CN104723579B - Assembling mold for all-composite corrugated sandwich cylindrical shells - Google Patents
Assembling mold for all-composite corrugated sandwich cylindrical shells Download PDFInfo
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- CN104723579B CN104723579B CN201510172294.0A CN201510172294A CN104723579B CN 104723579 B CN104723579 B CN 104723579B CN 201510172294 A CN201510172294 A CN 201510172294A CN 104723579 B CN104723579 B CN 104723579B
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- bar body
- core bar
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- side core
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Classifications
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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
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
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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
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/42—Moulds or cores; Details thereof or accessories therefor characterised by the shape of the moulding surface, e.g. ribs or grooves
-
- 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
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Insertion Pins And Rivets (AREA)
- Laminated Bodies (AREA)
Abstract
The invention discloses an assembling mold for all-composite corrugated sandwich cylindrical shells and relates to the assembling mold with an aim to overcome shortcomings about lack of special mold during production of existing all-composite corrugated sandwich cylindrical shells, skins and plates are not easy to be connected during production of other sandwich cylindrical shell, filament winding cannot be avoided, and the production process is complicated and not easy to for mass production. A core column is a split-type hollow column, two end caps are respectively detachably connected to the top surface and the bottom surface of the core column, multiple inner core strips and multiple outer core strips are alternatively arranged on the outer periphery of the core column along the axial direction of the core column, each inner core strip and each outer core strip are arranged at an interval, and a clamping fixture sleeves the core column provided with the inner core strips and the outer core strips. The cylindrical shells different in thickness can be produced, and mass production can be realized. The assembling mold is used for production of the all-composite corrugated sandwich cylindrical shells.
Description
Technical field
Present invention relates particularly to a kind of assembling die of full composite material ripple Cylindrical Sandwich Shells.
Background technology
With the development of Aeronautics and Astronautics and each engineering field, structure lightened design is particularly important, sandwich structure tool
The mechanical property for having higher specific strength, specific modulus etc. outstanding, is that grid adds currently used for the cylindrical shell of large space structure mostly
Muscle structure, including without skinned mesh reinforced structure, inside panel grid reinforced structure, exterior skin grid reinforced structure, interior exterior skin
Grid reinforced structure, its complicated process of preparation, for Composite Cylindrical Shell, are difficult to realize the effectively connection of eyelid covering and panel.
For Stiffened cylindrical shell, its more ripe technique is mainly carbon fiber winding technique and post forming
Technique.Pressure stochastic distribution can realize the mass of component and automated production, but the reinforcement that fiber winding is prepared is justified
Post shell has some shortcomings, such as cellosilk is continuous laying winding on mould, then necessarily deposit in rib infall
In the overlap of fiber, the fibre weight of non crossover point part is caused to have very big difference with the fibre weight of cross point part so that non-
The fiber volume fraction of zone of intersection reinforcement is less than 50%.In addition all there is molded body with mould when fiber winds and solidifies
Directly contact, inevitably causes the damage of product during the curing molding demoulding.At present, for prepared grid reinforcement is multiple
Rib of the condensation material cylindrical shell in the hand of spiral, its modulus are about the 80% of traditional unidirectional composite material, and compressive strength is reduced to
The 40% of only traditional unidirectional composite material.Secondary curing molding is also to carry out on the basis of fiber winding technology, therefore
This technique has the shortcomings that to avoid fiber from winding.
For pyramid dot matrix structure, its preparation technology is more complicated, cannot winding core using carbon fiber winding technology
Shape.Also there is the exploration of some time with regard to the people that prepare of lattice structure, spell including rod member packaging technology, Water Cutting single pole
Technique, Water Cutting interlocking packaging technology is connect, is interted weaving, RTM mold technique etc., but is all difficult to structure mass
Automatically producing, and prepare large-scale component has very big difficulty.Also scholar starts out prepreg integral forming process and prepreg
Secondary forming process and interlocking packaging technology, wherein interlocking packaging technology are built upon on grid basis, are to realize golden word
High-strength aluminum alloy is selected in the mass production of tower dot matrix cylindrical shell structure, its core material, with wire cutting mass production aluminum
Alloy lattice fuse, eyelid covering are composite, using circular dies pressure sintering molding.Using the connection side being glued between the core of face
Formula, inside and outside panel connect rear stick carbon fiber piece and reinforced sheet to make up the defect of structure.
The content of the invention
It is an object of the invention to provide a kind of assembling die of full composite material ripple Cylindrical Sandwich Shells, to solve existing system
Lack special mould during standby full composite material ripple Cylindrical Sandwich Shells, be difficult to realize eyelid covering dough-making powder using existing during other moulds
The effectively connection of plate, the shortcoming that cannot avoid fiber winding, complicated process of preparation are difficult to the problem of mass production.
The present invention is adopted the technical scheme that for solving above-mentioned technical problem:
Scheme one:A kind of assembling die of full composite material ripple Cylindrical Sandwich Shells, it include stem stem, matched moulds fixture, two
Individual end cap, multiple interior side core bar bodies and multiple outboard wick bar bodies, the stem stem is split-type hollow cylinder, described two end caps point
Top surface and the bottom surface of stem stem be not detachably connected on, the axial direction of multiple interior side core bar bodies and multiple outboard wick bar bodies along stem stem
It is arranged alternately on the excircle of stem stem, between the outboard wick bar body that side core bar body is adjacent in each, gap is arranged, described
Matched moulds fixture is cylindrical shape, and the matched moulds fixture is sleeved on the stem stem with multiple interior side core bar bodies and multiple outboard wick bar bodies
On, the inwall of the matched moulds fixture is arranged with interior side core bar body space, and inwall and the outboard wick bar body phase of the matched moulds fixture are pasted
Tightly.
Scheme two:A kind of assembling die of full composite material ripple Cylindrical Sandwich Shells, it includes stem stem, matched moulds fixture and two
Individual end cap, the stem stem are split-type hollow cylinder, and the outer surface of the stem stem is the curved surface of the radially uniform convex-concave in direction,
The shape of the matched moulds fixture inwall is arranged with the symmetrical shape of the outer surface of stem stem, and described two end caps are detachably connected respectively
In top surface and the bottom surface of stem stem, the matched moulds fixture is sleeved on outside stem stem.
Present invention beneficial effect compared with prior art:
1st, the present invention is the assembling die for preparing full composite material ripple Cylindrical Sandwich Shells, and the present invention includes two sides
Case, scheme one are longitudinal combination mould, in scheme one two end caps be disposed to it is solid respectively from the top surface of stem stem and bottom surface
Determine the basic structure of stem stem, prevent the stem stem of split-type from shifting because lacking stable fixing component, it is ensured that core column structure
Stablize indeformable;The arrangement mode of multiple interior side core bar bodies and multiple outboard wick bar bodies on stem stem effectively realizes that longitudinal convex-concave rises
The ripple struction of volt, prepreg is put between interior side core bar body and outboard wick bar body, so that prepreg is integrally formed to be formed
Longitudinal ripple fuse.Being disposed to of matched moulds fixture clamps and fixed stem stem, prepreg, multiple interior side core bar bodies and multiple outer
Side core bar body.
2nd, in the present invention, scheme two is ring assembling die, and in scheme two, two end caps is disposed to from the top of stem stem
Face and bottom surface fix the basic structure of stem stem respectively, and matched moulds fixture is to pressurize and fix all in which to prepreg molding
Internal component parts.
3rd, the present invention omits the step of fiber winding prepares full composite material ripple Cylindrical Sandwich Shells used in traditional handicraft,
The step of effectively prevent ups and downs ripple struction and be difficult to fiber and wind, the longitudinal wave for finishing will be prepared with pressure sintering
Stricture of vagina fuse and panel form full composite material longitudinal ripple Cylindrical Sandwich Shells by linking together by the way of being glued, together
Reason, ring ripple fuse dough-making powder plate form full composite material longitudinal ripple interlayer circle by linking together by the way of being glued
Post shell.
4th, present invention process is realized simply, and operation is simple and motility strong, by interior side core bar body and outboard wick
Add processing release paper between bar body or silica gel piece can prepare the cylindrical shell thinner than preset clearance, can so pass through one set of die
Prepare the different cylindrical shell of thickness.
5th, in the present invention, the fuse prepared and panel splicing area can be controlled, so as to realize the effective of fuse and panel
Connection, makes the annexation of the two stably firm.
6th, the present invention is cheap for manufacturing cost, is capable of achieving mass production.
Description of the drawings
Fig. 1 is the stereochemical structure installation diagram of scheme one,
Fig. 2 is the overlooking the structure diagram in scheme one without end cap 5,
Fig. 3 is the overlooking the structure diagram of interior side core bar body 2,
Fig. 4 is the left view structural representation of Fig. 3,
Fig. 5 is the overlooking the structure diagram of outboard wick bar body 3,
Fig. 6 is the left view structural representation of Fig. 5,
Fig. 7 is the main structure diagram of stem stem 1 in scheme one,
Fig. 8 is the overlooking the structure diagram of stem stem 1 in scheme one,
Fig. 9 is the overlooking the structure diagram of matched moulds fixture 4 in scheme one,
Figure 10 is the stereochemical structure installation diagram of scheme two,
Figure 11 is the main structure diagram of stem stem 1 in scheme two,
Figure 12 is the overlooking the structure diagram of stem stem 1 in scheme two,
Figure 13 is the overlooking the structure diagram of matched moulds fixture 4 in scheme two,
Figure 14 is the overlooking the structure diagram of end cap 5,
Figure 15 is the main structure diagram of panel mold.
Specific embodiment
Specific embodiment one:This reality is illustrated with reference to Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6, Fig. 7, Fig. 8, Fig. 9 and Figure 14
Mode is applied, it includes stem stem 1,4, two end caps 5 of matched moulds fixture, multiple interior side core bar bodies 2 and multiple outsides in present embodiment
Core bar body 3, the stem stem 1 be split-type hollow cylinder, described two end caps 5 be detachably connected on respectively stem stem 1 top surface and
Bottom surface, multiple interior side core bar bodies 2 and multiple outboard wick bar bodies 3 are arranged alternately the excircle in stem stem 1 along the axial direction of stem stem 1
On, between the outboard wick bar body 3 that side core bar body 2 is adjacent in each gap arrange, the matched moulds fixture 4 be cylindrical shape, institute
State matched moulds fixture 4 to be sleeved on the stem stem 1 with multiple interior side core bar bodies 2 and multiple outboard wick bar bodies 3, the matched moulds fixture 4
Inwall arrange with interior 2 gap of side core bar body, inwall and the outboard wick bar body 3 of the matched moulds fixture 4 are mutually adjacent to.Present embodiment
Middle stem stem 1 is split-type hollow cylinder, and every lobe during use in stem stem 1 is marked to easily facilitate and smoothly assembled.
Specific embodiment two:Present embodiment, core described in present embodiment are illustrated with reference to Fig. 2, Fig. 7, Fig. 8 and Figure 14
The top surface of post 1 and bottom surface are machined with end cap connecting hole 1-1 respectively;On the outer surface of the stem stem 1, radially direction processing is equal
Even being machined with ranked first core bar connecting hole 1-2 more.In present embodiment, end cap connecting hole 1-1 is to realize stem stem 1 and end cap 5
Connection;Being disposed to of first core bar connecting hole 1-2 realizes stem stem 1 with multiple interior side core bar bodies 2, multiple outboard wick bar bodies
3 connection.Also it is machined with end cap 5 in present embodiment and corresponds the connecting hole for arranging with end cap connecting hole 1-1, using spiral shell
End cap 5 and stem stem 1 are detachably connected by nail, so as to realize 1 effectively connection of end cap 5 and stem stem, it is ensured that the basic structure of stem stem 1
Frame.Other NM compositions and annexation are identical with specific embodiment one.
Specific embodiment three:Present embodiment is illustrated with reference to Fig. 1, Fig. 3 and Fig. 4, when interior side core bar in present embodiment
When body 2 is vertically placed, the cross section in the horizontal direction of interior side core bar body 2 is trapezoidal, is machined with and core on the interior side core bar body 2
The second core bar connecting hole 2-1 that the first core bar connecting hole 1-2 on post 1 is correspondingly arranged, when interior side core bar body 2 passes through the second core bar
When connecting hole 2-1 is detachably connected on stem stem 1, on interior side core bar body 2, the end face width close with stem stem 1 is to away from stem stem
1 other end taper in width.Interior 2 end face width of side core bar body in present embodiment on side core bar body 2 near 1 side of stem stem
Spend to the interior 2 end face taper in width of side core bar body away from 1 side of stem stem.The two ends of interior side core bar body 2 be machined with respectively one it is recessed
Platform, is machined with the second core bar connecting hole 2-1 in the plane that concave station is located, second core of the side core bar body 2 by its two ends in each
Bar connecting hole 2-1 realizations are stably connected with and dismantlement work with stem stem 1.Other NM compositions and annexation and concrete reality
Apply mode one identical with two.
Specific embodiment four:Present embodiment, outboard wick bar body 3 in present embodiment are illustrated with reference to Fig. 1, Fig. 5 and Fig. 6
Structure and interior side core bar body 2 symmetrical configuration arrange, be machined with the outboard wick bar body 3 and the first core bar on stem stem 1
The 3rd core article connecting hole 3-1 that connecting hole 1-2 is correspondingly arranged, when outboard wick article body 3 by the 3rd core article connecting hole 3-1 it is detachable
When being connected on stem stem 1, end face width close with stem stem 1 on outboard wick bar body 3 is to the other end width away from stem stem 1
Flaring.3 end face width of outboard wick bar body in present embodiment on outboard wick bar body 3 near 1 side of stem stem is to away from stem stem 1 one
The 3 end face width flaring of outboard wick bar body of side.3 cross section of outboard wick bar body is trapezoidal, and the two ends of each outboard wick bar body 3 may be used also
It is machined with boss, the width of the top surface width of boss less than the end face being adjacent to prepreg 6 on outboard wick bar body 3, when will be many
When individual interior side core bar body 2 is arranged on stem stem 1 one by one, embedded groove, outboard wick bar between two neighboring interior side core bar body 2, is formed
Body 3 is detachably connected in embedded groove, meanwhile, the concave station of interior side core bar body 2 is located at same circle with the boss of outboard wick bar body 3
On side face.Other NM compositions and annexation are identical with specific embodiment three.
Specific embodiment five:With reference to Fig. 1 and Fig. 9 explanation present embodiments, matched moulds fixture described in present embodiment 4 is
Split type fixture, the matched moulds fixture 4 include the first semi arch composition lamellar body 4-1 and the second semi arch composition lamellar body 4-2, described
It is detachably connected between first semi arch piece 4-1 and the second semi arch piece 4-2, the matched moulds fixture 4 also adds including four auxiliary
Press strip body 4-3, two auxiliary pressurized bar body 4-3 in four auxiliary pressurizeds bar body 4-3 are collinear to be arranged on the first semi arch
Outside piece 4-1, another two auxiliary pressurized bar body 4-3 in four auxiliary pressurizeds bar body 4-3 is collinear to be arranged on the second semi arch
Outside piece 4-2.In present embodiment, auxiliary pressurized bar body 4-3 is the bonding jumper for being drilled with bolt hole, due to interior side core bar body 2, outside
Core bar body 3 still has portion of material to expose after pressing, and for further giving mould pressurizing, needs outside matched moulds mould.First
The both sides external of semi arch piece 4-1 and the second semi arch piece 4-2 is respectively burn-on two bonding jumpers for being drilled with bolt hole, is easy to matched moulds mould
The fixation of tool and give whole model pressurization.The matched moulds fixture 4 being arranged such is easily installed and dismantles, it is to avoid to the multiple of its inside
Interior side core bar body 2, multiple outboard wick bar bodies 3, prepreg 6 and stem stem 1 are impacted.Other NM compositions and annexation
It is identical with specific embodiment one and four.
Specific embodiment six:Present embodiment is illustrated with reference to Fig. 8, the lobe number of stem stem 1 described in present embodiment is 4
It is individual.Prove through multiple sampling test, when the lobe number of stem stem 1 is less than 4, after preparation finishes fuse, stem stem 1 is difficult to take
Go out, when the lobe number by stem stem 1 is set to 4, stem stem 1 smoothly can take out, convenient and efficient.Other NM compositions and connection
Relation is identical with specific embodiment one and two.
The course of work of scheme one is illustrated with reference to specific embodiment one to six:
First, will be including stem stem 1,4, two end caps 5 of matched moulds fixture, multiple interior side core bar bodies 2 and multiple outboard wick bar bodies 3
Upper uniform application releasing agent, multiple interior side core bar bodies 2 are arranged on stem stem 1, and the prepreg 6 for finishing cutting again is overall to be spread
It is located at outside multiple interior side core bar bodies 2, by each outboard wick bar body 3 being sequentially arranged at its corresponding two neighboring interior side core bar body
Between 2, the extruding to prepreg 6 is realized, prepreg 6 is adjacent in embedded groove, matched moulds is carried out with matched moulds fixture 4, placed
In hot press, grinding process after temperature-pressure, is carried out again, you can overall to obtain longitudinal cylindrical shell fuse, finally preparation is finished
Panel be glued on the inside and outside circle side face of longitudinal cylindrical shell fuse respectively full composite material ripple Cylindrical Sandwich Shells be obtained.
Specific embodiment seven:Present embodiment, present embodiment are illustrated with reference to Figure 10, Figure 11, Figure 12, Figure 13 and Figure 14
In it includes stem stem 1, matched moulds fixture 4 and two end caps 5, the stem stem 1 is split-type hollow cylinder, the appearance of the stem stem 1
Face is the curved surface of the radially uniform convex-concave in direction, the shape pair of the shape of 4 inwall of matched moulds fixture and the outer surface of stem stem 1
Claim to arrange, described two end caps 5 are detachably connected on the top surface of stem stem 1 and bottom surface respectively, and the matched moulds fixture 4 is sleeved on stem stem
Outside 1.In present embodiment, stem stem 1 is split-type hollow cylinder, every lobe during use in stem stem 1 mark easily facilitate it is smooth
Assembling.
Specific embodiment eight:With reference to Figure 11 and Figure 12 explanation present embodiments, the top of stem stem 1 described in present embodiment
Face and bottom surface are machined with end cap connecting hole 1-1 respectively.In present embodiment, end cap connecting hole 1-1 is to realize stem stem 1 with end
The connection of lid 5;Also it is machined with end cap 5 and corresponds the connecting hole for arranging with end cap connecting hole 1-1, using screw by end cap 5
It is detachably connected with stem stem 1, so as to realize 1 effectively connection of end cap 5 and stem stem, it is ensured that the basic boom of stem stem 1.Other are not
The composition and annexation for referring to is identical with specific embodiment seven.
Specific embodiment nine:Present embodiment, stem stem described in present embodiment are illustrated with reference to Figure 10, Figure 11 and Figure 12
1 lobe number is 6.Prove through multiple sampling test, when the lobe number of stem stem 1 is less than 6, after preparation finishes fuse, core
Post 1 is not easily taken out, and when the lobe number by stem stem 1 is set to 6, stem stem 1 smoothly can take out, convenient and efficient.Other are NM
Composition and annexation are identical with specific embodiment seven and eight.
Specific embodiment ten:Present embodiment is illustrated with reference to Figure 13, matched moulds fixture described in present embodiment 4 is split
Formula fixture, the matched moulds fixture 4 include the first semi arch composition body 4-1, the second semi arch composition lamellar body 4-2, the first inner lining plate
It is detachably connected between 4-4 and the second inner lining plate 4-5, the first semi arch piece 4-1 and the second semi arch piece 4-2, in first
Liner 4-4 is fixedly connected on the inwall of the first semi arch composition lamellar body 4-1, and the second inner lining plate 4-5 is fixedly connected on the second half
On the inwall of circular arc composition lamellar body 4-2, it is outer with stem stem 1 that the first inner lining plate 4-4 and the second inner lining plate 4-5 closes the shape to be formed
The symmetrical shape on surface is arranged.
Matched moulds fixture described in present embodiment 4 also includes four auxiliary pressurized bar body 4-3, four auxiliary pressurized bars
Two auxiliary pressurized bar body 4-3 in body 4-3 are collinear to be arranged on outside the first semi arch piece 4-1, four auxiliary pressurizeds bar body
Another two auxiliary pressurized bar body 4-3 in 4-3 is collinear to be arranged on outside the second semi arch piece 4-2.Auxiliary pressurized bar body 4-3 is to be drilled with
The bonding jumper of bolt hole, the inwall of the matched moulds fixture 4 are engaged setting with the outer surface of stem stem 1, and being arranged such can be to pre-
6 pressurization of leaching material molding, after completing prepreg, all material is all an exposure to outside, needs to encase compacting with matched moulds mould 4
Molding.Respectively burn-on two metals for being drilled with bolt hole in the both sides external of the first semi arch piece 4-1 and the second semi arch piece 4-2
Bar, is easy to the fixation of matched moulds mould 4 and pressurizes to whole model.The matched moulds fixture 4 being arranged such is easily installed and dismantles, it is to avoid
The prepreg 6 and stem stem 1 of its inside are impacted.Other NM compositions and annexation and nine phase of specific embodiment
Together.
Specific embodiment 11:Present embodiment is illustrated with reference to Figure 15, scheme one and scheme in present embodiment, is prepared
Panel used in two is also adopted by special mould, and its concrete structure is:It includes three semi arch cylinders 7 and two fixations
Block 8 and two panel end caps, leave 1mm gaps in the middle of two neighboring semi arch cylinder in three semi arch cylinders 7;Two solid
Determine block 8 and be placed on panel mold both sides, prevent mould from rocking, affect operation.The top surface of each semi arch cylinder 7 and bottom surface are along its axle
The first screwed hole is machined with to direction, for installing panel end cap, 9 the second screwed holes on panel end cap, is machined with, from
And realize the positioning work of three semi arch cylinders 7.Other NM compositions and annexation and specific embodiment one and
Seven is identical.
The course of work of scheme two is illustrated with reference to specific embodiment seven to ten:
First, will be including uniform application releasing agent on stem stem 1,4, two end caps 5 of matched moulds fixture, by stem stem 1 and two ends
Lid 5 is attached, and the prepreg 6 for secondly finishing cutting is overall to be laid on outside stem stem 1, carries out matched moulds with matched moulds fixture 4 again,
It is placed in hot press, after temperature-pressure, carries out grinding process again, you can be overall to obtain ring cylindrical shell fuse, will finally prepares
The panel for finishing is respectively adhered on the inside and outside circle side face of ring cylindrical shell fuse and full composite material ripple interlayer circle is obtained
Post shell.
Claims (3)
1. a kind of assembling die of full composite material ripple Cylindrical Sandwich Shells, it includes stem stem (1), matched moulds fixture (4), two ends
Lid (5), multiple interior side core bar body (2) and multiple outboard wick bar bodies (3), described stem stem (1) be split-type hollow cylinder, described two
Individual end cap (5) are detachably connected on the top surface of stem stem (1) and bottom surface, multiple interior side core bar body (2) and multiple outboard wick bars respectively
Body (3) is arranged alternately on the excircle of stem stem (1) along the axial direction of stem stem (1), and in each, side core bar body (2) is adjacent
Outboard wick bar body (3) between gap arrange, described matched moulds fixture (4) be cylindrical shape, matched moulds fixture (4) are sleeved on and carry
On the stem stem (1) of multiple interior side core bar body (2) and multiple outboard wick bar bodies (3), inwall and the interior side core of matched moulds fixture (4)
Bar body (2) gap is arranged, and inwall and outboard wick bar body (3) of matched moulds fixture (4) are mutually adjacent to, the top surface of stem stem (1)
End cap connecting hole (1-1) is machined with respectively with bottom surface;On the outer surface of stem stem (1), radially direction processing is uniform processes
Have and ranked first core bar connecting hole (1-2) more, it is characterised in that:When interior side core bar body (2) vertically place, interior side core bar body (2)
Cross section in the horizontal direction is trapezoidal, is machined with and the first core bar connecting hole on stem stem (1) on interior side core bar body (2)
(1-2) the second core bar connecting hole (2-1) being correspondingly arranged, when interior side core bar body (2) by the second core bar connecting hole (2-1) it is removable
Unload when being connected on stem stem (1), on interior side core bar body (2), the end face width close with stem stem (1) is to away from the another of stem stem (1)
End face taper in width, the structure of outboard wick bar body (3) are arranged with the symmetrical configuration of interior side core bar body (2), the outboard wick bar
The 3rd core article connecting hole (3-1) being correspondingly arranged with the first core article connecting hole (1-2) on stem stem (1) is machined with body (3), when
When outboard wick article body (3) is detachably connected on stem stem (1) by the 3rd core article connecting hole (3-1), in outboard wick bar body (3) with
The close end face width of stem stem (1) is to the other end width flaring away from stem stem (1).
2. the assembling die of a kind of full composite material ripple Cylindrical Sandwich Shells according to claim 1, it is characterised in that:Institute
Matched moulds fixture (4) is stated for split type fixture, described matched moulds fixture (4) include the first semi arch composition lamellar body (4-1) and the second half
Circular arc composition lamellar body (4-2), can between first semi arch composition lamellar body (4-1) and the second semi arch composition lamellar body (4-2)
Dismounting connection, matched moulds fixture (4) also include four auxiliary pressurizeds bar body (4-3), four auxiliary pressurizeds bar body (4-3)
In two auxiliary pressurizeds bar body (4-3) it is collinear be arranged on the first semi arch composition lamellar body (4-1) outward, four auxiliary pressurizeds
Collinear second semi arch that is arranged on of another two auxiliary pressurized bar body (4-3) in bar body (4-3) constitutes lamellar body (4-2) outward.
3. the assembling die of a kind of full composite material ripple Cylindrical Sandwich Shells according to claim 1, it is characterised in that:Institute
The lobe number for stating stem stem (1) is 4.
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CN201510172294.0A CN104723579B (en) | 2015-04-13 | 2015-04-13 | Assembling mold for all-composite corrugated sandwich cylindrical shells |
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CN201510172294.0A CN104723579B (en) | 2015-04-13 | 2015-04-13 | Assembling mold for all-composite corrugated sandwich cylindrical shells |
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CN105172160A (en) * | 2015-07-14 | 2015-12-23 | 哈尔滨工业大学 | Preparing method for composite material periodic truss structure |
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