Eureka AIR delivers breakthrough ideas for toughest innovation challenges, trusted by R&D personnel around the world.

Aerospace thermal barrier material with low thermal conductivity and high fracture toughness and preparation thereof

A low thermal conductivity, aerospace technology, applied in the field of low thermal conductivity, high fracture toughness aerospace thermal barrier materials and their preparation, can solve the problem of high sintering temperature, material fracture toughness and thermal conductivity properties are difficult to achieve common improvement, sintering Long time and other problems, to achieve the effect of reducing the sintering temperature, shortening the sintering time, and high fracture toughness

Active Publication Date: 2021-06-18
LANZHOU INST OF CHEM PHYSICS CHINESE ACAD OF SCI
View PDF7 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the high sintering temperature and long sintering time of the high-entropy oxide ceramics reported so far make it difficult to improve the fracture toughness and thermal conductivity of the material.

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Aerospace thermal barrier material with low thermal conductivity and high fracture toughness and preparation thereof
  • Aerospace thermal barrier material with low thermal conductivity and high fracture toughness and preparation thereof
  • Aerospace thermal barrier material with low thermal conductivity and high fracture toughness and preparation thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0034] Example 1 Preparation (ZrO 2 ) 1 (CeO 2 ) 1 (HfO 2 ) 1 (Y 2 o 3 ) 0.5 (Sm 2 o 3 ) 0.5 , corresponding to (Zr 1 Ce 1 f 1 Y 1 SM 1 )O 9 High entropy oxides:

[0035](1) Powder mixing: Weigh ZrO according to the atomic ratio of 1:1:1:0.5:0.5 2 , CeO 2 , HfO 2 , Y 2 o 3 、Sm 2 o 3 Powder (particle size 0.5μm, purity ≥ 99.9%), put it into a ball mill jar for ball milling, add 1mL absolute ethanol per 100g of mixed powder as the grinding medium, and the grinding ball is ZrO 2 Balls, the ball-to-material ratio (g / g) is 0.5:1, the ball milling speed is 100r / min, and the ball milling time is 5h. After ball milling, it is dried in a drying oven. After grinding, it is sieved with 100 meshes to obtain a uniformly mixed raw powder. products.

[0036] (2) Sintering: Put the product obtained in step (1) into a graphite mold, and then place it in an SPS discharge plasma sintering furnace for sintering. The sintering temperature is 1550°C, the heating rate is 60°...

Embodiment 2

[0042] Example 2 Preparation (ZrO 2 ) 0.75 (CeO 2 ) 1.25 (HfO 2 ) 1 (Y 2 o 3 ) 0.3 (Sm 2 o 3 ) 0.45, Corresponding (Zr 0.75 Ce 1.25 f 1 Y 0.6 SM 0.9 )O 8.25 High entropy oxides:

[0043] (1) Powder mixing: Weigh ZrO according to the atomic ratio of 0.75:1.25:1:0.3:0.45 2 , CeO 2 , HfO 2 , Y 2 o 3 、Sm 2 o 3 Powder (particle size 30μm, purity ≥ 99.5%), put it into a ball mill jar for ball milling, add 5mL of absolute ethanol per 100g of mixed powder as the grinding medium, and the grinding ball is ZrO 2 Balls, the ball-to-material ratio is 5:1, the ball milling speed is 300r / min, and the ball milling time is 24h. After ball milling, it is dried in a drying oven. After grinding, it is sieved with 200 meshes to obtain a uniformly mixed original powder product.

[0044] (2) Sintering: Put the product obtained in step (1) into a graphite mold, and then place it in an SPS discharge plasma sintering furnace for sintering. The sintering temperature is 1750°C, th...

Embodiment 3

[0050] Example 3 Preparation (ZrO 2 ) 1 (CeO 2 ) 0.75 (HfO 2 ) 1.25 (Y 2 o 3 ) 0.6 (Nd 2 o 3 ) 0.65, Corresponding (Zr 1 Ce 0.75 f 1.25 Y 1.2 Nd 1.3 )O 9.75 High entropy oxides:

[0051] (1) Powder mixing: Weigh ZrO according to the atomic ratio of 1:0.75:1.25:0.6:0.65 2 , CeO 2 , HfO 2 , Y 2 o 3 、Nd 2 o 3 Powder (particle size 10μm, purity ≥ 99.5%), put it into a ball mill jar for ball milling, add 3mL of absolute ethanol per 100g of mixed powder as the grinding medium, and the grinding ball is ZrO 2 Balls, the ball-to-material ratio is 3:1, the ball milling speed is 200r / min, and the ball milling time is 12h. After the ball milling, it is dried in a drying oven. After grinding, it is sieved with 150 meshes to obtain a uniformly mixed original powder product.

[0052] (2) Sintering: Put the product obtained in step (1) into a graphite mold, and then place it in an SPS discharge plasma sintering furnace for sintering. The sintering temperature is 1600°C...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

PropertyMeasurementUnit
Hardnessaaaaaaaaaa
Hardnessaaaaaaaaaa
Hardnessaaaaaaaaaa
Login to View More

Abstract

The invention relates to an aerospace thermal barrier material with low thermal conductivity and high fracture toughness, which comprises the following components in atomic ratio: (ZrO2)a(CeO2)b(HfO2)c(Y2O3)d(A2O3)e corresponding to (ZraCeHf<c>Y<2d>A<2e>)Of, wherein A is Sm or Nd, a is equal to 0.75-1.25, b is equal to 0.75-1.25, c is equal to 0.75-1.25, d+e is equal to 0.75-1.25, d and e are in near equal atomic ratio, and f is equal to 2(a+b+c)+3(d+e). The invention further discloses a preparation method of the thermal barrier material. While a high lattice distortion solid solution is ensured, the grain size is reduced, the formation of a nano precipitated phase is promoted, and the improvement of the fracture toughness and the reduction of the heat conductivity are realized.

Description

technical field [0001] The invention relates to the field of thermal barrier coating materials, in particular to an aerospace thermal barrier material with low thermal conductivity and high fracture toughness and its preparation. Background technique [0002] Thermal barrier coatings can effectively protect key components such as turbine engines, rocket casings and manned cabins, ensuring the stable operation of engines and the completion of aerospace tasks. However, in order to realize manned spaceflight, the existing thermal barrier materials are insufficient, and it is difficult to meet the application requirements. [0003] YSZ material, which is widely used in thermal barrier materials in my country, still has a high intrinsic thermal conductivity (3.99~4.51 W.m -1 .K -1 ). However, the rare earth zirconate materials that are currently considered to replace YSZ have low fracture toughness (such as La 2 Zr 2 o 7 and Nd 2 Zr 2 o 7 0.89 MPa·m 1 / 2 、0.67 MPa·m 1 / 2...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
IPC IPC(8): C04B35/48C04B35/622C04B35/645
CPCC04B35/48C04B35/622C04B35/645C04B2235/3244C04B2235/3229C04B2235/3225C04B2235/3224C04B2235/5445C04B2235/602C04B2235/666C04B2235/656C04B2235/6562C04B2235/6567C04B2235/6581C04B2235/662C04B2235/96C04B2235/9607
Inventor 乔竹辉周峰郭旭鑫刘维民于源张立志马雯雯刘炯杰
Owner LANZHOU INST OF CHEM PHYSICS CHINESE ACAD OF SCI
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Eureka Blog
Learn More
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com