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60results about How to "Small porosity" patented technology

Pressure wave generator and process for manufacturing the same

Even when compression stress is generated because a volume of a thermal insulation layer 2 is expanded due to oxidized by oxygen in the air, occurrence of cracks and fractures of the thermal insulation layer and a heating conductor 3 caused by the cracks are prevented by dispersing the compression stress. A pressure wave generator comprises a substrate 1, the thermal insulation layer 2 of porous material which is formed on a surface of the substrate 1 in thickness direction, and the heating conductor 3 of thin film formed on the thermal insulation layer 2, and generates pressure waves by heat exchange between the heating conductor 3 and a medium. When a thickness at the center of the thermal insulation layer 2 in width direction W is used as a reference thickness, and it is assumed that distribution of thickness of thermal insulation layer in the width direction is averaged with the reference thickness, porosity in an outer peripheral portion of the thermal insulation layer is made smaller than porosity in the center portion. By making the porosity in the outer peripheral portion of the thermal insulation layer 2 smaller, a number of immovable points on the outer periphery of the thermal insulation layer 2 restricted by the substrate 1 is increased and the positions of them are dispersed, so that the compression stress compressed in the outer peripheral portion of the thermal insulation layer 2 can be dispersed.
Owner:MATSUSHITA ELECTRIC WORKS LTD

Pressure Wave Generator and Process for Manufacturing the Same

Even when compression stress is generated because a volume of a thermal insulation layer 2 is expanded due to oxidized by oxygen in the air, occurrence of cracks and fractures of the thermal insulation layer and a heating conductor 3 caused by the cracks are prevented by dispersing the compression stress. A pressure wave generator comprises a substrate 1, the thermal insulation layer 2 of porous material which is formed on a surface of the substrate 1 in thickness direction, and the heating conductor 3 of thin film formed on the thermal insulation layer 2, and generates pressure waves by heat exchange between the heating conductor 3 and a medium. When a thickness at the center of the thermal insulation layer 2 in width direction W is used as a reference thickness, and it is assumed that distribution of thickness of thermal insulation layer in the width direction is averaged with the reference thickness, porosity in an outer peripheral portion of the thermal insulation layer is made smaller than porosity in the center portion. By making the porosity in the outer peripheral portion of the thermal insulation layer 2 smaller, a number of immovable points on the outer periphery of the thermal insulation layer 2 restricted by the substrate 1 is increased and the positions of them are dispersed, so that the compression stress compressed in the outer peripheral portion of the thermal insulation layer 2 can be dispersed.
Owner:MATSUSHITA ELECTRIC WORKS LTD

Super-retarded concrete and preparation method thereof

The invention discloses super-retarded concrete and a preparation method thereof. The super-retarded concrete is prepared from the following raw materials in parts by weight: 165-180 parts of water, 280-335 parts of cement, 565-620 parts of sand, 990-1200 parts of stone, 70-85 parts of flyash, 85-110 parts of mineral powder and 7.8-9.4 parts of an additive, wherein the additive is prepared from aretarder and a water reducer according to a mass ratio of 1 to (3.5-4.1). The retarder is prepared from the following components in parts by weight: 10-15 parts of phosphogypsum, 70-100 parts of water, 26-38 parts of a titanate coupling agent, 80-90 parts of an ammonium hydroxide solution with a mass fraction of 15-20%, 28-34 parts of absolute ethyl alcohol with a mass fraction of 20-35% and 20-40parts of polypropylene. The preparation method of the super-retarded concrete comprises the following steps: S1, adding the water reducer and a defoamer into water and fully mixing to obtain a firstmixture; S2, fully mixing corresponding parts by weigh of cement, stone, sand, flyash and mineral powder to form a second mixture; and S3, adding the first mixture into the second mixture, uniformly stirring, then adding the retarder and fully mixing to form the super-retarded concrete. The super-retarded concrete has the advantages of long setting time and high later-stage strength.
Owner:青岛康兴混凝土有限公司

Surface wear-resisting layer of gas turbine compressor blade and blade root and manufacturing method thereof

InactiveCN101737352AEnhanced performance against fretting fatigueQuality improvementMolten spray coatingPump componentsPorosityIndium
The invention provides a surface wear-resisting layer of gas turbine compressor blade and blade root and a manufacturing method thereof. The surface wear-resisting layer is positioned on the contact surface of blade bottom and an impeller, and is a coating which is made of copper-nickel indium alloy powder; the copper-nickel indium alloy powder comprises the following components: 50-60 wt% of copper powder, 30-40 wt% of nickel powder, 3-10 wt% of indium powder; and a supersonic speed flame spraying method is used to spray the copper-nickel indium alloy powder on the surface of the blade root. The thickness of the coating is 0.07-0.09 mm. The surface wear-resisting layer of the invention is a fretting wear-resisting layer, which enhances blade fretting fatigue resistance, and prolongs the service life of products. the supersonic speed flame spraying (AC-HVAF) process method is adopted to prepare the copper-nickel-indium coating with lower porosity and high bonding strength; the method simplifies process flow, reduces production cost, plays a positive social benefit for the improvement of gas turbine product quality and the popularization of new technology and new process of the products, and greatly facilitates localization progress of heavy gas turbine products in China.
Owner:DONGFANG TURBINE CO LTD
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