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CN107574569A - A kind of set of T-shaped threeway control of two-dimensional braided prefabricated component compiles method - Google Patents

A kind of set of T-shaped threeway control of two-dimensional braided prefabricated component compiles method Download PDF

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Publication number
CN107574569A
CN107574569A CN201710967883.7A CN201710967883A CN107574569A CN 107574569 A CN107574569 A CN 107574569A CN 201710967883 A CN201710967883 A CN 201710967883A CN 107574569 A CN107574569 A CN 107574569A
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CN
China
Prior art keywords
prefabricated component
dimensional braided
control
core
yarn
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201710967883.7A
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Chinese (zh)
Inventor
孙颖
丁许
刘俊岭
陈利
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Tianjin Polytechnic University
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Tianjin Polytechnic University
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Tianjin Polytechnic University filed Critical Tianjin Polytechnic University
Priority to CN201710967883.7A priority Critical patent/CN107574569A/en
Publication of CN107574569A publication Critical patent/CN107574569A/en
Pending legal-status Critical Current

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  • Braiding, Manufacturing Of Bobbin-Net Or Lace, And Manufacturing Of Nets By Knotting (AREA)

Abstract

The set that the present invention discloses a kind of T-shaped threeway control of two-dimensional braided prefabricated component compiles method and apparatus.The equipment that this set volume method uses is common vertical control of two-dimensional braided machine, core is moved in the predetermined direction using mechanical arm, and the set for completing prefabricated component is compiled.In the braiding preparatory stage, yarn is fixed on core around outside larger-diameter forming ring.Then according to product needs, suitable braid angle is selected to be woven with braiding structure.Method provided by the invention is simple, and obtained prefabricated component yarn is completely preferable.Method provided by the invention reduces the difficulty of control of two-dimensional braided manufacture complicated shape prefabricated component, improves production efficiency.

Description

A kind of set of T-shaped threeway control of two-dimensional braided prefabricated component compiles method
Technical field
The present invention relates to control of two-dimensional braided technology, specifically a kind of T-shaped prefabricated component integrally covers volume method and apparatus.
Background technology
Control of two-dimensional braided is with a long history, in 18 th Century Germans and French can manufacture control of two-dimensional braided machine.Control of two-dimensional braided machine one As be used to produce rope, band, the fabric such as pipe.The moulding process of control of two-dimensional braided machine relative maturity at present is straight in general etc. Footpath pipe can reach relevant art requirement using common two-dimentional circular knitting machine.With the development of composite, two dimension is compiled Knit technology and the effect to become more and more important is played in the development of composite.Substantial amounts of polymer matrix composites have used two-dimentional volume Technology is knitted, it has following main feature:1. the mechanization degree of control of two-dimensional braided is higher, production efficiency is high;And it is adapted to two dimension to compile The moulding process species of Woven composite also compares more.2. the designability of control of two-dimensional braided is stronger, it is straight that braid angle, mandrel can be changed Footpath and section etc. change the structure of prefabricated component.But the conventional sleeve of control of two-dimensional braided compiles method and has complicated shape and one for manufacture The prefabricated component for determining thickness is relatively difficult.Presently mainly complicated shape complicated shape and certain thickness pre- is manufactured with 3 D weaving Product, but 3 D weaving automaticity is low, braiding is difficult, low production efficiency.
The content of the invention
For the technology for existing control of two-dimensional braided, the technical problem that the present invention intends to solve is to provide a kind of T-shaped threeway The set of control of two-dimensional braided prefabricated component weaves into type method and apparatus.This method can not only realize cylindrical cross-section or other cross sectional shapes T-shaped threeway, the overall set of T-shaped four-way or T-shaped five prefabricated component such as logical compiles., can be with and yarn is not broken in prefabricated component Ensure the overall integrity of preform structure.
The technical scheme that the present invention solves methods described technical problem is to design a kind of set of T-type two-dimensional woven preform Volume method, equipment include conventional control of two-dimensional braided machine, mechanical commutation draft arm and forming ring, there is drawing-off regulation dress on mechanical arm Put.
The drawing-off regulation of core is realized by the mechanical arm in front of prefabricated component forming direction, passes through programming It can make mechanical arm that direction set in advance and speed are installed and drawing-off is carried out to core.
A kind of set of T-type two-dimensional woven tubular prefabricated component compiles method, comprises the following steps:
The first step:According to the performance requirement of product, suitable yarn is selected.
Second step:Measure the broadening of yarn tow, for coverage rate needed for reaching and surface density, according to the number of spindles of yarn with And fabric construction parameters, the core diameter of design.
3rd step:According to required product, T-shaped composite core formwork is formed with two tubular core molds.
4th step:With above-mentioned core in braiding woven preform.
5th step:After fabric reaches the required number of plies, prefabricated component is removed, two cores are separated, taking out core is It can obtain required T-shaped prefabricated component.
Compared with prior art, forming method of the invention and device can control core with specific by mechanical arm Direction and speed motion, prevent yarn to core on yarn in the presence of forming ring along forming ring radial outward expansion Motion, which is formed, to be hindered.The present invention has following technological merit:(1) forming ring is added on ordinary two dimensional braider, beneficial to control The motion of coremaking mould.(2) carry out reciprocal set by drawing-off core to compile, obtain the prefabricated component of required thickness, and the yarn in prefabricated component Line splits, so the globality of prefabricated component is preferable without fracture.(3) compared to three-dimensional weaving method, technique is simple, easy making process, raw It is low to produce cost.
Brief description of the drawings
Fig. 1 is the schematic device being related in the embodiment of the present invention.
Fig. 2 is the side view of control of two-dimensional braided equipment in the embodiment of the present invention.
Fig. 3 is to weave process schematic in the embodiment of the present invention.
Fig. 4 is to weave process schematic in the embodiment of the present invention.
Fig. 5 is to weave process schematic in the embodiment of the present invention.
Fig. 6 is to weave process schematic in the embodiment of the present invention.
Fig. 7 is to weave process schematic in the embodiment of the present invention.
Fig. 8 is to weave process schematic in the embodiment of the present invention.
Label declaration:1- mechanical arms, 2- drawing-off fixtures, 3- yarns, 4- forming rings, 5- spindles, 6- cores, 7- looms bottom Disk.
Embodiment
The present invention is further described with reference to example and accompanying drawing.
The set for the T-shaped threeway control of two-dimensional braided prefabricated component that the present invention designs compiles method, after product demand selection yarn Carry out corresponding technology Calculation, from wider tow yarn when (yarn linear density selected here is consistent), in other conditions In the case of consistent, same equipment can weave larger sized prefabricated component.
Technology Calculation:Here T-shaped prefabricated component is tubulose (figure), and the diameters of two cylindric cores is all mutually R, yarn 3 Broadening be w, line density t, braid angle θ, the number of spindle unit of braider knitting yarn is m, and axle yarn is n, is generally woven The quantity of arbor yarn is the half of knitting yarn, then in theory and coverage rate as big as possible in core preferably when core diameter For:
If product requirement, using surface density ρ as basic principle, core is a diameter of:
Then the flower byte wide f of fabric construction is:
Then the stitch length h of fabric construction is:
Carry out weaving preceding preparation, after being ready to complete, start to weave by the technological parameter calculated.
The A ends (such as Fig. 3) that mechanical arm 1 first starts drawing-off core 6 take up one's knitting, and the direction of arrow is the motion side of core 6 To, when being woven into D ends, mechanical arm 1 adjusts the direction of core 6 and starts drawing-off D ends (such as Fig. 4), when being woven into B ends, machinery Arm 1 adjusts the direction of core 6 and starts drawing-off B ends (such as Fig. 5);When being woven into D ends again, mechanical arm 1 adjusts the direction of core 6 and opened Beginning drawing-off A ends (such as Fig. 6), when being woven into C-terminal, mechanical arm 1 adjusts the direction of core 6 and starts drawing-off C-terminal (such as Fig. 7), works as volume When knitting A ends, the once set for now completing prefabricated component is compiled, and set, which is organized on core, every time forms two-layer fabrics.If necessary to more The prefabricated component of more numbers of plies, repeat above step.

Claims (4)

1. a kind of set of T-shaped threeway control of two-dimensional braided prefabricated component compiles method, it is characterised in that conventional control of two-dimensional braided machine is used, into The overall set that type ring and mechanical arm complete T-shaped threeway prefabricated component is compiled.
2. the set of the T-shaped threeway control of two-dimensional braided prefabricated component according to right 1 compiles method, it is characterised in that this forming ring it is straight Footpath is greater than the full-size of core, and yarn is bypassed outside forming ring and is attached on core.
3. the set of the T-shaped threeway control of two-dimensional braided prefabricated component according to right 1 compiles method, it is characterised in that mechanical arm can change Become the direction of motion of core, carry out reciprocal set and compile, yarn is not broken in prefabricated component.
4. the set of the T-shaped threeway control of two-dimensional braided prefabricated component according to right 1 compiles method, it is characterised in that selects wider tow Yarn, in the case where other conditions are consistent, same equipment can weave larger sized prefabricated component.
CN201710967883.7A 2017-10-17 2017-10-17 A kind of set of T-shaped threeway control of two-dimensional braided prefabricated component compiles method Pending CN107574569A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710967883.7A CN107574569A (en) 2017-10-17 2017-10-17 A kind of set of T-shaped threeway control of two-dimensional braided prefabricated component compiles method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710967883.7A CN107574569A (en) 2017-10-17 2017-10-17 A kind of set of T-shaped threeway control of two-dimensional braided prefabricated component compiles method

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CN107574569A true CN107574569A (en) 2018-01-12

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114643725A (en) * 2020-12-21 2022-06-21 中国航发商用航空发动机有限责任公司 Manufacturing method of composite casing and composite casing

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3843488A1 (en) * 1988-12-23 1990-07-05 Ver Foerderung Inst Kunststoff Winding apparatus and winding process
JPH05302253A (en) * 1992-04-20 1993-11-16 Murata Mach Ltd Braider for braid structure
US5388497A (en) * 1990-08-25 1995-02-14 Murata Kikai Kabushiki Kaisha Braided structure forming apparatus
JPH07189096A (en) * 1993-12-27 1995-07-25 Murata Mach Ltd Braider
JPH07216701A (en) * 1994-02-07 1995-08-15 Murata Mach Ltd Braider
WO2012083921A1 (en) * 2010-12-20 2012-06-28 Eads Deutschland Gmbh Method and device for producing a ceramic composite material

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3843488A1 (en) * 1988-12-23 1990-07-05 Ver Foerderung Inst Kunststoff Winding apparatus and winding process
US5388497A (en) * 1990-08-25 1995-02-14 Murata Kikai Kabushiki Kaisha Braided structure forming apparatus
JPH05302253A (en) * 1992-04-20 1993-11-16 Murata Mach Ltd Braider for braid structure
JPH07189096A (en) * 1993-12-27 1995-07-25 Murata Mach Ltd Braider
JPH07216701A (en) * 1994-02-07 1995-08-15 Murata Mach Ltd Braider
WO2012083921A1 (en) * 2010-12-20 2012-06-28 Eads Deutschland Gmbh Method and device for producing a ceramic composite material

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114643725A (en) * 2020-12-21 2022-06-21 中国航发商用航空发动机有限责任公司 Manufacturing method of composite casing and composite casing
CN114643725B (en) * 2020-12-21 2024-04-26 中国航发商用航空发动机有限责任公司 Manufacturing method of composite casing and composite casing

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Application publication date: 20180112