Material for preparing turbine rotor of pressurizer and method for preparing turbine rotor by material

A technology of turbine rotor and supercharger, applied in mechanical equipment, machine/engine, blade supporting elements, etc., can solve the problems of unstable service environment performance, structural evolution damage, low service life, etc., to shorten the response time, Low price and high hardness

Inactive Publication Date: 2014-04-02
UNIV OF JINAN
View PDF4 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the intrinsic brittleness of silicon nitride ceramics faces the problem of thermal shock damage under extremely harsh service conditions, as well as the problem of structural evolution damage and sharp attenuation of performance of the formed thermal shock damage under long-term high temperature and complex loads. The reliability of ceramic turbine rotors is severely challenged
[0005] The inherent brittleness and harsh service environment of silicon nitride ceramic turbine rotors lead to unstable performance, flying blades, and low service life
In the past, the raw material formula of silicon nitride ceramic turbine rotors was only a mixture of different ceramic components. Such ceramic turbine rotors were extremely unstable due to their brittleness.

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
  • Material for preparing turbine rotor of pressurizer and method for preparing turbine rotor by material
  • Material for preparing turbine rotor of pressurizer and method for preparing turbine rotor by material
  • Material for preparing turbine rotor of pressurizer and method for preparing turbine rotor by material

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0032] A material for preparing a supercharger ceramic turbine rotor, comprising the following components by weight: 85 parts of silicon nitride powder, nitrogen

[0033] 5 parts of boron nanotube powder, 2 parts of metal aluminum powder, 3 parts of silicon powder, 5 parts of zirconia powder.

[0034] The method for preparing a turbine rotor using the material includes the following steps:

[0035] (1) Raw material preparation: Weigh 85 parts of silicon nitride powder, 5 parts of boron nitride nanotube powder, 2 parts of metal aluminum powder, 3 parts of silicon powder, and 5 parts of zirconia powder by weight to form raw materials.

[0036] (2) Paste preparation: add the raw materials obtained in step (1) to the silica sol in a weight ratio of 1:1.5 into a liftable forced mixer for mixing, at a mixing speed of 60 r / min, and after stirring for 50 minutes, add 3% of the raw material weight of yttrium trioxide sintering aid, while adding 14% of the raw material weight of distilled water...

Embodiment 2

[0044] A material for preparing a supercharger ceramic turbine rotor, comprising the following components by weight: 87 parts of silicon nitride powder, nitrogen

[0045] 3 parts of boron nanotube powder, 3 parts of metal aluminum powder, 4 parts of silicon powder, 3 parts of zirconia powder.

[0046] The method for preparing a turbine rotor using the material includes the following steps:

[0047] (1) Raw material preparation: Weigh 87 parts of silicon nitride powder, 3 parts of boron nitride nanotube powder, 3 parts of metal aluminum powder, 4 parts of silicon powder, and 3 parts of zirconia powder by weight to form raw materials.

[0048] (2) Paste preparation: add the raw materials obtained in step (1) to the silica sol in a weight ratio of 1:1.5 to a liftable forced mixer for mixing, stirring at a speed of 55r / min, after mixing for 60 minutes, add the raw materials 2% by weight of yttrium trioxide sintering aid, while adding 13% by weight of raw material, distilled water, continu...

Embodiment 3

[0056] A material for preparing a supercharger ceramic turbine rotor, comprising the following components by weight: 90 parts of silicon nitride powder, nitrogen

[0057] 1 part of boron nanotube powder, 2 parts of metal aluminum powder, 2 parts of silicon powder, 5 parts of zirconia powder.

[0058] The method for preparing a turbine rotor using the material includes the following steps:

[0059] (1) Raw material preparation: Weigh 90 parts of silicon nitride powder, 1 part of boron nitride nanotube powder, 2 parts of metal aluminum powder, 2 parts of silicon powder and 5 parts of zirconia powder by weight to form the raw materials.

[0060] (2) Paste preparation: Add the raw materials obtained in step (1) to the silica sol in a weight ratio of 1:1.5 into the liftable forced mixer for mixing, stirring at 65r / min, after stirring for 55 minutes, add the raw materials 4% by weight of yttrium trioxide sintering aid, while adding 15% by weight of raw materials, distilled water, continue t...

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
particle sizeaaaaaaaaaa
particle sizeaaaaaaaaaa
Login to view more

Abstract

The invention belongs to the technical field of manufacturing of turbine rotor of a pressurizer, in particular to a material for preparing a turbine rotor of the pressurizer and a method for preparing the turbine rotor by the material. The material for preparing the turbine rotor of the pressurizer comprises the components in parts by weight as follows: 85-90 parts of silicon nitride powder, 1-8 parts of boron nitride nanotube powder, 2-4 parts of aluminite powder, 2-4 parts of silicon powder and 3-5 parts of zirconium oxide powder. The method for preparing the turbine rotor by the material comprises the steps of: (1) preparing a raw material; (2) preparing a paste material; (3) injection moulding; (4) setting and drying; and (5) gas pressure sintering of mould constraint. The turbine rotor of the pressurizer prepared by the material is light in weight, good in toughness, high in strength, low in specific gravity and good in proportionality, and small in lag proportionality, small in deformation, small in accumulated carbon and long in service life under supernormal work conditions such as high temperature, high pressure and high speed. Meanwhile, the method for preparing the turbine rotor by the material is simple in steps, convenient to operate and is beneficial for industrialized production in a large scale.

Description

Technical field [0001] The invention belongs to the technical field of manufacturing turbocharger turbine rotors, and specifically relates to a preparation of ceramic turbine rotors for superchargers [0002] Sub-materials and methods for preparing turbine rotors using the materials. Background technique [0003] The use of exhaust gas turbocharging has become one of the most important methods for improving power, economy and emission characteristics of gasoline engines and diesel engines in the world. The turbocharger uses the energy of high-temperature exhaust gas discharged from the engine to drive the exhaust gas turbine in the turbine chamber to rotate at a high speed, thereby driving a compressor coaxial with the turbine to achieve supercharging, thereby improving the performance of the engine. Traditional turbine rotor materials generally use nickel-based alloys. However, under high temperature, high pressure, and high-speed environmental conditions, nickel-based turbine ro...

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 Patents(China)
IPC IPC(8): F01D5/02C04B35/78C04B35/584C04B35/622
Inventor 王守仁于航海王英姿乔阳宋令惠杨丽颖
Owner UNIV OF JINAN
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
Try Eureka
PatSnap group products