摘要
Spline geometries representing airfoil shapes have been found to present difficulties in manufacturing compatibility with design. This paper highlights these problems and discusses a solution to the problem of profile matching. A spline geometry system has been developed to simulate the design iteraction process with manufacturability as the criterion. The paper reports the results of a study of the effects of design knots and tolerance on the manufactured profile. A procedure to integrate design and manufacturing data for the production of spline profiles such as the turbine blade section is presented.
| 原文 | English |
|---|---|
| 出版狀態 | Published - 1988 1月 1 |
All Science Journal Classification (ASJC) codes
- 一般工程