本文主要利用SEM和TEM儀器,經過不同固溶與時效熱處理,分析鈦-4.5鋁-3釩-2鉬-2鐵合金顯微結構,相關研究結果如下所示︰ 一. 合金β/(α+β)轉換溫度約900℃,麻田散鐵轉換溫度(Ms)約825℃。 二. 原料具有α+β雙相結構,在α相基地內觀察到次晶粒及差排。 三. 固溶900℃經不同時效熱處理,低溫時效麻田散鐵有層狀組織之現象,並在基地析出β相晶粒,高溫時效時麻田散鐵產生粗大化現象,此時金相由α'轉變為α+β。 四. 固溶850℃經不同時效熱處理,低溫時效α和α邊界形成界面差排,在α'相晶粒形成高密度差排,高溫時效α'相晶粒形成高密度差排,此時α+α'轉變為α+(α+β)。 五. 固溶800℃經不同時效熱處理,低溫時β相晶粒形成界面差排,在α相形成高密度差排,高溫時效β相形成高密度差排。
1. The temperature of theβ/(α+β) and Ms transition is nearly 900℃ and 825℃, respectively. 2. The Microstructures of the raw Ti-4.5Al-3V-2Mo-2Fe alloy is duplex (α+β) phase . 3. Being solution heated treatment at 900℃ and then different aged, coarsening of the martensite.The coarsening of the martensite grain occurred at low temperature aging . The coarsening of the martensite grain and the martensite boundary occurred at low temperature aging. 4. Being solution heated treatment at 850℃and then different aged ,α and α' boundary becoming Interface dislocations of low temperature, α'becoming high density of dislocations of high temperature. 5. Being solution heated treatment at 800℃and then different aged,β becoming interface dislocations of low temperature, α becoming high density of dislocations.β becoming high density of dislocations at high temperature aging.