The invention provides a trailing edge variable camber wing driven by piezoelectric fiber materials. The wing comprises a leading edge fixing section with the invariable camber, a trailing edge flexible deformation section with the variable camber and a piezoelectric fiber composite material driver used for adjusting the change degree of the trailing edge flexible deformation section. The trailingedge flexible deformation section comprises a flexible wing rib, a stringer, a deformation skin, a segmented deformation skin and a segmented deformation skin fixing device. Voltage excitation is applied to the piezoelectric fiber composite material drivers, generated torque is transmitted to the flexible wing rib structure through the skin, and continuous and smooth change of the shape of the trailing edge of the wing is achieved. The wing structure mass can be greatly reduced, noise is reduced, the stealth characteristic is improved, the corresponding deformation control system is combined,accurate control over wing camber changes in the flight process can be achieved, the maneuvering and stall characteristics of an airplane are improved, and the task adaptability of the airplane is greatly enhanced.