CN108861145A - A kind of composite material aircraft container - Google Patents
A kind of composite material aircraft container Download PDFInfo
- Publication number
- CN108861145A CN108861145A CN201810970765.6A CN201810970765A CN108861145A CN 108861145 A CN108861145 A CN 108861145A CN 201810970765 A CN201810970765 A CN 201810970765A CN 108861145 A CN108861145 A CN 108861145A
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- CN
- China
- Prior art keywords
- composite material
- cabinet
- rectangular
- panel
- plate
- 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
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- 239000002131 composite material Substances 0.000 title claims abstract description 37
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 15
- 239000004744 fabric Substances 0.000 claims abstract description 11
- 239000000463 material Substances 0.000 claims abstract description 10
- 238000005452 bending Methods 0.000 claims abstract description 7
- 238000003825 pressing Methods 0.000 claims abstract description 5
- 239000011162 core material Substances 0.000 claims description 18
- 229920003023 plastic Polymers 0.000 claims description 16
- 239000004033 plastic Substances 0.000 claims description 16
- -1 polypropylene Polymers 0.000 claims description 12
- 239000000853 adhesive Substances 0.000 claims description 7
- 230000001070 adhesive effect Effects 0.000 claims description 7
- 239000000835 fiber Substances 0.000 claims description 7
- 239000004698 Polyethylene Substances 0.000 claims description 5
- 239000004743 Polypropylene Substances 0.000 claims description 5
- 239000011159 matrix material Substances 0.000 claims description 5
- 229920000515 polycarbonate Polymers 0.000 claims description 5
- 239000004417 polycarbonate Substances 0.000 claims description 5
- 229920000573 polyethylene Polymers 0.000 claims description 5
- 229920005989 resin Polymers 0.000 claims description 5
- 239000011347 resin Substances 0.000 claims description 5
- 238000001125 extrusion Methods 0.000 claims description 4
- 229920000139 polyethylene terephthalate Polymers 0.000 claims description 4
- 239000005020 polyethylene terephthalate Substances 0.000 claims description 4
- 229920001155 polypropylene Polymers 0.000 claims description 4
- 230000001413 cellular effect Effects 0.000 claims description 3
- 238000007731 hot pressing Methods 0.000 claims description 3
- 238000002844 melting Methods 0.000 claims description 3
- 230000008018 melting Effects 0.000 claims description 3
- 229920000915 polyvinyl chloride Polymers 0.000 claims description 3
- 239000004800 polyvinyl chloride Substances 0.000 claims description 3
- 210000002784 stomach Anatomy 0.000 claims description 3
- 229920001169 thermoplastic Polymers 0.000 claims description 3
- 239000004416 thermosoftening plastic Substances 0.000 claims description 3
- 238000010276 construction Methods 0.000 claims description 2
- 239000012779 reinforcing material Substances 0.000 claims description 2
- 229920005992 thermoplastic resin Polymers 0.000 claims description 2
- 230000037237 body shape Effects 0.000 claims 1
- 150000001875 compounds Chemical class 0.000 abstract description 3
- 230000007797 corrosion Effects 0.000 abstract description 3
- 238000005260 corrosion Methods 0.000 abstract description 3
- 239000003292 glue Substances 0.000 abstract description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 229920002748 Basalt fiber Polymers 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 2
- 239000004593 Epoxy Substances 0.000 description 2
- PEEHTFAAVSWFBL-UHFFFAOYSA-N Maleimide Chemical compound O=C1NC(=O)C=C1 PEEHTFAAVSWFBL-UHFFFAOYSA-N 0.000 description 2
- 229910000861 Mg alloy Inorganic materials 0.000 description 2
- 239000004677 Nylon Substances 0.000 description 2
- 239000004699 Ultra-high molecular weight polyethylene Substances 0.000 description 2
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 2
- SNAAJJQQZSMGQD-UHFFFAOYSA-N aluminum magnesium Chemical compound [Mg].[Al] SNAAJJQQZSMGQD-UHFFFAOYSA-N 0.000 description 2
- 229920006231 aramid fiber Polymers 0.000 description 2
- 239000004917 carbon fiber Substances 0.000 description 2
- XLJMAIOERFSOGZ-UHFFFAOYSA-M cyanate Chemical compound [O-]C#N XLJMAIOERFSOGZ-UHFFFAOYSA-M 0.000 description 2
- 125000003700 epoxy group Chemical group 0.000 description 2
- 239000003365 glass fiber Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 229920001778 nylon Polymers 0.000 description 2
- 229920000647 polyepoxide Polymers 0.000 description 2
- 229920002635 polyurethane Polymers 0.000 description 2
- 239000004814 polyurethane Substances 0.000 description 2
- 229920000785 ultra high molecular weight polyethylene Polymers 0.000 description 2
- SMZOUWXMTYCWNB-UHFFFAOYSA-N 2-(2-methoxy-5-methylphenyl)ethanamine Chemical compound COC1=CC=C(C)C=C1CCN SMZOUWXMTYCWNB-UHFFFAOYSA-N 0.000 description 1
- 150000001336 alkenes Chemical class 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- FYIBGDKNYYMMAG-UHFFFAOYSA-N ethane-1,2-diol;terephthalic acid Chemical compound OCCO.OC(=O)C1=CC=C(C(O)=O)C=C1 FYIBGDKNYYMMAG-UHFFFAOYSA-N 0.000 description 1
- LYCAIKOWRPUZTN-UHFFFAOYSA-N ethylene glycol Natural products OCCO LYCAIKOWRPUZTN-UHFFFAOYSA-N 0.000 description 1
- WGCNASOHLSPBMP-UHFFFAOYSA-N hydroxyacetaldehyde Natural products OCC=O WGCNASOHLSPBMP-UHFFFAOYSA-N 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000000088 plastic resin Substances 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- KUCOHFSKRZZVRO-UHFFFAOYSA-N terephthalaldehyde Chemical compound O=CC1=CC=C(C=O)C=C1 KUCOHFSKRZZVRO-UHFFFAOYSA-N 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D88/00—Large containers
- B65D88/02—Large containers rigid
- B65D88/12—Large containers rigid specially adapted for transport
- B65D88/127—Large containers rigid specially adapted for transport open-sided container, i.e. having substantially the whole side free to provide access, with or without closures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B27/08—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/18—Layered products comprising a layer of synthetic resin characterised by the use of special additives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/30—Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers
- B32B27/304—Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers comprising vinyl halide (co)polymers, e.g. PVC, PVDC, PVF, PVDF
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/32—Layered products comprising a layer of synthetic resin comprising polyolefins
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/34—Layered products comprising a layer of synthetic resin comprising polyamides
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/36—Layered products comprising a layer of synthetic resin comprising polyesters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/36—Layered products comprising a layer of synthetic resin comprising polyesters
- B32B27/365—Layered products comprising a layer of synthetic resin comprising polyesters comprising polycarbonates
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D90/00—Component parts, details or accessories for large containers
- B65D90/02—Wall construction
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/04—Impregnation, embedding, or binder material
- B32B2260/046—Synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0253—Polyolefin fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0261—Polyamide fibres
- B32B2262/0269—Aromatic polyamide fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/101—Glass fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
- B32B2307/714—Inert, i.e. inert to chemical degradation, corrosion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
- B32B2307/718—Weight, e.g. weight per square meter
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2439/00—Containers; Receptacles
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Laminated Bodies (AREA)
Abstract
The invention discloses a kind of composite material aircraft containers, including：Cabinet, the rectangular-shape structure that the cabinet is open in one side, the box opening is connect with frame base, form a complete container, a rectangular-shape structure side vertical with opening has entrance, the rectangular-shape structure passes through one piece of complete plate entirety bending forming, reinforcing rod is provided at the seamed edge of the rectangular-shape structure, the apex of the adjacent reinforcing rod is attached by corner block, its cabinet is bent by monolith plate, it is at low cost, light weight, intensity is high, it is corrosion-resistant, long service life and easy to maintain, the damage revamping of panel is simple and quick simultaneously, it need to only use the unidirectional cloth of identical material compound can repair damaged location by applying glue or heat cold pressing, greatly reduce the O&M cost of air container.
Description
Technical field
The present invention relates to technical field of aerospace, more particularly to a kind of composite material aircraft container.
Background technique
Air container is maximum load rate according to the design of the shape of aircraft hold, to guarantee the cargo hold confined space
Container generallys use aluminium alloy extrusions composition frame, reinforcing rib, aluminum alloy outer cover is then riveted on profile, form one
Air container cabinet.
Traditional air container has that structure is complicated, tie point is more, self weight is heavier, covering is easy to damage not easy to repair etc. scarce
It falls into, causes traditional air container there are high production cost, efficient loading amount is low, O&M cost is high, be unfavorable for air container
Production and operation.
Summary of the invention
It is an object of the invention to：Overcome the above-mentioned problems in the prior art, proposes a kind of composite material aircraft collection
Vanning, cabinet bent by monolith plate, and at low cost, light weight, intensity is high, corrosion-resistant, long service life and is easy to
Maintenance, while the damage revamping of panel is simple and quick, need to only use the unidirectional cloth of identical material by applying glue or heat
Be cold-pressed it is compound can repair damaged location, greatly reduce the O&M cost of air container.
The purpose of the present invention is realized by following technical proposals：
A kind of composite material aircraft container, including：Cabinet, rectangular-shape structure of the cabinet in one side opening, institute
It states box opening to connect with frame base, forms a complete container, the rectangular-shape structure is vertical with opening
One side has entrance, and the rectangular-shape structure is cut by one block of complete plate according to Container Dimensions earnestly
Whole bending forming after reserved crack arrest mouth and bending surplus is provided with reinforcing rod at the seamed edge of the rectangular-shape structure, adjacent
The apex of the reinforcing rod be attached by corner block.
A kind of composite material aircraft container of the invention, the cabinet include：Top plate surrounding described in top plate is respectively provided with
Foreboard, back plate, interior plate and outer panel, the entrance are located on foreboard, and the outer panel is bent to form outer panel under
Outer panel, so that cabinet be made to form polyhedral structure of the bottom side with unfilled corner.
A kind of composite material aircraft container of the invention, the plate include upper layer and lower layer panel, among the panel
It is provided with plastic honeycomb core material, is bonded between the panel and plastic honeycomb core material by adhesive.
A kind of composite material aircraft container of the invention, the panel are several layers unidirectional cloth, and the unidirectional cloth is with warm
Plastic resin is matrix, and continuous fiber is reinforcing material, and is soaked by resin melting stain, and extrusion forming is passed through.
A kind of composite material aircraft container of the invention, the panel be by several unidirectional cloths according to 0 °, 45 ° ,-
Thermoplastic composite made of hot pressing and/or cold pressing after 45 ° or 90 ° of layings.
Described matrix resin is one in nylon, polypropylene, polyethylene terephthalate, polyethylene or polycarbonate
Kind；Continuous fiber is one in glass fibre, carbon fiber, aramid fiber, ultra high molecular weight polyethylene fiber or basalt fibre
Kind, the adhesive is one of epoxies, acrylic compounds, polyurethanes, maleimide or cyanate adhesive.
A kind of composite material aircraft container of the invention, plastic honeycomb core material vertical section shape are several：Positive six side
Shape honeycomb, overstretching honeycomb, the regular hexagon honeycomb with middle part reinforcing plate or round en-block construction cellular on an empty stomach.
A kind of composite material aircraft container of the invention, the material of the plastic honeycomb core material are polycarbonate, poly- third
Alkene, polyvinyl chloride, polyethylene or polyethylene terephthalate.
The honeycomb core material aperture is generally divided into:Circle is 6mm or 8mm；Hexagon 3.6mm, 6mm or 8mm size.
A kind of composite material aircraft container of the invention, passes through cementing, riveting between the cabinet, reinforcing rod and corner block
It connects or is bolted.
A kind of composite material aircraft container of the invention, the material of the plate are aerolite plate, magnesium alloy plate
Or magnesium-aluminum alloy plate.
A kind of composite material aircraft container of the invention is provided with cloth curtain door at the entrance, sets on the cabinet
It is equipped with documents pouch.
According to the above technical scheme, the beneficial effects of the invention are as follows：It is proposed a kind of composite material aircraft container, cabinet
It is bent by monolith plate, at low cost, light weight, intensity is high, corrosion-resistant, long service life and easy to maintain, while face
The damage revamping of plate is simple and quick, only need to use identical material unidirectional cloth by apply glue or heat cold pressing it is compound can
To repair damaged location, the O&M cost of air container is greatly reduced.
Detailed description of the invention
Fig. 1 is a kind of composite material aircraft container schematic diagram of the present invention；
Fig. 2 is a kind of cabinet schematic diagram of composite material aircraft container of the present invention；
Fig. 3 is a kind of cabinet expanded view of composite material aircraft container of the present invention；
Fig. 4 is a kind of plate schematic diagram of composite material aircraft container of the present invention；
Fig. 5 is a kind of the first structure of composite material aircraft container plastic honeycomb core material of the invention；
Fig. 6 is a kind of second of structure of composite material aircraft container plastic honeycomb core material of the invention；
Fig. 7 is a kind of the third structure of composite material aircraft container plastic honeycomb core material of the invention；
Fig. 8 is a kind of the 4th kind of structure of composite material aircraft container plastic honeycomb core material of the present invention.
Specific embodiment
The present invention is further illustrated with attached drawing combined with specific embodiments below.
In order to make the objectives, technical solutions, and advantages of the present invention clearer, with reference to the accompanying drawings and embodiments, right
The present invention is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, and
It is not used in the restriction present invention.
If Fig. 1-8 is a kind of embodiment of composite material aircraft container of the present invention, a kind of composite material aircraft container,
Including：Cabinet 3, the rectangular-shape structure that the cabinet 3 is open in one side, 3 opening of cabinet are connect with frame base 4,
A complete container is formed, a rectangular-shape structure side vertical with opening has entrance 16, the length
After cube shape structure is cut reserved crack arrest mouth and bending surplus according to Container Dimensions by one block of complete plate 17 earnestly
Whole bending forming is provided with reinforcing rod 1, the apex of the adjacent reinforcing rod 1 at the seamed edge of the rectangular-shape structure
It is attached by corner block 6, the cabinet 3 includes：12 surrounding of top plate described in top plate 12 is respectively provided with foreboard 7, back plate 10, interior
Side plate 11 and outer panel, the entrance 16 are located on foreboard 7, and the outer panel is bent to form outer panel 8 and lower outer panel
9, so that cabinet 3 be made to form polyhedral structure of the bottom side with unfilled corner, the plate 17 includes upper layer and lower layer panel 13, institute
State and be provided with plastic honeycomb core material 15 among panel 13, between the panel 13 and plastic honeycomb core material 15 by adhesive 14 into
Row bonding, the panel 13 are several layers unidirectional cloth, and for the unidirectional cloth using thermoplastic resin as matrix, continuous fiber is strengthening material
Material, and soaked by resin melting stain, by extrusion forming, the panel 13 is by several unidirectional cloths according to 0 °, 45 °, -45 °
Or thermoplastic composite made of hot pressing and/or cold pressing after 90 ° of layings, described matrix resin is nylon PA, polypropylene PP, poly-
One of ethylene glycol terephthalate PET, polythene PE or polycarbonate；Continuous fiber be glass fibre, carbon fiber,
One of aramid fiber, ultra high molecular weight polyethylene fiber or basalt fibre, the adhesive 14 are epoxies, acrylic acid
One of class, polyurethanes, maleimide or cyanate adhesive, the 15 vertical section shape of plastic honeycomb core material
Shape is several：Regular hexagon honeycomb, overstretching honeycomb, the regular hexagon honeycomb with middle part reinforcing plate or round cellular whole on an empty stomach
Block structure, the material of the plastic honeycomb core material 15 are polycarbonate, polypropylene, polyvinyl chloride, polyethylene or poly- terephthaldehyde
Sour glycol ester, honeycomb core material aperture are generally divided into:Circle is 6mm or 8mm；Hexagon 3.6mm, 6mm or 8mm size, it is described
Between cabinet 3, reinforcing rod 1 and corner block 6 by it is cementing, rivet or be bolted, the material of the plate 17 is that aviation aluminium closes
Golden plate, magnesium alloy plate or magnesium-aluminum alloy plate are provided with cloth curtain door 5 at the entrance 16, are provided with documents pouch on the cabinet 3
2。
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the invention
Made any modifications, equivalent replacements, and improvements etc., should all be included in the protection scope of the present invention within mind and principle.
Claims (8)
1. a kind of composite material aircraft container, which is characterized in that including：Cabinet (3), the cabinet (3) is in one side opening
Rectangular-shape structure, cabinet (3) opening are connect with frame base (4), form a complete container, described rectangular
A body shape structure side vertical with opening has entrance (16), and the rectangular-shape structure passes through one block of complete plate
(17) whole bending forming, the rectangular-shape knot after reserved crack arrest mouth and bending surplus are cut earnestly according to Container Dimensions
It is provided at the seamed edge of structure reinforcing rod (1), the apex of the adjacent reinforcing rod (1) is attached by corner block (6).
2. a kind of composite material aircraft container according to claim 1, it is characterised in that：The cabinet (3) includes：Top
Plate (12) top plate (12) surrounding is respectively provided with foreboard (7), back plate (10), interior plate (11) and outer panel, the entrance
(16) it is located on foreboard (7), the outer panel is bent to form outer panel (8) and lower outer panel (9), to make cabinet (3) shape
Polyhedral structure at bottom side with unfilled corner.
3. a kind of composite material aircraft container according to claim 1, it is characterised in that：The plate (17) includes upper
Lower two-layer panel (13), the panel (13) is intermediate to be provided with plastic honeycomb core material (15), the panel (13) and plastic honeycomb
It is bonded between core material (15) by adhesive (14).
4. a kind of composite material aircraft container according to claim 3, it is characterised in that：The panel (13) is several
Layer unidirectional cloth, for the unidirectional cloth using thermoplastic resin as matrix, continuous fiber is reinforcing material, and is soaked by resin melting stain,
Pass through extrusion forming.
5. a kind of composite material aircraft container according to claim 4, it is characterised in that：The panel (13) is to pass through
Several unidirectional cloths are according to thermoplastic composite made of hot pressing after 0 °, 45 °, -45 ° or 90 ° laying and/or cold pressing.
6. a kind of composite material aircraft container according to claim 3, it is characterised in that：The plastic honeycomb core material
(15) vertical section shape is several：Regular hexagon honeycomb, overstretching honeycomb, regular hexagon honeycomb or circle with middle part reinforcing plate
The cellular en-block construction of shape empty stomach.
7. a kind of composite material aircraft container according to claim 6, it is characterised in that：The plastic honeycomb core material
(15) material is polycarbonate, polypropylene, polyvinyl chloride, polyethylene or polyethylene terephthalate.
8. a kind of composite material aircraft container according to claim 1, it is characterised in that：The cabinet (3), reinforcing rod
(1) between corner block (6) by it is cementing, rivet or be bolted.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201810970765.6A CN108861145A (en) | 2018-08-24 | 2018-08-24 | A kind of composite material aircraft container |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201810970765.6A CN108861145A (en) | 2018-08-24 | 2018-08-24 | A kind of composite material aircraft container |
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| CN108861145A true CN108861145A (en) | 2018-11-23 |
Family
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| CN201810970765.6A Pending CN108861145A (en) | 2018-08-24 | 2018-08-24 | A kind of composite material aircraft container |
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| CN (1) | CN108861145A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN112061610A (en) * | 2020-10-20 | 2020-12-11 | 谢国华 | Be applied to aviation container that aviation loaded |
| CN112239030A (en) * | 2019-07-17 | 2021-01-19 | 公众科技解决方案有限公司 | Light-weight metal transport container with metal porous floor with multiple cell wall thicknesses |
| CN112248561A (en) * | 2020-10-19 | 2021-01-22 | 上海龙胜实业有限公司 | Bendable composite board and bending method thereof |
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