子分类：
| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 101 | JPH0142742B2 - | JP21036684 | 1984-10-09 | JPH0142742B2 | 1989-09-14 | HAYASHI CHIKARA; KASHU SEIICHIRO |
| 102 | Corrosion resistant structural parts | JP388186 | 1986-01-10 | JPS62161946A | 1987-07-17 | HORIE TAKAO; KATO AKIHIKO; SAKAI SHOICHI |
| PURPOSE:To improve the corrosion resistance of parts buried in the ground by tearing spheroidal graphite particles from the surface of spheroidal graphite cast iron as a base material and by thermally spraying ceramics on the surface of the cast iron. CONSTITUTION:Structural parts buried in the ground such as a bolt and a nut are made of spheroidal graphite as a base material. Spheroidal graphite particles 4 are torn from the surfaces of the matrixes 2 of the structural parts and ceramics is thermally sprayed on the surfaces of the parts to a prescribed thickness so that holes 6 formed by tearing the particles 4 are filled with the resulting thermally sprayed ceramic layers 8. Thus, structural parts having superior corrosion preventing performance and improved durability can be provided. | ||||||
| 103 | Manufacture of corrosion resistant tank | JP10907885 | 1985-05-20 | JPS61266561A | 1986-11-26 | IGAWARA KEIICHI |
| PURPOSE:To obtain a tank usable for a long period by coating the surfaces of an annular plate with a corrosion resistant material for thermal spraying. CONSTITUTION:The surfaces, especially the underside of the annular plate 1 of a tank are coated 2 with a material for thermal spraying such as Zn, Al, a Zn-Al alloy, plastics or ceramics by thermal spraying. At this time, protective plates 6, 61 are preferably placed on the parts 5, 51 of the plate 1 to be welded to other members so as to prevent the sticking of the thermally sprayed material to the parts 5, 51. By this method, the corrosion resistance and insulation of the annular plate 1 of the corrosion resistant tank are enhanced. | ||||||
| 104 | Manufacturing method of three-layer structural cylindrical body | JP15724783 | 1983-08-30 | JPS6052226A | 1985-03-25 | FUJI AKIRA |
| PURPOSE:To raise the mechanical strength of a three-layer structural cylindrical body, by manufacturing it upon heat treatment in spraying copper and copper alloy to both large and small diametral outer and inner cylinders, an intermediate cylinder and both inner and outer cylinders of copper and copper alloy, in case of a manufacturing method of the three-layer structural cylindrical body of a rotor for a superconductivity motor. CONSTITUTION:A cylindrical body of an intermediate diameter composed of a copper system material is produced as an intermediate cylinder 5, while a larger cylindrical body than the intermediate cylinder 5 is set down to an outer cylinder 6 and a smaller cylindrical body than the intermediate cylinder 5 is set down to an inner cylinder 7 whereby each of them is manufactured with precipitation hardening system stainless steel. A copper system material 8 of the same quality of material as the intermeditate cylinder 5 is firmly stuck to an outer circumference of the cylinder 7 in uniform thickness by means of a metal-spraying process, At this time, this spraying also takes place on an inner circumference of the outer cylinder 6. A three-layer cylinder 10 is manufactured by means of shrinkage fit or expansion fit of those of inner cylinder 7, intermeditate cylinder 5 and outer cylinder 6. Setting them within the range of a temperature of 700-1,000 deg.C, the three-layer cylinder 10 is heated whereby metallugical binding in a boundary surface of these cylinder 7, 5 and 6 is accelerated in this way. | ||||||
| 105 | Process for selectively producing thermal barrier coatings on turbine hardware | US13724324 | 2012-12-21 | US10100650B2 | 2018-10-16 | Thomas Edward Mantkowski; John Maynard Crow; Shawn Michael Pearson; Stephen Mark Molter |
| A process of depositing a ceramic coating on an airfoil component and the component formed thereby is provided. The process includes depositing a bond coat on an airfoil component including on a trailing edge region thereof that defines a trailing edge of the airfoil component, within holes located within the trailing edge region and spaced apart from the trailing edge, and on lands located within the trailing edge region and between the holes. A ceramic coating is then deposited on the bond coat including on the trailing edge region of the airfoil component, within the holes located within the trailing edge region, and on the lands between the holes. The ceramic coating within the holes is selectively removed without completely removing the ceramic coating on the trailing edge region and the lands between the holes. | ||||||
| 106 | COATING SYSTEM AND METHOD | US15966350 | 2018-04-30 | US20180250688A1 | 2018-09-06 | Ambarish Kulkarni; Byron Pritchard; Hrishikesh Keshavan; Mehmet Dede; Bernard Patrick Bewlay |
| An atomizing spray device includes a housing having inlets that receive a first fluid and a slurry of ceramic particles and a second fluid. The inlets are fluidly coupled with outlets by an interior chamber that mixes the first fluid with the slurry to form a primary mixture of the first fluid and first atomized droplets of the slurry. A first outlet on a first side of the housing and a second outlet on the first side of the housing are shaped to change the primary mixture to form a secondary mixture of the first fluid and second atomized droplets of the slurry. The first outlet sprays the secondary mixture onto a first surface as a first layer of coating and the second outlet sprays the secondary mixture onto the first surface as a second layer of coating while the housing moves in a direction along the first surface. | ||||||
| 107 | METHOD OF DEPOSITING ONE OR MORE LAYERS OF MICROSPHERES TO FORM A THERMAL BARRIER COATING | US15394214 | 2016-12-29 | US20180185876A1 | 2018-07-05 | Michael J. Walker |
| A method of forming a thermal barrier coating onto a surface of a ferrous alloy or nickel alloy component part involves depositing a layer of hollow microspheres to a surface of the component part or to a previously deposited layer of hollow microspheres through heating and cooling of a metallic precursor setting layer composed of copper, a copper alloy, or a nickel alloy. Once deposited in place, the layer(s) of hollow microspheres are heated to sinter the hollow microspheres to each other and to the surface of the ferrous alloy or nickel alloy component part to form an insulating layer. | ||||||
| 108 | SPUTTER TRAP HAVING MULTIMODAL PARTICLE SIZE DISTRIBUTION | US15824802 | 2017-11-28 | US20180171465A1 | 2018-06-21 | Jaeyeon Kim; Patrick K. Underwood; Susan D. Strothers; Michael D. Payton; Scott R. Sayles |
| A sputter trap formed on at least a portion of a sputtering chamber component has a plurality of particles and a particle size distribution plot with at least two different distributions. A method of forming a sputter trap having a particle size distribution plot with at least two different distributions is also provided. | ||||||
| 109 | MANUFACTURING METHOD OF POROUS THERMAL INSULATION COATING LAYER | US15587186 | 2017-05-04 | US20180161807A1 | 2018-06-14 | Bokyung KIM; In Woong LYO; Woong Pyo HONG; Hong Kil BAEK; Su Jung NOH; Seung Jeong OH; Seungkoo LEE; Seung Woo LEE |
| Disclosed herein is a manufacturing method of a porous thermal insulation coating layer. In the manufacturing method, a porous thermal insulation coating layer having excellent close adhesion may be uniformly formed within a shorter time and the porous thermal insulation coating layer may be applied to an internal combustion engine, thereby making it possible to secure low thermal conductivity and low volume thermal capacity. | ||||||
| 110 | METHOD AND DEVICE FOR PRODUCING AN ARMOR PLATING FOR PROTECTED VEHICLES | US15485783 | 2017-04-12 | US20170307338A1 | 2017-10-26 | Werner Krömmer; Jörg Lorenz |
| A method for producing an armor plating for protected vehicles is described. The method employs the following steps: supplying a substrate made of a metal and/or a nonmetal and coating the substrate with the aid of a thermal spraying process. A device for producing an armor plating is also described herein. | ||||||
| 111 | SYSTEMS AND METHODS FOR TEXTURING METAL | US15384452 | 2016-12-20 | US20170297059A1 | 2017-10-19 | David Pavlick |
| Systems and methods disclosed herein relate to texturing a metal surface. A method for texturing a metal surface comprises disposing a first ceramic coating onto a first surface on the metal surface, applying a media to the first ceramic coating, disposing a second ceramic coating onto the media, and/or heat treating the metal surface for an end duration. | ||||||
| 112 | MINIMIZATION OF RING EROSION DURING PLASMA PROCESSES | US15335074 | 2016-10-26 | US20170200588A1 | 2017-07-13 | Olivier JOUBERT; Olivier LUERE; Vedapuram S. ACHUTHARAMAN |
| Methods are disclosed for etching a substrate. The method includes preferentially coating cover ring relative other chamber components in the processing chamber, while under vacuum, and while a substrate is not present in the processing chamber. The substrate is subsequently etched the processing chamber. After etching, the interior of the processing chamber is cleaned after the substrate has been removed. | ||||||
| 113 | THERMAL BARRIER COATING SYSTEMS AND METHODS OF MAKING AND USING THE SAME | US15384712 | 2016-12-20 | US20170101875A1 | 2017-04-13 | Larry Steven Rosenzweig; James Anthony Ruud; Shankar Sivaramakrishnan |
| A method for coating a surface of a substrate is provided. The method includes providing a suspension or a precursor comprising feedstock material suspended in a liquid medium. Further, the method includes spraying the suspension or the precursor onto the surface at a spray angle less than about 75 degrees to a tangent of the surface. | ||||||
| 114 | PLASMA NON-STICK PAN AND MANUFACTURING METHOD THEREOF | US15362843 | 2016-11-29 | US20170071401A1 | 2017-03-16 | Cheng Fang; Qiang Cheng |
| The present invention discloses a plasma non-stick pan and manufacturing method thereof. The plasma non-stick pan comprises a pan body and a non-stick layer applied to the pan body; a plasma layer is provided between the non-stick layer and the pan body, and the plasma layer comprises a MCrALY layer sprayed to the surface of the pan body and a mixture layer sprayed outside of the MCrALY layer, and the mixture layer is composed of MCrALY particles and metal oxide particles. The MCrALY layer has good toughness and strong adhesion, and it is easy to bind with the substrate with high fastness after binding, playing a buffering role and laying a foundation for the subsequent spraying of mixture layer. | ||||||
| 115 | TURBINE BLADE COATING COMPOSITION AND METHOD THEREOF | US14514455 | 2014-10-15 | US20160108509A1 | 2016-04-21 | Krishnamurthy Anand; Surinder Singh Pabla; Eklavya Calla |
| A composition for a reinforced metal matrix coating, and a method of preparing and coating the composition. The composition includes a plurality of sacrificial metallic binder particles that is anodic with respect to a base substrate, and a plurality of hard particles. | ||||||
| 116 | METHOD OF MANUFACTURING GAS TURBINE ENGINE ELEMENT HAVING AT LEAST ONE ELONGATED OPENING | US14338480 | 2014-07-23 | US20160024966A1 | 2016-01-28 | Marc CAMPOMANES; Orlando SCALZO; Bruno CHATELOIS |
| A method of manufacturing a gas turbine engine element, for example a shroud segment. An insert has at least one elongated feature received in a mold cavity. A powder injection molding feedstock is injected. When the green part is disengaged from the mold, each elongated feature is slid out of the green part to define a respective elongated passage. The cross-sectional dimension of the elongated feature may be 0.020 inches or less, and/or a ratio between the length and cross-sectional dimension of the elongated feature may be at least 25. The method may include, after debinding and sintering, projecting a coating material while defining an obstruction between source of coating material and the open end of each elongated feature with a shoulder of the element to prevent the coating material from reaching the open end, followed by machining to remove at least a part of the shoulder. | ||||||
| 117 | JET NOZZLE, JET PROCESSING DEVICE, PROCESSING METHOD, METHOD FOR MANUFACTURING CELL COMPONENT, AND SECONDARY CELL | US14801321 | 2015-07-16 | US20150325835A1 | 2015-11-12 | Mohammad Saeed SEPASY ZAHMATY; Tatsuya SEKIMOTO |
| A jet nozzle includes: a jet opening through which a fluid mixture of particles and gas is jetted; a first flow channel extending along a first direction to the jet opening; a flow diverging region located in the first flow channel at opposite the jet opening and comprises a plurality of flow diverging channels arranged in a direction intersecting with the first direction; a second flow channel that makes the particles join in the flow diverging region in a second direction which is at a predetermined angle to the first direction; and a third flow channel through which the gas is jetted to the first flow channel. | ||||||
| 118 | METHOD FOR MANUFACTURING A TURBINE ASSEMBLY | US14431949 | 2013-08-23 | US20150266143A1 | 2015-09-24 | Jonathan Mugglestone |
| A method for manufacturing a turbine assembly, which includes at least two aerofoils arranged adjacent towards each other and embodied as a twin vane segment, is provided. The method includes: processing the turbine assembly with a first protection technique providing a first protection for the at least two adjacent aerofoils, wherein at least one region of one aerofoil remains unprocessed; pre-processing of the at least one region that will remain unprocessed or post-processing of the at least one region that remained unprocessed with a second protection technique to provide a second protection for the at least one region of the one aerofoil, wherein the first and the second protection techniques differ from one another. | ||||||
| 119 | Deposition of Integrated Protective Material Into Zirconium Cladding for Nuclear Reactors by High-Velocity Thermal Application | US14548630 | 2014-11-20 | US20150098545A1 | 2015-04-09 | Jason P. Mazzoccoli; Edward J. Lahoda; Peng Xu |
| A zirconium alloy nuclear reactor cylindrical cladding has an inner Zr substrate surface (10), an outer volume of protective material (22), and an integrated middle volume (20) of zirconium oxide, zirconium and protective material, where the protective material is applied by impaction at a velocity greater than 340 meters/second to provide the integrated middle volume (20) resulting in structural integrity for the cladding. | ||||||
| 120 | THERMALLY COATED COMPONENT WITH A FRICTIONALLY OPTIMIZED RACEWAY SURFACE | US14373409 | 2012-12-21 | US20140363629A1 | 2014-12-11 | Jens Boehm; Martin Hartweg; Tobias Hercke; Patrick Izquierdo; Manuel Michel; Guenter Rau; Stefan Schweickert |
| A thermally coated component that has a frictionally optimized surface of a raceway for a frictional counterpart. The frictionally optimized surface has a theoretical oil retention volume VOil of 10 to 800 μm3/mm2, which can be pre-determined by a component coating surface simulation. A method for the component coating surface simulation of a thermally coated component is furthermore disclosed, with parameter determination for surface structures of the component coating surface, wherein a parameter simulates a function between the component coating surface and the frictional counterpart. | ||||||
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