CN104373301B - Metal carry fixing point structure and its manufacture method on core filled composite material - Google Patents

Metal carry fixing point structure and its manufacture method on core filled composite material Download PDF

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Publication number
CN104373301B
CN104373301B CN201410598786.1A CN201410598786A CN104373301B CN 104373301 B CN104373301 B CN 104373301B CN 201410598786 A CN201410598786 A CN 201410598786A CN 104373301 B CN104373301 B CN 104373301B
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CN
China
Prior art keywords
composite material
core filled
filled composite
hole
fixing point
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.)
Withdrawn - After Issue
Application number
CN201410598786.1A
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Chinese (zh)
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CN104373301A (en
Inventor
唐若辰
宋力
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.)
TPI Composites Taicang Co Ltd
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TPI Composites Taicang Co Ltd
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Publication date
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Priority to CN201410598786.1A priority Critical patent/CN104373301B/en
Publication of CN104373301A publication Critical patent/CN104373301A/en
Application granted granted Critical
Publication of CN104373301B publication Critical patent/CN104373301B/en
Withdrawn - After Issue legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • B29C65/52Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the way of applying the adhesive
    • B29C65/54Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the way of applying the adhesive between pre-assembled parts
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50Manufacturing or production processes characterised by the final manufactured product

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)

Abstract

The present invention relates to metal carry fixing point structure and its manufacture method on a kind of core filled composite material, the structure includes sandwich composite, pultrusion bar, steel plate and steel bushing, wherein having through hole on the core filled composite material;The pultrusion bar is fixed on the outside of the steel bushing, and the steel bushing and the pultrusion bar are co-located in the through hole;The hole alignd with the through hole on the core filled composite material is provided with the steel plate;The core filled composite material is connected with the steel plate.The core filled composite material metal carry fixing point structure that the present invention is provided is reliable and easy for installation, its processing and implementation method is easy to be reliable, user satisfaction is high, and the heater that the present invention is successfully used for certain large-scale transnational enterprise's latest model deicing version wind power generation blade is fixed.

Description

Metal carry fixing point structure and its manufacture method on core filled composite material
Technical field
The present invention relates to the connection between metalwork and composite material element, more particularly, to a kind of core filled composite material Upper metal carry fixing point structure, and the processing and implementation structures method.
Background technology
As composite is more and more applied in wind-powered electricity generation/automobile and other industries, between metalwork and composite material element Connection is also more and more, however, at present due to that can add many cores when large-scale composite material is designed, and core compressive strength one As it is very low, therefore user's directly fixed metal in will cause the deformation and failure of composite, and user satisfaction is not high, and And, the method for processing and implementation is also unreliable.
The content of the invention
For above-mentioned problems of the prior art, it is an object of the invention to provide metal on a kind of core filled composite material Carry fixing point structure, the structure is reliable and easy for installation, and the method for its processing and implementation is also easy to be reliable, user satisfaction pole It is high.
In order to realize the purpose of foregoing invention, the present invention is adopted the following technical scheme that:
Metal carry fixing point structure on a kind of core filled composite material, including sandwich composite, pultrusion bar, steel plate with And steel bushing, wherein having through hole on the core filled composite material;The pultrusion bar is fixed on the outside of the steel bushing, and institute State steel bushing and the pultrusion bar is co-located in the through hole;Be provided with the steel plate with the core filled composite material The hole of through hole alignment;The core filled composite material is connected with the steel plate.
Further, the core filled composite material passes through epoxy construction gemel connection with the steel plate.
Further, the pultrusion bar is vertically fixed on the outside of the steel bushing by using instant drying adhesive.
Further, described steel bushing one end is sealed using adhesive tape.
Further, the pultrusion bar is fiberglass pultrusion bar.
Further, the epoxy structural rubber fills up the through hole.
Further, the steel plate is fixed by installation bolt nut.
The method of processing and implementation said structure comprises the following steps:
1) corresponding through hole is got on core filled composite material;
2) fiberglass pultrusion bar is vertically fixed using instant drying adhesive outside steel bushing, and composite wood is filled up using epoxy structural rubber Through hole on material;
3) one end of steel bushing is sealed with adhesive tape, the steel bushing of the glass pultrusion bar glued is filled in composite through hole, After steel bushing in place after, by pre-production it is good offer corresponding aperture steel plate align composite through hole, applied with epoxy glue Composite and steel plate joint face are covered, installation bolt nut is unified to fix steel plate using torsion;
4) be heating and curing overall structure, treats after the completion of epoxy construction adhesive curing, removes all bolt and nuts, and use drill bit Foreign matter on steel bushing endoporus and cleaning steel plate is cleared up, that is, obtains core filled composite material metal carry fixing point structure.
Due to using above technical scheme, beneficial effects of the present invention include:
1) present invention efficiently solves the structure of modification of large-scale carry metal parts on core filled composite material, and the present invention is provided Core filled composite material on metal carry fixing point structure it is reliable and easy for installation.
2) method of processing and implementation structure of the present invention is simple and reliable, and user satisfaction is high.
3) metal carry fixing point structure is successfully used for certain large-scale transnational enterprise on the core filled composite material that the present invention is provided The heater of industry latest model deicing version wind power generation blade is fixed.
Brief description of the drawings
The schematic diagram of metal carry fixing point structure on the core filled composite material that Fig. 1 provides for the present invention.Reference is said It is bright
1 core filled composite material, 2 steel plates, 3 steel bushings, 4 pultrusion bars, 5 epoxy structural rubbers, 6 through holes.
Embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, below in conjunction with the accompanying drawings and embodiment pair The present invention is described in further detail.It should be appreciated that specific embodiment described herein is only to explain the present invention, and without It is of the invention in limiting.
As shown in figure 1, metal carry fixing point structure on a kind of core filled composite material, including core filled composite material 1, pultrusion Bar 4, steel plate 2, steel bushing 3 and epoxy structural rubber 5, have through hole 6 wherein on core filled composite material;Steel bushing 3 and pultrusion bar 4 Fixed, steel bushing 3 is located in through hole 6;The hole alignd with through hole on core filled composite material 6 is provided with steel plate 2;Core filled composite material 1 is connected with steel plate 2 by epoxy structural rubber 5.
In the above-mentioned technical solutions, steel bushing 3 is outer vertically fixes pultrusion bar 4 using instant drying adhesive;The one end of steel bushing 3 uses adhesive tape Seal;Pultrusion bar 4 is fiberglass pultrusion bar;Epoxy structural rubber 5 fills up through hole 6;Steel plate 2 is carried out by installation bolt nut It is fixed.
The step of processing and implementation foregoing invention structure, is as described below, and the present embodiment is specifically 9mm in just to make internal diameter The description for the method for implementing foregoing invention structure is processed exemplified by 4 square metal fixing points.First, in sandwich composite wood 28mm through holes are got on material 1, then, in outer 3 glass that 4mm is vertically fixed using instant drying adhesive of internal diameter 9mm external diameters 20mm steel bushing 3 Glass steel pultrusion bar 4, and the 28mm through holes 6 filled up using epoxy structural rubber 5 on composite;Steel bushing 3 is sealed with adhesive tape again One end, the steel bushing 3 of the glass pultrusion bar glued is filled in composite through hole 6, after steel bushing 3 in place after, by pre-production The good 5mm steel plates 2 (mount point used as later user) for offering 4 holes of correspondence, 4 of alignment composite are led to Hole, with the coating composite materials 1 of epoxy structural rubber 5 and the joint face of 5mm steel plates 2, installs M8 bolt and nuts, unified to be turned round using 25Nm Power fixes steel plate 2;Finally, 80 DEG C of solidification overall structure 5h (being determined according to the performance of epoxy structural rubber) are heated, epoxy knot is treated After the completion of structure glue 5 solidifies, all M8 bolt and nuts are removed, and using different on the M9 drill bits cleaning endoporus of steel bushing 3 and cleaning steel plate 2 Thing, that is, obtain core filled composite material metal carry fixing point structure as shown in Figure 1.
The foregoing is only presently preferred embodiments of the present invention, not for limit the present invention practical range;If do not taken off From the spirit and scope of the present invention, the present invention is modified or equivalent substitution, all should covered in the claims in the present invention Among protection domain.

Claims (8)

1. metal carry fixing point structure on a kind of core filled composite material, it is characterised in that including core filled composite material, drawing and extruding bar Material, steel plate and steel bushing, wherein having through hole on the core filled composite material;The pultrusion bar is fixed on the outer of the steel bushing Side, and the steel bushing and the pultrusion bar be co-located in the through hole;It is provided with the steel plate multiple with the sandwich The hole of through hole alignment on condensation material;The core filled composite material is connected with the steel plate.
2. metal carry fixing point structure on core filled composite material according to claim 1, it is characterised in that the sandwich Composite passes through epoxy construction gemel connection with the steel plate.
3. metal carry fixing point structure on core filled composite material according to claim 2, it is characterised in that the pultrusion Bar is vertically fixed on the outside of the steel bushing by using instant drying adhesive.
4. metal carry fixing point structure on core filled composite material according to claim 3, it is characterised in that the steel bushing One end is sealed using adhesive tape.
5. metal carry fixing point structure on core filled composite material according to claim 3, it is characterised in that the pultrusion Bar is fiberglass pultrusion bar.
6. metal carry fixing point structure on core filled composite material according to claim 2, it is characterised in that the epoxy Structure glue fills up the through hole.
7. metal carry fixing point structure on core filled composite material according to claim 1, it is characterised in that the steel plate It is fixed by installation bolt nut.
8. metal carry fixing point knot on the core filled composite material described in a kind of any one of manufacturing claims 1-7 claim The method of structure, it is characterised in that comprise the steps of:
1) corresponding through hole is got on core filled composite material;
2) fiberglass pultrusion bar is vertically fixed using instant drying adhesive outside steel bushing, and sandwich composite wood is filled up using epoxy structural rubber Through hole on material;
3) one end of steel bushing is sealed with adhesive tape, the steel bushing of the fiberglass pultrusion bar glued is filled in into core filled composite material through hole It is interior, after steel bushing in place after, by pre-production it is good offer corresponding aperture steel plate align core filled composite material through hole, use ring Oxide structure glue coats core filled composite material and steel plate joint face, and installation bolt nut is unified to fix steel plate using torsion;
4) be heating and curing overall structure, treats after the completion of epoxy construction adhesive curing, removes all bolt and nuts, and clear up using drill bit Foreign matter on steel bushing endoporus and cleaning steel plate, that is, obtain core filled composite material metal carry fixing point structure.
CN201410598786.1A 2014-10-30 2014-10-30 Metal carry fixing point structure and its manufacture method on core filled composite material Withdrawn - After Issue CN104373301B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410598786.1A CN104373301B (en) 2014-10-30 2014-10-30 Metal carry fixing point structure and its manufacture method on core filled composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410598786.1A CN104373301B (en) 2014-10-30 2014-10-30 Metal carry fixing point structure and its manufacture method on core filled composite material

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Publication Number Publication Date
CN104373301A CN104373301A (en) 2015-02-25
CN104373301B true CN104373301B (en) 2017-11-03

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Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114986921B (en) * 2022-05-31 2023-11-07 宁波曙翔新材料股份有限公司 Stepped hole for sandwich composite material and preparation method thereof

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3970149B2 (en) * 2002-10-07 2007-09-05 セントラル硝子株式会社 Glass plate support structure
EP2330294B1 (en) * 2009-12-02 2013-01-16 Bladena ApS Reinforced airfoil shaped body
KR101153303B1 (en) * 2010-05-28 2012-06-05 한국과학기술원 Insert, sandwich panel having the same and method for manufacturing the sandwich panel
CN103470456B (en) * 2013-09-23 2016-04-13 华北电力大学(保定) A kind of segmented wind power generation blade with interchangeability
CN204186537U (en) * 2014-10-30 2015-03-04 迪皮埃复材构件(太仓)有限公司 Metal carry immovable point structure on core filled composite material

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