Patent · US Active

Active vibration control system in a gunfire vibration environment

US11745861B2 · kind B2 · utility

0Cited by
2References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 25, 2020
Grant dateSep 5, 2023
Priority date
Expiry dateAug 26, 2040

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C2027/004
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

Systems and method for active vibration control on an aircraft. An active vibration control system (AVCS) is configured for an aircraft having an aircraft structure and a gun. The AVCS includes at least one control sensor on the aircraft, at least one force generator on the aircraft, and at least one controller in electronic communication with the sensor and the force generator. The controller is configured for determining, using the at least one control sensor, force generating commands for controlling vibrations acting on the aircraft structure, sending the force generating commands to the at least one force generator, causing the at least one force generator to produce a vibration canceling force, determining that the gun is firing, and in response to determining that the gun is firing, determining different force generating commands and sending the different force generating commands to the at least one force generator.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.