The application discloses a pre-pressure controllable
piezoelectric bimorph deformation wing based on a flexible hinge parallel connection and a method. The deformation wing mainly comprises four
layers of
piezoelectric composite bimorphs fixed at a
leading edge, the two sides of the four
layers of bimorphs are short and the middle is long, and the four
layers of bimorphs are connected in parallel through four interlayer connecting rib structures; the third group of interlayer connecting rib structures are provided with protruding shafts at positions corresponding to the two sides of the rotation shafts of the uppermost and lowermost
piezoelectric composite bimorphs, bearings and prefabricated clamping groove bearing sleeves are sleeved on the protruding shafts,
polymer spiral winding actuators fixed at the
leading edge are sleeved on the bearing sleeves to load and unload
axial pressure; one of the two middle layers of longer bimorphs is fixedly connected with a
trailing edge, and the other layer can slide in a prefabricated slot at a
tail edge; finally, upper and lower skins are fixed with upper and lower sides of a large end of the
leading edge, four groups of ribs and upper and lower sides of a large end of the
trailing edge in sequence. The application can greatly improve the output power of the pre-compressed
piezoelectric bimorph deformation wing and prolong the service life of the
piezoelectric bimorph deformation wing.