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125results about How to "Improve interlayer strength" patented technology

Carbon nano-tube connecting carbon fiber multi-scale reinforcing body and method for producing the same

InactiveCN101173386ATake full advantage of mechanical propertiesRealize chemical bond connectionFibre treatmentArtificial filament chemical after-treatmentFiberCarbon fibers
The invention discloses a multi-scale reinforcement body that carbon nano-tube is connected with carbon fiber and a preparation method aiming at solving the drawbacks of increasing rigidity at the interface, lowering toughness of material and not improving performance of resin base between the fibers and between carbon fiber plywoods after prior carbon fiber treatment is made. The multi-scale reinforcement body of carbon nano-tube connecting carbon fiber is made through combining between a carbon nano-tube decorated by 1, 6 hexamethylenediamine and carbon fiber with acyl chloride functional group on the surface. The preparation method comprises: the carbon nano-tube decorated by 1, 6 hexamethylenediamine and the carbon fiber with acyl chloride functional group on the surface are prepared before put into N,N-dimethylformamide for reaction, thereby getting the multi-scale reinforcement body of carbon nano-tube connecting carbon fiber. The invention has the advantages of big activity on the surface, a plurality of chemical activated functional groups, strong reactive activity, good cohesiveness with the base, improving shearing intensity at the interface for composite material by 127.5% to 144.7% and improving toughness for the base by 34.43% to 48.67%.
Owner:HARBIN INST OF TECH

Heat preventing and insulating stealth compound material with broad-band wave absorption and preparation method thereof

ActiveCN107555940AMeet the needs of impedance matchingRealize broadband absorbing functionLamination ancillary operationsLaminationWeight gainingControllability
The invention discloses a heat preventing and insulating stealth compound material with broad-band wave absorption and a preparation method thereof. The compound material comprises a cold-faced panel,a first aerogel compound material heat-insulating layer, a first resistance high-temperature super-material layer, a second aerogel compound material heat-insulating layer, a second resistance high-temperature super-material layer, a third aerogel compound material heat-insulating layer and a hot-faced panel from inside to outside sequentially. In the aspect of heat preventing and insulating performance, compared with existing heat insulating tiles and cover plate type heat prevention systems, the integrated heat preventing and insulating stealth compound material has the advantages of good heat insulating performance, excellent mechanical performance, large component preparation availability, high reliability, easiness in maintenance and the like; and in the aspect of stealth performance, the technical scheme adopting the high temperature super-material has the advantages of strong designability and easiness in broad-band wave absorption implementation, weight gain is hardly generated in comparison with the technical scheme of a cold-faced by adopting a wave absorbing material, absorbent is not required to be added into a heat preventing and insulating material, the heat preventing and insulating performance is not influenced, and the material has good uniformity and strong controllability.
Owner:NAT UNIV OF DEFENSE TECH

Carbon fiber composite material laminated plate with piezoelectric damping and preparation method thereof

InactiveCN102700203AExcellent piezoelectric damping performanceIncrease dampingSynthetic resin layered productsLaminationCarbon nanotubeGreek letter sigma
The invention provides a carbon fiber composite material laminated plate with piezoelectric damping and a preparation method thereof, and relates to a carbon fiber composite material laminated plate and a preparation method thereof. The invention aims to solve the problems that a polarization process is complex and a practical application is bad in the prior art. The carbon fiber composite material laminated plate comprises piezoelectric ceramic powder, carbon nano-tube and bismaleimide carbon fiber prepreg. The preparation method comprises the following steps of: preparing bismaleimide resin solution into the carbon fiber prepreg; grinding the polarized piezoelectric ceramic into the piezoelectric ceramic powder, and mixing the piezoelectric ceramic powder with the bismaleimide resin solution and the acidized carbon nano-tube so as to obtain pre-mixing sizing material after ultrasound; and laying the carbon fiber prepreg in a mold, painting the pre-mixing sizing material on the carbon fiber prepreg, and placing the carbon fiber prepreg into a hot press for processing so as to obtain the product. The damping los factor Delta tan sigma of the carbon fiber composite material laminated plate is more than or equal to 0.016 under a normal temperature, and the interlayer strength is improved by 3%-7%. The carbon fiber composite material laminated plate is applied to fields of aerospace crafts, naval vessels which have special usage requirements on material mechanical property and vibration and noise reduction.
Owner:HARBIN INST OF TECH

High-thermal-conductivity laminated graphene composite material and preparation method thereof

ActiveCN108276615ALarge size adjustabilityImprove thermal conductivityCvd grapheneSolvent
The invention discloses a high-thermal-conductivity laminated graphene composite material, and a preparation method thereof. The high-thermal-conductivity laminated graphene composite material comprises reduced graphene oxide, oxidized cellulose nanocrystalline, and epoxy resin; possesses a laminated structure which is mainly alternatively composed of reduced graphene oxide layers and oxidized cellulose nanocrystalline/epoxy resin layers; the oxidized cellulose nanocrystalline/epoxy resin layer is a mixture of oxidized cellulose nanocrystalline and the epoxy resin; the mass ratio of reduced graphene oxide to oxidized cellulose nanocrystalline is controlled to be 2:1-1:9; the mass ratio of reduced graphene oxide to epoxy resin is controlled to be 6:1-1:15. According to the preparation method, modification on the internal composition and the structure of the high-thermal-conductivity laminated graphene composite material, the whole process technology design and the steps of the preparation method is carried out, solvent volatilization self assembling is adopted to prepare the high-thermal-conductivity laminated graphene composite material, so that problems in the prior art such as small graphene composite size and poor thermal conductivity are solved, and the thermal conductivity of the high-thermal-conductivity laminated graphene composite material is capable of reaching 9 to 30W*m<-1>*K<-1>.
Owner:HUAZHONG UNIV OF SCI & TECH

Multi-dimensional Weaving Shaping Machine of Composite Materials

The disclosure provides a multi-dimensional weaving shaping machine of composite materials, including: a guide template including a plurality of cylindrical guiders arranged according to the geometrical shape of a prefabricated member; an electrical control three-dimensional motion mechanism including: a control signal receiving terminal configured to receive motion control signals corresponding to the geometrical shape of the prefabricated member; and a three-dimensional motion output terminal configured to form a motion track according to the motion control signals; a weaving needle being connected with the three-dimensional motion output terminal and making weave fibers distribute among the cylindrical guiders according to the geometrical shape of the prefabricated member. The multi-dimensional weaving shaping machine of composite materials of the disclosure utilizes the cylindrical guiders and the electrical control three-dimensional motion mechanism to make the weaving needle to drive braided cords to distribute among the cylindrical guiders along the motion track to form the guide template. The disclosure is applicable to multi-dimensional weaving shaping of large-scale and complicated materials and capable of improving the interlaminar strength of composite materials. The shaping machine applies a rapid shaping technology to multi-dimensional weaving shaping of composite materials and the technical processes are automatic.
Owner:ADVANCED MFG TECH CENT CHINA ACAD OF MASCH SCI & TECH

Manufacturing method of all-composite case of rocket engine

The invention discloses a manufacturing method of an all-composite case of a rocket engine. The manufacturing method comprises the following steps: 1) manufacturing joints; 2) manufacturing a core mold middle section; 3) manufacturing a skirt; 4) manufacturing a heat insulation core mold: manufacturing a rubber layer on the end face, close to the core mold, of each joint manufactured in the step 1), then installing the joints and seal head rubber layers at the two ends of the core mold, and finally, laying a heat insulation layer on the surface of the core mold middle section, manufactured inthe step 2), by employing a laying process, and performing vacuumizing and pre-compacting after heat insulation layer laying to obtain the heat insulation core mold; (5) performing fiber winding: winding carbon fiber yarns impregnated with resin around the heat insulation core mold by cooperating spiral inclined winding with hoop winding, wherein a glue solution on the surface of a winding layer needs to be scraped off in the winding process; after fiber winding is finished, making the skirt manufactured in the step 3) sleeve the two ends of the core mold wound with the fibers, and performinghoop winding after fixation is completed; 6) curing; and 7) demolding. The manufacturing method has the characteristics of that the weight reduction effect is obvious, the reliability is high, the cost is low and the bursting pressure is high.
Owner:JIANGSU XINYANG NEW MATERIALS CO LTD

Construction method using glass fiber reinforced plastics as inner cavity protective materials for steel and concrete chimney

InactiveCN103397803AThere will be no delaminationImprove flatnessTowersGlass fiberFlue gas
The invention discloses a construction method using glass fiber reinforced plastics as inner cavity protective materials for a steel and concrete chimney, and belongs to the field of flue gas emission. A novel structure is proposed to enable the chimney to be higher in strength and longer in service life. Firstly, a mold having an identical shape and a slightly smaller diameter with the steel and concrete chimney is made, the mold is formed by at least one single mold body, a gel coat with the thickness of 0.3mm to 0.4mm coats or is sprayed on the outer surface of the single mold body, then a glass fiber reinforced plastics composite reinforcement layer is made in a pasting mode, then the single mold body is assembled in the chimney, then resin slurry is injected between the glass fiber reinforced plastics composite reinforcement layer and the inner surface of the chimney, and finally the mold is demounted. The construction method using the glass fiber reinforced plastics as the inner cavity protective materials for the steel and concrete chimney is widely applied to the field of flue gas emission, and prevents sulfur dioxide, smog and other harmful gases which are not eliminated completely from bringing adverse effects on the steel and concrete chimney.
Owner:QINGSHAN ENVIRONMENTAL PROTECTION PROJECT

Thin-walled tubular model slicing method and system of five-axis 3D printer and printing method

The invention provides a thin-walled tubular model slicing method and system of a five-axis 3D printer and a printing method. The thin-walled tubular model slicing method comprises the steps that a coordinate system is established, and a three-dimensional model of a to-be-printed workpiece is read; the gravity center of each height cross section of the three-dimensional model is extracted, and all gravity centers are sequentially connecting to obtain a gravity center curve; rotation transformation is performed on a working turntable to enable the projection of a curvature vector of the gravity center curve of the current height layer of the three-dimensional model on the horizontal plane to be zero, the rotating posture information of the working turntable corresponding to the current height layer of the three-dimensional model is obtained, and the slicing information of the current height layer of the three-dimensional model is obtained through calculation; and the current height layer of the three-dimensional model is updated, and the steps are repeated until hierarchical slicing is completed, and the hierarchical slicing information of the to-be-printed workpiece is obtained; According to the thin-walled tubular model slicing method, the projection of the curvature vector of the gravity center curve of the current height layer of the three-dimensional model on the horizontal plane is enabled to be zero through rotation transformation of the table top of the turntable, the posture of the three-dimensional model is adjusted to be vertically upward, support-free printing is realized, the printing effect is good, and the surface precision of a formed part is high.
Owner:XI AN JIAOTONG UNIV
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