Parametric modeling method for integrated design and manufacturing of radial compressor impeller

  • PDF / 2,902,932 Bytes
  • 15 Pages / 595.276 x 790.866 pts Page_size
  • 95 Downloads / 159 Views

DOWNLOAD

REPORT


ORIGINAL ARTICLE

Parametric modeling method for integrated design and manufacturing of radial compressor impeller Yu Zhou 1,2

& Yue Song

2,3

1

1

& Tong Xing & Yan Wang & Qi Zhang

1,2

& Longtao Shao

2,3

& Farong Du

2,3

& Shuiting Ding

2,3

Received: 26 July 2020 / Accepted: 29 October 2020 # Springer-Verlag London Ltd., part of Springer Nature 2020

Abstract Radial compressor impeller (RCI) manufacturing is moving toward to improve competitiveness through smart manufacturing. Although current CAD (computer-aided design) and CAM (computer-aided manufacturing) techniques provide multiple tools to construct and optimize complicated geometries of RCI, an adjustment of blade shape often leads to nonparametric geometric reconstruction. As the key geometric elements in RCI, set of streamlines (SSL) and meridional section (MS) play vital roles in modeling and aerodynamic optimization. This paper presents a novel approach for automatic extraction of SSL and MS from a RCI 3D model or workpiece. Furthermore, the presented method can interactively construct a parameterized RCI platform, which inputs and outputs the presented RCI parameters to existing CFD and CAM systems rapidly and effectively. An integrated acquisition is employed. The straight generatrix vectors (SGVs) are identified and their boundary points are defined. After the uniform partition of SGV segments, the sequent equant points along spanwise direction are packaged to fit SSL. To manipulate the smoothness and approximation, a double-fitting method is performed to generate SSL. A parameterized system for extracting SSL and modeling RCI is developed. The validities of the presented method in different systems are demonstrated. Furthermore, the presented method breaks conventional RCI development procedure and shortens RCI product cycles, which is desirable and significative for integrated RCI design and manufacturing. Keywords Radial compressor impeller (RCI) . Ruled-surface blade . Straight generatrix vector (SGV) . Aerodynamic optimization . Flank milling . Reverse engineering

1 Introduction Radial compressor impeller (RCI) [1] has been extensively used in turbo-shaft engine and turbocharger [2–4] due

to low manufacturing cost and better performance under low flow rate. In order to obtain a high-performance RCI, accurate aerodynamic performance prediction and highefficiency machining are pretty essential, which is

* Yan Wang [email protected]

Farong Du [email protected]

Yu Zhou [email protected]

Shuiting Ding [email protected]

Yue Song [email protected]

1

School of Transportation Science and Engineering, Beihang University, Beijing 100191, China

2

Aircraft/Engine Integrated System Safety Beijing Key Laboratory, Beihang University, Beijing 100191, China

3

School of Energy and Power Engineering, Beihang University, Beijing 100191, China

Tong Xing [email protected] Qi Zhang [email protected] Longtao Shao [email protected]

Int J Adv Manuf Technol

demanding substantial improvement in the precision of geometric model