Unlock instant, AI-driven research and patent intelligence for your innovation.

Corrosion-resistant high-heat-insulation low-emissivity zirconium oxide-based thermal barrier coating and preparation method thereof

A thermal barrier coating, zirconia-based technology, applied in the coating, metal material coating process, sputtering plating, etc., can solve the problems of accelerated material degradation, unstable structure, harsh service conditions, etc., to achieve strong The effect of thermal protection

Active Publication Date: 2022-05-13
SINOSTEEL LUOYANG INST OF REFRACTORIES RES +1
View PDF5 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

With the continuous improvement of the thrust-to-weight ratio of engines, the service conditions of high-temperature alloys are more stringent, and the various degradation rates of materials are accelerated in high-temperature environments, which are prone to structural instability, deformation and cracks under the action of temperature and stress during use. Growth, oxidation and corrosion on the surface of the material, the single crystal alloy material has been developed to the fourth generation, and the temperature bearing capacity has increased to 1140°C, which is close to the temperature limit of the metal material, and cannot further meet the needs of advanced aero-engines
The emergence of thermal barrier coating technology provides an effective means of protection for key hot-end components. Due to its relatively high thermal conductivity and emissivity, low thermal expansion coefficient, and high temperature The high oxygen flux and the volume phase transition at about 1200 °C make the YGO layer grow rapidly after the temperature is higher than the phase transition point, and cannot effectively adhere to the alloy matrix and provide a suitable cooling gradient. The more stringent service environment requirements limit the rapid development of hypersonic aircraft and high-performance large aircraft

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
  • Corrosion-resistant high-heat-insulation low-emissivity zirconium oxide-based thermal barrier coating and preparation method thereof
  • Corrosion-resistant high-heat-insulation low-emissivity zirconium oxide-based thermal barrier coating and preparation method thereof
  • Corrosion-resistant high-heat-insulation low-emissivity zirconium oxide-based thermal barrier coating and preparation method thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0052] (1) Select Φ24.9mm high-temperature alloy Inconel718 rods, prepare alloy test pieces with a thickness of 6mm on a precision wire-cutting machine tool, completely submerge the high-temperature alloy substrate in an ethanol ultrasonic oscillator for 20 minutes, and use absorbent cotton to conduct a preliminary test on the surface of the high-temperature alloy. Wipe and clean, place in a vacuum drying oven at 80°C for 3 hours, then use white corundum to roughen the clean surface at 0.65Mpa pressure, and clean the surface scum with purge gas;

[0053] (1) Clamp the clean sandblasted Inconel718 superalloy substrate on a specific tooling, control the flame to preheat the test piece including the clamping tooling twice, keep the preheating temperature below 350°C, and spray it by supersonic flame spraying A NiCoCrAlYHf bonding layer with a thickness of 150 μm and a porosity of 4% was prepared on the surface of the superalloy Inconel 718 by using the above method; HVOF parameter...

Embodiment 2

[0097] (1) Except that the superalloy is changed to Incoloy825 superalloy, other steps are the same as step 1 of embodiment 1;

[0098] (2) Clamp the Incoloy825 high-temperature alloy base material in the clean sandblasting state on a specific tooling, and preheat the test piece including the clamping tooling twice by controlling the flame, keeping the preheating temperature below 360°C, and spraying it by supersonic flame A NiCoCrAlYRh bonding layer with a thickness of 100 μm and a porosity of 3% was prepared on the surface of the superalloy Incoloy825 by using the above method; HVOF parameter settings: the x-axis and y-axis spray gun speeds were 450mm / s and 200mm / s respectively, and the spray gun pitch was 5.5 mm, spray gun distance 330mm, combustion chamber pressure 72.4Pa, powder feeding 2.5rpm, oxygen and carrier gas flow rates 1500scfh and 19scfh respectively, inlet water temperature and return water temperature 43.1°C and 70°C;

[0099] (3) Replace the Incoloy825 supera...

Embodiment 3

[0109] (1) A bonding layer with a thickness of 200 μm and a porosity of 5% NiCoCrAlYRu was prepared on the surface of superalloy Monel400 by supersonic flame spraying; during the preparation process, the workpiece was preheated twice in the early stage, and the maximum temperature of the workpiece was 360 °C. Parameter settings: x-axis and y-axis spray gun speeds are 700mm / s and 400mm / s respectively, spray gun step distance is 9.5mm, spray gun distance is 350mm, combustion chamber pressure is 84.5Pa, powder feeding is 5.5rpm, oxygen and carrier gas flow rates are 1695scfh and 19.5scfh, the inlet water temperature and return water temperature are 56.6℃ and 94℃ respectively;

[0110] (2) The surface of the bonding layer is prepared by atmospheric plasma spraying with a thickness of 100 μm, a porosity of 10%, and Gd(Ta 0.5 Nb 0.5 )O 4 Oxygen barrier cooling layer; first use Gd 2 o 3 , Nb 2 o 5 and Ta 2 o 5 Spherical Gd (Ta 0.5 Nb 0.5 )O 4 Spherical powder, preheated on...

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
thicknessaaaaaaaaaa
thicknessaaaaaaaaaa
thicknessaaaaaaaaaa
Login to View More

Abstract

The invention discloses a high-temperature thermal fatigue resistant and low-emissivity zirconia-based composite thermal barrier coating and a preparation method thereof. The thermal barrier coating is composed of a bonding layer, an oxygen-blocking cooling ceramic layer, a corrosion-resistant heat-insulating ceramic layer and a low-radiation layer which are sequentially arranged from bottom to top. A bonding layer, an oxygen-blocking cooling layer, a corrosion-resistant heat-insulating layer and a low-radiation layer are sequentially prepared on the surface of a high-temperature alloy substrate, and the composite coating material is prepared by pertinently adopting supersonic flame and plasma spraying according to different functions and properties of all the layers. The surface radiance of the prepared thermal barrier coating at 1400 DEG C is 0.19-0.20, the measurement result is far lower than that of a common thermal barrier coating material, and high heat insulation protection is provided for an internal high-temperature alloy substrate. Besides, based on the excellent coating material, the spraying technology and the coating structure design scheme, the thermal fatigue test of the thermal barrier coating reaches up to 11000 times at the temperature of 1150 DEG C, and the thermal barrier coating is suitable for the harsh service environment and is a great leap of the existing coating technology.

Description

technical field [0001] The invention belongs to the technical field of thermal barrier coatings, and in particular relates to a low-emissivity zirconia-based thermal barrier coating with corrosion resistance and high heat insulation and a preparation method thereof. Background technique [0002] As a major core equipment for national defense security, hypersonic vehicles, rockets, missiles, high-power aero-engines, and heavy-duty gas turbines, etc., are constantly making breakthroughs in the technical field, and the service environment of their hot-end components is getting worse. The requirements are also constantly increasing. Superalloys have high high-temperature strength, good oxidation resistance and corrosion resistance, good fatigue performance, fracture toughness and other comprehensive properties, and are widely used in aerospace, petrochemical and other important fields. With the continuous improvement of the thrust-to-weight ratio of engines, the service conditi...

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
Patent Type & Authority Applications(China)
IPC IPC(8): C23C28/00C23C4/02C23C4/073C23C4/10C23C4/129C23C4/134C23C14/16C23C14/35
CPCC23C28/3215C23C28/3455C23C4/02C23C4/129C23C4/134C23C4/073C23C4/10C23C14/35C23C14/165
Inventor 李红霞张陆洋冯晶陈琳王建坤荣菊王刚赵世贤粱鹏鹏
Owner SINOSTEEL LUOYANG INST OF REFRACTORIES RES