Powder metallurgy titanium alloy and preparation method thereof
A powder metallurgy and titanium alloy technology is applied in the field of the preparation of the powder metallurgy titanium alloy, and can solve the problems such as the inability to meet the requirements of the anti-fatigue properties of the titanium alloy, the inability of the titanium alloy to meet the high-strength anti-fatigue resistance, and the density lower than 97%, and the like, Achieve high density and comprehensive performance, improve mechanical properties, and improve the effect of density
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Examples
Embodiment 1
[0023] The preparation composition is Ti-5Al-4Mo-4V-2Ag-0.1LaB 6 powder metallurgy titanium alloy. The raw materials used are -100 mesh titanium powder, -500 mesh aluminum powder, -100 mesh molybdenum powder, -300 mesh Al-58V master alloy powder, -100 mesh silver powder, -250 mesh lanthanum hexaboride powder. The raw material powder is weighed according to the alloy ratio, and the raw material powder is mixed evenly by ball milling on a ball mill, and then molded into a green body under a pressure of 500MPa, and the green body is put into a vacuum hot-pressing sintering furnace for high-temperature sintering, and the vacuum degree is controlled at 1 ×10 -2 MPa, the sintering temperature is 1300°C, the sintering time is 3h, and the applied pressure is 25MPa. The compressive strength of the powder metallurgy titanium alloy obtained after cooling with the furnace is 1750MPa, and the compactness of the sintered body obtained by the drainage method is 99.1%.
Embodiment 2
[0025] The preparation composition is Ti-2Al-8Mo-2V-5Ag-2.5LaB 6 powder metallurgy titanium alloy. The raw materials used are -200 mesh titanium powder, -300 mesh aluminum powder, -200 mesh molybdenum powder, -150 mesh Al-58V master alloy powder, -200 mesh silver powder, -100 mesh lanthanum hexaboride powder. The raw material powder is weighed according to the alloy ratio, and the raw material powder is ball milled on a ball mill to mix evenly, and then molded into a green body under a pressure of 300MPa, and the green body is put into a vacuum hot-pressing sintering furnace for high-temperature sintering, and the vacuum degree is controlled at 1. ×10 -3 MPa, the sintering temperature is 1500°C, the sintering time is 3h, and the applied pressure is 25MPa. The compressive strength of the powder metallurgy titanium alloy obtained after cooling in the furnace is 2010MPa, and the compactness of the sintered body obtained by the drainage method is 99.7%.
Embodiment 3
[0027] The preparation composition is Ti-5Al-4Mo-4V-3Ag-1.0LaB 6 powder metallurgy titanium alloy. The raw materials used are -300 mesh titanium powder, -300 mesh aluminum powder, -300 mesh molybdenum powder, -150 mesh Al-58V master alloy powder, -200 mesh silver powder, -100 mesh lanthanum hexaboride powder. The raw material powder is weighed according to the alloy ratio, and the raw material powder is ball milled and mixed evenly on a ball mill, and then molded into a green body under a pressure of 400MPa, and the green body is put into a vacuum hot-pressing sintering furnace for high-temperature sintering, and the vacuum degree is controlled at 1. ×10 -1 MPa, the sintering temperature is 1250°C, the sintering time is 6h, and the applied pressure is 15MPa. The compressive strength of the powder metallurgy titanium alloy obtained after cooling with the furnace is 1862MPa, and the density of the sintered body obtained by the drainage method is 99.3%.
PUM
Property | Measurement | Unit |
---|---|---|
Compressive strength | aaaaa | aaaaa |
Compressive strength | aaaaa | aaaaa |
Compressive strength | aaaaa | aaaaa |
Abstract
Description
Claims
Application Information
- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
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