TY - JOUR
T1 - Multi-type ribs of turbine blade modeling method fitting bowed-twist wall
AU - Yang, Jiong
AU - Xi, Ping
AU - Hu, Bifu
AU - Zhang, Baoyuan
PY - 2014/6
Y1 - 2014/6
N2 - Considering the geometric features of ribs in a bowed-twist cooling passage, a modeling method based on equidistant was presented. It generated rib tools, which was a tablet trimmed by equidistant surfaces of walls in intracavity of blade and pressure slide or suction slide, and then conducted modeling of ribbed channels. Furthermore, the principle of the modeling method was deeply analyzed, and two algorithms were developed, one recognized surfaces of walls in intracavity of blade automatically, the other matched two surfaces. The main parameters were determined as well. Meanwhile, a means based on sketch to parameterize ribbed channels was provided. Eventually, the parametric design module of ribbed channels was developed on unigraphics (UG), which achieved multiple ribbed channels modeling.
AB - Considering the geometric features of ribs in a bowed-twist cooling passage, a modeling method based on equidistant was presented. It generated rib tools, which was a tablet trimmed by equidistant surfaces of walls in intracavity of blade and pressure slide or suction slide, and then conducted modeling of ribbed channels. Furthermore, the principle of the modeling method was deeply analyzed, and two algorithms were developed, one recognized surfaces of walls in intracavity of blade automatically, the other matched two surfaces. The main parameters were determined as well. Meanwhile, a means based on sketch to parameterize ribbed channels was provided. Eventually, the parametric design module of ribbed channels was developed on unigraphics (UG), which achieved multiple ribbed channels modeling.
KW - Bowed-twist wall
KW - Equidistant surface
KW - Ribs
KW - Turbine blade
KW - UG Open API
UR - https://www.scopus.com/pages/publications/84904726015
U2 - 10.13700/j.bh.1001-5965.2013.0440
DO - 10.13700/j.bh.1001-5965.2013.0440
M3 - 文章
AN - SCOPUS:84904726015
SN - 1001-5965
VL - 40
SP - 775
EP - 781
JO - Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
JF - Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
IS - 6
ER -