复杂高筋薄壁构件旋压-增材复合制造技术发展与展望

doi:10.7527/S1000-6893.2022.27493

Abstract

Abstract:

Complex thin-walled component with high ribs has wide application prospect in aerospace vehicles. Integral forming is an important technology to realize the lightweight component processing， and is also one of the engineering challenges in current manufacturing field. In integral manufacturing processes， metal spinning-additive hybrid manufacturing represents the academic frontier and development trend of the integral forming of complex thin-walled component with high ribs. In recent years， the research teams of the authors work on the spinning-additive hybrid manufacturing of complex aerospace thin-wall cylinder. This paper reviews the research status of spinning of stiffened cylinder and transformative-additive hybrid manufacturing， respectively， and systematically introduces the preliminary achievements of our teams， including the fracture mechanism and microstructure evolution of aluminum alloy stiffened cylinder during the flow spinning， the thermodynamic behavior and microstructure control during additive manufacturing based on the inner wall of spun cylinder， and spinning-additive hybrid manufacturing process； and prospects the development of spinning-additive hybrid manufacturing as well. Furthermore， this paper presents the technology status and trend of the hybrid manufacturing of complex thin-walled cylinder with high ribs， which provides a guide for developing integral forming technology of complex thin-walled components.

Key words: aluminum alloy, thin-walled component, metal spinning, additive manufacturing, hybrid manufacturing

CLC Number:

V261.3⁺3

Zhongqin LIN, Zhongqi YU, Donghua DAI, Xiaoguang FAN, Shengfu YU, Dongdong GU, Shuhui LI, Yusheng SHI. Development and prospect of metal spinning: Additive hybrid manufacturing technology for complex thin⁃walled component with high ribs[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(9): 627493-627493.

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材料（等材+增材）	工艺	界面			基体			断裂区
材料（等材+增材）	工艺	σ_0.2/MPa	σ_b/MPa	ε/%	σ_0.2/MPa	σ_b/MPa	ε/%	断裂区
CMnAlNb+18Ni300^［92］	锻造+SLM	502±19	841±26	7±1	385±1	719±1	21±0
AerMet100 +AerMet100^［93］	锻造+LMD	1 047	1 223	10.3	840	1 192	16.8	锻件区
TC4+ TC4^［94］	锻造+SLM	972±6	1 061±12	9.3±0.8	855±2	905±4	16.1±2.8	增材区
TC4+ TC4^［95］	锻造+LMD	962	1 029	12	825	895	10
TC4+ TC4^［88］	锻造+WAAM	850±8.1	934±10	8±0.4	920±9.1	998±14.2	17±0.7	增材区
TC4+ TC4^［96］	锻造+LMD	927	1 005	14.3	970	1 032	17	增材区
TC4+ TC4^［97］	CMT+ 层间锻造	850±20	930±20	6±3	827	896	10

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Development and prospect of metal spinning: Additive hybrid manufacturing technology for complex thin⁃walled component with high ribs

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