TY - JOUR
T1 - External pressure forming of thin walled W-shaped sealing rings in aircraft engines using movable dies
AU - Zhu, Yu
AU - Wan, Min
N1 - Publisher Copyright:
©, 2015, AAAS Press of Chinese Society of Aeronautics and Astronautics. All right reserved.
PY - 2015/7/25
Y1 - 2015/7/25
N2 - Hydroforming is an effective method for manufacturing complex and thin walled parts. In order to develop a forming process of complicated thin walled superalloy W-shaped sealing rings, a technology scheme is proposed consisting of external pressure forming using movable dies and its finite element model is built. The deformation rule and destabilization mechanism are discussed at different forming stages. Moreover, the effects of key process parameters, including the heights of blank forming area and loading paths of cavity pressure on the quality of the parts, are explored with the assistance of numerical simulations and verification experiments. Furthermore, the failure modes during the forming process, including wrinkling in the circumferential direction, configurational asymmetry and accumulation folding are discussed, while the technological parameters are optimized. The results indicate that the proposed technological method is feasible for the accurate integral forming of W-shaped sealing rings; moreover, the parts with smooth surfaces and high quality can be successfully formed using optimal parameters.
AB - Hydroforming is an effective method for manufacturing complex and thin walled parts. In order to develop a forming process of complicated thin walled superalloy W-shaped sealing rings, a technology scheme is proposed consisting of external pressure forming using movable dies and its finite element model is built. The deformation rule and destabilization mechanism are discussed at different forming stages. Moreover, the effects of key process parameters, including the heights of blank forming area and loading paths of cavity pressure on the quality of the parts, are explored with the assistance of numerical simulations and verification experiments. Furthermore, the failure modes during the forming process, including wrinkling in the circumferential direction, configurational asymmetry and accumulation folding are discussed, while the technological parameters are optimized. The results indicate that the proposed technological method is feasible for the accurate integral forming of W-shaped sealing rings; moreover, the parts with smooth surfaces and high quality can be successfully formed using optimal parameters.
KW - Aircraft engines
KW - Cavity pressure
KW - External pressure
KW - Height of blank forming area
KW - Movable dies
KW - Thin walled structures
KW - W-shaped sealing ring
UR - https://www.scopus.com/pages/publications/84939178914
U2 - 10.7527/S1000-6893.2015.0065
DO - 10.7527/S1000-6893.2015.0065
M3 - 文章
AN - SCOPUS:84939178914
SN - 1000-6893
VL - 36
SP - 2457
EP - 2467
JO - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
JF - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
IS - 7
ER -