Study on residual stress produced in milling of aeronautic structure

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 24, Issue 3, 2003, Pages 286-288

  Wang, Li Tao ^a   Ke, Ying Lin ^a   Huang, Zhi Gang ^a   Xu, De ^b   Wu, Qun ^b  

^a ZHEJIANG UNIVERSITY   (China)

^b CHENGDU AIRCRAFT INDUSTRIAL GROUP CO LTD   (China)

Author keywords

Dimension stability; FEM; Load step; Milling residual stress; Tool route

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; ALUMINUM ALLOYS; COMPUTER SIMULATION; DIMENSIONAL STABILITY; FINITE ELEMENT METHOD; NUMERICAL CONTROL SYSTEMS; RESIDUAL STRESSES;

AERONAUTIC STRUCTURE; DYNAMIC LOADING STEP; MILLING RESIDUAL STRESS; MILLING TOOL ROUTES; NUMERICAL CONTROL MILLING;

MILLING (MACHINING);

EID: 0347408954     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (3)

1. Fang G, Zeng P. Advances in numerical simulation technology for cutting process [J]. Advances in Mechanics, 2001, 31(3): 394-404.
2. Wang L T. Study on residual stresses and distortion theory of aeronautic frame structure in the milling [D]. Hangzhou: Zhejiang University, 2003.
3. Ceretti E, Lazzaroni C, Menegardo L, et al. Turning simulations using a three dimensional FEM code [J]. Journal of Materials Processing Technology, 2000, 98: 99-103.