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229results about How to "Low areal density" patented technology

Anode or cathode pole piece of lithium ion battery and coating method thereof

The present invention relates to a lithium-ion battery anode or cathode pole piece and a spreading method of the anode pole piece or the cathode pole piece, wherein, the anode pole piece and the cathode pole piece consists of a foil, a conducting adhesive thin layer and an electrode active material layer in turn; the thickness of the conducting adhesive thin layer is five to ten microns. The electrode pole piece is made in the procedures that a layer of conducting adhesive thin layer in the thickness of five to ten microns are pre-coated on the surface of the foil before the sizing agent is spread, so that a conducting adhesive thin layer having good adhesive force, good conductivity and compact structure is formed on the surface of the foil. Then the electrode active material sizing agent is spread on the conducting adhesive thin layer, and is dried under an appropriate temperature to produce a required pole piece. The present invention can reduce the surface of the foil, and can improve the wetting quality of the sizing agent, thereby improving the adhesion performance of the anode material and the collecting body (aluminum foil) so as to reduce the powder-dropping of the battery during the cycling process, and to prolong the cycling service life of the battery; moreover, the present invention can reduce the content of the adhesive agent in the sizing agent, and improve the utilization rate of the active substance, and the method of the present invention does not produce negative influence on the performance of the battery.
Owner:CENT SOUTH UNIV

Novel infrared and radar integrated stealth fabric and preparation method thereof

The invention discloses a novel infrared and radar integrated stealth fabric and a preparation method thereof. The stealth fabric comprises an infrared camouflage surface layer and an antistatic bottom layer in turn from outside to inside; the infrared camouflage surface layer comprises an infrared stealth layer, a fabric layer and a radar wave absorption attenuation layer in turn from outside toinside; the infrared stealth layer is compounded by using a coating coated by an infrared stealth coating and a magnetron sputtering ITO (indium tin oxide) film arranged on the surface of the coating; the radar wave absorption attenuation layer comprises a sponge body; and a wave absorption material is adsorbed on the sponge body. The stealth fabric can realize radar stealth function and infraredstealth function at the same time, has good integral wave absorption effect and low surface density of materials, and has good effects on the aspects of breaking strength, bursting strength and the like. Moreover, excessive complex processes are not adopted for manufacturing the stealth fabric, and the stealth fabric can be produced by using a conventional fabric production method, so the stealthfabric is convenient for production and easy for implementation.
Owner:WUYI UNIV

Deployable surface device with fixed truss structure

The invention discloses a deployable surface device with a fixed truss structure, which mainly aims to solve the problems of high areal density, complicated structure, low deployable reliability and the like in the prior art. The device comprises a plurality of folded rings and connection joints, wherein every two folded rings (2) are connected by one ring connection joint (1) so as to form a circular foldable and deployable ring structure; each folded ring adopts a rectangular or regular triangle hollow straight bar single-rowed truss structure; driven or locked by the ring connection joints, the folded rings are unfolded into an approximately curve working state from a vertically folded state; staggered flexible pulling ropes are arranged on the folded rings; and a wire mesh or a film of which the surface is coated with aluminum is bound to the pulling ropes, so that the deployable surface device with the fixed truss structure is formed. The deployable surface device with the fixed truss structure has high composite performance indexes such as low areal density, simple structure, high deployable reliability, capacity of transmitting or converging electromagnetic waves in a long distance and the like, and can be used as a reflector or a converging device in space or on the ground.
Owner:XIDIAN UNIV

Inflatable and deployable systems with three dimensionally reinforced membranes

An illustrative embodiment of the invention includes an apparatus and method for making air and space inflatables and deployables using three dimensionally reinforced (3DR) membranes. A 3DR process preferably takes plural substantially flat gore segments, each segment made of plural membranes and reinforcing fibers, and joins adjacent gores so the seams on opposite sides are offset. Single ply seam tape may be used. When all gores are joined, a three dimensional deployable or inflatable (e.g., balloon) structure with a minimized seam is produced. Further, localized fiber reinforcement may be used, with different characteristics depending on the desired placement in the gore, allowing the substantially flat gores, when joined and loaded, to strain to the desired three dimensional shape. In doing so, the required number of gores and seams may be reduced, while using materials with significantly lower areal densities. Thus, the 3DR process allows one to make locally reinforced materials that optimize strength to weight ratios; permits single ply and sub-gore width seam tapes; permits multi-phase optimized envelope shapes, designed to efficiently handle multiple loading conditions; and provides increased design flexibility for a wide range of shapes and characteristics impractical or unavailable under prior techniques.
Owner:LACHENMEIER TIMOTHY T

System and methods for radar and communications applications

A system and methods for radar and communications applications. In one embodiment the present system comprises a wireless, space-fed, phased array of antennas including a plurality of unit cells. A first one of the unit cells includes a first one of the antennas and a unit cell command interpreter configured to receive a command, determine whether the command is intended for the first unit cell, and relay the command to logic for enabling a phase shift controller of the first antenna. In one embodiment the present methods comprise the step of wirelessly beaming microwave power from a power and control beam transmit unit to illuminate a wireless, space-fed, phased array of antennas including a plurality of unit cells. The method further comprises the steps of beaming a command to the array and converting the microwave power into direct current within a first one of the unit cells. The first unit cell includes a first one of the antennas. The method further comprises the steps of supplying the direct current to components of the first unit cell to power the first unit cell, receiving the command within the first unit cell, determining whether the command is intended for the first unit cell, and relaying the command to logic for enabling a phase shift controller of the first antenna.
Owner:THE BOEING CO

Armour splicing-type stab-proof vest based on hollow micro-egg shell structure

PendingCN108095222AIncrease flexibilityReduce heat and moisture resistanceProtective garmentPlastic materialsMoisture permeability
The invention discloses an armour splicing-type stab-proof vest based on a hollow micro-egg shell structure. The stab-proof vest comprises a plurality of stab-proof sheet sets, each stab-proof sheet set comprises a first stab-proof base plate and a second stab-proof base plate connected with the first stab-proof base plate, the first stab-proof base plate and the second stab-proof base plate are made of a plastic material by means of a 3D printing-laser sintering technology, and the first stab-proof base plate in each stab-proof sheet set is connected with the first stab-proof base plate and the second stab-proof base plate in adjacent stab-proof sheet set. Compared with an existing stab-proof vest, the armour splicing-type stab-proof vest uses an arrangement mode of hierarchical overlapping of animal scales and shells for reference, all the stab-proof base plates are horizontally arranged according to the arrangement of upper-lower layering, overall surface density is reduced, overallcomfort and flexibility are improved, and diathermanous effects and moisture permeability effects are improved; a plurality of hollow semi-ellipsoidal shells are sequentially arranged in a staggeredmanner to effectively disperse the impact force of sword stabbing, and the stab-proof performance of the stab-proof base plates can be enhanced; the stab-proof vest has the advantages of simple production process, high efficiency, light weight, raw materials savings, low cost and good market competitiveness.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

Method for preparing active layer structure with high-density gallium nitride quantum dots

The invention relates to a method for preparing an active layer structure with high-density gallium nitride quantum dots; the method comprises the following steps of: (1). depositing a layer of SiO or SiNx dielectric thin film material with the thickness of 10-50nm on a GaN template or surfaces of other semiconductor films, painting a mixing copolymer of PS (Polystyrene) and PMMA (Polymenthyl Methacrylate) on the surface of the dielectric thin film, obtaining a PS nanometer column graph after cleaning the PMMA, transferring the PS nanometer column graph to the dielectric thin film layer by adopting plasma etching, wherein the PS nanometer column graph is prepared according to the following parameters: (1) the surface density reaches 0.8-1.0*1011cm<-2>; (2) the PS nanometer column graph istransferred to the SiNx or SiO2 dielectric thin film layer by adopting reactive ion etching, the PP is removed to obtain a template on which a GaN nanometer point structure grows for the second time through MOCVD (Metal-organic Chemical Vapor Deposition); and (3) a GaN-base quantum dot structure grows, emits strong royal purple light and is used for manufacturing the active layer structure in a light-emitting diode (LED) with high efficiency and a laser device (LD) optoelectronic device.
Owner:NANJING UNIV

Ferrite wave-absorbing material used for injection moulding, preparation method thereof and magnetic wave-absorbing element

The invention discloses a ferrite wave-absorbing material used for injection moulding, a preparation method thereof and a magnetic wave-absorbing element. The molecular formula of the wave-absorbing material is A2(Bx+C2-x)Fe12O22, wherein A is Sr or Ba, B and C are selected from Mn, Ni, Zn, Mg, Co, Cu or Ca, x is no less than 0 and no more than 2. The invention also provides the preparation method of the wave-absorbing material and the magnetic wave-absorbing element. A fluxing agent is introduced in the preparation of the ferrite wave-absorbing material, thus the free growth of crystal particles can be ensured, the bond strength between crystal particles can be reduced simultaneously, ideal hexagonal flaky crystal particles can be obtained, and the surface density of the wave-absorbing material can be effectively reduced; and injection moulding is utilized for moulding, thus the wave-absorbing element with order crystal particles and complex shape can be prepared. The wave-absorbing material disclosed by the invention can be used in different electromagnetic environments and have wide application value in the aspects for preventing the influences of electromagnetic radiation on a human body and equipment, improving the pollutions of the space electromagnetic environment and the like.
Owner:BGRIMM TECH CO LTD

Method for manufacturing carbonyl iron foam wave-absorbing material

The invention relates to a carbonyl iron foam wave-absorbing material. Carbonyl iron which is large in magnetic loss, wave-absorbing strength and density is used as an absorbent to be added into a soft polyurethane foam base body, and the density and the mass of the carbonyl iron foam wave-absorbing material can be effectively reduced; the wave-absorbing performance of the material can be adjusted by changing the dipping times and the thickness of the base body, and the wave-absorbing material excellent in whole performance can be obtained. A method for manufacturing the carbonyl iron foam wave-absorbing material comprises the steps of preparing an adhesive glue solution, preparing an absorbent glue solution, dipping the soft polyurethane foam base body into the absorbent glue solution at multiple times repeatedly, removing an excess glue solution, placing the base body into a vacuum drying box to be dried, carrying out machining according to the specified dimension, and obtaining a finished product of the carbonyl iron foam wave-absorbing material. The overall wave-absorbing performance of the carbonyl iron foam wave-absorbing material is good, the surface density is low, the absorbed frequency is wide, the technology is simple and efficient, the repeatability is good, the radar wave absorbing effect is obvious, and the wide application prospect of the method in the radar camouflage field and the electromagnetic shielding field is displayed.
Owner:PLA SECOND ARTILLERY ENGINEERING UNIVERSITY

Material with characteristics of fire retardation, thermal insulation and wave absorption, and preparation method thereof

The present invention provides a material with characteristics of fire retardation, thermal insulation and wave absorption. The material comprises a base layer, wherein the base layer is mesh fabric, both sides of the mesh fabric are coated with an adhesive coating layer, and the adhesive coating layer is a polyvinylchloride adhesive coating layer. The adhesive coating layer comprises a wave absorption agent, wherein the wave absorption agent comprises nickel-plated glass beads, and a mass ratio of the wave absorption agent powder to the adhesive is 0.17-1.85:1. The present invention further provides a preparation method for the material. According to the material with characteristics of fire retardation, thermal insulation and wave absorption in the present invention, the polyvinylchloride adhesive is added with the wave absorption agent, such that functions of fire retardation, thermal insulation and wave absorption can be concurrently provided; the material of the present invention can concurrently has functions of fire retardation and thermal insulation, and characteristics of high wave absorption strength, wide wave absorption frequency band, and small surface density; and the material of the present invention can be used for wave absorption defilading, electromagnetic shielding, and the like.
Owner:ACADEMY OF ARMORED FORCES ENG PLA

Method for producing composite non-woven cloth material from irradiated ultrahigh molecular weight polyethylene fiber

The invention relates to a method for producing a composite non-woven fabric material from irradiated ultrahigh molecular weight polyethylene (UHMWP) fiber. The method comprises the following steps of: (1) spreading a plurality of strands of ultrahigh molecular weight polyethylene fiber in parallel by using a guide roller after passing through a buncher, and impregnating the fiber in a grafting liquid; (2) irradiating the fiber impregnated in the grafting liquid to realize grafting, and sending the fiber into a glue dipping groove; (3) processing glue on double surfaces of adhesive-containing filament bundles by using parallel scrappers, and drying the filament bundles to obtain a one-way non-woven fabric; (4) producing composite non-woven fabric sheets or coils to obtain a composite non-woven fabric material. Compared with the prior art, the method has the advantages that an electron beam irradiation grafting technology is introduced into a UD cloth production method in the invention, so that the UHMWP fiber can be grafted and modified through mutual irradiation, and interfacial adhesive performances of the fiber and the adhesive can be improved; and therefore, the consumption of the adhesive is reduced during the production of the one-way non-woven fabric, application of a protective film is eliminated, and finally surface density of the composite non-woven fabric material is reduced.
Owner:SURREY HI TECH INC +1

Waves-absorbing material for Ku waveband radar with film structure

The invention relates to a wave-absorbing material for a Ku waveband radar with a film structure, mainly comprising six wave-absorbing material layers and five plastic films, wherein the plastic films are arranged between every two wave-absorbing material layers of the six wave-absorbing material layers; the first wave-absorbing material layer is a mixture of 1.50 parts of coupling agents, 50 parts of diluents, 150 parts of ferrites and 53.67 parts of 60% epoxy resins; the second wave-absorbing material layer is a mixture of 1.50 parts of the coupling agents, 50 parts of the diluents, 150 parts of carbonyl iron absorbents, 39.83 parts of the 60% epoxy resins and 12.93 parts of curing agents; the third wave-absorbing material layer is a mixture of 1.50 parts of the coupling agents, 50 parts of the diluents, 150 parts of the carbonyl iron absorbents, 109.02 parts of the 60% epoxy resins and 33.10 parts of the curing agents; and the fourth wave-absorbing material layer, the fifth wave-absorbing material layer and the sixth wave-absorbing material layer are mixtures of 1.50 parts of the coupling agents, 50 parts of the diluents, 150 parts of the carbonyl iron absorbents, 39.83 parts of the 60% epoxy resins and 12.93 parts of the curing agents. The wave-absorbing material combines an impedance gradual change principle with an electromagnetic wave trap principle, has high wave-absorbing property within a Ku waveband range, little thickness, low surface density, light weight and good mechanical property and is suitable for resisting the Ku waveband radar.
Owner:江苏万华拓谷新材料科技有限公司

Device for unfolding surface of space rope system

The invention discloses a device for unfolding a surface of a space rope system, and is mainly used for solving the problems that the prior art is difficult to mold and has bad stability. The device comprises a plurality of reflectors or transmission surfaces (1), a plurality of flexible pulling cables (2), a satellite platform (4) and a plurality of control mechanisms (3) of the pulling cables, wherein each reflector or transmission surface (1) is composed of a folding ring (4) and a ring connecting joint (5), and is stacked according to the caliber size; one end of each flexible pulling cable (2) penetrates through a corresponding hole of the folding ring (4) of the reflector or transmission surface with the biggest caliber to be tied fixedly, and then penetrates through the folding ring (4) of the other reflector or transmission surface to be tied fixedly; the other end of each flexible pulling cable (2) is connected with the control mechanisms (3) on the satellite platform; and the reflectors or transmission surfaces are connected hierarchically to form a stacked structure composed of the satellite platform and all reflectors or transmission surfaces so as to form a space rope system. The device can achieve effective molding structure, autonomous orbit and pose stability of the whole system, so that the device can be applied in a large antenna or telescope in space.
Owner:XIDIAN UNIV
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