5results about How to "Improve load transfer efficiency" patented technology

The application discloses a kind of high-performance outdoor full package imitation wood composite board and preparation method thereof, relate to polyurethane composite board technical field, the full package imitation wood composite board includes base board, and the polyurethane material of setting in the lower surface and the four around of base board, and the resin material of setting in upper surface.Its preparation method includes the following steps: pouring polyurethane material in the silica gel mould after surface treatment, place base board, mould pressing, make the polyurethane material with wood texture around and lower surface of base board composite, obtain intermediate product A;Resin material is rolled on the upper surface of intermediate product A, and is dried, to obtain full package imitation wood composite board;The silica gel mould after surface treatment is prepared by transferring real solid wood board texture.

The invention provides a carbon fiber reinforced polyether-ether-ketone self-lubricating composite material and a preparation method and application thereof.The preparation method comprises the steps that carbon fiber serves as an anode, voltage is applied to an electrolyte solution, electrochemical oxidation treatment is conducted, hydroxylated carbon fiber is obtained, the hydroxylated carbon fiber and 2-amino-5-nitrobenzothiazole are mixed, and the carbon fiber reinforced polyether-ether-ketone self-lubricating composite material is obtained. Adding an anhydrous modified reaction solvent, and reacting at 25-40 DEG C for 4-10 hours to obtain modified carbon fibers; and melting and granulating the self-lubricating composite material: mixing the modified carbon fiber, polyether-ether-ketone, a lubricant and an auxiliary agent in a high-speed mixer for 10-20 minutes, extruding by using a double-screw extruder, cooling, and granulating to obtain the carbon fiber reinforced polyether-ether-ketone self-lubricating composite material. The carbon fiber reinforced polyether-ether-ketone self-lubricating composite material is applied to self-lubricating mechanical parts. According to the self-lubricating composite material, the self-lubricating performance is improved, the interface bonding energy between the carbon fibers and the polyether-ether-ketone is enhanced, and the self-lubricating composite material has good mechanical performance.

This invention belongs to the field of thermoplastic composite material joining technology, and specifically relates to a method for preparing a silane-modified thermoplastic composite resistance welding heating element. The invention first performs a cleaning pretreatment on a carbon nanotube film to remove surface contaminants. Then, plasma treatment technology is used to etch and activate the film surface, introducing oxygen-containing groups to provide active sites for silane grafting. Finally, silane is grafted onto the plasma-activated film using a silane coupling agent, utilizing its bifunctional properties to construct a molecular bridge between the carbon nanotubes and the resin, thereby improving the interfacial bonding force between the film heating element and the resin, and increasing the resistance welding strength. The heating element prepared by this invention has high specific strength, corrosion resistance, and better homogeneity with the base material, making it more suitable for complex welding joint service environments.

A butt joint structure of an aircraft fuselage comprises a plurality of first stringer joints and a plurality of second stringer joints which are respectively connected with a metal fuselage stringer and a composite material fuselage stringer. The butt-joint structure further comprises a butt-joint frame and a butt-joint belt plate which are fixed together. The butt-joint frame comprises a butt-joint frame web, a first outer edge strip and a second outer edge strip, the first stringer connector is fixedly connected to one of the first outer edge strip and the second outer edge strip, and the second stringer connector is fixedly connected to the other one of the first outer edge strip and the second outer edge strip. The second stringer joints are disposed in pairs, each pair of second stringer joints corresponding to one of the first stringer joints such that a longitudinal axis of each metal fuselage stringer is aligned with a longitudinal axis of a corresponding composite fuselage stringer. According to the butt joint structure, butt joint between two fuselage sections made of different materials can be accurately achieved, eccentricity of the overall force transmission path of the fuselage of the aircraft is avoided, and the load transmission efficiency is improved.

The utility model relates to the technical field of iron tower precast concrete, in particular to an anti-seismic and anti-skid electric power iron tower precast concrete foundation structure which comprises a concrete foundation body and connecting supporting columns. A bump, an extension rod and a clinging plate in the anti-skid positioning assembly, and a rubber plate, a shock-absorbing damper, a supporting plate, a connecting column and the like in the shock-absorbing buffering assembly are arranged; through the mutual matching relation between the connection of the convex block and the extension rod, the vibration energy absorption of the rubber plate and the shock absorption damper, the load transmission of the supporting plate and the connecting column and other components, the convex block can be embedded into a foundation soil layer through the inverted convex structure to form mechanical anchoring; the rubber plate buffers earthquakes or dynamic loads through elastic deformation and the shock absorption damper through the energy dissipation effect, and then the effects that the device can enhance the friction force and anchoring force of the soil body through the anti-skid positioning assembly, reduce vibration impact through the shock absorption buffering assembly and effectively improve the anti-seismic performance and anti-sliding capacity of the electric power iron tower foundation are achieved.