CN101761758A - Copper-alloy honeycomb core and weaving-forming method thereof - Google Patents

Copper-alloy honeycomb core and weaving-forming method thereof Download PDF

Info

Publication number
CN101761758A
CN101761758A CN200810243376A CN200810243376A CN101761758A CN 101761758 A CN101761758 A CN 101761758A CN 200810243376 A CN200810243376 A CN 200810243376A CN 200810243376 A CN200810243376 A CN 200810243376A CN 101761758 A CN101761758 A CN 101761758A
Authority
CN
China
Prior art keywords
alloy
honeycomb core
honeycomb
copper
weaving
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
CN200810243376A
Other languages
Chinese (zh)
Inventor
陶春有
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN200810243376A priority Critical patent/CN101761758A/en
Publication of CN101761758A publication Critical patent/CN101761758A/en
Pending legal-status Critical Current

Links

Landscapes

  • Laminated Bodies (AREA)

Abstract

The invention discloses a copper-alloy honeycomb core and a weaving-forming method thereof. The method uses flexible fiber to weave copper-alloy sheets together, and then overlaps and sticks the copper-alloy sheets into a honeycomb core block, and finally unfolds the honeycomb core block to serve as the honeycomb core. The copper-alloy honeycomb core can be broadly applied to producing sandwich products in each field.

Description

Copper-alloy honeycomb core and method for weaving and forming thereof
The invention belongs to composite material sandwich structure and make the field with honeycomb core, particularly relating to interweaves alcu alloy film material and flexible fibrous material manufactures the method for honeycomb core.
At present, the honeycomb structure composite material has light weight, intensity is big, rigidity is high, have functions such as buffering, shock insulation, insulation, heat insulation and sound insulation, obtain extensive use, it is applied to aerospace field the earliest, be widely used in fields such as building industry, car and boat manufacturing industry, furniture manufacturing, packing and transport service now, in order to alternative metals, plastics, timber, clay brick and highly foamed polystyrene etc.For satisfying the user demand of variety classes honeycomb structure composite material, there to be many kinds of honeycomb cores to be designed, to produce, mainly contain: paper honeycomb core, Copper Alloy Steel honeycomb core, cotton honeycomb core, aramid fiber honeycomb core, aluminium honeycomb core, various plastic honeycomb core, die mould steel honeycomb core or the like.These honeycomb cores all adopt homogeneous material to produce, paper honeycomb core low price application area is wider, but a variety of causes such as its protection against the tide, waterproof, fire prevention and intensity index have all limited its application area, die mould steel honeycomb core is to adopt the whole piece steel plate to be pressed into behind the ladder type welding or bond together, various aspects of performance such as intensity are all fine, but not flexible suitable plane sandwiched product, this has limited its application in various curved surface use occasions.Aspect of performances such as the compressive strength of other honeycomb core and temperature tolerance are limited, and price is more expensive, and these all are that these honeycomb cores of these particular application such as its obstacle, particularly High Voltage of enlarging application area, high temperature, shaped face are inefficient.
The objective of the invention is in order to overcome the shortcoming of above-mentioned honeycomb core, adopt a kind of forming method that one or more alcu alloy film made are become copper-alloy honeycomb core.The Cu alloy material that we use is now compared with above-mentioned honeycomb core material therefor has very high compressive strength and resistance to heat, the compressive strength of copper-alloy honeycomb core can design by usage requirement, hard material is of a great variety, as: the steel plate class, the cast iron class, ceramic-like, alloy type, the non-ferrous alloy class, the cement class, copper alloys, bamboo wood class, all hard materials of rock type or the like, performance and price are different, the honeycomb core of different hard material manufacturings has different performances, choose the collocation of one or more and Cu alloy material by the performance of usage requirement, one chooses suitable compositional system surely, produce the suitable copper-alloy honeycomb core of price, these copper-alloy honeycomb cores can satisfy the flat clevis layer cellular structure of various material panels, the demand of special-shaped interlayer cellular structure.
The present invention adopts following technical step for achieving the above object: at first one or more alcu alloy films of the same a kind of specification that will use are ready to; Select for use the flexible fiber of satisfying the demand to make warp thread; Then with same Albatra metal-sheet or multiple alcu alloy film by design sequence go into latitude by shedding mechanism with flexible warp thread be woven into the Cuprum alloy fabric; In the rule gluing of the corresponding alcu alloy film of Cuprum alloy fabric being pressed four times of sheet width; And make it back and forth to fold into and need the thickness end socket to cut off; Pressurize as required, heating or pressurized, heated be solidified into Cuprum alloy fabric honeycomb pellet; This honeycomb pellet is fit to the uniform thickness plane or curved surface sandwich structure is used.Also can arrange one or more alcu alloy films of the different size that will use in proper order by use; Select for use the flexible fiber of satisfying the demand to make warp thread; Then use with a kind of different size alcu alloy film or multiple different size alcu alloy film by design sequence go into latitude by shedding mechanism with flexible warp thread be woven into the Cuprum alloy fabric, of the rule gluing of the corresponding alcu alloy film of Cuprum alloy fabric by four times of sheet width; And make it back and forth to fold into and need the thickness end socket to cut off; Pressurize as required, heating or pressurized, heated become Cuprum alloy fabric honeycomb pellet; This honeycomb pellet is fit to sandwich structurees such as non-uniform thickness concave and convex plane, inclined-plane or concave-convex curved surface, inclined-plane curved surface to be used.Four times of gluings are meant that sheet width equates with the regular hexagon honeycomb is monolateral, are three times of sheet width if select the monolateral width of regular hexagon honeycomb, and then the gluing width should be 4 * 3=12 doubly, the adjacent layer gluing half-distance that staggers; The adhesive tape width is slightly less than monolateral width.Other pattern honeycomb core can calculate the width rule and the gluing rule of thin slice by design pattern.The honeycomb pellet can directly stretch as modular honeycomb core plate, also can be stretched as continuous honeycomb core through continuous splicing lengthening and use; Widen through lengthening and can satisfy all usage requirements.The width that back and forth is folded into each layer of honeycomb pellet can equate, also can be unequal.Heating process is to determine by the requirement of used adhesive, but as the needs gluing, folding again after the heating.
The invention has the beneficial effects as follows: the performance of Cu alloy material and lamination coating is all fully played, and has accomplished mutual supplement with each other's advantages, and this has improved utilization efficiency of material widely, also uses for the Cu alloy material light simultaneously to lay the foundation.Flexible fiber makes it not only can make the plane comb core material facility that can make the curved surface comb core material also is provided.The flexible fiber of whole honeycomb pellet is not cut off, and this has improved the overall performance of honeycomb pellet greatly, some occasion honeycomb core need not spray adhesive curing just directly composite cover become cellular board and use.Can be used as raw material of building materials such as making building wall board, floor, roofer and can reduce the building deadweight greatly, create conditions for reducing support system.Use as various man-made board honeycomb core plates, can reduce consumption greatly, alleviated environment damage simultaneously wood materials.

Claims (10)

1. copper-alloy honeycomb core method for weaving and forming of the present invention, its essential characteristic is: at first one or more alcu alloy films of the same a kind of specification that will use are ready to; Select for use the flexible fiber of satisfying the demand to make warp thread; Then with same Albatra metal-sheet or multiple alcu alloy film by design sequence go into latitude by shedding mechanism with flexible warp thread be woven into the Cuprum alloy fabric; In the rule gluing of the corresponding alcu alloy film of Cuprum alloy fabric being pressed four times of sheet width; And make it back and forth to fold into and need the thickness end socket to cut off; Pressurize as required, heating or pressurized, heated be solidified into Cuprum alloy fabric honeycomb pellet; This honeycomb pellet is launched into honeycomb core and is fit to uniform thickness plane or the use of curved surface honeycomb structure.Also can arrange one or more alcu alloy films of the different size that will use in proper order by use; Select for use the flexible fiber of satisfying the demand to make warp thread; Then use with a kind of different size alcu alloy film or multiple different size alcu alloy film by design sequence go into latitude by shedding mechanism with flexible warp thread be woven into the Cuprum alloy fabric, the corresponding alcu alloy film of Cuprum alloy fabric by the rule gluing of four times of sheet width, and make it back and forth to fold into and need the thickness end socket to cut off; Pressurize as required, heating or pressurized, heated become Cuprum alloy fabric honeycomb pellet; This honeycomb pellet is launched into honeycomb core and is fit to honeycomb structures uses such as non-uniform thickness concave and convex plane, plane, inclined-plane or concave-convex curved surface, inclined-plane curved surface.
2. copper-alloy honeycomb core method for weaving and forming according to claim 1, its essential characteristic is: alcu alloy film can partly substitute with other hard sheet, and hard sheet is meant the thin slice of steel plate class, cast iron class, ceramic-like, category of glass, alloy type, non-ferrous alloy class, cement class, bamboo wood class, rock type or the like all hard materials.As: titanium alloy sheet, stainless steel sheets, cast iron sheet, cement bonded sand lodicule, glass flake, flag, ceramic plate or the like.
3. copper-alloy honeycomb core method for weaving and forming according to claim 1, its essential characteristic is: flexible fiber is meant all spendable fibers such as inorfil, organic fiber, artificial fiber, natural plant fibre, animal fibre, steel fiber, non-metallic fiber; As: glass fibre, carbon fiber, aramid fibre, vinylon fibre, nylon fiber, cotton fiber, bastose or the like.
4. copper-alloy honeycomb core method for weaving and forming according to claim 1, its essential characteristic is: interleaving mode can be make by any way the mechanism of flexible fiber opening cooperate with the mode that makes alcu alloy film go into latitude can, manual, semi-automatic, full-automatic, single station, multi-position or the like.
5. copper-alloy honeycomb core method for weaving and forming according to claim 1, its essential characteristic is: the honeycomb core shape can be a regular hexagon, also can be rhombus, rectangle, sinusoidal, trapezoidal and other shape of reinforcing strip Hexagon or the like arranged.
6. according to claim 1,5 described copper-alloy honeycomb core method for weaving and forming, its essential characteristic is: four times of gluings are meant that sheet width equates with the regular hexagon honeycomb is monolateral, if selecting the monolateral width of regular hexagon honeycomb is three times of sheet width, then the gluing width should be 4 * 3=12 doubly, the adjacent layer gluing half-distance that staggers; The adhesive tape width is slightly less than monolateral width; Other pattern honeycomb core can calculate the width rule and the gluing rule of thin slice by design pattern.
7. copper-alloy honeycomb core method for weaving and forming according to claim 1, its essential characteristic is: the width that back and forth is folded into each layer of honeycomb pellet can equate, also can be unequal.
8. copper-alloy honeycomb core method for weaving and forming according to claim 1, its essential characteristic is: heating process is to determine by the requirement of used adhesive, but as the needs gluing, folding again after the heating.
9. copper-alloy honeycomb core method for weaving and forming according to claim 1, its essential characteristic is: can be directly with the Cuprum alloy fabric along the various honeycomb cores of wanting shape of the bonding one by one one-tenth of any direction.
10. copper-alloy honeycomb core method for weaving and forming according to claim 1, its essential characteristic is: select the different of alcu alloy film and flexible fiber for use, select for use the adhesive also can be different, so technology also can be variant.
CN200810243376A 2008-12-22 2008-12-22 Copper-alloy honeycomb core and weaving-forming method thereof Pending CN101761758A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN200810243376A CN101761758A (en) 2008-12-22 2008-12-22 Copper-alloy honeycomb core and weaving-forming method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN200810243376A CN101761758A (en) 2008-12-22 2008-12-22 Copper-alloy honeycomb core and weaving-forming method thereof

Publications (1)

Publication Number Publication Date
CN101761758A true CN101761758A (en) 2010-06-30

Family

ID=42493090

Family Applications (1)

Application Number Title Priority Date Filing Date
CN200810243376A Pending CN101761758A (en) 2008-12-22 2008-12-22 Copper-alloy honeycomb core and weaving-forming method thereof

Country Status (1)

Country Link
CN (1) CN101761758A (en)

Similar Documents

Publication Publication Date Title
CN102990988B (en) Continuous glass-fiber cloth reinforced thermoplastics honeycomb sandwich panel
CN101761738A (en) Hard honeycomb core and bonding and forming method thereof by adopting strips
TWI708799B (en) CFRP sheet, laminates using CFRP sheet, and manufacturing method of CFRP sheet
CN101761759A (en) Mica honeycomb core and braiding method thereof
CN201883606U (en) Special-shaped aluminium cellular board
CN101761756A (en) Ceramic honeycomb core and weaving forming method thereof
CN102174978A (en) Cast steel honeycomb core and weaving and forming method thereof
CN101761744A (en) Stainless steel honeycomb core and knitting forming method thereof
CN102174976A (en) Wood honeycomb core and weaving and forming method thereof
CN101761758A (en) Copper-alloy honeycomb core and weaving-forming method thereof
CN101761760A (en) Mica honeycomb core and weaving method thereof
CN101761754A (en) Titanium alloy honeycomb core and weaving forming method thereof
CN101761751A (en) Plastic honeycomb core and braiding shape method thereof
CN101761742A (en) Glass honeycomb core and weaving and forming method thereof
CN101761748A (en) Aluminum alloy honeycomb core and method for weaving and forming same
CN101761752A (en) Plastic honeycomb core and braiding shape method thereof
CN101761737A (en) Hard honeycomb core and weaving and forming method thereof
CN101761750A (en) Cement sheet honeycomb core and weaving molding method thereof
CN102174979A (en) Stone honeycomb core and weaving and shaping method thereof
CN101761746A (en) Steel sheet honeycomb core and method for weaving and forming same
CN101761762A (en) Bamboo honeycomb core and weaving and forming method thereof
CN101761747A (en) Aluminum alloy honeycomb core and method for weaving and forming same
CN101761749A (en) Stone cellular core and braiding shaping method thereof
CN101761755A (en) Ceramic honeycomb core and weaving forming method thereof
CN101761745A (en) Steel sheet honeycomb core and method for weaving and forming same

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Open date: 20100630