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79 results about "Kevlar" patented technology

Kevlar is a heat-resistant and strong synthetic fiber, related to other aramids such as Nomex and Technora. Developed by Stephanie Kwolek at DuPont in 1965, this high-strength material was first commercially used in the early 1970s as a replacement for steel in racing tires. Typically it is spun into ropes or fabric sheets that can be used as such or as an ingredient in composite material components.

Environmental-protection high-speed car brake sheet and warm-pressing process of brake sheet

The invention discloses an environmental-protection high-speed car brake sheet and a warm-pressing process of the brake sheet. A frictional material of the environmental-protection high-speed car brake sheet comprises the following components in parts by weight: 6-8 parts of phenolic resins, 2 parts of acrylonitrile rubber powder, 1-3 parts of Kevlar fibers, 5-7 parts of stannic sulfide, 5-7 parts of artificial graphite, 2 parts of polytetrafluoroethylene, 18-20 parts of steel fibers, 4-6 parts of red copper fibers, 2 parts of aluminum oxide, 3-5 parts of zirconium silicate, 5-7 parts of iron oxide black, 7-9 parts of titanium white, 6-8 parts of mineral fibers, 7-9 parts of white vermiculite, 8-10 parts of grammite and 5-9 parts of barium sulfate. The warm-pressing process of the environmental-protection high-speed car brake sheet comprises the steps of material burdening, material mixing, warm-pressing formation, thermal treatment, grinding and spraying. The high-speed car brake sheet has the advantages of safe and comfortable brake, no noise, low high-temperature and high-speed recession, stable frictional factor, environmental protection, long service life and the like; and the warm-pressing process of the environmental-protection high-speed car brake sheet has the advantages of high rate of finished products, high mechanical degree, high production efficiency and low energy consumption.
Owner:YANTAI WINHERE AUTO PART MFG

Aramid fiber blended yarn and preparation technology thereof

InactiveCN103498228AChange in fastnessFlame Retardancy ChangeYarnYarnMachine parts
The invention relates to the field of textile production, in particular to aramid fiber blended yarn and a preparation technology thereof. The aramid fiber blended yarn is characterized in that 1414.Kevlar aramid fiber, 1313.T450 aramid fiber, flame retardant glue, modacrylic, combed cotton, conducting fiber, chinlon and tencel are adopted as raw materials, fineness degrees of the materials are respectively 1.7, 2.2 and 3 deniers, any four materials in the raw materials are selected as main raw materials, the length of the four materials selected as the main materials at will is 48-51 millimeters, the lengths of the remaining auxiliary raw materials are respectively 28 millimeters and 38 millimeters. Compared with the prior art, the processing technology is simple in process, produced products have good performance such as high strength, high modulus, high-temperature resistance, acid resistance, alkali resistance and light weight, are high in strength, and can solve the problem that a machine part is damaged easily. The development of the aramid fiber blended yarn and the success of matched military supplies can bring markets for enterprises and innovation conceptions. Meanwhile, firmness, flame-retarding performance and anti-static electricity capacity of the military supplies are changed in nature compared with prior fiber blended yarn.
Owner:SHANGHAI SHENAN TEXTILE

Thermal insulation/protection integrated space debris protection structure and application thereof

ActiveCN105109709ARealize three-dimensional comprehensive protectionPlay anti-heat insulation/protection functionCosmonautic thermal protectionThermal insulationKevlar
The invention discloses a thermal insulation / protection integrated space debris protection structure and an application thereof. The protection structure is formed by stacking a front plate and a filled layer, wherein the filled layer is formed by alternately stacking SiC fibre fabrics and ceramic fibre-reinforced SiO2 nanometre aerogel plates in pairs, and one side of each SiC fibre fabric is close to the front plate. The protection structure is applied to thermal insulation and debris protection for a spacecraft, the protection performance is obviously superior to the protection performance of a Nextel / Kevlar filled protection structure under the same surface density, puncture damages are avoided, the thermal insulation performance is good, and the thermal conductivity is not greater than 0.023W / m.K; the mass of the filled layer of the protection structure is not greater than 1.08kg, and the thermal insulation / protection integrated effect can be acted at a higher temperature in case of an equivalent mass compared with the traditional filled Whipple protection structure; and the different requirements of thermal insulation, debris protection and weight reduction can be met by changing the thickness of the filled layer, and the designability is high.
Owner:NAT UNIV OF DEFENSE TECH

Method for preparing phosphoric acid doped high temperature proton exchange membrane with layer-by-layer assembly structure based on spin coating technique

The invention belongs to the technical field of fuel cells, and relates to a preparation technology of a proton exchange membrane electrolyte, in particular to a method for preparing a phosphoric aciddoped, high temperature proton exchange membrane with a layer-by-layer assembly structure based on a spin coating technique. Kevlar nanofibers, cadmium telluride nanocrystals and phosphoric acid arespin-coated respectively to complete 2-5 layer assembly, and a 2-5 composite membrane with an ordered structure (Kevlar-CdTe-PA) is prepared; an oven-dried membrane is soaked in a phosphoric acid solution with a mass fraction of 40 to 85%, and the phosphoric acid doped (Kevlar-CdTe-PA) 2-5 / (40 to 85%) PA composite membrane based on the cadmium telluride nanocrystals is prepared. The method for preparing the phosphoric acid doped, high temperature proton exchange membrane with the layer-by-layer assembly structure based on the spin coating technique realizes the assembly of the Kevlar nanofibers and the cadmium telluride nanocrystals, and prepares the high-temperature proton exchange membrane with an ordered structure and good proton conductivity, and has potential application value in thefield of fuel cells. In addition, the method for preparing the phosphoric acid doped high temperature proton exchange membrane with the layer-by-layer assembly structure based on the spin coating technique provides a new research method and idea for preparing a novel composite membrane based on nanomaterials and the Kevlar nanofibers.
Owner:NORTHEASTERN UNIV

Kevlar nanofiber composite forward osmosis membrane, and preparation method and application thereof

The invention belongs to the technical field of membrane materials, and discloses a Kevlar nanofiber composite forward osmosis membrane, and a preparation method and application thereof. The preparation method comprises the following steps: stirring Kevlar fibers with an auxiliary agent, strong base and an organic solvent and dispersing to form a stable Kevlar nanofiber dispersion solution; adding a pore-foaming agent, and uniformly stirring to obtain a membrane casting solution; coating a glass plate with the membrane casting solution through blade coating to form a membrane, and soaking into a gel bath to form a gel membrane; soaking the gel membrane into an organic solution for solvent replacement to obtain a Kevlar nanofiber porous membrane; using the porous membrane as a substrate, diluting the Kevlar nanofiber dispersion solution, forming a membrane on the substrate through blade coating, soaking into the gel bath, taking out, and airing to obtain the Kevlar nanofiber composite forward osmosis membrane. The Kevlar nanofiber composite forward osmosis membrane has the advantages of high strength, high water flux and high salt intercepting rate, and is applicable to the field of water treatment.
Owner:广州粤禹环保科技有限公司

Method for preparing pre-tension membrane structure antenna

ActiveCN102593576ASolve size-constrained challengesGuaranteed fixed spacing requirementsAntenna arraysAntenna supports/mountingsNomex honeycombMembrane surface
The invention relates to a method for preparing a pre-tension membrane structure antenna. The method comprises the following steps: designing a membrane surface into a base membrane and electric membranes, splicing the base membrane and forming the electric membranes; marking out a bottom membrane according to a designed paste range, pasting the electric membranes; processing catenaries, splicing auxiliary strengthening plates, positioning the membrane surface by utilizing installation holes of a support framework of the membrane antenna and placing the first membrane surface on a corresponding position of the support framework; reversely loading pretightening force on the long side of the membrane surface by utilizing auxiliary loaded ropes and the support of the support framework, pre-tensioning tension ropes by an adjustment device and adjusting the tension ropes to designed positions for splicing and fixing; and installing a dielectric Kevlar/Nomex honeycomb panel so as to finally realize an antenna array surface. In the method, a phased-array antenna array surface is realized through a membrane structure; the weight of a traditional phased-array antenna structure is lightened; and the method provided by the invention has the characteristics that the pre-tension membrane structure antenna is capable of being continuous loaded; the membrane tension can be accurately controlled, the operation is convenient, a special membrane tying tool is not needed, and the like.
Owner:XIAN INSTITUE OF SPACE RADIO TECH

Armored sensing optical cable

The invention discloses an armored sensing optical cable, which comprises a tightly packaged fiber, a metal hose, a metal mesh grid and an outer jacket layer, wherein the tightly packaged fiber is wrapped by the metal hose; the metal mesh grid is coated out of the tightly packaged fiber; the outer jacket layer is coated on the metal mesh grid; when one tightly packaged fiber is provided, a laeyr of Kevlar is arranged between the metal hose and the metal mesh grid; when multiple tightly packaged fibers are provided, a layer of Kevlar and a flameproof inner jacket are arranged between the metal hose and the tightly packaged fiber in sequence. The armored sensing optical cable is armored by the small metal hose, the minimum outer diameter is only 0.9 mm after armored, and the minimum outer diameter of the optical cable is only 1.8 mm after the optical cable is formed. The interval between the tightly packaged fiber of the armored sensing optical cable and the external environment is small, the temperature measuring speed of the armored optical cable is quicker than that of the common optical cable, and the temperature measuring precision is accurate. The problems of complicated structure of a common outdoor optical cable structure, isolation of the optical fiber and the external environment and poor temperature measuring effect are solved.
Owner:东捷光电科技(苏州)有限公司

Method for preparing aramid nanofibers based on deprotonation of Kevlar and nanofiber prepared thereby

The invention provides a method for preparing aramid nanofibers based on Kevlar deprotonation. The method comprises the following steps: stirring and pretreating a mixed system of aramid fibers, an organic solvent and alkali to obtain an aramid fiber dispersion liquid; and adding a proton donor and/or an ionic reaction aid into the aramid fiber dispersion liquid to regulate and control the deprotonation degree so as to obtain an aramid nanofiber colloidal dispersion liquid. The invention further provides the aramid nanofiber colloidal dispersion liquid prepared by the method. According to the method, the nanocrystallization rate (within 1-4 hours) and the concentration (can reach 4 wt% or above) of a reaction system of the aramid fiber are increased, and the prepared aramid nanofibers are uniform in size, high in stability (the length is 5-20 microns and 5-30 nanometers), large in specific surface area and length-diameter ratio and excellent in high temperature resistance; and the method is simple in equipment and process and high in applicability, solves the problems of long preparation period, low reaction concentration, low production efficiency and the like, and has extremely high actual production and application values.
Owner:AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH

Composite spraying material and frame for downhole quick leaking stoppage and filling and implementing method thereof

The invention discloses a composite spraying material and frame for downhole quick leaking stoppage and filling and an implementing method thereof, and belongs to the composite spraying material and the sealing frame, and the implementing method thereof. A set reasonable proportion of phenolic foam, polyurethane foam and urea formaldehyde foam is selected, a base material of the spraying materialis synthesized, a proper flame retardant is added, and the properties of the base material are increased; an antistatic material, a catalyst, a curing agent, a surfactant, a foaming agent and other materials are added, and the flame-retardant and anti-static composite macromolecular spraying material is formed through specific technological process. Fiber-Kevlar is selected as a raw material to form the sealing frame and is used as a carrier of the spraying material, the structure deformation is flexible, and a whole for quick sealing and leaking stoppage is formed jointly. Through different embodiments, the composite spraying material is verified to have the characteristics of light mass, fast forming, strong sealing and good fire prevention and leaking stoppage effects, can effectively prevent downhole air leakage and harmful gas gushing and ensures the safety of workers.
Owner:CHINA UNIV OF MINING & TECH

Innovative flagpole lifting device

The invention discloses an innovative flagpole lifting device. The innovative flagpole lifting device comprises a base, a flag column tube and a basement winch reel, wherein the flag column tube is arranged on the base, and the basement winch reel is arranged at the bottom of the base; the flag column tube is provided with a rectangular opening in the top, a Kevlar belt transition wheel is installed on the lower edge of the inner side of the rectangular opening, a Kevlar belt is connected with a flagpole frame outside the flag column tube, and the other end of the Kevlar belt penetrates through the rectangular opening, climbs over the Kevlar belt transition wheel, rotates by 360 degrees, passes through the hollow flag column tube and is wound around the reel. Electric soft iron is arrangedat the lower end of the flagpole frame, a horse shoe magnet is arranged on the inner wall of the top segment of the flag column tube, in the center line of the rectangular opening and at the positionof equal distance to the electric soft iron of the flagpole frame, and after a flag on the flagpole frame is lifted to the top of the flag column tube, the electric soft iron and the horse shoe magnet are right located at the same position to generate strong-magnetism attraction force for fixing. With the innovative flagpole lifting device, the three problems can be solved that after the flag islifted to the top, a rope, a column winding ring, hanging weight objects on the lower portion of a flagpole and others are arranged outside the flag column tube; when the flag encounters strong wind or due to the fact that compressed air is jetted and blown, the flag leaves from the column tube; the pull rope of the flag leaves from the top of the column tube under influencing of all kinds of factors. With the innovative flagpole lifting device, the solemnity and liberality of a flag-raising ceremony are kept, and the effects of attractiveness and vitality are realized.
Owner:黄劲鸣

Method for preparing pre-tension membrane structure antenna

ActiveCN102593576BSolve size-constrained challengesGuaranteed fixed spacing requirementsAntenna arraysAntenna supports/mountingsNomex honeycombMembrane surface
The invention relates to a method for preparing a pre-tension membrane structure antenna. The method comprises the following steps: designing a membrane surface into a base membrane and electric membranes, splicing the base membrane and forming the electric membranes; marking out a bottom membrane according to a designed paste range, pasting the electric membranes; processing catenaries, splicing auxiliary strengthening plates, positioning the membrane surface by utilizing installation holes of a support framework of the membrane antenna and placing the first membrane surface on a corresponding position of the support framework; reversely loading pretightening force on the long side of the membrane surface by utilizing auxiliary loaded ropes and the support of the support framework, pre-tensioning tension ropes by an adjustment device and adjusting the tension ropes to designed positions for splicing and fixing; and installing a dielectric Kevlar / Nomex honeycomb panel so as to finally realize an antenna array surface. In the method, a phased-array antenna array surface is realized through a membrane structure; the weight of a traditional phased-array antenna structure is lightened; and the method provided by the invention has the characteristics that the pre-tension membrane structure antenna is capable of being continuous loaded; the membrane tension can be accurately controlled, the operation is convenient, a special membrane tying tool is not needed, and the like.
Owner:XIAN INSTITUE OF SPACE RADIO TECH
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