Blades are critical components that determine the energy conversion efficiency of an aeroengine. The size of the blade profile and the surface quality must meet the requirements of high strength and reliability. Therefore, precision inspection and quality control are important in manufacturing and assembly. However, the technical characteristics of blades, such as complex profile, thin and distorted structure, high manufacturing accuracy and so on, make the measurement of blades difficult. Existing measurement and inspection methods based on highprecision three-coordinate measurement machine (CMM) and a single optical sensor have obvious technical limitations, which are difficult to satisfy of rapid measurement speed, high accuracy and data integrity of aviation blade profile, and more difficult to achieve accurate measurement of the inlet and exhaust edges. In view of the above problems, this paper studies the measurement method of aviation blade based on the fusion of optical sensors with different principles, and gives full play to the advantages of holographic interferometry and structural scanning, and develops a set of precise and rapid three-dimensional measurement system of aviation blade based on the combination of fringe projection profilometry and conoscopic holography. The measurement experiments and results show that the developed measurement system has high measurement speed and accuracy, and has great potential for popularization and application.