Abstract: A global active noise control method for a rotorcraft, including: acquiring the acoustic pressure signal at a measuring point of the rotorcraft; predicting the holographic and global sound field of noise of the rotor; reconstructing the reverse sound field of the noise of the rotor; and performing adaptive sound field adjustment based on the optimal phase search.
Type:
Grant
Filed:
March 23, 2022
Date of Patent:
December 12, 2023
Assignee:
NANJING UNIVERSITY OF AERONAUTICS AND ASTRONUATICS
Inventors:
Yang Lu, Xice Xu, Mengxue Shao, Jinru Chen