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

A kind of nickel-based alloy material of supercharger nozzle ring blade resistant to 1050 ℃ and its manufacturing method

A nickel-based alloy and nozzle ring technology, applied in the field of alloy metals, can solve the problems that iron-based materials cannot meet the requirements

Active Publication Date: 2021-12-03
蜂巢蔚领动力科技(江苏)有限公司
View PDF0 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

As VGT technology is more and more applied to gasoline engines, the exhaust temperature of VGT blades generally reaches above 950°C, and the iron-based material HK30 basically cannot meet the requirements

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
  • A kind of nickel-based alloy material of supercharger nozzle ring blade resistant to 1050 ℃ and its manufacturing method
  • A kind of nickel-based alloy material of supercharger nozzle ring blade resistant to 1050 ℃ and its manufacturing method
  • A kind of nickel-based alloy material of supercharger nozzle ring blade resistant to 1050 ℃ and its manufacturing method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0033] This embodiment provides a nickel-based alloy material for a turbocharger nozzle ring vane resistant to 1050°C and its manufacturing method:

[0034] (1) Nickel-based alloy materials for turbocharger nozzle ring blades resistant to 1050 °C: including elements C, Mn, Si, S, P, Cr, Fe, Al, Ti, Co, Cu, Nb and Ni; The mass is expressed as a percentage, based on the mass of the blade nickel-based alloy material as a percentage, the C content is 0.5%, the Mn content is 1.00%, the Si content is 1.00%, and the S content is 0.015% %, the P content is 0.02%, the Cr content is 18.0%, the Fe content is 1.00%, the Al content is 1.5%, the Ti content is 1.0%, and the Co content is 5.0%, The Cu content is 0.20%, the Nb content is 1.5%, and the balance is Ni.

[0035] (2) Nickel-based alloy material for turbocharger nozzle ring blades resistant to 1050°C and its manufacturing method: MIM process is adopted, the sintering temperature is 1240°C, and the sintering atmosphere is argon; wit...

Embodiment 2

[0037] This embodiment provides a nickel-based alloy material for a turbocharger nozzle ring vane resistant to 1050°C and its manufacturing method:

[0038] (1) Nickel-based alloy materials for turbocharger nozzle ring blades resistant to 1050 °C: including elements C, Mn, Si, S, P, Cr, Fe, Al, Ti, Co, Cu, Nb and Ni; The mass is expressed as a percentage, based on the mass of the nickel-based alloy material of the blade as a percentage, the C content is 1.0%, the Mn content is 1.00%, the Si content is 1.00%, and the S content is 0.015% %, the P content is 0.02%, the Cr content is 21.0%, the Fe content is 1.00%, the Al content is 2.5%, the Ti content is 2.0%, and the Co content is 8.0%, The Cu content is 0.20%, the Nb content is 2.5%, and the balance is Ni.

[0039] (2) Nickel-based alloy material for turbocharger nozzle ring blades resistant to 1050°C and its manufacturing method: MIM process is adopted, the sintering temperature is 1240°C, and the sintering atmosphere is arg...

Embodiment 3

[0041] This embodiment provides a nickel-based alloy material for a turbocharger nozzle ring vane resistant to 1050°C and its manufacturing method:

[0042] (1) Nickel-based alloy materials for turbocharger nozzle ring blades resistant to 1050 °C: including elements C, Mn, Si, S, P, Cr, Fe, Al, Ti, Co, Cu, Nb and Ni; The mass is expressed as a percentage, based on the mass of the nickel-based alloy material of the blade as a percentage, the C content is 1.0%, the Mn content is 1.00%, the Si content is 1.00%, and the S content is 0.015% %, the P content is 0.02%, the Cr content is 19.8%, the Fe content is 1.00%, the Al content is 2%, the Ti content is 1.5%, and the Co content is 6%, The Cu content is 0.20%, the Nb content is 2%, and the balance is Ni.

[0043] (2) Nickel-based alloy material for turbocharger nozzle ring blades resistant to 1050°C and its manufacturing method: MIM process is adopted, the sintering temperature is 1240°C, and the sintering atmosphere is argon; wi...

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
thicknessaaaaaaaaaa
Login to View More

Abstract

The invention provides a 1050°C-resistant supercharger nozzle ring blade nickel-based alloy material and a manufacturing method thereof, including C, Mn, Si, S, P, Cr, Fe, Al, Ti, B, Co, Cu, Nb and Ni; based on the mass of the nickel-based alloy material of the blade, the content of C is 0.5-1.0%, the content of Mn is 1.00%, the content of Si is 1.00%, and the content of S is 0.015%. , the P content is 0.02%, the Cr content is 18.0-21.0%, the Fe content is 1.00%, the Al content is 1.5-2.5%, the Ti content is 1.0-2.0%, and the Co The content is 5.0-8.0%, the Cu content is 0.20%, the Nb content is 1.5-2.5%, and the balance is Ni. The VGT blade of the present invention has reduced processing difficulty. After 400h exhaust temperature of 980°C engine reliability test, the blade is intact without deformation after the test, the thickness of the blade oxide layer is less than 10 μm, the increase of the shaft hole matching clearance is less than 100 μm, and the blade shaft and the mounting plate The amount of wear of the shaft hole is within an acceptable range.

Description

technical field [0001] The invention belongs to the field of alloy metals, and in particular relates to a 1050°C-resistant supercharger nozzle ring vane nickel-based alloy material and a manufacturing method thereof. Background technique [0002] Variable geometry turbocharger nozzle ring (hereinafter referred to as VGT) blades (see figure 1 , referred to as VGT blades) are guide vanes, whose function is to change the direction and speed of engine exhaust entering the turbocharger under the control of the linkage mechanism. With the development of technology, people have more and more stringent requirements for automobile engines, not only must have strong power, but also must have extremely high efficiency and sufficiently clean emissions. This requires the engine to achieve its most efficient working state under various working conditions, so it is necessary to meet the requirements of the engine for the intake air volume under various working conditions. This requires t...

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): C22C19/05B22F3/22B22F3/10B22F3/24C22F1/10
Inventor 王澎潘红军李猛吴少祥段冲张哲魏明波
Owner 蜂巢蔚领动力科技(江苏)有限公司
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