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158results about How to "Good anti-icing effect" patented technology

Polymer ice-coating-preventing coating containing modified nano particles and preparing method thereof

The invention discloses a polymer ice-coating-preventing coating containing modified nano particles and a preparing method of the polymer ice-coating-preventing coating containing modified nano particles. The ice-coating-preventing coating comprises, by mass, 1-15% of silicone oil, 1-40% of modified nano particle with the particle diameter of 10-100nm, 15-75% of monomer or prepolymer used for bonding, 1-12% of hydrophobic resin, 1-30% of curing agent and 10-80% of thinning agent. The preparing method of the polymer ice-coating-preventing coating includes the steps that preparing of the modified nano particles is performed, preparing of the hydrophobic resin is performed, and the modified nano particles, the hydrophobic resin, the monomers or the prepolymers used for bonding, the curing agents, the thinning agent and silicone oil are evenly mixed to obtain the coating. The polymer ice-coating-preventing coating containing modified nano particles and the preparing method of the polymer ice-coating-preventing coating containing the modified nano particles have the advantages that raw materials for preparing the coating are easy to get, the process is simple, operation is convenient to carry out, a coating layer prepared by spraying the coating on a metal or glass substrate has a contact angle of 160 degrees in static water under a normal temperature and a low temperature, has a rolling angle of 4 degrees and has the good ice-coating-preventing effect.
Owner:XI AN JIAOTONG UNIV +1

Two-component waterborne wear-resisting and low-ice-adhesion anti-icing coating and coating layer, and preparation methods and applications thereof

The invention provides preparation methods of a two-component waterborne wear-resisting and low-ice-adhesion anti-icing coating and a coating layer thereof. The two-component waterborne anti-icing coating is composed of a component A containing a core-shell structure polymer emulsion and inorganic nanoparticles and a component B containing a curing agent. An outer layer of the core-shell structure polymer emulsion in the component A of the anti-icing coating is a hydrophilic shell layer, so that polymer emulsion particles can be stably dispersed in water, and the advantages of being green and environmentally friendly are provided. The inorganic nano particles in the component A are rigid particles, can improve the mechanical properties of the anti-icing coating layer, endow the coating layer with excellent wear resistance and prolong the service life of the coating layer. After the coating is cured into a film, the hydrophilic shell layer of the polymer emulsion particles can absorb moisture, and thus a water lubricating layer is formed on the surface of the coating layer; when the coating layer surface is iced, due to the existence of the water lubricating layer, the acting force between ice and the coating layer is decreased, besides, the substrate surface roughness is also reduced, and the contact area between the ice and the substrate is decreased.
Owner:CHINA SCI INTELFUSION INT TECH (BEIJING) CO LTD

Super-hydrophobic and anti-icing transparent coating and preparation method thereof

The invention discloses a super-hydrophobic and anti-icing transparent coating. The super-hydrophobic and anti-icing transparent coating is prepared by mixing super-hydrophobic inorganic nanoparticles, fluoroalkyl silane, fluorocarbon varnish, curing agents and organic diluents. A preparation method of the super-hydrophobic and anti-icing transparent coating comprises the following steps: adding a silane coupling agent into an organic solvent, uniformly mixing and then adding deionized water, uniformly dispersing the inorganic nanoparticles into the organic solvent containing the silane coupling agent through ultrasonic wave or a mechanical stirring method and dispersing for 2-4 hours; carrying out suction filtration, washing, drying, grinding via a mortar to obtain super-hydrophobic and anti-icing inorganic nanoparticle fillers; adding transparent fluorocarbon varnish into corresponding mass of fluoroalkyl silane, uniformly mixing at normal temperature, then uniformly dispersing the prepared super-hydrophobic and anti-icing inorganic nanoparticle fillers into the commercial fluorocarbon varnish by mechanically stirring, finally uniformly mixing the composition with the curing agents and the diluents, wherein the curing agents account for 0-10% of the total mass, and the diluents account for 8-18% of the total mass; and preparing the super-hydrophobic and anti-icing transparent coating. The coating has the advantages of strong binding force, super-hydrophobic property, anti-icing property and self-cleaning property.
Owner:LIAONING NORMAL UNIVERSITY

Anti-icing method of carbon crystal and wind power generator anti-icing system employing method

The invention relates to an anti-icing method of a carbon crystal and a wind power generator anti-icing system employing the method. The method comprises the steps of printing the nanosized conductive carbon crystal on a carrier surface, preparing a thinner carbon crystal electric hot plate with two electrodes by a curing technology and a hot-pressing technology, taking one out of layers forming a blade as a heating layer, dividing the heating layer into a plurality of heating zones, arranging on-line temperature monitoring in each heating zone, performing temperature rising control with power units in corresponding zones in a heating control cabinet, and keeping the surface temperature of zones to be heated higher than and approximate to 0 DEG C. The anti-icing control system controls the heating zones in a simultaneous or alternant operation mode, and conducts on-line automatic ice prevention or ice melting. According to the method and the wind power generator anti-icing system, since the carbon crystal electric hot plate is adopted as an electric heating material of an anti-icing blade, the manufacturing technology is simple, and the heating is uniform and controllable; and since the surface adopts an on-line temperature monitoring closed-loop control mode, the anti-icing operation is stable, safe, and energy-saving.
Owner:XEMC NEW ENERGY

Preparing method for aluminum surface super-hydrophobic coating with micro-nano composite structure

The invention discloses a preparing method for an aluminum surface super-hydrophobic coating with a micro-nano composite structure. The method mainly comprises the steps that firstly, an aluminum sheet is ultrasonically cleaned for 10 min through acetone and methylbenzene and then flushed thoroughly through distilled water, and the aluminum sheet is dried in an oven at the temperature being 100 DEG C; secondly, the cleaned and dried aluminum sheet is immersed in an acid etching agent to be etched, and an aluminum surface with a micron rough structure is obtained; thirdly, after the etched aluminum sheet is ultrasonically cleaned thoroughly, the aluminum sheet is immersed in a nano particle solution, and after the aluminum sheet is treated at the high temperature, an aluminum surface with a micro-nano composite rough structure is obtained; and fourthly, after low-surface-energy fluorosilicone modified polyester resin is sprayed to the aluminum surface with the micro-nano composite rough structure, an aluminum surface with super-hydrophobic performance can be obtained. The super-hydrophobic aluminum sheet prepared through the preparing method has the superior icing preventing performance and very good mechanical strength and can be applied to an air conditioner heat exchange sheet, and frosting and icing of the heat exchange sheet are effectively restrained.
Owner:ZHEJIANG UNIV

Addition fluorinated silicone rubber nano antifreezing adhesive paint and preparation method thereof

InactiveCN103725199ADoes not affect the anti-icing effectGood anti-icing effectCoatingsPolymer scienceSilanes
The invention discloses addition fluorinated silicone rubber nano antifreezing adhesive paint and a preparation method thereof, belongs to the field of organic fluorinated silicon polymer materials, and overcomes the problems of the prior art that the coating curing temperature is high and the anti-icing effect is poor. The addition fluorinated silicone rubber nano antifreezing adhesive paint consists of a component A and a component B, wherein the component A comprises the following ingredients in parts by weight: 100 parts of vinyl-terminated polysiloxane, 30 to 50 parts of vinyl-terminated trifluoropropyl polysiloxane, 20 to 30 parts of nano particles and 20 to 30 parts of solvent; the component comprises the following ingredients in parts by weight: 9 to 12 parts of end hydrogen-containing silicone oil, 9 to 10 parts of end hydrogen-containing fluorine silicone oil, 20 to 30 parts of solvent, 0.0074 to 0.012 part of Karstedt catalyst, 0.05 to 1 part of defoaming agent and 1 to 2 parts of dispersing agent. The preparation method comprises the following steps of (1) uniformly mixing the ingredients according to the weight parts to obtain the component A, ball-milling the component A, and uniformly mixing the ingredients according to the weight parts to obtain the component B; (2) uniformly mixing the component A and the component B, uniformly smearing onto the surface of the workpiece which is coated with silane undercoat, and then curing the workpiece at room temperature. By adopting the paint, the anti-icing effect is good.
Owner:JILIN UNIV

Method for preparing perfluor liquid injection type transparent flexible anti-icing thin film through electrostatic spinning

The invention provides a method for preparing a perfluor liquid injection type transparent flexible anti-icing thin film through electrostatic spinning and belongs to the field of interface chemistry. An electrospinning film is prepared on the surface of aluminum foil through the electrospinning technology; the electrospinning film on the surface of the aluminum foil is transferred to the surface of a propping material through alcohol soaking, hot pressing and drying processes, and a porous electrostatic spinning nanofiber film is prepared; perfluor liquid is added to the surface of the porous electrostatic spinning nanofiber membrane dropwise, and the perfluor liquid injection type transparent flexible anti-icing thin film is obtained. The visible light transmittance of the prepared transparent flexible anti-icing thin film is more than 80%, the contact angles between water drops and the surface of the flexible anti-icing thin film are 113 degrees, and the rolling angles are 3 degrees. Most of the regions of the surface of the transparent flexible anti-icing thin film are frostless after 60 min under the condition of the -5 DEG C temperature and the 50% humidity, and the drop setting time is obviously prolonged compared with a traditional hydrophobic film.
Owner:BEIHANG UNIV

Nano-composite superhydrophobic icing-proof coating material and preparation method thereof

ActiveCN103819995AExcellent performancePersistent low surface energyCoatingsSurface energyDichloromethane
The invention discloses a nano-composite superhydrophobic icing-proof coating material. The nano-composite superhydrophobic icing-proof coating material comprises the following components in percentage by mass: 5-50% of fluorine-containing acrylate copolymer-modified inorganic nanoparticles and 50-95% of an organic solvent. A preparation method for the nano-composite superhydrophobic icing-proof coating material comprises the following steps: uniformly mixing nano-SiO2, methylbenzene and 3-aminopropyl triethoxysilane, and performing refluxing reaction in an oil bath to obtain amino-modified SiO2-NH2 inorganic nanoparticles; uniformly mixing the SiO2-NH2, dichloromethane, triethylamine and 2-bromoisobutyryl bromide, and reacting in an ice-water bath to obtain 2-bromoisobutyryl bromide-grafted nanoparticle SiO2-NH-Br; uniformly mixing the SiO2-NH-Br, an acrylate monomer, fluorine-containing acrylate, CuX, methylbenzene and a ligand, deoxidizing, precipitating, performing centrifugal separation, and dissolving a product into the organic solvent to obtain the nano-composite superhydrophobic icing-proof coating material. The nano-composite superhydrophobic icing-proof coating material has excellent performance, lasting low surface energy and superhydrophobicity, and good icing-proof performance and has the effect of prolonging the icing time, and can be widely used for prevention and control of icing on the surfaces of communication lines, fan blades, airport facilities, airplane wings and the like.
Owner:ZHEJIANG UNIV

Dielectric barrier discharge plasma anti-icing device and method

The invention discloses a dielectric barrier discharge plasma anti-icing device and method. A plurality of layers of polyimide adhesive tape are overlapped and pasted to serve as an insulation layer. Upper electrodes and lower electrodes are pasted along the two side faces of the insulation layer in a staggered mode. The upper electrodes are connected in parallel to be connected with a positive electrode of a plasma power source. The lower electrodes are connected in parallel to be connected with a negative electrode of the plasma power source. The insulation layer is fixed into a groove in the surface of an aircraft skin, and efficient anti-icing of the surface of an aircraft is achieved. Due to the fact that the thickness of the electrodes and the thickness of the insulation layer are very small, the effect of the electrodes and the insulation layer on the aerodynamic performance of the aircraft can be ignored. The dielectric barrier discharge plasma anti-icing device is simple in structure, and the electrodes can be flexibly distributed according to the different geometrical shapes of the frozen positions of the aircraft. When the voltage of the plasma power source is adjusted to 70 V and the current strength ranges from 1.5 A to 2.5 A, the voltage actually loaded to the electrodes can reach 10 KV or more, the responding time is short, the anti-icing effect is good, the implement method is convenient to implement and easy to achieve and has good application prospects, and no pollution exists.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Ice prevention and removal system for wing

PendingCN110834734ATo achieve the purpose of full coverage anti-icingImprove aerodynamic performanceDe-icing equipmentsWingsLeading edgeEngineering
The invention discloses an ice prevention and removal system for a wing. The system comprises a wing, wherein an electric heating system is distributed in the leading edge skin of the wing. The systemalso comprises a synthetic jet exciter distributed in the wing, wherein the synthetic jet outlet of the synthetic jet exciter is positioned on the surface of the wing and is positioned on the rear side of the ice prevention area of the electric heating system; and after a synthetic jet in the synthetic jet exciter is injected from the synthetic jet outlet, the synthetic jet mutually acts with water drops on the surface of the wing so as to change the movement trajectory of each water drop. By use of the ice prevention and removal system, the leading edge surface of the wing is heated throughthe electric heating system, so that the leading edge of the wing is kept in a certain temperature range. When cold water drops knock on the leading edge of the wing, since a surface temperature is high, water drops are not iced on the leading edge of the wing but flow form one layer of water film, and the water film flows to the back of the wing. When the water film flows to the synthetic jet outlet, due to the function of the synthetic jet, the water film changes an original movement locus so as to be far away from the rear surface of the wing, the formation of overflowing ice is avoided, and the aerodynamic performance and the safety performance of the wing are improved.
Owner:中国人民解放军63831部队

Wind turbine blade ice prevention and removal mechanism

Disclosed is a wind turbine blade ice prevention and removal mechanism belonging to ice prevention and removal technology. A hub is provided with a blade through a rotary joint B. A condenser is installed in the blade. Two ends of the condenser are respectively connected with the rotary joint B. A rotary joint A is installed on the rear end portion of a main shaft. A steam transfer pipe B and a liquid return pipe A are arranged in a shaft cavity of the main shaft. Two ends of the steam transfer pipe B are connected with the rotary joint A and the rotary joint B correspondingly. Two ends of theliquid return pipe A are connected with the rotary joint B and the rotary joint A correspondingly. A gear transmission box and a generator communicate with a heat accumulator through heat transfer pipes. An evaporator is installed in the heat accumulator. Two ends of the steam transfer pipe A are connected to the evaporator and the rotary joint A correspondingly. Two ends of a liquid return pipeB are connected to the rotary joint A and the evaporator correspondingly. A liquid pump and a valve are installed on the liquid return pipe B. The wind turbine blade ice prevention and removal mechanism uses waste heat energy generated by a wind turbine to carry out blade ice prevention and removal, thereby saving energy and being low in operation cost and good in operation effect.
Owner:NORTHEAST AGRICULTURAL UNIVERSITY

Anti-thunder and anti-icing pin type composite insulator for 10 kV transmission line

The invention discloses an anti-thunder and anti-icing pin type composite insulator for a 10 kV transmission line. The composite insulator comprises a mandrel, a composite insulator assembly, an insulating shed housing, a trunking fitting and a steel leg fitting, wherein the composite insulator assembly comprises a lower conductive heel block, a metal oxide resistor disc group and an upper conductive heel block which are sequentially arranged on the mandrel in a sleeving manner and are tightly attached; the composite insulator assembly is wrapped with the insulating shed housing; an insulating layer is arranged between the composite insulator assembly and the insulating shed housing; the trunking fitting penetrates through the insulating shed housing and is in threaded connection with the upper conductive heel block; the steel leg fitting penetrates through the insulating shed housing and is in threaded connection with the lower conductive heel block; two ends of the mandrel are connected with the trunking fitting and the steel leg fitting respectively. The anti-thunder and anti-icing pin type composite insulator for the 10 kV transmission line has the advantages of good anti-thunder and anti-icing effects, simplicity and convenience in installation, long service life, facilitation of reconstruction of a conventional electric transmission line and the like.
Owner:STATE GRID CORP OF CHINA +2

Non-Newtonian fuselage deicing and anti-icing fluid and preparation method thereof

ActiveCN103059813AExcellent shear recovery abilityLong anti-icing timeOther chemical processesPhysical chemistryRheopecty
The invention relates to a deicing and anti-icing fluid, particularly a non-Newtonian fuselage deicing and anti-icing fluid and a preparation method thereof. The non-Newtonian fuselage deicing and anti-icing fluid can reduce adhesion of ice on the object surface to eliminate and prevent icing on the aircraft fuselage surface, and has superlong anti-icing retention time. The non-Newtonian fuselage deicing and anti-icing fluid comprises the following components in parts by mass: 40-60 parts of freezing-point depressant, 0.05-1.2 parts of rheologic modifier, 0.01-0.3 part of anti-icing compounding agent, 0.01-3 parts of pH regulator, 0.01-3 parts of corrosion inhibitor, 0.01-0.5 part of staining agent and 40-60 parts of deionized water. The invention is based on the low-temperature rheologic research, especially aims at the low-temperature operating environment and characteristics of the deicing and anti-icing fluid, and determines the distribution and arrangement of the main chain and branch chain of the rheologic modifier as well as the preparation and acquisition method of the low-temperature conformation. By combining the anti-icing compounding agent, corrosion inhibitor and other assistants in the formula, the prepared deicing and anti-icing fluid has the characteristics of excellent shearing restorability, excellent ice adhesion inhibition capacity at 0 to -20 DEG C, and long anti-icing time.
Owner:成都民航六维航化有限责任公司

Self-repairing anti-icing aluminum stranded wire with composite holes and preparation method of self-repairing anti-icing aluminum stranded wire

The invention relates to a self-repairing anti-icing aluminum stranded wire with composite holes and a preparation method of the self-repairing anti-icing aluminum stranded wire, and belongs to the technical field of anti-icing material preparation. According to the self-repairing anti-icing aluminum stranded wire with the composite holes provided by the invention, the uniform porous aluminum oxide film grows on the surface of the aluminum substrate to form small-aperture inner layer holes (for storing a repairing agent for a long time) and large-aperture outer layer holes (for improving the anti-icing performance by increasing the air cushion proportion), the anti-icing aluminum wire with lasting and excellent anti-icing self-repairing performance is prepared by optimizing the aperture and thickness of the large holes (outer holes) and the small holes (inner holes) and filling a low-surface-energy repairing agent in the holes under the action of air pressure, capillary force and surface energy. The anti-icing performance of the aluminum stranded wire in practical application and self-repairing of the anti-icing performance after the aluminum stranded wire is damaged are improved, so that the anti-icing service life of the aluminum stranded wire is prolonged, and the lasting anti-icing performance of the aluminum stranded wire is improved. According to the self-repairing anti-icing aluminum stranded wire with the composite holes, repeated self-repairing of the anti-icing performance is achieved, and meanwhile, the hardness and the abrasion resistance of the film layer are improved.
Owner:CHONGQING UNIV
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