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Composite insulating layer for thin film sensor and preparation method of composite insulating layer

A thin-film sensor and composite insulation technology, which is applied in the coating, instrument, superimposed layer plating, etc., can solve the problems of high energy of metal atoms, affecting the compactness of the thin-film insulating layer, and the failure of thin-film sensors

Inactive Publication Date: 2016-09-28
UNIV OF ELECTRONICS SCI & TECH OF CHINA +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Among them, the insulating layer has a crucial influence on the reliability and stability of the thin film sensor. The conventional insulating layer is a single layer of Al deposited by electron beam evaporation. 2 o 3 Thin film has the advantages of simple process and fast film forming speed, but due to the Al 2 o 3 It grows in a columnar shape, and the shadow effect between the columns will produce larger holes and gaps, and in the subsequent high-temperature annealing process, due to the amorphous Al 2 o 3 Crystalline as well as functional layers with Al 2 o 3 The difference in thermal expansion coefficient between layers, the stress release will make the Al 2 o 3 Microcracks appear in the film, affecting the Al 2 o 3 Density of thin-film insulating layers
When the noble metal functional layer is prepared by subsequent sputtering, due to the high energy of the sputtered metal atoms, it is easy to penetrate the loose Al 2 o 3 The insulating layer is connected to the lower alloy layer. At the same time, the thin film sensor works in a high temperature environment, and metal atoms are easy to diffuse into the lower alloy layer, resulting in the failure of the thin film sensor.

Method used

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  • Composite insulating layer for thin film sensor and preparation method of composite insulating layer

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preparation example Construction

[0038] A method for preparing a film sensor based on a composite insulating layer provided by the invention, specifically comprising the following steps:

[0039]Step 1. Surface treatment of the alloy substrate: first, polish the alloy substrate, then use acetone, ethanol and deionized water to clean the surface of the alloy substrate in turn, and dry it with nitrogen after cleaning;

[0040] Step 2, depositing a NiCrAlY alloy transition layer on the alloy substrate: using DC sputtering to deposit the NiCrAlY alloy on the alloy substrate treated in step 1 to obtain a composite substrate with a NiCrAlY alloy transition layer;

[0041] Step 3, Al 2 o 3 Preparation of thermally grown layer: place the composite substrate obtained after step 2 in a vacuum heat treatment furnace, -3 Aluminum precipitation treatment in a vacuum environment below Pa and a temperature of 800-1200°C for 1-10 hours; then, maintain a temperature of 800-1200°C and feed oxygen to normal pressure, perform ...

Embodiment

[0049] With the nickel-based alloy plate as the alloy substrate to be tested, the process of preparing the S-type thin-film thermocouple with the composite insulating layer of the present invention thereon specifically includes the following steps:

[0050] Step 1. Surface treatment of the alloy substrate: first, polish the surface of the nickel-based alloy substrate with a size of 70mm×15mm×2mm, and then use industrial degreaser, acetone, ethanol, and deionized water to soak the nickel-based alloy substrate successively and ultrasonically Clean for 15 minutes each, after cleaning, dry the surface with dry nitrogen and dry it at 150°C for later use;

[0051] Step 2. Preparation of NiCrAlY alloy transition layer: place the nickel-based alloy substrate cleaned in step 1 on the back with a vacuum degree of 5.0×10 -3 In the vacuum environment of Pa, argon gas with a purity of 99.999% (volume percentage) is introduced as the sputtering medium, and the NiCrAlY alloy is used as the t...

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Abstract

The invention belongs to the technical field of thin film sensors, and relates to a composite insulating layer for a thin film sensor. The composite insulating layer comprises four layers of structures which comprise the amorphous Al-O-N diffusion impervious layer, the Al-O-N-to-Al2O3 transition layer, the electron beam evaporation Al2O3 thin film layer and the microcrystal Al2O3 oxygen diffusion barrier layer in sequence from bottom to top. An amorphous Al-O-N thin film in the composite insulating layer is good in compactness and is in an amorphous state, and a good diffusion barrier effect is achieved for metal atoms. The adhesive force between the amorphous Al-O-N layer and the Al2O3 layer can be effectively improved through the transition layer. The microcrystal layer on the Al2O3 thin film layer can effectively prevent outside oxygen atoms from diffusing into the Al-O-N layer at a high temperature, the amorphous state of the Al-O-N thin film in the high-temperature oxygen-enriched environment is kept, and therefore the composite insulating layer still has good insulation performance in the high-temperature oxygen-enriched work environment, and the stability and the service life of the thin film sensor in the high-temperature environment are effectively guaranteed.

Description

technical field [0001] The present invention is mainly devoted to the research and preparation of thin-film sensors, and belongs to the technical field of thin-film sensors, especially the research on thin-film sensors on the surface of aerospace turbine engine blades. Such thin-film sensors can be used to measure the temperature and stress distribution on the surface of turbine blades, etc. , providing relevant basic data for the research and design of the engine. Background technique [0002] The turbine engine is an important part of the aerospace aircraft. The turbine blades inside the engine work in the harsh environment such as high temperature and high pressure generated by gas combustion for a long time. The distribution of stress and temperature on the blade surface greatly affects the performance and performance of the engine. Therefore, the measurement of the distribution of temperature and stress on the surface of the engine turbine blade becomes very important. ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C23C14/34C23C14/30C23C14/06C23C14/08C23C14/58G01D21/02
CPCC23C14/0036C23C14/0676C23C14/081C23C14/30C23C14/34C23C14/5806C23C28/046G01D21/02
Inventor 赵晓辉李海涛蒋洪川张万里
Owner UNIV OF ELECTRONICS SCI & TECH OF CHINA
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