CN105881930A - Forming device and forming method of I-shaped part - Google Patents

Forming device and forming method of I-shaped part Download PDF

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Publication number
CN105881930A
CN105881930A CN201610203906.2A CN201610203906A CN105881930A CN 105881930 A CN105881930 A CN 105881930A CN 201610203906 A CN201610203906 A CN 201610203906A CN 105881930 A CN105881930 A CN 105881930A
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CN
China
Prior art keywords
work
main body
frock
position block
font
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.)
Granted
Application number
CN201610203906.2A
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Chinese (zh)
Other versions
CN105881930B (en
Inventor
闫恩玮
武彬彬
王莹
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.)
AVIC Xian Aircraft Industry Group Co Ltd
Original Assignee
AVIC Aircraft Corp Xian Aircraft Branch
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 AVIC Aircraft Corp Xian Aircraft Branch filed Critical AVIC Aircraft Corp Xian Aircraft Branch
Priority to CN201610203906.2A priority Critical patent/CN105881930B/en
Publication of CN105881930A publication Critical patent/CN105881930A/en
Application granted granted Critical
Publication of CN105881930B publication Critical patent/CN105881930B/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/342Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44Shaping 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/30Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076Aircrafts

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Road Paving Machines (AREA)
  • Road Signs Or Road Markings (AREA)

Abstract

The invention provides a forming device and a forming method of an I-shaped part. The forming device comprises a tooling main body shaped like the Chinese character ji, a locating stop block and a non-metal pressure pad, wherein the tooling main body is placed at the bottom layer. The forming method comprises the steps of firstly, paving one C-shaped structure part of the I-shaped part on the surface of the tooling main body; then, fixing the locating stop block to two side lugs of the tooling main body for paving and locating the upper and lower edge surfaces of the I-shaped part; and finally, putting the non-metal pressure pad in a groove of another C-shaped structure of the I-shaped part for tightly pressing the part and uniformly transferring pressure. According to the forming device and the forming method, the structure of a tooling is simple, the manufacturing cost of the part is low, the same tooling is utilized in the paving and curing processes, after curing, the demolding is convenient, and the part is not damaged due to demolding.

Description

The shaped device of a kind of " work " font part and forming method
Technical field
The present invention relates to composite and manufacture " work " font in field, particularly aviation aircraft The shaped device of part and method.
Background technology
Owing to there is the features such as specific strength, specific modulus height, lightweight, corrosion resistance and good, closely Nian Lai, composite material parts is obtained in fields such as Aeronautics and Astronautics, boats and ships, automobile makings Extensively application.
Having benefited from the comprehensive mechanical property of its excellence, " work " font part is aviation aircraft neck Composite material parts version relatively conventional in territory, specifically includes " work " font reinforcement wall Plate, " work " font stringer, " work " font beam, " work " font reinforcement, " work " font rib Deng." work " font part typically can be subdivided into 6 ingredients (such as Fig. 1), including 2 Individual " C " type part, lower edge face, upper limb face and 2 Zone R implants.Manufactured at part Journey needs each ingredient of independent paving, and it is assembled together accurately, compress sturdy.
For ensureing its serviceability, axis degree and internal soundness to " work " font part all have The strictest regulation.This just requires in the fabrication process, it is necessary to control two " C " type portions That divides is accurately positioned and the most involutory;Further, each several part of " work " font part is combining Cheng Hou, it is necessary to assure its relative position is constant in bag and solidification process, and this is to shaped device Design and manufacture be proposed extremely harsh requirement.
Complicating with in the Enlargement Tendency at composite, " work " font part is at aviation flight Importance and range in device field constantly increase.Large scale, variable cross-section, Varying-thickness " work " font part is on the increase, and design and user require increasingly stringent, therefore, and Yi Zhongneng Enough axis degree ensureing " work " font part, overall dimensions and internal soundness, use simple, Reliably, pressure conduction is uniform, the shaped device being convenient in demoulding and method, its important type do not say and Analogy.
Summary of the invention
In order to solve the most right of 2 " C " type parts during " work " font forming parts Connect problem, the invention provides shaped device and the forming method of one " work " font part.
The shaped device of a kind of " work " font part, including " several " type frock main body, location Block, non-metallic pressure pad, frock main body is placed in bottom, " C " of " work " font part Type structure division paving is in frock body surfaces;Frock main body two is picked up the ears and the phase of position block Answering position to be provided with hole, location, position block is fixed on frock main body two picks up the ears, for paving Upper and lower edge face with location " work " font part;Non-metallic pressure pad is placed in " work " font In the groove of another " C " type structure of part, for compressing component and uniformly transfer pressure. " several " type frock main body and position block, all use identical material manufacture, have consistent Thermal coefficient of expansion.Non-metallic pressure pad, its thermal coefficient of expansion is also close with frock main body.
The method carrying out forming parts with the shaped device of this " work " font part includes following step Rapid:
1) at " several " type frock main body, even application releasing agent on position block, and dry;
2) along frock projection section profile successively paving on " several " type frock body upper surface 1 " C " type structure of " work " font part;
3) on position block on frock one side surface successively paving " work " font part Upper and lower edge face;
4) position block is individually positioned in by position, hole, location the both sides of frock main body;
5) gap of position block and frock main body, fixed position block after meeting the requirements are checked And fit tightly with frock main body;
6) complete the Zone R implant of lower edge face part respectively on " work " font part,
7) successively paving " work " font zero in frock main body with the groove of position block composition Another " C " type structure of part;
8) in groove, non-metallic pressure pad in another " C " type structure, is placed;
9) make vacuum bag, by the frock that combines with part integral coating in vacuum bag;
10) curing molding;
11) vacuum bag, non-metallic pressure pad, all keepers, position block are removed;
12) by part removal, qualified parts are gone out according to part theory sharp processing.
The shaped device of the present invention possesses following advantage:
1) tool structure is simple, and part manufacturing cost is low: paving, solidification share 1 set frock;
2) position block is fixed in position, axis of workpiece direction, is being perpendicular to axis of workpiece direction On can be movable within the specific limits, such location mode is capable of resilient engagement.Solid Changing under pressure, position block can be together with " several " type frock main body fits tightly, part Between internal each laying the finest and close;
3) 2 " C " type structures molding in same set of frock of " work " font part, work Assembling structure is simple, process is easy, and matching relationship is few, it is to avoid 2 " C " type structures To closing operation, shaft parts dimension is accurate;
4) pressure pad can uniform conductive solidifying pressure, inside parts laminating closely, smooth surface;
5) tool structure is simple, and curing and demolding is convenient, will not be because of demoulding injuring part.
Accompanying drawing explanation
Fig. 1 " work " font design of part schematic diagram
Fig. 2 " work " font part layering structural representation
The shaped device of " work " font part that Fig. 3 the present invention relates to
Fig. 4 part placement schematic diagram in frock
Numbering explanation in figure: 1-upper limb face;2-C type structure;4-R district implant;Under 5- Edge face;6-non-metallic pressure pad;7-position block;8-frock main body;9-part.
Detailed description of the invention
As shown in Figure 3,4, the shaped device of a kind of " work " font part, including " several " Type frock main body 8, position block 7, non-metallic pressure pad 6.Frock main body 8 is placed in bottom, One " C " type structure 2 paving of " work " font part is on frock main body 8 surface;Work Dress main body 8 liang is picked up the ears and the relevant position of position block 7 is provided with hole, location, position block 7 It is fixed on frock main body 8 liang picks up the ears, for paving and the upper limb of location " work " font part Face 1 and lower edge face 5;Non-metallic pressure pad 6 is placed in " work " font part another " C " In the groove of type structure 2, for compressing component and uniformly transfer pressure.
As a example by the manufacture of " work " font stringer, as Figure 1-4, concrete forming process is such as Under:
1) in " several " type frock main body 8, even application releasing agent on position block 7, and Dry;
2) successively spread along frock projection section profile on " several " type frock main body 8 upper surface 1 " C " type structure 2 of patch " work " font part;
3) on position block 7 on frock one side surface successively paving " work " font zero The upper limb face 1 of part, lower edge face 5;
4) position block 7 is individually positioned in by position, hole, location the both sides of frock main body 8;
5) gap of position block 7 and frock main body 8, stationary positioned after meeting the requirements are checked Block 7 also fits tightly with frock main body 8;
6) complete " work " font part 9 upper limb face 1, the R of lower edge face 5 part respectively District's implant 4,
7) successively paving " work " word in frock main body 8 with the groove of position block 7 composition Another " C " type structure 2 of type part;
8) in groove, non-metallic pressure pad 6 in another " C " type structure 2, is placed;
9) make vacuum bag, by the frock that combines with part 9 integral coating in vacuum bag;
10) curing molding;
11) vacuum bag, non-metallic pressure pad 6, all keepers, position block 7 are removed;
12) by part removal, qualified parts are gone out according to part theory sharp processing.
" several " type frock main body 8 and position block 7, use identical material manufacture, have Consistent thermal coefficient of expansion.It can be that silicone rubber etc. is nonmetal that non-metallic pressure pad 6 manufactures material Material, its thermal coefficient of expansion is close with frock main body.
The relative position of position block 7 can be controlled with alignment pin." several " type frock main body 8 The bottom outlet of upper correspondence is circular hole, inlays lining, it is ensured that life-time service is indeformable in bottom outlet, location Hole, location on block 7 is slotted hole, it is ensured that position block 7 can move within the specific limits. Alignment pin ensure that position block 7 is fixed position on axis of workpiece direction.And be perpendicular to On axis of workpiece direction, then can be movable within the specific limits, thus realize resilient engagement, " work " Between each laying within word part 9 the finest and close.Non-metallic pressure pad 6 is in free state, With part resilient engagement, for uniform conductive pressure.
This apparatus structure is simple, easy to use, solves 2 " C " type portions in forming process The problem of accurately docking divided, after having assembled, the relative position between each ingredient is at bag With solidification process keeps constant, shaft parts dimension is accurate, the overall dimensions of product and internal matter Amount has all obtained effective control.After having solidified, it is convenient in demoulding, it is possible to avoid at knockout course Middle injuring part.

Claims (4)

1. the shaped device of " work " font part, including " several " type frock main body, Position block, non-metallic pressure pad, described frock main body is placed in bottom, " work " font part The structure paving of " C " type in frock body surfaces;Described frock main body two pick up the ears and The relevant position of described position block is provided with hole, location, and described position block is fixed on frock master On body two is picked up the ears, for paving and the upper and lower edge face of location " work " font part;Nonmetal Pressure pad is placed in the groove of another " C " type structure of " work " font part, is used for compressing Part and uniformly transfer pressure.
The shaped device of one the most according to claim 1 " work " font part, it is special Levy and be described " several " type frock main body and position block, use identical material manufacture, There is consistent thermal coefficient of expansion.
3. according to the shaped device of one " work " the font part described in claim 1, its feature Being described non-metallic pressure pad, its thermal coefficient of expansion is close with frock main body.
4. use the shaped device of " work " the font part described in claim 1 to carry out part one-tenth The method of type comprises the following steps:
1) at " several " type frock main body, even application releasing agent on position block, and dry;
2) along frock projection section profile successively paving on " several " type frock body upper surface 1 " C " type structure of " work " font part;
3) on position block on frock one side surface successively paving " work " font part Upper and lower edge face;
4) position block is individually positioned in by position, hole, location the both sides of frock main body;
5) gap of position block and frock main body, fixed position block after meeting the requirements are checked And fit tightly with frock main body;
6) complete the Zone R implant of lower edge face part respectively on " work " font part,
7) successively paving " work " font zero in frock main body with the groove of position block composition Another " C " type structure of part;
8) in groove, non-metallic pressure pad in another " C " type structure, is placed;
9) make vacuum bag, by the frock that combines with part integral coating in vacuum bag;
10) curing molding;
11) vacuum bag, non-metallic pressure pad, all keepers, position block are removed;
12) by part removal, qualified parts are gone out according to part theory sharp processing.
CN201610203906.2A 2016-04-01 2016-04-01 A kind of shaped device and forming method of " work " font part Active CN105881930B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
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Application Number Priority Date Filing Date Title
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CN105881930B CN105881930B (en) 2018-04-10

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107263887A (en) * 2017-07-04 2017-10-20 西安飞机工业(集团)有限责任公司 A kind of vacuum aided positioner and localization method
CN108248071A (en) * 2018-01-15 2018-07-06 成都市泰格尔航天航空科技有限公司 The manufacturing method of degree of lip-rounding beam
CN109591321A (en) * 2018-12-18 2019-04-09 江苏新扬新材料股份有限公司 A kind of engine contains the forming method and its manufactured outer culvert casing of casing outside
CN109849369A (en) * 2019-03-20 2019-06-07 成都联科航空技术有限公司 A kind of processing method of composite skirt

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03119138A (en) * 1989-09-29 1991-05-21 Shikishima Kanbasu Kk Fiber reinforced composite material
JP2004249593A (en) * 2003-02-20 2004-09-09 Shin Meiwa Ind Co Ltd Method for manufacturing fiber composite material and hollow structure equipped with the fiber composite material
CN101391488A (en) * 2008-08-22 2009-03-25 成都飞机工业(集团)有限责任公司 Curing formation method for non-flat plate composite product and shaping mould
CN101666290A (en) * 2009-10-14 2010-03-10 黄争鸣 Wind turbine blade structure, processing and forming method and applications thereof
CN102152481A (en) * 2010-12-23 2011-08-17 东方电气集团东方汽轮机有限公司 Integrated molding and pouring process for semi-enclosed glass fiber reinforced plastic products with infolded flanges
CN102909866A (en) * 2012-10-24 2013-02-06 中国航空工业集团公司北京航空材料研究院 Method for forming control of long joist axial line of composite material stiffened wall panel
CN102963009A (en) * 2012-12-11 2013-03-13 成都飞机工业(集团)有限责任公司 Composite material multi-cavity structure piece manufacturing method
CN103496179A (en) * 2013-10-10 2014-01-08 航天海鹰(镇江)特种材料有限公司 Molding method for composite material structural member with I-shaped section
CN105082565A (en) * 2015-09-15 2015-11-25 沈阳飞机工业(集团)有限公司 Automatic lay-up forming method of I-shaped beam made from composite materials

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03119138A (en) * 1989-09-29 1991-05-21 Shikishima Kanbasu Kk Fiber reinforced composite material
JP2004249593A (en) * 2003-02-20 2004-09-09 Shin Meiwa Ind Co Ltd Method for manufacturing fiber composite material and hollow structure equipped with the fiber composite material
CN101391488A (en) * 2008-08-22 2009-03-25 成都飞机工业(集团)有限责任公司 Curing formation method for non-flat plate composite product and shaping mould
CN101666290A (en) * 2009-10-14 2010-03-10 黄争鸣 Wind turbine blade structure, processing and forming method and applications thereof
CN102152481A (en) * 2010-12-23 2011-08-17 东方电气集团东方汽轮机有限公司 Integrated molding and pouring process for semi-enclosed glass fiber reinforced plastic products with infolded flanges
CN102909866A (en) * 2012-10-24 2013-02-06 中国航空工业集团公司北京航空材料研究院 Method for forming control of long joist axial line of composite material stiffened wall panel
CN102963009A (en) * 2012-12-11 2013-03-13 成都飞机工业(集团)有限责任公司 Composite material multi-cavity structure piece manufacturing method
CN103496179A (en) * 2013-10-10 2014-01-08 航天海鹰(镇江)特种材料有限公司 Molding method for composite material structural member with I-shaped section
CN105082565A (en) * 2015-09-15 2015-11-25 沈阳飞机工业(集团)有限公司 Automatic lay-up forming method of I-shaped beam made from composite materials

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107263887A (en) * 2017-07-04 2017-10-20 西安飞机工业(集团)有限责任公司 A kind of vacuum aided positioner and localization method
CN108248071A (en) * 2018-01-15 2018-07-06 成都市泰格尔航天航空科技有限公司 The manufacturing method of degree of lip-rounding beam
CN109591321A (en) * 2018-12-18 2019-04-09 江苏新扬新材料股份有限公司 A kind of engine contains the forming method and its manufactured outer culvert casing of casing outside
CN109849369A (en) * 2019-03-20 2019-06-07 成都联科航空技术有限公司 A kind of processing method of composite skirt

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