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Grant: Discovery Grants Program - Individual

Carleton University

$44,000.00

Advanced Processing of a Near Beta Titanium Alloy

EF 2022-23

Résumé
Summary of ProposalTitanium alloys have been widely used in the aerospace, chemical, and biomedical industries due to their high specific strength and excellent corrosion resistance. For the next generation of lighter and energy-efficient aircraft structures, the use of high strength near- Ti-alloys in the fuselage, bogie beam, flap track, nacelles, pylon, and la195nding gear assemblies will be cost effective from the perspective of weight reduction and mechanical properties compared to the industry workhorse Ti-6Al-4V, the most widely used + alloy. Major aerospace manufacturers like Airbus and Boeing have started to use forged near- Ti-alloys as landing gear components. It is expected that near- Ti-alloys will gain wider applications in the future. However, while significant research has been conducted on near- Ti-alloy design, little work has been done to understand the microstructure-mechanical properties correlations from the industrial manufacturing point of view, especially during processes such as, welding, forming, and additive manufacturing (AM).The properties of near- Ti-alloys are highly dependent on their internal microstructure, which often is composed of multiple phases and precipitates. The volume fraction, size, morphology, and distribution of these precipitates can significantly influence the mechanical properties of the near- Ti-alloys. Therefore, a complete and detailed understanding on phase transformations and microstructural evolution are crucial to optimize the mechanical properties for various applications. I am proposing a detailed study on a near- Ti-alloy using various industrial manufacturing processes, such as joining, forming, and AM. The main objectives of this proposed research program for the next five years are:(1) To optimize the processing parameters for various industrial manufacturing methods.(2) To learn how to control the microstructures through different thermal and thermo-mechanical processing. (3) To study individual microstructural features quantitatively and correlate it to the corresponding mechanical properties.
Programme
Discovery Grants Program - Individual
Bénéficiaire
Emplacement
Ontario, Canada
Type de bénéficiaire
Academia
Type
Grant
Source
NSERC's Awards Data

Tel que publié

Application id
RGPIN-2017-06347
Name nom
Kabir, Abu Syed Humaun
Department département
Mechanical & Aerospace Engineering - Mechanical & Aerospace Engineering
Organization id
23
Institution établissement
Carleton University
Province en
Ontario
Province fr
Ontario
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2022
Competition year année de concours
2017
Award amount
44000
Program id
RGPIN
Program name en
Discovery Grants Program - Individual
Program name fr
Programme de subventions à la découverte - individuelles
Group en
DISCOVERY RESEARCH
Group fr
RECHERCHE AXÉE SUR LA DÉCOUVERTE
Committee code
1511
Committee name en
Materials and Chemical Engineering
Committee name fr
Génie chimique et des matériaux
Area of application code
500
Area of application group en
Manufacturing processes and products
Area of application group fr
Procédés et produits industriels
Area of application en
Manufacturing processes and products
Area of application fr
Procédés et produits industriels
Research subject code
2000
Research subject group en
Materials science and technology
Research subject group fr
Science et technologie des matériaux
Research subject en
Materials science and technology
Research subject fr
Science et technologie des matériaux
Installment
inst:6;7
Partie
2
Nb partie
7
Application title
Advanced Processing of a Near Beta Titanium Alloy
Application summary
Summary of ProposalTitanium alloys have been widely used in the aerospace, chemical, and biomedical industries due to their high specific strength and excellent corrosion resistance. For the next generation of lighter and energy-efficient aircraft structures, the use of high strength near- Ti-alloys in the fuselage, bogie beam, flap track, nacelles, pylon, and la195nding gear assemblies will be cost effective from the perspective of weight reduction and mechanical properties compared to the industry workhorse Ti-6Al-4V, the most widely used + alloy. Major aerospace manufacturers like Airbus and Boeing have started to use forged near- Ti-alloys as landing gear components. It is expected that near- Ti-alloys will gain wider applications in the future. However, while significant research has been conducted on near- Ti-alloy design, little work has been done to understand the microstructure-mechanical properties correlations from the industrial manufacturing point of view, especially during processes such as, welding, forming, and additive manufacturing (AM).The properties of near- Ti-alloys are highly dependent on their internal microstructure, which often is composed of multiple phases and precipitates. The volume fraction, size, morphology, and distribution of these precipitates can significantly influence the mechanical properties of the near- Ti-alloys. Therefore, a complete and detailed understanding on phase transformations and microstructural evolution are crucial to optimize the mechanical properties for various applications. I am proposing a detailed study on a near- Ti-alloy using various industrial manufacturing processes, such as joining, forming, and AM. The main objectives of this proposed research program for the next five years are:(1) To optimize the processing parameters for various industrial manufacturing methods.(2) To learn how to control the microstructures through different thermal and thermo-mechanical processing. (3) To study individual microstructural features quantitatively and correlate it to the corresponding mechanical properties.