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90results about How to "Improves Antioxidant Properties" patented technology

Premix mate for laying hens in egg producing period and preparation and application of premix mate

The invention provides a premix mate for laying hens in an egg producing period and a preparation and application of the premix mate and belongs to the field of animal feeds. The premix mate for the laying hens in the egg producing period is prepared from the following raw materials in parts by weight: peanut meal, hot chili residues, fermented cake meal and amino acid, sodium bicarbonate, betaine, hemoprotein, limestone powder, mycoprotein, a shell treasure, calcium hydrophosphate, quercetin, a mildew inhibitor, perennial sowthistle powder, compound probiotics and the like. According to the premix mate for the laying hens in the egg producing period, one part of bean pulp in a complete formula feed can be replaced, the antioxidant activity of the laying hen bodies can be effectively improved, the digestion and absorption rate and the conversion rate of the laying hens in the egg producing period are effectively improved, the immunity is significantly improved, healthy intestinal tracts of the laying hens are ensured, too thin faeces are prevented, unhairing of the egg producing period is improved and slow growth condition of feather is improved. For the conditions of poor quality of egg shells, multiple broken eggs and a short peak laying period, the colors and the quality of the egg shells are effectively improved, the health of bodies is promoted, the production performance is improved and the egg production period is prolonged.
Owner:ZHENGZHOU HEFENG ANIMAL HUSBANDRY +1

High-Mo Ni3Al-based monocrystal high-temperature alloy modified by rare earth and preparation method of high-Mo Ni3Al-based monocrystal high-temperature alloy

The invention discloses high-Mo Ni3Al-based monocrystal high-temperature alloy modified by rare earth and a preparation method of the high-Mo Ni3Al-based monocrystal high-temperature alloy and belongs to the technical field of high-temperature alloy. The alloy comprises Ni, Al, Mo, Re, Ta, Cr, C, Y and Dy or Ce, an alloy casting-state structure comprises three phase structures including the gamma' phase, the gamma phase and the white precipitated phase rich in Mo and Re, the density is 7.9-8.1 g/cm<3>, and the alloy can reach the complete oxidization resistance level or the oxidization resistance level or the secondary oxidization resistance level at the temperature of 1100 DEG C. The method comprises the steps of preparing a liquid metal cooling medium, preparing a mother alloy bar, preparing Ni3Al-based monocrystal alloy seed crystals not containing rare earth elements, preparing high-Mo Ni3Al-based high-temperature alloy containing the rare earth elements through a direction monocrystal furnace, and conducting post heat treatment. The Ni3Al-based monocrystal high-temperature alloy provided by the invention is low in density and can meet the low-density requirement of aircraft engines, and the oxidization resistance of the alloy can reach the complete oxidization resistance level or the oxidization resistance level or the secondary oxidization resistance level at the temperature of 1100 DEG C.
Owner:BEIHANG UNIV

Multilayer antioxidant high-temperature-resistant SiC/Ta/C/Ta/SiC coating and preparation method thereof

ActiveCN103722849AImproves antioxidant propertiesMitigates differences in coefficient of thermal expansionLayered productsOxidation resistantMicrostructure
The invention discloses a multilayer antioxidant high-temperature-resistant SiC/Ta/C/Ta/SiC coating and a preparation method thereof. The multilayer antioxidant high-temperature-resistant SiC/Ta/C/Ta/SiC coating is formed by laminating SiC layers, Ta layers and C layers, and is characterized in that the laminating sequence is the SiC layer, the Ta layer, the C layer, the Ta layer and the SiC layer, or SiC layer, the Ta layer, the C layer, the Ta layer, the SiC layer, SiC layer, the Ta layer, the C layer, the Ta layer, and the SiC layer, or SiC layer, the Ta layer, the C layer, the Ta layer, the SiC layer, SiC layer, the Ta layer, the C layer, the Ta layer, the SiC layer, SiC layer, the Ta layer, the C layer, the Ta layer and the SiC layer; both sides of the C layer are Ta layers; the innermost layer and the outermost layer are SiC layers; and the Ta layer, the C layer, the Ta layer and the SiC layer are sequentially deposited on the prepared SiC layer with a chemical vapor deposition method so as to obtain the multilayer antioxidant high-temperature-resistant SiC/Ta/C/Ta/SiC coating. According to the coating and the preparation method thereof, the outer SiC layer forms a layer of SiO2 film in a high-temperature aerobic environment, so that diffusion of oxygen atoms can be prevented effectively, and meanwhile, a TaC layer can be formed on a contact surface of the Ta layer and the C layer to further improve the antioxidation performance. Alternate deposition of coatings can effectively relieve differences of coefficients of thermal expansion of the coatings and improve the thermal shock performance of the coatings remarkably, the thickness and lay number of a matrix can be controlled by controlling deposition time and deposition times, and the microstructure of the composite coating can be controlled.
Owner:TAICANG PAIOU TECH CONSULTING SERVICE

Gate device for small water conservancy project

The invention relates to a gate device for a small water conservancy project, and relates to the technical field of water conservancy projects. The lower end of a guiding rod is fixed to a protectingplate, and the surface of the protecting plate is coated with an anti-oxidation coating, the protecting plate is arranged on the side face of a gate plate and is in fit arrangement with the side faceof the gate plate, the protecting plate is movably arranged in a gate frame below a cross bar in an up and down mode, a second bearing base is fixed to the top surface of the protecting plate, the lower end of a screw rod is inserted into a bearing fixed in the second bearing base, the screw rod is rotationally fixed on the cross bar through a screw rod base, the upper part of the screw rod is rotationally connected with an inner threaded sleeve through a ball bearing, the ball bearing is embedded in the first bearing base, the first bearing base is fixed on the side surface of the top edge ofthe gate frame, and an protecting plate lifting hand wheel sleeves the outer part of the inner threaded sleeve. The gate device can increase the oxidation resistance of the gate plate according to the using condition, the service life of the gate is effectively prolonged, meanwhile, impurities deposited at the bottom of the gate frame can be effectively eliminated, and the sealing performance ofthe gate plate is improved.
Owner:河南省河川工程监理有限公司

Repairing method of SiC/SiC ceramic-based composite material

A repairing method of a SiC/SiC ceramic-based composite material comprises the following steps: polishing the surface of a test sample, cleaning and drying, corroding the test sample by HF, cleaning and drying, ultrasonically cleaning, drying and soaking into a catalyst solution prepared from iron, cobalt or nickel, performing vacuum drying, wrapping the test sample with graphite paper and only exposing a fracture; and putting the test sample into a vacuum furnace, introducing methyltrichlorosilane, H2 and Ar, preserving heat for 5 to 20 hours, closing methyltrichlorosilane and H2, preservingheat for 10 to 100 minutes, closing Ar, introducing NH3, BCl3, H2 and N2, preserving heat for 5 to 20 hours, closing NH3 and BCl3, introducing methyltrichlorosilane and H2, preserving heat for 50 to 300 hours, taking out the test sample, removing the graphite paper, polishing and repairing the surface, putting the treated sample into the vacuum furnace, introducing methyltrichlorosilane, H2 and Ar, preserving heat for 5 to 30 hours, and spray-coating a composite coating consisting of yttrium silicate and mullite by a plasma spray-coating method. Main injury that the SiC/SiC composite materialis liable to generate can be repaired, the material composition is not changed after repairing, and the anti-oxidation property of the material under the high-temperature environment is improved.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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