This invention discloses a parametric design method for a helicopter particle separator. The method first sets control points at key locations and constructs the central
body contour of the separator using a cubic
Hermite interpolation polynomial with weighted terms. Next, based on the cross-sectional areas of key locations such as the separator inlet, bifurcation, and
throat, the outer wall surface of the core region and part of the bifurcation profile are derived. Subsequently, by adding control points again and combining the cubic
Hermite interpolation polynomial with weighted terms, a complete outer wall
surface contour curve is generated. Simultaneously, the bifurcation curve is designed using circular arcs and tangents. This method not only meets the structural design requirements of the particle separator but also precisely controls the
changing trend of its
internal pressure gradient and supports flexible adjustment of key geometric parameters, thereby achieving efficient parametric design and optimization of the particle separator.