure.When material is molded, offer simultaneously in autoclave is utilized
Uniform temperature and well-distributed pressure and solidify, complex-shaped so it is high to can obtain surface and internal soundness, huge compound of area
Material.
Autoclave molding method is one of widely used process both at home and abroad at present, be mainly used in large scale, profile compared with
The manufacture of complicated Aeronautics and Astronautics FRP components, such as Skin Parts, beam, frame, various wallboard parts, floor and radome fairing.Autoclave into
The general principle of type method is：Prepreg is laid on mould by laying requirement, and be put into autoclave after being sealed in vacuum bag
In, by the heating of autoclave equipment, pressurization, material solidification reaction is completed, prepreg blank is turned into required shape and is met matter
Measure the process of desired component.
Carbon fiber enhancement resin base composite material has specific strength and specific modulus is high and designability is strong and is easy to overall
The advantages such as shaping, therefore be widely used in aviation field, especially in terms of civil aircraft.Composites Molding Techniques are very
Many, prepreg-autoclave technique, in occupation of critical positions, there is co-curing with its excellent product quality, cementing altogether, secondary cementing
Etc. mode.
The composite torsion-box structural member at home and abroad employed in army's civil aircraft project generally uses following several sides at present
Formula is manufactured：
1st, after composite material skin and beam part are separately fabricated by assembly connection into box section；
2nd, RTM techniques；
3rd, rubber pneumatic bag moulding process.
In three of the above process, the 1st kind of method is using splicing frock, the covering and beam part positioning error of box section
Greatly, it is impossible to ensure depth of beam and the up and down depth of parallelism of covering, and the manufacturing cycle is long, cost is big.2nd kind of method and the 3rd kind of side
Method is overall co-curing shaping, although shortens the cycle, reduces cost, but can not ensure the Forming Quality of part.2nd kind
Method requires very high to Resin Flow, may be only available for specific resin system, and the product resin gel content being molded compared with
It is high and unstable, it is impossible to be used in the load box section structure of aircraft.3rd kind of method uses rubber pneumatic bag expandable pressurized, due to air bag
In die cavity, cause the temperature homogeneity of whole product and mould poor, and there is ageing of rubber, swell increment dyscalculia etc. to ask
Topic, easily causes pressurization inequality, so as to cause the problems such as position skew, flexural deformation, overall box section quality cannot be ensured.
The content of the invention
It is an object of the invention to：For prior art Forming Quality it is poor the problem of there is provided a kind of many beams of composite
Box section co-curing shaping makes frock and manufacture craft with enhancement layer；The enhancement layer makes frock and manufacture craft existing many
Secondary solidification is reassembled on the basis of technique, is improved the intensity of part, can be ensured Forming Quality.
To achieve these goals, the technical solution adopted by the present invention is：
A kind of making frock of many beam box section co-curing shaping enhancement layers of composite, including enhancement layer are made in frock
Die body and enhancement layer make frock lower mold body, and both include coplanar side, and the side is angled with enhancement layer institute is
On-right angle.
The weak link of part is typically that the setting of enhancement layer improves the part of junction in the junction of beam and covering
Thickness, improves the shaping strength of part.If by prepreg by sideline be right angle in the way of set, its be molded zero
Part, is easily deformed in beam with covering contact position, thus it is in oblique angle mode that enhancement layer sideline, which is set, then can avoid out
Existing above mentioned problem.Because prepreg is very soft and frivolous so that the operation for cutting oblique angle in its side becomes very difficult.This
Enhancement layer prepreg is clamped between two die bodys by the making frock of invention, and prepreg is extended to outside die body, in two die bodys
Side be provided with inclined-plane, then two die bodys will presoak material clamping it is close after, you can carry out cutting operation.
Preferably, the enhancement layer makes frock upper die body and enhancement layer makes frock lower mold body and is halfpace
Shape, and the homonymy inclined-plane difference of two halfpaces is coplanar.Prepreg is held between the two by upper halfpace with lower halfpace, utilizes halfpace two
The coplanar inclined-plane in side, can once cut into the enhancement layer shape finally needed.
Further, during the two ends that the enhancement layer making frock upper die body and enhancement layer make frock lower mold body are portrayed
Line.The setting of center line is more accurately cut, and is more convenient operation.
Utilize the work of the making frock making enhancement layer of the above-mentioned many beam box section co-curing shaping enhancement layers of composite
Skill, comprises the following steps：
F1, on a table top upper berth enhancement layer prepreg is folded, surplus is left in the both sides of the enhancement layer prepreg；
F2, enhancement layer prepreg is placed on to the enhancement layer makes frock upper die body and enhancement layer makes frock lower mold body
Between, and clamping makes both inclined-planes coplanar；
F3, with knife close to enhancement layer make frock upper die body and enhancement layer and make the inclined-plane of frock lower mold body and cut out reinforcement
The oblique angle of layer prepreg；
F4, the enhancement layer made is placed between covering blank and beam blank.
By said modules and step, enhancement layer of the side with oblique angle can be produced, enhancement layer is mated formation in beam blank
Between covering blank, three in one co-curing is molded, the Forming Quality of part is improved.
Preferably, the surplus in the step F1 is 10-20mm.
Preferably, the step of also being alignd in the step F2 including center line：Enhancement layer is made into frock upper die body
The center line positioned in alignment of frock lower mold body is made with enhancement layer.The setting of center line is more accurately cut, and is more convenient operation.
In summary, by adopting the above-described technical solution, the present invention is relative to the beneficial effect of prior art：
1st, the present invention has ensured the shaping strength of part central sill and covering junction, further ensures the shaping matter of part
Amount.
2nd, present invention process is simple to operate, and repeatability is strong.
Brief description of the drawings
Fig. 1 is firm template schematic diagram.
Fig. 2 is outside soft mould frock schematic diagram.
Fig. 3 is soft mode sectional drawing on the outside of the firm template of soft mould frock making band of outside.
Fig. 4 is with soft mode schematic diagram on the outside of firm template.
Fig. 5 is inner side soft mould frock schematic diagram one.
Fig. 6 is inner side soft mould frock schematic diagram two.
Fig. 7 is soft mode sectional drawing on the inside of the soft mould frock making of inner side.
Fig. 8 is inner side soft mode schematic diagram.
Fig. 9 is outside soft mould frock making without soft mode sectional drawing on the outside of firm template.
Figure 10 is without soft mode schematic diagram on the outside of firm template.
Figure 11 is rib laying mould schematic diagram.
Figure 12 is beam mould component locating support schematic diagram.
Figure 13 is the assembling schematic diagram one of beam mould component and rib.
Figure 14 is the assembling schematic diagram two of beam mould component and rib.
Figure 15 is the assembling schematic diagram three of beam mould component and rib.
Figure 16 is lower wall plate forming die schematic diagram.
Figure 17 is upper wall plate forming die schematic diagram.
Figure 18 is that enhancement layer makes frock schematic diagram.
Figure 19 is the assembling schematic diagram of beam mould component and rib, enhancement layer and lower wall plate forming die.
Figure 20 is that beam mould component locating support removes schematic diagram.
Figure 21 is support member schematic diagram.
Figure 22 is beam and covering co-curing forming frock schematic diagram.
Figure 23 is beam and covering co-curing forming frock side view.
Figure 24 is A portions enlarged drawing.
Filling region a in accompanying drawing 24 represents rib blank, and b represents covering blank, and c represents enhancement layer blank.
Embodiment
Below in conjunction with the accompanying drawings, the present invention is described in detail.
In order to make the purpose , technical scheme and advantage of the present invention be clearer, it is right below in conjunction with drawings and Examples
The present invention is further elaborated.It should be appreciated that specific embodiment described herein is only to explain the present invention, not
For limiting the present invention.
Embodiment 1
A kind of making frock of many beam box section co-curing shaping enhancement layers of composite, as shown in figure 18, including strengthens
Layer makes frock upper die body 610 and enhancement layer makes frock lower mold body 620, and both include coplanar side, and the side
Angled with enhancement layer institute is on-right angle.
Specifically, as shown in figure 18, the enhancement layer makes frock upper die body 610 and enhancement layer makes frock lower mold body
620 are halfpace shape, and the homonymy inclined-plane difference of two halfpaces is coplanar.The enhancement layer makes frock upper die body 610 and enhancement layer
Portray center line in the two ends for making frock lower mold body 620.
Utilize the work of the making frock making enhancement layer of the above-mentioned many beam box section co-curing shaping enhancement layers of composite
Skill, comprises the following steps：
F1, on a table top upper berth enhancement layer prepreg is folded, surplus is left in the both sides of the enhancement layer prepreg；
F2, strong layer prepreg be placed on to the enhancement layer makes frock upper die body 610 and enhancement layer makes mould under frock
Between body 620, and clamping makes both inclined-planes coplanar；
F3, with knife close to enhancement layer make frock upper die body 610 and enhancement layer makes the inclined-plane of frock lower mold body 620 and cut
Go out the oblique angle of enhancement layer prepreg；
F4, the enhancement layer made is placed between covering blank and beam blank.
Surplus in the step F1 is 10-20mm.
The step of also being alignd in the step F2 including center line：Enhancement layer is made into frock upper die body 610 and enhancement layer system
Workmanship loads the center line positioned in alignment of die body 620.
Each forming frock and auxiliary mould are introduced below：
Beam mould component, including at least three beam moulds being set up in parallel are used in many beam box section co-curing shapings of composite；
Two adjacent beam moulds, the template for clamping beam blank, and the type of the clamping beam blank are included in adjacent side
It is rigidity to have one in plate, and another is flexibility.
Specifically, as shown in figure 4, the beam mould component is included with soft mode 120 on the outside of firm template, outside the firm template of band
Side soft mode 120 is a U-type groove body.
As shown in figure 8, the beam mould component includes inner side soft mode 130, the inner side soft mode 130 is a cylinder.
As shown in figure 8, being provided with unfilled corner structure on the cylinder of the inner side soft mode 130.
Soft mode 120 and inner side soft mode 130 connect flexible template system by the firm both sides of template 100 on the outside of the firm template of band
Into.Specifically, as shown in figure 3, the flexible template of soft mode 120 is by with rubber on the outside of soft mode on the outside of firm template on the outside of the firm template of the band
Glue 121 and with soft mode inner rubber 122 on the outside of firm template, soft mode prepreg 123 is constituted on the outside of the firm template of centre entrainment；Such as Fig. 7
Shown, the flexible template of the inner side soft mode 130 is middle by inner side soft mode outer rubber 131 and inner side soft mode inner rubber 132
Folder inner side soft mode prepreg 133 is constituted.
As shown in Fig. 3,7, the both sides of the firm template 110 are inclined-plane, and the inclined-plane is towards the inner side of firm template 110
Face.
As shown in figure 1, the two ends of the firm template 110 are provided with fixed ear 111；The medial surface of the firm template 110
It is additionally provided with reinforcement 112.
The beam mould component is included without soft mode 140 on the outside of firm template, and described is one without soft mode 140 on the outside of firm template
U-type groove body.
It is described to be made up without soft mode 140 on the outside of firm template of flexible template, as shown in figure 9, described without on the outside of firm template
The flexible template of soft mode 140 is by without soft mode outer rubber 142 on the outside of firm template and without soft mode inner rubber on the outside of firm template
141, centre folder is constituted without soft mode prepreg 143 on the outside of firm template.
Above-mentioned prepreg uses Fabric prereg laying layer 2-3.
The many beam box section co-curing shaping beam mould assembly forming frocks of composite, including outside soft mould frock
400 and inner side soft mould frock 500, as shown in Fig. 2 the outside soft mould frock 400 is a U-type groove body；Such as Fig. 5 institutes
Show, the inner side soft mould frock 500 is a cylinder combined by two U-type groove bodies.
As shown in Fig. 2 the two ends of the outside soft mould frock 400 are provided with outside soft mode limited block 410.
As shown in fig. 6, the inner side soft mould frock 500 includes inner side soft mould frock upper die body 520 and inner side
Soft mould frock lower mold body 530, the inner side soft mould frock upper die body 520 and inner side soft mould frock lower mold body
530 are U-type groove body, and both are combined into a cylinder by being arranged on the locating piece 540 of side.
As shown in figure 5, the inner side soft mould frock upper die body 520 and inner side soft mould frock lower mold body 530
Two ends are respectively arranged with inner side soft mode limited block 510.
As shown in figure 5, the top of the inner side soft mould frock upper die body 520 is provided with inner side soft mode lifting plate 521
With inner side soft mode rotating shaft 522.
As shown in figure 5, the two ends of the inner side soft mould frock upper die body 520, which are additionally provided with firm template, fixes ear 523.
The many beam box section co-curing shaping beam mould component locating supports of composite, as shown in figure 12, including two groups of phases
To the locating support 300 of setting, at least two groups positions are respectively arranged with the locating support 300 and are relatively fixed plate 330.
As shown in figure 12, it is provided with the locating support 300 on location-plate, the location-plate and is provided with dowel hole.
The locating support 300 is made up of the crossbeam 310 and vertical beam 320 interfixed, and the fixed plate 330 is arranged on the vertical beam
On 320.The crossbeam 310 and the vertical beam 320 are orthogonal.The vertical beam 320 is provided with least two.The locating support
300 height is less than the height of beam mould component.
Composite many beam boxes section co-curing moulding process is introduced below, so that those skilled in the art can be real
Apply the present invention.A kind of many beam box section co-curing moulding process of composite, comprise the following steps：
A, beam mould component making step；
B, beam blank making step；
C, beam mould component and beam blank number of assembling steps；
D, covering die component and covering blank making step；
E, beam mould component and beam blank and covering die component and covering blank number of assembling steps.
Auxiliary mould and process that each step of A, B, C, D, E described in detail below is used：
A, the making step of the beam mould component include：
A1, the outside beam form with rigid template making step：
A1.1, as shown in figure 1, make a firm template 110, the firm template 110 is identical with the profile of its preforming beam,
Its relative two ends is respectively arranged with fixed ear 111；Profile, size and the hole position parameter of firm template 110 are special by beam part physics
Property determine；
A1.2, as shown in Fig. 2 make an outside soft mould frock 400, the outside soft mould frock 400 be a U
Type groove body, its bottom land is identical with the profile of the firm template 110；
A1.3, as shown in figure 3, the firm template 110 to be placed on to the bottom land of the outside soft mould frock 400, and
The flexible template of laying rubber folder prepreg on the cell wall of the outside soft mould frock 400, and the flexible template and institute
The both sides for stating firm template 110 are connected respectively；
A1.4, as shown in figure 4, by firm template 110 and rubber press from both sides the flexible template of prepreg together with solidified, be stripped place again
Reason, is obtained with soft mode 120 on the outside of firm template；Type face precision and quality with soft mode 120 on the outside of firm template and part checking and accepting technology
Condition is identical；This soft mode is molded for lateral face；
A2, inner side beam form making step：
A2.1, as shown in figure 1, make a firm template 110, the firm template 110 is identical with the profile of its preforming beam,
The relative two ends of the firm template 110 are respectively arranged with fixed ear 111；Profile, size and the hole position parameter of firm template 110 are by beam
Part physical characteristic is determined；
A2.2, as shown in Figure 5,6, makes an inner side soft mould frock 500, and the inner side soft mould frock 500 is
One cylinder combined by two U-type groove bodies, the bottom land of one of U-type groove body is identical with the profile of the firm template 110；
A2.3, as shown in fig. 7, by the firm template 110 be placed on its profile identical bottom land, it is and soft in the inner side
The flexible template of laying rubber folder prepreg on remaining inner tube wall of mold forming frock 500, and the flexible template and the firm type
The both sides of plate 110 are connected respectively；
A2.4, as shown in figure 8, by firm template 110 and rubber press from both sides the flexible template of prepreg together with solidified, be stripped place again
Reason, obtains inner side soft mode 130；The type face precision and quality of inner side soft mode 130 are identical with part inspection specifications, as needed
Make respective numbers；This soft mode is molded for osculant face；
A3, without rigid template outside beam form making step：
A3.1, as shown in Fig. 2 make an outside soft mould frock 400, the outside soft mould frock 400 be a U
Type groove body, its bottom land is identical with the profile of its preforming beam；
A3.2, as shown in figure 9, on the bottom land and cell wall of the outside soft mould frock 400 laying rubber folder preimpregnation
The flexible template of material；
A3.3, as shown in Figure 10, presss from both sides the flexible template of prepreg by rubber and is solidified, is stripped processing again, obtain without firm
Soft mode 140 on the outside of template；This soft mode is molded for outermost type face.
Wherein, step A1, A2, A3 can be parallel, has no sequencing limitation, and parallel work-flow can improve operating efficiency.Note
The soft mode made is protected with isolated material.
B, the making step of the beam blank include：
B1, as shown in figure 11, making rib laying mould 700, the rib laying mould 700 includes one and beam profile identical
Outer surface；
B2, the side laying prepreg in the outer surface of rib laying mould 700 and outer surface, then prepreg is removed, obtain
To the rib of a U-type groove shape；
B3, repeat aforesaid operations, make at least four ribs.
C, the beam mould component and beam blank number of assembling steps include：
C1, as shown in figure 12, one beam mould component locating support of making, the beam mould component locating support is including two groups
At least two groups positions are respectively arranged with the locating support 300 being oppositely arranged, the locating support 300 to be relatively fixed plate 330；
C2, as shown in figure 13, the fixation ear 111 with soft mode 120 on the outside of firm template is installed on the locating support 300
In outermost one group of fixed plate 330, and on the outside of the firm template of the band soft mode 120 notch towards the outside of locating support 300；
C3, as shown in figure 14, the outside placement rib of soft mode 120 on the outside of with firm template, and the notch court of the rib
The side of soft mode 120 on the outside of with firm template；Oppositely positioned another rib again；
C4, as shown in figure 14, the fixation ear 111 of inner side soft mode 130 is installed in next group of fixed plate 330, and described
The flexible template side of inner side soft mode 130 is adjacent with soft mode 120 on the outside of firm template；
C5, as shown in figure 15, places rib on inner side soft mode 130, and the rib notch towards inner side soft mode 130
Side；Oppositely positioned another rib again；
C6, place on rib described without soft mode 140 on the outside of firm template and described without soft mode 140 on the outside of firm template
Notch towards the outside of locating support 300.
D, the covering die component and covering blank making step include：
D1, as shown in figure 16, making lower wall plate forming die 210, and in the lower covering template 214 of lower wall plate forming die 210
On mat formation covering blank；
D2, as shown in figure 17, making upper wall plate forming die 230, and in the upper covering template 235 of upper wall plate forming die 230
On mat formation covering blank.
E, the beam mould component and beam blank and covering die component and covering blank number of assembling steps include：
E1, as shown in figure 19, installation locating dowel 150, the positioning on the lower wall plate forming die 210 for covering blank of mating formation
The top of post 150 is provided with the mounting hole for fixing the fixed ear 111, and locating dowel 150 is arranged in pairs at least two groups；
E2, as shown in figure 20, the fixation ear 111 of soft mode 120 and inner side soft mode 130 on the outside of the firm template of the band is pacified respectively
Loaded in locating dowel 150, then unload locating support 300；
E3, as shown in figure 21, the installation support member 220 on the lower wall plate forming die 210；
E4, as shown in figure 22, the upper wall plate forming die 230 for covering blank of mating formation is installed on the another of the support member 220
One end.
Finally, will be arranged on the outermost of beam mould component without soft mode 140 on the outside of firm template, that is, with firm template outside
The opposite side of side soft mode 120；Encapsulate again and check vacuum system, vacuum must be reached below -0.88Bar, vacuum in 5 minutes
Leakage must not exceed 0.17Bar.Enter autoclave immediately and carry out curing process, after the solidification is complete disassembling fixture, you can from work
Load onto and remove part, realize the demoulding.
As shown in figure 23, beam mould component collectively forms blank with lower wall plate forming die 210 and upper wall plate forming die 230 and filled out
Fill region, the position of as final beam blank and covering blank.As shown in figure 24, it is A portions enlarged diagram in Figure 23, a is to cut
Face is in the rib of C fonts, and mutually privately combination is in an I-shaped beam blank to two rib openings, and beam blank connects with covering blank b
Connect, centre folder enhancement layer blank c realizes overall co-curing shaping.
Presently preferred embodiments of the present invention is the foregoing is only, is not intended to limit the invention, all essences in the present invention
Any modification, equivalent and improvement made within refreshing and principle etc., should be included within the scope of the present invention.
Claims (6)
1. a kind of making frock of many beam box section co-curing shaping enhancement layers of composite, it is characterised in that：Including enhancement layer
Make frock upper die body (610) and enhancement layer makes frock lower mold body (620), both include coplanar side, and the side
It is on-right angle that face is angled with enhancement layer institute.
2. the making frock of many beam box section co-curing shaping enhancement layers of composite according to claim 1, its feature
It is：The enhancement layer makes frock upper die body (610) and enhancement layer makes frock lower mold body (620) and is halfpace shape, and two
The homonymy inclined-plane difference of halfpace is coplanar.
3. the making frock of many beam box section co-curing shaping enhancement layers of composite according to claim 2, its feature
It is：During the two ends of the enhancement layer making frock upper die body (610) and enhancement layer making frock lower mold body (620) are portrayed
Line.
4. the making frock making using many beam box section co-curing shaping enhancement layers of composite described in claim 3 is strengthened
The technique of layer, it is characterised in that comprise the following steps：
F1, on a table top upper berth enhancement layer prepreg is folded, surplus is left in the both sides of the enhancement layer prepreg；
F2, strong layer prepreg is placed on the enhancement layer makes frock upper die body (610) and enhancement layer making frock lower mold body
(620) between, and clamping makes both inclined-planes coplanar；
F3, with knife close to enhancement layer make frock upper die body (610) and enhancement layer make frock lower mold body (620) inclined-plane cutting
Go out the oblique angle of enhancement layer prepreg；
F4, the enhancement layer made is placed between covering blank and beam blank.
5. the making frock making of many beam box section co-curing shaping enhancement layers of composite according to claim 4 is strengthened
The technique of layer, it is characterised in that：Surplus in the step F1 is 10-20mm.
6. the making frock making of many beam box section co-curing shaping enhancement layers of composite according to claim 4 is strengthened
The technique of layer, it is characterised in that：The step of also being alignd in the step F2 including center line：Enhancement layer is made into frock upper die body
(610) and enhancement layer make frock lower mold body (620) center line positioned in alignment.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201710296952.6A CN106945311A (en) | 2017-04-28 | 2017-04-28 | A kind of many beam box section co-curing shapings of composite make frock and manufacture craft with enhancement layer |
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| CN201710296952.6A CN106945311A (en) | 2017-04-28 | 2017-04-28 | A kind of many beam box section co-curing shapings of composite make frock and manufacture craft with enhancement layer |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112265288A (en) * | 2020-09-02 | 2021-01-26 | 长春长光宇航复合材料有限公司 | Preparation method of single-side reinforced structure carbon fiber composite material plate |
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| RU2057004C1 (en) * | 1993-03-19 | 1996-03-27 | Малое научно-производственное предприятие "АНХ" | Method of pipe cutting at angle |
| US20020031641A1 (en) * | 2000-02-25 | 2002-03-14 | The Boeing Company | Laminated composite radius filler |
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Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2057004C1 (en) * | 1993-03-19 | 1996-03-27 | Малое научно-производственное предприятие "АНХ" | Method of pipe cutting at angle |
| US20020031641A1 (en) * | 2000-02-25 | 2002-03-14 | The Boeing Company | Laminated composite radius filler |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112265288A (en) * | 2020-09-02 | 2021-01-26 | 长春长光宇航复合材料有限公司 | Preparation method of single-side reinforced structure carbon fiber composite material plate |
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Application publication date: 20170714 |