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64results about How to "Good blendability" patented technology

Three-layer co-extruded EVA (ethylene-vinyl acetate copolymer) long-life fog-dissipation environment-friendly multifunctional greenhouse film

The invention discloses a nano fog-dissipation multifunctional greenhouse agricultural film, and in particular relates to a three-layer co-extruded EVA (ethylene-vinyl acetate copolymer) long-life fog-dissipation environment-friendly multifunctional greenhouse film, belonging to the field of agricultural mulching films. The raw material formula of an outer layer comprises the following components in percentage by weight: 20-50% of linear low-density polyethylene (LLDPE), 20-50% of low-density polyethylene (LDPE), 10-20% of metallocene polyethylene (mPE) and 5-10% of double-prevention masterbatch; the raw material formula of a middle layer comprises the following components in percentage by weight: 30-40% of ethylene-vinyl acetate copolymer (EVA), 20-40% of linear low-density polyethylene (LLDPE), 20-40% of low-density polyethylene (LDPE) and 5-10% of three-prevention masterbatch; the raw material formula of an inner layer comprises the following components in percentage by weight: 30-40% of ethylene-vinyl acetate copolymer (EVA), 10-20% of linear low-density polyethylene (LLDPE), 20-50% of low-density polyethylene (LDPE) and 5-10% of three-prevention masterbatch; and the formulas of the outer layer, the middle layer and the inner layer are uniformly mixed respectively, master batches are prepared by using a double-head thread screw double-screw extruding machine, a three-layer film is formed through a co-extrusion die head and is extruded out to prepare the multifunctional agricultural greenhouse film. Every quality technical index of the film reaches or exceeds a national standard, and a small part of the indexes is more than 2 times better than the national standard, so that the film is excellent in antiaging performance and cannot generate fog drops, and the service life of the film reaches more than 3 years.
Owner:HENAN YINFENG PLASTIC

Gas turbine combined type fuel evaporating and atomizing combustion apparatus

InactiveCN101435585AIncrease the pre-mixed pre-evaporation processImprove atomization and evaporationContinuous combustion chamberAviationCyclone
The invention provides a combined fuel oil atomizing, evaporating and combusting device for a gas turbine, relates to an air inlet device of the gas turbine, a fuel oil atomizing, evaporating and blending device, and core technology of organized combustion and stable flame, and belongs to the power field of an aeronautic power propulsion system and a ground gas turbine. A nozzle 1 is arranged at a central position of an inlet of a premixing chamber 2; an evaporator 3 is fixed in an inner cavity of the premixing chamber 2; double cyclones 4 are arranged at the inside of the outlet end of the premixing chamber 2 and connected hermetically; a centrifugal nozzle 5 is arranged at a central position of the double cyclones 4; a venturi 6 is welded at a transition position of an outlet of internal and external cyclones of the double cyclones 4; a sleeve 7 is hermetically welded with the outside of an outlet of the premixing chamber 2; and the head of a combustion chamber 8 is hermetically welded with the sleeve 7. Compared with the prior fuel oil combined nozzle, the device has the advantages of improving properties of fuel oil atomizing, evaporating and blending and evenness of oil-gas space distribution, improving combustion performance, shortening flame length and reducing discharge of pollutant, and is a comparatively ideal combined fuel oil atomizing and combusting device for a high-performance gas turbine.
Owner:PEKING UNIV

Jet pump

The invention provides a jet pump, and relates to a mixed flow jet apparatus. The jet pump is composed of a current distributing assembly, an inner pipe assembly and an outer sleeve assembly which have a same shaft core, wherein the current distributing assembly and the inner pipe assembly are fixedly connected in series, thereby forming a blind top centre cavity and a centre mixing tube; the outer sleeve assembly is sleeved outside the current distributing assembly and the inner pipe assembly, thereby forming an annular mixing chamber, an annular mixing pipe, a total mixing chamber and a total mixing output pipe; an internal ring nozzle and an external ring nozzle are arranged between the current distributing assembly and the inner pipe assembly, a mainstream body sprayed by the internal ring nozzle carries out jet-suction on a secondary fluid of the blind top centre cavity so as to spray to the centre mixing tube, and the secondary fluid is mixed in the centre mixing tube so as to output a centre mixed flow; a mainstream body sprayed by the external ring nozzle carries out jet-suction on a secondary fluid of the blind top centre cavity so as to spray to the annular mixing pipe, and the secondary fluid is mixed in the annular mixing pipe so as to output an annular mixed flow; and the two mixed flows are mutually injected to enter the total mixing chamber and the total mixing output pipe so as to further output in an isotrope voltage-sharing manner. The jet pump provided by the invention has the advantages of smaller weight and axial direction size, high injection rate, great suction force and good property in large flow.
Owner:韩铁夫

Mixing flame stabilizing device

The invention relates to the technical field of engines, and discloses a mixing flame stabilizing device. The mixing flame stabilizing device comprises a lobe mixer, a cover plate and turbulent flow columns, wherein a gas collecting cavity is formed between the cover plate and the lobe mixer; the turbulent flow columns are arranged at the position of an outer culvert air flow outlet of the lobe mixer; inner cavities of the turbulent flow columns communicate with the gas collecting cavity; the side walls of the turbulent flow columns and the cover plate are provided with spraying holes a and spraying holes b correspondingly; combustible gas is subjected to secondary flow dividing through the spraying holes a and the spraying holes b and then enters a combustion chamber to be mixed with air,the spraying pressure of the combustible gas is increased, accordingly, the penetrating capacity of the combustible gas in the gaseous environment is improved, and accordingly efficient mixing of twoair flows is achieved; and the turbulent flow columns are arranged at the position of the outer culvert air flow outlet of the lobe mixer, a large-scale radial vortex can be formed on the downstreamportion of the turbulent flow columns, outer culvert air is forced to flow in the circumferential direction of the turbulent flow columns at an outlet of the mixer, the mixing distance of the outer culvert air and inner culvert combustible gas is shortened, the mass exchange rate of the air and the combustible gas at an inner culvert outlet of the mixer is increased, and the mixing effect is improved.
Owner:XIAN AEROSPACE PROPULSION INST

Specially-shaped mixing holes for adjusting outlet temperature distribution of combustion chamber

ActiveCN112146127AIncrease the divergence angleExpand space coverageContinuous combustion chamberCombustion chamberEngineering
The invention discloses specially-shaped mixing holes for adjusting outlet temperature distribution of a combustion chamber, and belongs to the field of combustion of gas turbines. The specially-shaped mixing holes are formed in the inner ring wall surface and the outer ring wall surface of a flame tube of the combustion chamber correspondingly; the specially-shaped mixing holes divide the wall surface of the flame tube into a flame tube front section and a flame tube back section; the specially-shaped mixing holes are evenly distributed in the circumferential direction of the wall surface ofthe flame tube to form mixing jet flows evenly distributed in the circumferential direction, the penetration depth of the mixing jet flows is increased, the contact area of mixing cold air and high-temperature main stream gas is increased, the mixing effect is improved, and the outlet temperature distribution quality of the combustion chamber is improved; the effect of adjusting outlet temperaturedistribution of the combustion chamber is achieved by changing the jet flow penetration depths, the jet flow circumferential expansion angles and the jet flow directions of the mixing holes; and outlet temperature distribution of the combustion chamber is adjusted, so that the temperature quality of an inlet of a turbine is improved, the service life of the turbine is prolonged, and the heat-proof design difficulty of the turbine is reduced.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Modification water reduction agent for concrete

InactiveCN110395933AReduce waste water pollutionReduce manufacturing costChemistryCorrosion
The invention discloses a modification water reduction agent for concrete and relates to the technical field of water reduction agent. The modification water reduction agent comprises the following components in parts by mass: 30-50 parts of methyl allyl polyoxyethylene ether, 25-40 parts of a sodium beta-naphthalenesulfonate wastewater mixed liquid, 10-20 parts of sulfite, 4-8 parts of a modifier, 0.75-2 parts of polyvinylpyrrolidone, 0.65-1.4 parts of dodecylpyridinium bromide, 3-4 parts of 30% hydrogen peroxide, 5-8 parts of a viscosity adjustment agent, 8-11 parts of an air entraining agent and 7-10 parts of an early-strength agent. By adopting the modification water reduction agent for concrete, the blending performance of the water reduction agent can be improved, the strength and the hardness of the concrete can be improved in application, and the viscosity of the water reduction agent can be adjusted in the use process through the viscosity adjusting agent, the air entraining agent and the early-strength agent, so that the concrete can be well laid, the curing time of the concrete can be shortened, and the modification water reduction agent for concrete has good effects inimproving the corrosion resistance of the concrete, increasing the water reduction rate and prolonging the service life of an engineering structure.
Owner:江苏博思通新材料有限公司

Closed-cell foaming material as well as manufacturing formula and manufacturing method thereof

The invention relates to the technical field of foaming materials, and in particular relates to a closed-cell foaming material as well as a manufacturing formula and a manufacturing method thereof. The closed-cell foaming material comprises a body, wherein the body is integrally molded through continuous foaming; the body comprises an upper surface skin, a middle core layer and a lower surface skin; the upper surface skin, the middle core layer and the lower surface skin are integrally molded through continuous closed-cell foaming; a formula of the foaming material comprises 10 to 40 parts of elastomers (including EVA (Ethylene-vinyl Acetate copolymer), POE (Polyolefin Elastomer), TPE (Thermoplastic Elastomer), TPR (Thermoplastic Rubber) and MPP (Modified Polypropylene)), 10 to 50 parts of polyethylene, 30 to 60 parts of a filling material, 6 to 20 parts of a foaming agent, 0 to 5 parts of a catalyst, 0.1 to 2 parts of a cross-linking agent, 0 to 3 parts of a lubricant and 0 to 2 parts of toner; the manufacturing method of the foaming material comprises the following steps: mixing; extruding; calendering to form a master batch; carrying out primary cooling and winding; adding the master batch into a continuous foaming tunnel furnace and carrying out closed-cell cross-linking foaming under normal pressure; carrying out secondary cooling; printing to obtain a finished product and winding. The method provided by the invention completely meets European Union standards and user requirements especially in the aspect of formamide; the closed-cell foaming material provided by the invention can be used for continuously carrying out chemical cross-linking closed-cell foaming without electron irradiation crosslinking and mould pressing.
Owner:广东富利时实业有限公司

Phase change type paraffin-containing fuel ramjet engine

The invention discloses a phase change type paraffin-containing fuel ramjet engine, which adopts an integrated design of a combustion chamber and a gasification chamber, and is compact in structure and high in energy utilization rate. A shell is heated by a large amount of heat released by combustion reaction in the combustion chamber, the surface of paraffin-containing fuel can be preheated under the action of radiation and heat convection, and meanwhile, ram air is heated, so that the surface of the fuel has higher temperature, and phase change of the fuel is facilitated. Mode conversion is easy to achieve, and automatic switching between a boosting section and a ramming section can be completed through change of pressure intensity. The head of the combustion chamber is provided with a conical hole with a certain inclination, so that the rotational flow of gas can be realized, and higher combustion efficiency can be further obtained. When the boosting section and the ramming section are switched, a mixture of a phase change product and air generates rotational flow under the action of the conical hole when flowing into the combustion chamber, so that the mixing effect is good. The engine is adjustable in size, wide in application range, and suitable for power systems of supersonic aircrafts.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Self-adaptive rocket spray tube applied to rocket based combined circulating engine

ActiveCN109915282AReduce overexpansionReduce bottom resistanceRocket engine plantsSelf adaptiveJet flow
The invention discloses a self-adaptive rocket spray tube applied to a rocket based combined circulating engine. The self-adaptive rocket spray tube comprises a spray tube body, wherein a flow-supplementing sucking channel and a pneumatic tab channel are arranged on the spray tube body; when the rocket based combined circulating engine works in an ejector mode, the rocket engine sprays high-speedgas flow to the outer side of the spray tube body along a pneumatic tab channel, and high-speed gas flow mutually acts with gas flow on the outer part of the spray tube body to form streamwise vortex,so that mixing between rocket jet flow and outer gas flow is strengthened; and moreover, along with different working conditions of the rocket engine, penetrating depth of a pneumatic tab generates changes. When the rocket based combined circulating engine is in a sub-combustion or super-combustion mode, the rocket engine is switched off; and gas flow on the outer part of the spray tube body automatically flows into the spray tube body from the outer side of the spray tube body along the flow-supplementing sucking channel as a result of internal and external pressure difference, so that bottom resistance generated by the spray tube is reduced. The self-adaptive rocket spray tube has certain self-adaptive regulating ability, and facilitates integral pneumatic performance.
Owner:NAT UNIV OF DEFENSE TECH

Particle image velocimetry (PIV) experimental particle mixing device based on pneumatic lug technology

InactiveCN102513012BShorten the core area of ​​potential flowWell mixedAerodynamic testingTransportation and packagingEngineeringMixing effect
The invention discloses a particle image velocimetry (PIV) experimental particle mixing device based on a pneumatic lug technology, which comprises a mixing tank and a filtering element disk for containing PIV trace particles; the filtering element disk is arranged in the mixing tank; moreover, the mixing tank is respectively provided with an air-inlet main pipe and an air outlet pipe, the circumferential direction nearby the position of an outlet of the air-inlet main pipe is evenly distributed with pneumatic lugs, the pneumatic lugs comprise the jetting pipes of the pneumatic lugs and flow-jetting control mechanisms for controlling the jetting flow rate of the jetting pipes of the pneumatic lugs, and the jetting ports of the jetting pipes of the pneumatic lugs are arranged in a way of facing to a main flow area of the air-inlet main pipe; furthermore, the air inlets of the jetting pipes of the pneumatic lugs are communicated with bypass airflow; and moreover, the total pressure of airflow jetted by the jetting pipes of the pneumatic lugs is higher than the total pressure of airflow in the air-inlet main pipe. Therefore, flowing vortex is formed at the positions of the outlets of the jetting pipes by arranging the pneumatic lugs on the air-inlet main pipe according to the PIV experimental particle mixing device based on the pneumatic lug technology, so that the mixing effect of PIV particles in a particle mixer is improved.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Double-layer mixing pipe and residue-free mixing bin

According to the double-layer mixing pipe and the residue-free mixing bin, a mixing pipe in the bin is the double-layer mixing pipe, a mixing pipe bundle in the double-layer mixing pipe is fixedly connected with a vibration supporting plate arranged on an end cover, an outer sleeve is fixedly connected with a barrel-shaped support arranged on the end cover, an oval hole is formed in the outer sleeve, and the outer sleeve is fixedly connected with the barrel-shaped support. The feeding hole of the mixing pipe is provided with the inclined feeding duckbilled pipe extending out of the oval hole, the oval hole reserves a vibration space for the feeding duckbilled pipe, interference of the inner pipe and the outer pipe is avoided, and when the mixing pipe bundle vibrates to discharge materials, the outer sleeve bears the pressure of materials in the stock bin, so that the mixing effect is good. The problem of different vertical vibration amplitudes caused by different pressures of materials at the upper part and the lower part of the internal mixing tube bundle is solved, the flows of the materials at the upper part and the lower part entering the mixing tube are the same, and the materials are mixed more uniformly; in addition, each mixing tube bundle transmits vibration force to the auxiliary mixing tube in the conical bin bottom through the cross-shaped support, materials in different batches in the conical bin bottom can be mixed and discharged, and the whole mixing is more uniform.
Owner:NANJING XIANGRUI INTELLIGENT EQUIP TECH CO LTD +2

Injection mould shoe insole for manufacturing bottom face anti-sliding protruding points and manufacturing method of injection mould shoe insole

The invention discloses an injection-molded shoe midsole for manufacturing anti-skid protrusions on the bottom surface and a preparation method thereof, comprising a base and a lower mold, a shock-absorbing pad is fixedly installed on the upper end of the base, and a fixing hole is arranged above the shock-absorbing pad. No. 1 horizontal workbench, No. 2 horizontal workbench and heat dissipation guide fins, one side of the convex groove is provided with a convex nail structure, and the other side of the convex groove is provided with a convex groove and a rectangular groove, and the bottom of the lower mold An upper base, a lower base and screws are provided, the upper end of the upper base is provided with a connecting plate, and the upper base is fixedly connected with the lower mold through the connecting plate, and a light strip is fixedly installed on the upper surface of the No. 2 horizontal workbench. An injection-molded shoe midsole for manufacturing anti-slip protrusions on the bottom surface and a preparation method thereof according to the present invention are provided with shock absorbing pads and light strips, which can ensure the convenience of equipment operation, and can be operated at night, effectively making the shoe midsole non-slip , suitable for different working conditions, bringing better prospects for use.
Owner:东莞市鹏翼自动化科技有限公司

Adaptive rocket nozzle for rocket-based combined cycle engines

The invention discloses a self-adaptive rocket spray tube applied to a rocket based combined circulating engine. The self-adaptive rocket spray tube comprises a spray tube body, wherein a flow-supplementing sucking channel and a pneumatic tab channel are arranged on the spray tube body; when the rocket based combined circulating engine works in an ejector mode, the rocket engine sprays high-speedgas flow to the outer side of the spray tube body along a pneumatic tab channel, and high-speed gas flow mutually acts with gas flow on the outer part of the spray tube body to form streamwise vortex,so that mixing between rocket jet flow and outer gas flow is strengthened; and moreover, along with different working conditions of the rocket engine, penetrating depth of a pneumatic tab generates changes. When the rocket based combined circulating engine is in a sub-combustion or super-combustion mode, the rocket engine is switched off; and gas flow on the outer part of the spray tube body automatically flows into the spray tube body from the outer side of the spray tube body along the flow-supplementing sucking channel as a result of internal and external pressure difference, so that bottom resistance generated by the spray tube is reduced. The self-adaptive rocket spray tube has certain self-adaptive regulating ability, and facilitates integral pneumatic performance.
Owner:NAT UNIV OF DEFENSE TECH

Foaming material applied to musical instrument box and preparation method thereof

The invention belongs to the technical field of musical instrument box manufacturing materials, and particularly relates to a foaming material applied to a musical instrument box and a preparation method thereof. According to the foaming material applied to the musical instrument box, the inner wall surface of the musical instrument box is filled with the foaming material, the Shore C hardness of the foaming material is 10-80 degrees, and the rebound rate of the foaming material is 25-65%. The inner wall surface of the musical instrument box is filled with the foaming material with the Shore C hardness of 10-80 degrees and the rebound rate of 25%-65%, so that the musical instrument box has an excellent protection effect, and the musical instrument in the musical instrument box is still intact after being impacted violently. The foaming material is a thermoplastic POE foaming material, and the thermoplastic POE foaming material is prepared from the following raw materials in parts by weight: 25 to 35 parts of a first POE material, 20 to 30 parts of a second POE material, 20 to 30 parts of a third POE material, 7 to 13 parts of talcum powder, 3 to 8 parts of zinc oxide, 0.5 to 1.5 parts of a lubricating agent, 0.5 to 1.5 parts of zinc stearate, 0.5 to 1.5 parts of a wear-resistant agent, 0.5 to 1.5 parts by weight of a bridging agent; and 0.5 to 1.5 parts by weight of a foaming agent.
Owner:DONGGUAN HUAJIN GIFTS
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