The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jul. 29, 2025

Filed:

Jan. 25, 2022
Applicant:

Nanjing University of Aeronautics and Astronautics, Jiangsu, CN;

Inventors:

Yongjie Shi, Jiangsu, CN;

Taihang Ma, Jiangsu, CN;

Zhiyuan Hu, Jiangsu, CN;

Guohua Xu, Jiangsu, CN;

Yang Liu, Jiangsu, CN;

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/00 (2006.01); G06F 30/15 (2020.01); G06F 30/28 (2020.01); G10K 11/178 (2006.01);
U.S. Cl.
CPC ...
B64C 27/001 (2013.01); G10K 11/17875 (2018.01); G10K 11/17883 (2018.01); B64C 2027/004 (2013.01); B64C 2220/00 (2013.01); G06F 30/15 (2020.01); G06F 30/28 (2020.01);
Abstract

A helicopter active noise suppression device integrating a sound array and on-propeller control, which relates to the technical field of helicopter noise reduction, includes an annular loudspeaker array, a plurality of force exciters, an error microphone, an Active Noise Cancellation (ANC) controller, a cockpit sensor, and an airborne computer. The annular loudspeaker array is arranged at a rotor hub and unsteady force exciters are arranged at each blade trailing edge to construct a sound field in an reversed phase to the sound wave of an original sound field with an ANC principle, thereby counteracting the noise and realizing the noise reduction of all-domain and all-type helicopter noise.


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