CN204717238U - A kind of ultralight high strength ventilating and thermal insulating pipeline - Google Patents

A kind of ultralight high strength ventilating and thermal insulating pipeline Download PDF

Info

Publication number
CN204717238U
CN204717238U CN201520427308.4U CN201520427308U CN204717238U CN 204717238 U CN204717238 U CN 204717238U CN 201520427308 U CN201520427308 U CN 201520427308U CN 204717238 U CN204717238 U CN 204717238U
Authority
CN
China
Prior art keywords
cured layer
thermal insulation
layer
compounded
insulation layer
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.)
Active
Application number
CN201520427308.4U
Other languages
Chinese (zh)
Inventor
毛雪琪
毛素真
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.)
Jilin Hao Yuan agriculture and forestry planning and Design Co., Ltd.
Original Assignee
Jilin Jinyu Technology Co Ltd
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 Jilin Jinyu Technology Co Ltd filed Critical Jilin Jinyu Technology Co Ltd
Priority to CN201520427308.4U priority Critical patent/CN204717238U/en
Application granted granted Critical
Publication of CN204717238U publication Critical patent/CN204717238U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Laminated Bodies (AREA)

Abstract

The utility model relates to a kind of ultralight high strength ventilating and thermal insulating pipeline, and this insulation pipe comprises interior cured layer from inside to outside successively, the first honeycomb thermal insulation layer be compounded on interior cured layer, the middle cured layer be compounded on the first honeycomb thermal insulation layer, the second honeycomb thermal insulation layer be compounded on middle cured layer, the outer cured layer be compounded on the second honeycomb thermal insulation layer; Described interior cured layer, middle cured layer and outer cured layer adopt cyanamide esters resin or carbon-fiber cloth to make; Described first honeycomb thermal insulation layer and the second honeycomb thermal insulation layer adopt aramid fiber cellular material to make.The utility model is simple and reasonable, processing and convenient for production, have lightweight, insulation, fire prevention and resistance to high temperature.

Description

A kind of ultralight high strength ventilating and thermal insulating pipeline
Technical field
The utility model relates to the production field of insulation pipe, relates to a kind of ultralight high strength ventilating and thermal insulating pipeline specifically.
Background technique
The upper conventional ventilation themral insulation pipe of existing motion carrier (as high ferro, track traffic, aerospace vehicle) uses glass wool and epoxy resin composite structure.Utilize heat pressing process successively alternately by 4 layers of glass wool and 4 layers of epoxy resin compound finally shaping, complex process and process cycle is long.Above-mentioned insulating structure is because by raw material, the impact of structure and processing technology factor, easily causes the tube wall of finished product, caliber low precision, finished weight weight, intensity is low, above-mentioned insulating structure is used on motion carrier and not only wastes energy, and easily brings potential safety hazard.
Summary of the invention
The purpose of this utility model is to provide a kind of simple and reasonable, processing and convenient for production, has lightweight, insulation, fire prevention and resistance to high temperature.
The purpose of this utility model is achieved in that this insulation pipe comprises interior cured layer from inside to outside successively, the first honeycomb thermal insulation layer be compounded on interior cured layer, the middle cured layer be compounded on the first honeycomb thermal insulation layer, the second honeycomb thermal insulation layer be compounded on middle cured layer, the outer cured layer be compounded on the second honeycomb thermal insulation layer.
Described interior cured layer, middle cured layer and outer cured layer adopt cyanamide esters resin or carbon-fiber cloth to make.
Described first honeycomb thermal insulation layer and the second honeycomb thermal insulation layer adopt aramid fiber cellular material to make.
Described insulation pipe structure can be different according to service condition, make different pipe thickness, different rigidity intensity, different according to transport agent in pipeline, can select different interior cured layers.
Described cyanamide esters resin has excellent mechanical behavior under high temperature, and flexural strength and tensile strength are all high than difunctional epoxy resin; Extremely low water absorption rate (<1.5%); Molding shrinkage is low, good stability of the dimension; Good heat resistance, vitrification point is at 240 ~ 260 DEG C, and most high energy reaches 400 DEG C, modified can 170 DEG C of solidifications; Humidity resistance, flame retarding, cohesiveencess are all fine, and the adhesive property of the reinforcing material such as glass, carbon fibre, quartz fibre, whisker is good; Excellent electrical property, has extremely low permittivity (2.8 ~ 3.2) and dielectric loss angle tangent value (0.002 ~ 0.008), and the change of fire retardant to temperature and wave frequency all shows distinctive stability (namely having wide band).Cyanamide esters resin can be used for the structural member making military affairs, Aeronautics and Astronautics, navigational field, such as wing, ship shell etc., also can be made into foam sandwich construction material conventional in aerospace, cyanamide esters resin has good compatibility, heat resistance and the mechanical property of material can be improved with the copolymerization such as epoxy resin, unsaturated polyester, also can be used to, to other resin modified, be used as adhesive, coating, syntactic foam, artificial dielectric material etc.
Described aramid fiber cellular composite material is the structure be made up of multiple hexagonal cells, the favous cross section of outer appearnce, 90% to 99% of cellular material is empty, and aramid fiber honeycomb core and upper and lower cyanamide esters resin or carbon-fiber cloth close adhesion compound just form core plate structure.Feature after compound: quality is one of conventional thermal insulation pipe about five parts weight only, and aramid fiber honeycomb has good heat insulating ability, substitutes conventional glass completely, and intensity after compound, rigidity is large.(can significantly improve flexural rigidity and the intensity of material under equivalent weight condition, rigidity can improve 37 times, and intensity can improve 9 times).Because of its lightweight of aramid fiber honeycomb, the characteristic of high strength, is widely used in track traffic, Aero-Space, and other motion carriers.Under given density, aramid fiber honeycomb is better than other materials in conjunction with the impact resistance of structure after carbon fiber prepreg or cyanamide esters resin compound.
Described carbon-fiber cloth, by materials such as carbon fiber yarn, epoxy resin, release paper, is called carbon fiber prepreg through film, hot pressing, cooling, overlay film, the composite material that the processes such as to batch, has another name called carbon fibre initial rinse fabric.Why make prepreg cloth be because this is the preliminary impregnation of resin and carbon fiber, be only the cause of final impregnation when formed product.Carbon fiber is compared with traditional glass fibre, and Young's modulus is that they are more than 3 times; It is compared with Kafra fiber, and Young's modulus is its about 2 times, insoluble not swollen in organic solvent, acid, alkali, and corrosion resistance is given prominence to.
Described vacuum bag complex technique, according to wanting the shape making pipeline to make mould, each Rotating fields of hand lay-up, puts into vacuum bag, is evacuated to the fixed time, and this technology is vacuum bag complex technique.
Described hot-forming complex technique, by mould, lay complete by each Rotating fields, and lay release paper, by specified pressure, temperature, fast shaping, and slow cooling, this forming technique is hot-forming complex technique.
Adopt the comb core that overstretching technology is made, its tangent plane is shaped to approximate rectangular, and the bendable curvature of its transverse direction is very good, and simultaneously longitudinal intensity is very large, can according to different shaping needed for pipeline, as circle, square etc., Appropriate application small space.
The utility model has the following advantages and good effect:
1, its number of plies of insulation pipe structure described in the utility model can use desirable strength by reality, the changes such as fire-proof high-temperature resistant grade.
2, the utility model composite curing layer selects cyanamide esters resin, the prepreg such as carbon-fiber cloth, can realize good flame retardant property, can accomplish very high strength with the compound of core simultaneously.Keriotheca raw material is aramid paper honeycomb, and outer composite curing layer the selection of material also can adopt cyanamide esters resin except carbon-fiber cloth, to reach the different requirements of different application occasion to tube performance.
3, the pipeline of the utility model structure can have the lightweight of aramid fiber honeycomb, thermal insulation property, utilize again cyanamide esters resin, obtain and epoxy resin similarity surface, there is again the fire prevention similar to phenol and resistance to high temperature simultaneously, greatly reduce the weight of pipeline, improve intensity and the thermal insulation property of pipeline, this structure is not limited to tubular shape.
Accompanying drawing explanation
Fig. 1 is the utility model perspective view.
Fig. 2 is the radial cross section enlarged view of the utility model Fig. 1.
embodiment:
Shown in accompanying drawing 1,2: this insulation pipe comprises interior cured layer 1 from inside to outside successively, the first honeycomb thermal insulation layer 2 be compounded on interior cured layer 1, the middle cured layer 3 be compounded on the first honeycomb thermal insulation layer 2, the second honeycomb thermal insulation layer 4 be compounded on middle cured layer 3, the outer cured layer 5 be compounded on the second honeycomb thermal insulation layer 4.
Wall thickness after the solidification of described interior cured layer 1, middle cured layer 3 and outer cured layer 5 is 1mm, adopts cyanamide esters resin or carbon-fiber cloth to make its composite curing connect shaping making by hot-forming compound or vacuum bag complex technique.
The wall thickness of described first honeycomb thermal insulation layer 2 and the second honeycomb thermal insulation layer 4 is that 5mm(increases according to the large I of internal diameter or reduces thickness), adopt aramid fiber cellular composite material to make.
Described insulation pipe structure can be different according to service condition, make different pipe thickness, different rigidity intensity, different according to transport agent in pipeline, can select different interior cured layers.
The internal diameter of described interior cured layer 1 is D30mm ~ D500mm.
Embodiment 1
Internal diameter is the ultralight high strength ventilating and thermal insulating pipeline of D100mm, and pipe thickness is 13mm; Tube wall arranges in cyanuric acid salt resinae, domestic and abroad cured layer, and honeycomb insulation layer thickness is respectively 5mm, and this ultralight high strength ventilating and thermal insulating pipeline weight is about 1/5th of conventional material pipeline, and strength and stiffness is 9-37 times of conventional material pipeline.30 years can be run at 0 DEG C-150 DEG C.

Claims (4)

1. a ultralight high strength ventilating and thermal insulating pipeline, is characterized in that: this insulation pipe comprises interior cured layer (1) from inside to outside successively, the first honeycomb thermal insulation layer (2) be compounded on interior cured layer (1), the middle cured layer (3) be compounded on the first honeycomb thermal insulation layer (2), the second honeycomb thermal insulation layer (4) be compounded on middle cured layer (3), the outer cured layer (5) be compounded on the second honeycomb thermal insulation layer (4).
2. one according to claim 1 ultralight high strength ventilating and thermal insulating pipeline, it is characterized in that: the wall thickness after described interior cured layer (1), middle cured layer (3) and outer cured layer (5) solidification is 1mm, adopt cyanamide esters resin or carbon-fiber cloth to make its composite curing connect shaping making by hot-forming compound or vacuum bag complex technique.
3. one according to claim 1 ultralight high strength ventilating and thermal insulating pipeline, is characterized in that: the wall thickness of described first honeycomb thermal insulation layer (2) and the second honeycomb thermal insulation layer (4) is 5mm, adopts aramid fiber cellular composite material to make.
4. one according to claim 1 ultralight high strength ventilating and thermal insulating pipeline, is characterized in that: the internal diameter of described interior cured layer (1) is D30mm ~ D500mm.
CN201520427308.4U 2015-06-19 2015-06-19 A kind of ultralight high strength ventilating and thermal insulating pipeline Active CN204717238U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520427308.4U CN204717238U (en) 2015-06-19 2015-06-19 A kind of ultralight high strength ventilating and thermal insulating pipeline

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520427308.4U CN204717238U (en) 2015-06-19 2015-06-19 A kind of ultralight high strength ventilating and thermal insulating pipeline

Publications (1)

Publication Number Publication Date
CN204717238U true CN204717238U (en) 2015-10-21

Family

ID=54316239

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520427308.4U Active CN204717238U (en) 2015-06-19 2015-06-19 A kind of ultralight high strength ventilating and thermal insulating pipeline

Country Status (1)

Country Link
CN (1) CN204717238U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017101492A1 (en) * 2015-12-16 2017-06-22 上海晋飞新材料科技有限公司 Process for manufacturing bottom plate of high-speed rail equipment cabin using composite material
CN109616299A (en) * 2018-12-21 2019-04-12 江苏源通电气有限公司 A kind of half latent type ring oxygen resin casting dry-type transformer
WO2021035878A1 (en) * 2019-08-28 2021-03-04 澳科利高新技术(无锡)有限公司 Flexographic honeycomb support printing sleeve

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017101492A1 (en) * 2015-12-16 2017-06-22 上海晋飞新材料科技有限公司 Process for manufacturing bottom plate of high-speed rail equipment cabin using composite material
CN109616299A (en) * 2018-12-21 2019-04-12 江苏源通电气有限公司 A kind of half latent type ring oxygen resin casting dry-type transformer
CN109616299B (en) * 2018-12-21 2021-04-13 江苏源通电气有限公司 Semi-submersible epoxy resin cast dry-type transformer
WO2021035878A1 (en) * 2019-08-28 2021-03-04 澳科利高新技术(无锡)有限公司 Flexographic honeycomb support printing sleeve

Similar Documents

Publication Publication Date Title
CN104761880B (en) Short fiber reinforced pultrusion composite materials solar components frame and preparation method thereof
CN102424574B (en) Carbon fiber reinforced phosphate composite material forming process
CN105500837B (en) The technique that composite makes high ferro equipment compartment apron board
CN204717238U (en) A kind of ultralight high strength ventilating and thermal insulating pipeline
CN104589672A (en) Preparation method of shape memory composite material
CN105904741B (en) A kind of high temperature resistant composite bay section forming method of band edge frame
CN105799185B (en) A kind of forming method of advanced High Temperature Resistant Polyimide Composites thin-walled helical antenna Supporting Media pipe
CN103991225B (en) The curing of three dimensional separation disjunctor reinforced resin based composites and the micro-wave oven of solidification
CN113427793B (en) High-strength high-temperature-resistant composite material air inlet channel and forming method thereof
CN101736476A (en) Foam filled stereoscopic reinforced material
CN204527613U (en) A kind of aircraft D braided composites propeller blade
CN104743099B (en) A kind of aircraft D braided composites propeller blade and preparation method thereof
CN104725779A (en) Glass fiber reinforced plastic
WO2015153475A1 (en) Systems and methods of producing a structural and non-structural homogeneous and hybrid composite panels, prepregs, hand layup panels with &#34;basalt&#34; fiber, various composite materials, and additives
CN106739009A (en) A kind of cellular stereo fabric composite of global formation and preparation method thereof
CN104499149B (en) A kind of hollow sandwich revolving body fabric and application thereof
CN108327168A (en) The production method of D braided composites cored screw spring
US11504922B2 (en) Multi-layered composite structures and methods for the preparation thereof
CN105895837A (en) Application of carbon fiber composite material in battery box body for electric vehicle
CN107081917A (en) A kind of deep camber Foam Core Sandwich Structure moulding technique
CN201648829U (en) Foam-filled stereoscopic reinforcing material
CN205724730U (en) A kind of high strength glass fiber reinforced plastics cable duct tube
CN101787602A (en) Three-dimensional reinforced fabric knitted with foam strips
CN111098526B (en) Preparation method of high-strength pressure-resistant arc-shaped top head workpiece
CN106584701A (en) Forming method for sewing body enhanced composite steering engine protection plate

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C41 Transfer of patent application or patent right or utility model
TR01 Transfer of patent right

Effective date of registration: 20160914

Address after: 130000 Jilin province Changchun city two District Road No. 1250 Huigong inland port inspection building 11 floor

Patentee after: Jilin Hao Yuan agriculture and forestry planning and Design Co., Ltd.

Address before: 130000 Jilin province Changchun city two District Road No. 1250 Huigong inland port inspection building room 1003

Patentee before: JILIN JINYU TECHNOLOGY CO., LTD.