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205results about How to "Improve impregnation efficiency" patented technology

Novel liquid polycarbosilane as well as preparation method and application thereof

The invention discloses novel liquid polycarbosilane which is low in viscosity and high in storage stability and is crosslinkable, a preparation method of novel liquid polycarbosilane, and an application of novel liquid polycarbosilane. Polycarbosilane is prepared by adopting chloromethyl alkoxy silane or mixtures of chloromethyl alkoxy silane as raw materials by virtue of Grignard coupling reaction and reduction reaction, and the structure of polycarbosilane is shown in a formula (I) in the specification. The structure simultaneously contains Si-H bonds and unsaturated bonds such as C=C bonds, can be subjected to self-crosslinking and curing under a certain condition, has relatively high ceramic yield, and can be used as a silicon carbide precursor of a polymer precursor impregnation pyrolysis (PIP) process. Polycarbosilane disclosed by the invention is adjustable in structural composition, good in storage stability, low in viscosity and relatively low in boiling point, and has the utilization potentiality of being used as a silicon carbide ceramic precursor for chemical vapor deposition/chemical vapor infiltration (CVD/CVI). In addition, polycarbosilane can also be used for replacing commonly-used divinyl benzene to serve as a crosslinking agent of solid-state polycarbosilane (PCS).
Owner:淄博市临淄齐泉工贸有限公司

High-temperature-resistant high-strength aluminum oxide fiber enhanced composite material and preparation method thereof

The invention relates to a high-temperature-resistant high-strength aluminum oxide fiber enhanced composite material and a preparation method thereof. The preparation method comprises the following steps of: by taking a two-dimensional cloth paving layer and 2.5D woven or orthogonally three-dimensional woven continuous aluminum oxide fiber preform as an enhancer, preparing a matrix through a double nano composite impregnation liquid where silicon dioxide and aluminum oxide are uniformly mixed; and finally obtaining the aluminum oxide fiber enhanced composite material through the process of vacuum pressure impregnation, micro-positive pressure medium and low temperature pre-curing, micro-positive pressure curing and atmosphere temperature programming sub-sectional thermal treatment, wherein the mass ratio of silicon dioxide to aluminum oxide in the composite material is (19:1)-(12:8), and the volume content of the aluminum oxide fibers is 30-60%. The prepared composite material has a high-temperature-resistant property and a high-temperature mechanical property, and is high in compactness; the room temperature tensile strength of the material reaches 310+/-30MPa, the tensile strength at 1100 DEG C reaches 135+/-20MPa, and the tensile strength at 1200 DEG C reaches 90+/-10MPa; and compared with a similar quartz fiber enhanced silicon dioxide oxide/oxide composite material, the performance is improved by 4-5 times.
Owner:AEROSPACE RES INST OF MATERIAL & PROCESSING TECH +1

Fast impregnation method for capacitor core package and device thereof

The invention discloses a fast impregnation method for a capacitor core package. The method comprises the following steps of putting the core package required to be impregnated into an impregnation tank, and sealing the impregnation tank; opening a liquid storing barrel, pouring the impregnation liquid into the liquid storing barrel; vacuumizing the impregnation tank through a vacuum constant pressure device; during vacuumizing, extracting moisture and air in the core package of the capacitor at the same time; injecting the impregnation liquid from the liquid storing barrel in the impregnation tank in a vacuum state; immersing the core package of the capacitor in the impregnation liquid, fast penetrating the impregnation liquid in the core package of the capacitor to be impregnated by the vacuum state in the impregnation tank, keeping the vacuum state in the impregnation tank; releasing the vacuum state in the impregnation tank instantaneously to be normal atmosphere, and penetrating the impregnation liquid in the core package of the capacitor to be impregnated by the atmospheric pressure. The invention further discloses a device for implementing the method. The method and device provided by the invention has the advantages of short impregnation time, high efficiency, good impregnation quality and low energy consumption.
Owner:李玉祥

Three-dimensional fiber prefabricated-part enhancement mullite composite and preparation method thereof

The invention discloses a three-dimensional fiber prefabricated-part enhancement mullite composite and a preparation method thereof. The preparation method comprises impregnating three-dimensional fiber prefabricated parts in an A1203-SiO2 composite sol to be impregnated, dried and subjected to low-temperature thermal processing to obtain the A1203-SiO2 impregnated three-dimensional fiber prefabricated parts; repeating the process till the weight gaining of the A1203-SiO2 impregnated three-dimensional fiber prefabricated parts is lower than 1% to obtain three-dimensional fiber prefabricated-part first intermediates, performing medium-temperature thermal processing, subjecting the medium-temperature thermal processed three-dimensional fiber prefabricated-part first intermediates to impregnation, high-pressure processing, drying, low-temperature thermal processing and medium-temperature thermal processing, circulation the process till the weight gaining is lower than 1%, and performing high-temperature thermal treatment. According to the composite and the preparation method thereof, by three-stage thermal treatment, the compactness of the three-dimensional fiber prefabricated-part enhancement mullite can be further improved, and the mechanical performance and the oxidation resistance of the enhancement composite are enhanced.
Owner:NAT UNIV OF DEFENSE TECH

Composite rubber hose for conveying LPG, LNG and strongly corrosive chemical solvent and preparation method thereof

The invention discloses a composite rubber hose for conveying LPG, LNG and strongly corrosive chemical solvent and a preparation method thereof. Low density polyethylene, ultra-high molecular weight polyethylene and macromolecule cross-linked polyethylene serve as raw materials; after scientific compound and vulcanization of a rubber hose, a chemical substance with a good adhesive property is obtained for preparing a liner film; meanwhile, corona treatment is carried out on the bonding face of the liner film and the bonding face of the rubber hose, and fiberglass reinforcing fiber with radiation protection performance is compounded on the surface layer; therefore, the surface layer of the rubber hose has good radiation protection performance, hidden danger of conveying pipelines caused by ionizing radiation is avoided, and finally the composite rubber hose which has the firmly bonded liner film, and is high in radiation protection and capable of conveying LPG, LNG and strongly corrosive chemical solvents is prepared, the hose can absorb as much as 97.5% to 99.5% of X-rays, gamma-rays and various neutrons in nuclear radiation, and the adhesive force (N/25mm) between the liner film and a rubber layer reaches 160-180.
Owner:河北泽邦塑胶科技有限公司

Thermoplastic composite preimpregnation body plate

InactiveCN103613775ASolving Effective Impregnation ProblemsGuaranteed to pass the siphon testSynthetic resin layered productsEnvironmental resistancePolymer science
The invention discloses a thermoplastic composite preimpregnation body plate, which is prepared by a thermoplastic composite preimpregnation body or is compounded by the thermoplastic composite preimpregnation body and thermoplastic polymer through hot melting. The thermoplastic composite preimpregnation body is prepared by steps of steeping fabric prepared by reinforced fibers in thermoplastic polymer aqueous dispersion, drying and dehydrating, melting the polymer, cooling and shaping, and the length of the reinforced fibers is more than 2cm. According to the preparation method of the thermoplastic composite preimpregnation body, an organic solvent is not used, water is taken as a dispersion medium, the aqueous dispersion of polymer substitutes for the organic solvent, so that the preparation method is environment-friendly; the aqueous dispersion used by the preparation method has low viscosity and is beneficial to steeping of the polymer on fiber bundles, the immersion treatment is convenient, the production efficiency is high, the production cost is low, and the problem of effectively steeping the reinforced fiber fabric by the thermoplastic polymer is solved; compared with the composite board prepared by the prior art, the preimpregnation body plate is sharply improved in tensile strength and deformation performance.
Owner:南京彤天广元高分子材料有限公司

Method for improving high temperature mechanical properties of hollow turbine blade ceramic mold

The invention discloses a method for improving high temperature mechanical properties of a hollow turbine blade ceramic mold. According to the invention, a yttrium-aluminum garnet high temperature strengthening phase is synthesized from yttrium oxide and alumina through high temperature sintering, magnesium oxide is utilized at the same time for inhibiting growth of an alumina crystal grain under the condition of high temperature sintering, and titanium oxide is used for solution strengthening of alumina so as to improve high temperature strength of an alumina-based ceramic mold; finally, an yttrium chloride ion solution is used for dipping of the alumina-based ceramic mold to allow yttrium ions to be uniformly distributed in the alumina-based ceramic mold with a complex structure, so on the one hand, chloride ions are enabled to react with impurity Na and K ions in an alumina ceramic material to form sodium chloride and potassium chloride under high temperature sintering, thereby removing the Na element and the K element, and on the other hand, the yttrium ions are enabled to react with alumina under high temperature sintering for secondary formation of the yttrium-aluminum garnet high temperature strengthening phase. The method provided by the invention can be used for improving high temperature mechanical properties of a core-shell integrated alumina-based ceramic mold for a hollow turbine blade and improves a qualified rate of a directionally solidified high temperature alloy blade.
Owner:XI AN JIAOTONG UNIV +1

Insulating impregnating treatment technology of alternating current motor stator and treatment device thereof

The invention discloses an insulating impregnating treatment technology of an alternating current motor stator. The technology comprises the following steps that 1, the alternating current motor stator is loaded at an impregnating treatment station, and a three-phase winding of the alternating current motor stator is plugged into a three-phase alternating power; 2, the three-phase alternating current is applied to the three-phase winding of the alternating current motor stator, so that the alternating current motor stator is preheated; 3, the alternating current motor stator is cooled; 4, a paint tank is controlled to go up, so that the alternating current motor stator is soaked in the paint tank for impregnating treatment, and after impregnating treatment is completed, the paint tank is controlled to go down; 5, the three-phase alternating current is applied to the three-phase winding of the alternating motor stator to make paint of the winding of the alternating current motor statorheated and solidified; 6, the alternating current motor stator is unloaded, a wire between the three-phase winding of the alternating current motor stator and the power is disconnected, and finally, discharging is conducted. The invention further discloses a treatment device for achieving the insulating impregnating treatment technology of the alternating current motor stator. By means of the technology and the device, the impregnating efficiency is high, the impregnating filling effect is better, and energy consumption is lower.
Owner:CHUANGQU SHANGHAI NEW ENERGY TECH CO LTD

Method for preparing HfC-SiC modified C/C composite with high-temperature infiltration-pyrolysis process

The invention relates to a method for preparing an HfC-SiC modified C / C composite with a high-temperature infiltration-pyrolysis process. The method comprises the following steps: a carbon felt is cleaned and dried, and a low-density porous preform is prepared through isothermal chemical vapor deposition; an HfC precursor and polycarbosilane mixed solution is prepared to be taken as a precursor of an HfC-SiC ceramic phase, subjected to vacuum infiltration in an environment at about 110 DEG C and infiltrated into the preform, pyrolysis is performed, the high-temperature infiltration-pyrolysis process is repeated until the material gets densified, and the HfC-SiC modified C / C composite is prepared. The method has the beneficial effects as follows: based on the characteristic that the viscosity of the high-concentration polycarbosilane and HfC precursor mixed solution decreases with increasing temperature, the precursor mixed solution with high concentration is infiltrated into the porous C / C preform when the temperature is 90-110 DEG C, so that the porous C / C preform is filled fully faster, ceramic is uniformly and densely distributed in the preform, the final density reaches 2.4-2.7 g / cm<3>, the material preparing period is shortened, and the material preparing efficiency and the distribution uniformity of the ceramic phase in the material are improved.
Owner:NORTHWESTERN POLYTECHNICAL UNIV
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