張凌云 湯海波 王向明 王華明 田象軍

摘 要：激光快速成形技術(shù)是一項(xiàng)“變革性”的無(wú)模、短流程、短周期、低成本、數(shù)字化、“近凈成形”先進(jìn)制造技術(shù)，特別是為大型復(fù)雜梯度材料高性能鈦合金構(gòu)件的制造提供了可行途徑。為提高我國(guó)航空航天等領(lǐng)域裝備研制生產(chǎn)能力、縮短研制生產(chǎn)周期和降低生產(chǎn)成本，本研究采用激光成形技術(shù)開(kāi)展了大型復(fù)雜梯度材料高性能鈦合金構(gòu)件的制造和基礎(chǔ)研究。主要結(jié)果如下： （1）基于組織梯度高性能鈦合金構(gòu)件制造，完成了激光成形鈦合金移動(dòng)熔池（基本單元）非平衡快速凝固形核和生長(zhǎng)行為研究，建立激光成形大型復(fù)雜梯度鈦合金構(gòu)件凝固組織晶粒形態(tài)控制技術(shù)，為組織梯度高性能鈦合金構(gòu)件激光近凈成形制造奠定了理論基礎(chǔ)和提供了工藝控制方法。（2）基于鈦合金梯度結(jié)構(gòu)材料設(shè)計(jì)基本原則，面向飛機(jī)框梁、發(fā)動(dòng)機(jī)整體葉盤等大型復(fù)雜關(guān)鍵鈦合金構(gòu)件需求，設(shè)計(jì)三類梯度結(jié)構(gòu)材料體系：高強(qiáng)/低強(qiáng)（TA15/TA2）、中強(qiáng)/高強(qiáng)（TC4/TC11、TA15/TC11）、高強(qiáng)/高損傷容限（TC18/TC21），開(kāi)展合金過(guò)渡區(qū)域顯微組織、化學(xué)成分、顯微硬度梯度變化規(guī)律研究，并測(cè)試了其拉伸等基本力學(xué)性能。（3）基于激光成形梯度鈦合金構(gòu)件熱處理工藝匹配及通過(guò)熱處理挖掘材料性能潛力的目標(biāo)，在已有激光成形TA15鈦合金熱處理工藝研究基礎(chǔ)上，完成了激光成形TC11、TC4、TC18等鈦合金固態(tài)相變行為研究，掌握非平衡熱處理特種雙態(tài)顯微組織形成機(jī)理及其控制方法，為激光成形梯度鈦合金構(gòu)件熱處理工藝制度制定和構(gòu)件綜合性能優(yōu)化提供了理論指導(dǎo)與技術(shù)途徑。（4）基于梯度過(guò)渡區(qū)的研究，提出設(shè)計(jì)并激光成形制備出了TA15/TA2、TC4/TC11、TC18/TC21等梯度鈦合金構(gòu)件的過(guò)渡區(qū)新型鈦合金材料，開(kāi)展其顯微組織、化學(xué)成分、力學(xué)性能等分析測(cè)試，為梯度過(guò)渡區(qū)的優(yōu)化設(shè)計(jì)提供了理論指導(dǎo)和實(shí)驗(yàn)數(shù)據(jù)支撐。（5）開(kāi)展了激光成形高性能梯度鈦合金構(gòu)件力學(xué)性能評(píng)價(jià)研究，初步制定試驗(yàn)大綱，開(kāi)展部分性能測(cè)試和斷裂機(jī)理研究。

關(guān)鍵詞：激光成形 鈦合金 梯度材料

Abstract：In order to improve production capacity of the equipment in China's aeronautics and astronautics industry， shorten the production cycle and reduce the cost of production，the laser forming is applied to fabricate the large complex high-performance graded titanium alloy structural components，and the basic research is carried out in the present project. The main findings can be summarized as follows：（1）Based on the purpose of fabricating titanium alloy with graded microstructure， the investigation about the unique non-equilibrium rapidly solidified structures （including nucleation and growth behavior） during laser forming process is carried out.According to the investigation，the technologies of controling solidified structures are developed，which provide the theoretical basis and the methods for laser forming titanium alloy with graded microstructure.（2）Based on designing principles of graded titanium alloy structural components， and according to the requirement of the large complex graded titanium alloy structural components in aircraft beam frame，bisk of aeroengine etc，three types of graded titanium alloy structural components were designed， including high strength/low strength（TA15/TA2），medium strength/high strength （TC4/TC11、TA15/TC11） and high strength/high damage tolerance（TC18/TC21）. The graded microsturcture，chemical composition and microhardness in the graded transitional region of these alloys are studied.（3）Based on the purpose of improving the mechanical properties of the graded titanium alloy by optimize heat treatment，the solid-state phase transformation during heat treatment in laser forming TA15，TC11，TC4，TC18 etc.were investigated. An unique bi-modal microstructure is obtained，and its formation mechanism is revealed，which shed light on improving the mechanical properties of the graded titanium alloy by heat treatment.（4）To investigate details of the graded transitional region，the TA15/TA2，TC4/TC11 and TC18/TC21 mixed titanium alloys are designed and fabricated.The mircostructures，chemical composition and mechanical properties are investigated， which shed light on the optimization design of the graded transitional region.（5）The comprehensive mechanical properties of laser near-net forming graded titanium alloy are investigated.The experimental program has been established， and parts of mechanical properties have been tested. Furthermore，the fracture mechanism of the graded titanium alloy is studied.

Key Words：Laser forming；Titanium alloy；Gradient material

閱讀全文鏈接（需實(shí)名注冊(cè)）：http：//www.nstrs.cn/xiangxiBG.aspx？id=51166&flag=1