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44results about How to "Good phase stability at high temperature" patented technology

Multielement rare earth oxide doped zirconia thermal barrier coating with craze crack structure and preparing method thereof

The invention discloses a method for preparing a rare earth oxide doped zirconia thermal barrier coating with a craze crack structure, which solves the problems of low thermal shock resistance property, difficult further thermal conductivity reduction and the like of the thermal coating prepared by conventional plasma spraying. Under the condition of the plasma spraying technology, the preheating temperature of a base body, the moving speed of a plasma spraying gun and a powder delivery rate are adjusted, then a rare earth oxide doped zirconia thermal barrier coating (BH-TBCO1) with a craze crack structure and stable thermodynamics is prepared. The rare earth oxide doped zirconia thermal barrier coating with a craze crack structure has good high-temperature phase stability at the temperature below 1300 DEG C; the thermal insulation property of the thermal barrier coating is further enhanced, and the thermal insulation temperature achieves more than 150 DEG C and is enhanced by more than 50% when compared with the coating prepared by the conventional plasma spraying; the thermal shock life of the coating exceeds 4000 cycles and is enhanced by more than 1 time when compared with the coating prepared by the conventional plasma spraying.
Owner:BEIHANG UNIV

Novel perovskite structure high-entropy ceramic and preparation method thereof

The invention discloses a novel perovskite structure high-entropy ceramic and a preparation method thereof. The structure of the ceramic is an ABO3 type perovskite structure, the A-site element is Sr, and the B-site element is Zr, Hf, Ce, Yb and Me which are in an equal molar ratio. The preparation method comprises the following steps: putting the components into a mortar, adding absolute ethyl alcohol, and performing grinding; performing drying in a drying oven after the grinding, then transferring dried material into a muffle furnace for pre-calcining, and naturally cooling obtained material to room temperature to obtain a ceramic powder; putting the ceramic powder into the mortar, adding a polyvinyl alcohol aqueous solution and absolute ethyl alcohol, performing grinding again, and performing drying and sieving after the grinding is sufficient, adding the sieved ceramic powder into a steel mold of a table type powder tablet press, pre-pressing into a disc-shaped or strip-shaped block material, and then putting the block material into a cold isostatic press for cold isostatic pressing treatment to obtain a ceramic green body; and finally, calcining the ceramic green body in a muffle furnace, and performing cooling in the furnace to obtain the novel perovskite structure high-entropy ceramic. The high-entropy ceramic has the advantages of high stability, low thermal conductivity and relatively high hardness and density.
Owner:INNER MONGOLIA UNIV OF TECH

Low-thermal-conductivity high-entropy ceramic thermal barrier coating material

A preparation method of the low-thermal-conductivity high-entropy ceramic thermal barrier coating material comprises the steps that A, nitrate of trivalent rare earth elements and acetate of tetravalent metal elements serve as raw materials, and high-entropy ceramic powder of a hollow spherical structure is prepared through a plasma spraying technology; step B, sequentially adding a polyvinyl alcohol aqueous solution and an ethanol solution into the high-entropy ceramic powder for grinding, and then putting the high-entropy ceramic powder into a drying oven for drying to obtain precursor powder; step C, pre-pressing the precursor powder into a disc-shaped or strip-shaped block material, putting the block material into a disposable rubber fingerstall, vacuumizing, and carrying out cold isostatic pressing treatment to obtain a ceramic green body; and D, firing the ceramic body, namely calcining the ceramic body in a muffle furnace, and cooling the ceramic body along with the furnace after calcining is finished. The high-entropy ceramic thermal barrier coating material disclosed by the invention is a pyrochlore phase, and compared with a YSZ material, the high-entropy ceramic thermal barrier coating material has lower thermal conductivity, good high-temperature phase stability and a thermal expansion coefficient closer to that of a base material.
Owner:INNER MONGOLIA UNIV OF TECH

Shining thermal barrier coating system of rare earth niobate based on defective fluorite structure and preparation method of shining thermal barrier coating system

The invention provides a shining thermal barrier coating system of rare earth niobate based on a defective fluorite structure and a preparation method of the shining thermal barrier coating system. The preparation method comprises the following steps that Ln2O3 powder and Nb2O3 powder are calcined for one hour at the temperature of 1000 DEG C and mixed at the stoichiometric ratio, absolute ethyl alcohol serves as mixing graft, zirconia is used as a ball-milling medium ball-milling mixed material, and after rotary evaporation and drying, presintered powder is obtained; dry pressing and forming are conducted to obtain a blank; the blank is subjected to pressureless sintering in air and then uniformly mixed with Ln3NbO3, and high-fluidity powder is formed through spray granulation and dry treatment; and a layer of metal bonding layer McrAlY alloy is deposited on the surface of a cobalt-based or nickel-based metal substrate, the high-fluidity powder is deposited on the surface of a metal bonding layer to form a ceramic layer through an ion spray technology, an electron beam physical vapor deposition technology or other spray technologies, and the thermal barrier coating system is formed. The shining thermal barrier coating system of the rare earth niobate is integrated in structure and function, and low in heat conductivity.
Owner:乐延伟

Preparation method of thermal barrier coating and thermal barrier coating prepared through preparation method

InactiveCN108441806AOptimal Control StructureSimplify the tedious process of granulationMolten spray coatingPlasma jetNano structuring
The invention provides a preparation method of a thermal carrier coating and the thermal barrier coating prepared through the preparation method. According to the preparation method, a precursor solution prepared from zircon salt and ytterbium salt is used as a spraying raw material, and in a liquid-phase plasma spraying device, the precursor solution is delivered into plasma jet flow through a two-flow atomization nozzle and then deposits on a matrix to form the thermal barrier coating provided with evenly-distributed pores and vertical crack structures. The thermal barrier coating prepared through the method is a nano-structure thermal barrier coating provided with vertically-cracked columnar crystals and the evenly-distributed pores. According to the preparation method of the thermal carrier coating and the thermal barrier coating prepared through the preparation method, the precursor solution replaces agglomeration powder to serve as the raw material, so that a complex traditionalraw material pelletizing process based atmosphere plasma spraying is greatly simplified, the production efficiency is improved, and the cost is reduced. The structure of the coating is controllable, and the thermal barrier coating prepared through the preparation method is of a nano-structure and is provided with vertical crack structures. A ceramic material YbSZ has high phase stability and low thermal conductivity.
Owner:TIANJIN UNIV

High-fracture-toughness thermal barrier coating material of high-entropy rare earth aluminate toughened high-entropy rare earth zirconate as well as preparation method and application of high-fracture-toughness thermal barrier coating material

The invention discloses a high-fracture-toughness thermal barrier coating material of high-entropy rare earth aluminate toughened high-entropy rare earth zirconate and a preparation method of the high-fracture-toughness thermal barrier coating material. The thermal barrier coating material is x [nRE1 / nAlO3]-(1-x) [n (RE1 / n) 2Zr2O7] (x is more than 0 and less than or equal to 0.5, and n is more than or equal to 5 and less than or equal to 13). The preparation method comprises the following steps: S1, preparing a rare earth source, a zirconium source and an aluminum source according with a stoichiometric ratio into a mixed solution; s2, the mixed solution is added into an ammonia water solution in a stirring state, and the pH value of the system is always kept to be larger than or equal to 10.0; s3, washing and drying a precipitation product obtained in S2; and S4, heat treatment is conducted, and heat treatment is conducted for 2-20 h at the temperature of 950-1600 DEG C. The double-phase high-entropy thermal barrier coating material has good high-temperature phase stability and high fracture toughness, and the fracture toughness of the double-phase high-entropy thermal barrier coating material reaches 1.92 MPa.m < 1 / 2 > to 2.77 MPa.m < 1 / 2 >.
Owner:CHINA UNIV OF GEOSCIENCES (WUHAN)

In-situ generated SiC -doped Gd2Zr2O7 thermal barrier coating ceramic material and preparation method thereof

The invention discloses a SiC-doped Gd2Zr2O7 thermal barrier coating ceramic layer material and a preparation method thereof. The SiC-doped Gd2Zr2O7 thermal barrier coating ceramic layer material has the chemical formula of Gd2Zr2O7-XTiSi2-YC (X = 0-5 wt%, Y = 0-1.7 wt%), and the Gd2Zr2O7-XTiSi2-YC (X = 0-5 wt%, Y = 0-1.7 wt%) series thermal barrier coating ceramic layer material has the following remarkable advantages: after being doped in-situ generated second-phase substance SiC with different contents, the material has high temperature phase stability and sintering resistance at 1500 DEG C; compared with a traditional Gd2Zr2O7 thermal barrier coating ceramic material, the SiC-doped Gd2Zr2O7 thermal barrier coating ceramic layer material has the advantages that the thermal expansion coefficient at the high temperature of 1000 DEG C can reach 11 W / m.K, the thermal conductivity at the temperature of 1000 DEG C can reach 0.6-0.7 W.m-1. k-1, the fracture toughness is improved to 1.5-1.6 MPa.m1 / 2, and the SiC-doped Gd2Zr2O7 thermal barrier coating ceramic layer material has the potential to serve as a high-temperature-resistant thermal barrier coating ceramic layer material.
Owner:江苏航运职业技术学院

TiSi2 doped Gd2Zr2O7 ceramic material, preparation method and thermal barrier coating

The invention discloses a TiSi2-doped Gd2Zr2O7 ceramic material, a preparation method and a thermal barrier coating, and the design idea is that the Gd2Zr2O7 thermal barrier coating ceramic material is doped by using the TiSi2 material with excellent fracture toughness, and the order degree of the original internal crystal structure is changed, so that the toughening effect is achieved; and meanwhile, related thermal physical properties such as thermal expansion coefficient and thermal conductivity can be improved, so that related problems existing in the original Gd2Zr2O7 material are solved. Compared with the prior art, the Gd2Zr2O7 thermal barrier coating ceramic material and the preparation method thereof have the following remarkable advantages that the Gd2Zr2O7 thermal barrier coating ceramic material doped with different contents of TiSi2 can still keep good high-temperature phase stability and relatively good sintering resistance at 1500 DEG C; the high-temperature-resistant thermal barrier coating ceramic layer material has higher thermal expansion coefficient, lower thermal conductivity and better fracture toughness at high temperature, and is suitable for being used as a high-temperature-resistant thermal barrier coating ceramic layer material.
Owner:江苏航运职业技术学院

High-temperature thermal barrier coating material and preparation method thereof

The invention belongs to material technology, a high-temperature thermal barrier coating material and a preparation method thereof. When used at a high temperature, the conventional thermal barrier coating material is easy to undergo phase change and cause the failure of a coating. The general formula of a multi-component rare-earth high-temperature thermal barrier coating material is that: LnyLn<'>zLn<''>1-y-zMexAl12-xO19+delta, wherein Ln, Ln<'> and Ln<''> are rare earth elements such as La, Ce, Nd, Sm, Gd, Dy, Er and Yb; Me is metal elements such as Mn, Mg, Ni, Co, Sr, Ca and Ba; x is between 0 and 12; y is between 0 and 1; z is between 0 and 1; and y+z is less than or equal to 1. The preparation method comprises the following steps of: preparing mixed metal salt solution; preparing complexing agent solution; preparing mixed metal ion sol; and drying the mixture at the temperature of between 70 and 180 DEG C, and grinding and calcining the dried product to obtain the high-temperature thermal barrier coating material. The high-temperature thermal barrier coating material has the advantages of high temperature resistance, melting point of over 2,000 DEG C, high stability of high-temperature phase, no phase change from room temperature to 2,000 DEG C or higher temperature and low thermal conductivity.
Owner:SHANGHAI UNIV OF ENG SCI
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