59results about How to "Achieve thickness" patented technology

The invention relates to a vertical cavity surface emitting laser and method for fabricating the same. The vertical cavity surface emitting laser of the invention comprises: a substrate, a first reflector, an active layer, a second reflector, a first electrode layer and a second electrode layer. The second reflector has a first confinement layer with a first aperture and a second confinement layer with a second aperture. The second aperture is smaller than the first aperture. According to the invention, because the second confinement layer is formed by implanting oxygen ion into the second reflector and heating to let the oxygen ion and Al content in the second reflector react to form an oxide layer, the second confinement layer can be used as an optical and electronic confinement layer. Therefore, the width and depth of the second confinement layer can be achieved precisely and easily.

The present invention relates to a controllable polymeric surface coating including a macromolecule, which is covalently bound to the surface of a substrate, the macromolecule including a plurality of polymerisation initiators and a plurality of surface binding groups; and pendant polymers grafted from at least some of the polymerisation initiators.

A rotor blade for a wind power plant, comprises an upper shell and a lower shell which are joined to each other and have a trailing edge each, and which has a profile extending in the direction of flow and, at its rear end, exhibiting a profile trailing edge of a thickness, wherein the trailing edges of the upper and lower shells are spaced apart in at least one area of the rotor blade such that the thickness of the profile trailing edge is defined by one of the shells.

The present invention relates to a method for casting an acryl film, which includes the steps of injecting a material of the acryl film into a space that is formed from a pair of substrates and a gasket positioned between a pair of substrates, and curing the material of the acryl film. The shrinkage ratio of the gasket is not less than 10% after the acryl film is subjected to the curing step, or the shrinkage ratio of the gasket after the acryl film is subjected to the curing step is the same as or larger than the shrinkage ratio of the material of the acryl film.

The invention relates to a method of processing the surfaces of light alloy, in particular to a method of processing the surfaces of aluminium alloy pistons and precision friction pairs. The method comprises the steps that (1) washing is performed; (2) oxidization is performed; (3) hole plugging is performed. Nanoscale metal matrix ceramic oxidation film layers with the density up to the standard are respectively grown on the aluminium alloy pistons and precision friction pairs processed in the method, the density is increased, the diameters of blind holes are decreased obviously, nanometer penetrant blind holes are sealed, roughness is reduced, the friction coefficient is reduced, and the geometric dimensions are unchanged basically. The aluminium alloy pistons and precision friction pairs processed in the method can be installed for use in a matched mode without finish machining, industrial mass production can be achieved, and the method reduces production cost greatly compared with original technical methods.

The invention discloses a multilayer antenna structure and antenna. The multi-layer antenna structure includes an upper dielectric substrate, an intermediate dielectric substrate, a lower dielectric substrate and a reflector arranged in sequence, wherein: the upper surface of the upper dielectric substrate is provided with a parasitic patch; the intermediate dielectric substrate and the upper dielectric substrate are arranged at intervals. The upper surface of the intermediate dielectric substrate is provided with a radiation patch, and the lower surface is integrally attached with a first metal grounding layer; the upper surface of the lower dielectric substrate is arranged in close contact with the lower surface of the intermediate dielectric substrate, and the lower surface of the lower dielectric substrate is provided with The feeding structure has a second metal ground layer attached to the entire upper surface, wherein the feeding structure and the radiation patch are connected through metal probes; and the reflector is located on the lower surface side of the lower dielectric substrate, and there is an air layer between the lower dielectric substrate and the lower dielectric substrate. . The invention solves the technical problem that the performance and thickness requirements of the antenna cannot be balanced.

The present invention provides a surface-modified porous metal implant and a preparation method thereof. The porous metal implant has a structural hole, and the preparation method comprises a step of micro-arc oxidation by using a plurality of power sources for power supply. The power sources comprise a first power source and a second power source. The step of micro-arc oxidation comprises connecting a first anode connector of the porous metal implant with an anode of the first power source; arranging a connection cathode in the structural hole and connecting the connection cathode with a cathode of the first power source; connecting a second anode connector of the porous metal implant with an anode of the second power source; connecting an electrolytic bath with a cathode of the second power source; and immersing the porous metal implant into a bath solution and using the first power source and the second power source for power supply to carry out micro-arc oxidation treatment. The first power source and the second power source are controlled in a mutually independent manner. With power supply by the multiple power sources, an electric field intensity difference and an electric field energy intensity difference between the inner wall and the outer wall of the structural hole can be reduced, thereby obtaining an in-situ growth film with a good quality.

The invention discloses a metal layer pulsed eddy current thickness measurement method. The phase jump point of a signal in a time-frequency domain acts as thickness measurement characteristic quantity, a pulsed eddy current detection experiment is performed on multiple standard test pieces of which the thickness is known, and a relation curve between the metal layer thickness and the phase jump point is established and acts as a thickness calibration curve to assist completion of thickness measurement of workpieces to be measured in actual detection. According to the method, extraction of the thickness measurement characteristic quantity is extended to the time-frequency domain from a time domain, and resolution of the signal for parameters to be measured is fully utilized so as to be particularly suitable for thickness measurement of a nonmetal coating layer or a multilayer metal structure. Besides, thickness measurement is realized by utilizing the phase so that probe lift-off interference and metal layer thickness change can be effectively distinguished, anti-interference capacity of detection can be enhanced and accuracy of the measurement result can be guaranteed in comparison with the existing device method of directly adopting the time-domain characteristic quantity.