The centrifugal compressor impeller is an important component in the
field of aerospace and precision machine industry. Traditionally,
there have been two methods for manufacturing the impellers :
casting and machining. Both methods have advantages and
disadvantages, respectively. Due to the complex geometry of the
centrifugal compressor impellers, it is a challenging technology to
machine the impellers.
Referring to the machining technology,
there have been two cutting strategies : point cutting and flank
cutting. Based on the consideration of cost, efficiency, and surface
roughness, flank cutting is a promising way to machine the blade
surfaces of impeller by using a 5-axis machining center with two
more degrees of freedom than the traditional 3-axis machining
center. However, the complexity of the tool paths generation
increased with the flexibility of the used equipment.
In this thesis, a flank cutting technology
for centrifugal compressor impellers is proposed by using the B-spline
curve interpolation, ruled surface construction, and coordinate
transformation. And an impeller is machined actually to verify the
proposed method. In addition, a windows-interfaced CAD/ CAM software
is developed to make the 5-axis NC code generation more easily and
friendly. |