Active cabin noise and vibration control for turboprop aircraft using multiple piezoelectric actuators

Journal of Intelligent Material Systems and Structures

Volumn 11, Issue 6, 2000, Pages 438-447

  Grewal, A ^a   Zimcik, D G ^a   Hurtubise, L ^a   Leigh, B ^b  

^a NATIONAL RESEARCH COUNCIL CANADA   (Canada)

^b BOMBARDIER AEROSPACE   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELEROMETERS; ACTUATORS; AIRCRAFT PROPELLERS; CERAMIC MATERIALS; COMPUTER SIMULATION; FEEDBACK CONTROL; FUSELAGES; NOISE ABATEMENT; PIEZOELECTRIC DEVICES; VIBRATION CONTROL;

ACTIVE STRUCTURAL ACOUSTIC CONTROL (ASAC);

CABINS (AIRCRAFT);

EID: 0034197104     PISSN: 1045389X     EISSN: None     Source Type: Journal    
DOI: 10.1106/VYJR-2UGX-UD2F-DAHX     Document Type: Article

References (11)

1. Use of piezoelectric actuators as elements of intelligent structures
2. In-flight experiments on the active control of propeller-induced cabin noise
3. Active control of aircraft cabin noise using collocated structural actuators and sensors
4. Review of recent research on interior noise of propeller aircraft
5. A comparison of speakers and structural-based actuators for aircraft cabin noise control
6. Mechanisms of active control in cylindrical fuselage structures
7. Digital control of local sound fields in an aircraft passenger compartment