Patents
Literature
Hiro is an intelligent assistant for R&D personnel, combined with Patent DNA, to facilitate innovative research.
Hiro

14 results about "Carbon fiber composite" patented technology

Device and method for detecting debonding defects of carbon fiber composite material

ActiveCN106596714AUniform excitation magnetic fieldAvoid missing detectionMaterial resistanceMaterial magnetic variablesMagnetic fieldCarbon fiber composite
The invention discloses a device and a method for detecting debonding defects of a carbon fiber composite material. The device comprises a stimulating component and a plurality of detecting components, wherein the stimulating component is used for generating a stimulating magnetic field and comprises a cuboid magnetic core and an exciting coil winding the cuboid magnetic core; the detecting components are used for detecting induced magnetic fields influenced by a disturbed magnetic field and are uniformly arrayed below the stimulating component, the arraying direction of the detecting component is parallel with long sides of the cuboid magnetic core, and the detecting components are distributed opposite to the stimulating component; and a detecting coil is located between the exciting coil and a to-be-detected carbon fiber composite material during the detection. According to the detecting device and method provided by the invention, the rapid and real-time local detection can be realized, and furthermore, the detection range is not influenced by the space size of the detecting device.
Owner:NANCHANG HANGKONG UNIVERSITY

Combined tool for carbon fiber aramid paper honeycomb sandwich composite board

PendingCN109591079AExtended service lifeLow costMetal working apparatusHoneycombComposite plate
The invention discloses a combined tool for a carbon fiber aramid paper honeycomb sandwich composite board. The combined tool for the carbon fiber aramid paper honeycomb sandwich composite board comprises a tool bar and a tool bit, wherein the tool bit comprises a first cutting component and a plurality of second cutting components, the first cutting component is used for machining an upper carbonfiber layer and a lower carbon fiber layer of the composite board, and comprises an upper tool disc and a lower tool disc, a plurality of first spiral grooves are formed in the periphery of each tooldisc correspondingly, and first tool teeth of the tool discs are formed between every two adjacent first spiral grooves; the plurality of second cutting components are used for machining an aramid paper honeycomb sandwich layer of the composite board, and the second cutting components are stacked together; each second cutting component comprises two blades which are adjacent to each other up anddown, and a plurality of second spiral grooves are formed in the periphery of each blade correspondingly, and second tool teeth of each blade are formed between every two adjacent second spiral grooves; the second cutting components are located between the two tool discs, and the cutting directions of the first tool teeth of the tool discs and the cutting directions of the second tool teeth of each blade are consistent. According to the combined tool for the carbon fiber aramid paper honeycomb sandwich composite board, synchronous cutting of carbon fiber composite material and aramid paper honeycomb core material can be realized, the machining quality and the machining efficiency are improved, and the service life of the tool is prolonged.
Owner:JIMEI UNIV

Method for designing and checking torsional rigidity of carbon fiber composite winding pipe fitting

PendingCN114297839ADesign optimisation/simulationComplex mathematical operationsCarbon fiber compositeTorsional rigidity
The invention belongs to the field of composite material structure design and analysis, and particularly relates to a method for designing and checking torsional rigidity of a carbon fiber composite material winding pipe fitting. Comprising the following stages: (1) a data preparation stage: drawing a change process curve (hereinafter referred to as a shear modulus process curve) of an equivalent shear modulus Gxy of a virtual winding pipe fitting along with a winding angle +/-theta on the basis of basic mechanical property parameters of a composite material in combination with a classical composite material mechanical basic principle; (2) a rigidity design stage: calculating an equivalent shear modulus Gxy meeting the rigidity requirement according to information such as the inner diameter, the outer diameter, the length and the torsional rigidity index of the winding pipe fitting, and then reversely checking a shear modulus process curve to obtain an available winding angle range; and (3) a rigidity checking stage: querying the corresponding equivalent shear modulus Gxy according to the inner diameter, the outer diameter, the length and the winding angle +/-theta of the winding pipe fitting, and then directly obtaining the torsional rigidity of the structure at the current winding angle by applying a torsional rigidity calculation formula.
Owner:西安科为智通复合材料技术有限公司

A kind of carbon fiber composite bulletproof plate and preparation method thereof

ActiveCN104197786BShorten the timeIncrease productivityLaminationLamination apparatusEnergy absorptionFiber-reinforced composite
The invention relates to a bulletproof plate made of carbon fiber composites and a method for manufacturing the bulletproof plate. The bulletproof plate comprises a rigid face layer, a face layer connecting transition layer, an energy absorption layer, a back layer connecting transition layer and a rigid back layer which are formed by means of hot pressing. The rigid face layer is made of carbon fiber resin-based composites; the face layer connecting transition layer and the back layer connecting transition layer are made of prepreg, and energy absorption fibers and carbon fibers with immersed thermosetting resin are braided to form the prepreg; multilayer plates made of energy absorption fiber-reinforced composites are pressed to form the energy absorption layer; toughened and modified thermosetting resin and one type or a plurality of types of high-performance carbon fibers, basalt fibers and ceramic fibers are composited and pressed to form the rigid back layer. The bulletproof plate and the method have the advantages that the bulletproof plate is made of multilayer composite materials, can effectively resist impact force of bullets and is light as compared with the traditional bulletproof materials, and the bullet penetration depths can be effectively reduced.
Owner:SHANDONG UNIV

Display and control console support arm and forming method thereof

PendingCN114407384ACarbon fiber compositeEngineering
The invention provides a display and control console support arm and a forming method thereof. The display and control console support arm is provided with a special-shaped closed cavity. The method comprises the following steps: respectively paving a first film and a second film which are made of a carbon fiber prepreg carbon fiber composite material on the inner walls of an upper die and a lower die of a die; an air pipe is laid in the lower mold where the second film is laid, and then the lower mold and the upper mold where the first film is laid are assembled; after die assembly, high-pressure gas is introduced into the air pipe, so that the first film and the second film are attached to the upper die and the lower die respectively; after high-pressure gas is introduced, the first film and the second film are heated and cured, so that the first film and the second film are formed and combined together; the upper die and the lower die are removed; wherein the shape of the shell of the air pipe is the same as that of the display and control console support arm. According to the forming method of the display and control console supporting arm, the process flow can be shortened, and the forming efficiency can be improved. And moreover, the risk of glue joint cracking can be controlled, and the product stability is improved.
Owner:CETC WUHU DIAMOND AIRCRAFT MFG +1

Carbon fiber composite plate and manufacturing method thereof

ActiveCN106760152AConstruction materialSynthetic resin layered productsCarbon fiber compositeFiber
The invention provides a carbon fiber composite plate and a manufacturing method thereof. The carbon fiber composite plate comprises protection layer plates which include the first protection layer plate and the second protection layer plate. A plate core is inlaid between the first protection layer plate and the second protection layer plate. The plate core is a carbon fiber plate core. Through holes are formed in the first protection layer plate and the second protection layer plate, penetrate through the first protection layer plate and the second protection layer plate and communicate with the plate core. By adoption of the technical scheme, the static bending intensity of the carbon fiber composite plate can be improved, and the nonaqueous property, watertightness, non-deformation, concrete non-adhesion, high temperature resistance, abrasion resistance, acid and alkali resistance and the like of the composite plate can be improved; meanwhile, by applying the carbon fiber composite plate to building construction, the problems of plate surface expansion, delaminating, plumping up, thickness non-uniformity and the like can be avoided; and the carbon fiber composite plate provided by the invention is simple in structure and can be manufactured directly through an old formwork, thereby being economical and practical.
Owner:湖州优研知识产权服务有限公司
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products