A method for preparing a centrifugal ventilator
impeller with
carbon fiber composite materials is characterized in that the
impeller is decomposed into three independent parts, namely an
impeller cover, a blade and an impeller disk, the three parts are formed individually, and then the three parts are assembled into a whole; the impeller cover, the blade and the impeller disk are made of T300 orthogonal carbon
fiber sheet prepreg and T700 homotaxial carbon
fiber sheet prepreg which are laid into multiple
layers in a certain laying direction sequence in a circulating mode; after the
layers are laid ready, the impeller cover, the blade and the impeller disk are vacuumized and sent into a furnace to be cured at a medium temperature, and finally the integral whole is formed. The impeller is made of the
carbon fiber composite materials,
carbon fibers in the structure of the
carbon fiber composite materials serve as main materials for bearing the force, the fibers are different in
bearing capacity in different directions, and therefore the carbon
fiber composite materials has designability. The '
fiber orientation' design aims to utilize the
directivity of carbon fiber materials and maintain the continuity of a force transmission path in the structure to the maximum extent, and a laminated board subjected to in-plane loads can be designed into
layers in different directions in the structural
design process so that structure demands can be met.