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Edoardo Vigoni
Edoardo Vigoni
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Improvement of structures vibroacoustics by widespread embodiment of viscoelastic materials
GL Ghiringhelli, M Terraneo, E Vigoni
Aerospace Science and Technology 28 (1), 227-241, 2013
392013
MANOEUVRES-an effort towards quieter, reliable rotorcraft terminal procedures
L Trainelli, ALM Rolando, E Zappa, S Manzoni, M Lovera, M Gennaretti, ...
Greener Aviation: Clean Sky breakthroughs and worldwide status-3AF/CEAS …, 2014
122014
Contactless rotor flapping sensor design, implementation and testing
A Cigada, A Colombo, P Cordisco, A Ferrario, R Grassetti, R Liu, ...
ANNUAL FORUM PROCEEDINGS, 1315-1325, 2016
82016
A novel contactless sensor for helicopter blade motion in-flight measurements
E Zappa, L Trainelli, P Cordisco, E Vigoni, A Rolando, M Redaelli, F Rossi, ...
52016
Developing a novel contactless sensor for helicopter rotor state measurements
P Cordisco, R Liu, M Redaelli, L Riviello, ALM Rolando, F Rossi, ...
etc2016-36. European Telemetry and Test Conference, 69-77, 2016
52016
Comparison of Feedback and Feedforward Strategies for Active Structural-Acoustic Control of Broadband Sound Transmission Into a Cavity
L Dozio, A Toso, W Corbetta, E Vigoni, GL Ghiringhelli
13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference …, 2007
52007
Active Solutions for Reduction of the Transmission of Structure-Borne Noise to the Cabin Structure on a A109 Mockup
L Dozio, W Corbetta, E Vigoni, A Forghieri, G Ghiringhelli, F Cenedese
Proceedings of ISMA2006: International Conference on Noise and Vibration …, 2006
42006
Real time contactless sensor for helicopter blade angle measurement
E Zappa, L Trainelli, R Liu, A Rolando, F Rossi, P Cordisco, E Vigoni, ...
2016 IEEE Metrology for Aerospace (MetroAeroSpace), 239-244, 2016
32016
Active control of helicopter's gearbox vibrations and effects on the cabin noise
W Corbetta, E Vigoni, A Toso, G Ghiringhelli, L Dozio, F Cenedese
34th European Rotorcraft Forum 2008 (ERF34), 2297-2326, 2008
32008
Rotor for a hover-capable aircraft and method for detecting the attitude of a blade with respect to a hub of such a rotor
M Redaelli, L Riviello, A Colombo, L Trainelli, E Zappa, A Rolando, ...
US Patent 10,793,263, 2020
12020
Active control of helicopter's gearbox vibrations and effects on teh cabin noise
W Corbetta, E Vigoni, A Toso, GL Ghiringhelli, L Dozio, F Cenedese
12008
Recent results in active control of structure-borne noise on a helicopter mockup
A Toso, W Corbetta, E Vigoni, G Ghiringhelli, L Dozio
12007
Application of FXLMS algorithm to active control of vibration in thin plates
A Toso, W Corbetta, E Vigoni, G Ghiringhelli, L Dozio
12007
Viscoelastic shear damping mechanism for vibration reduction on a helicopter anti-torque beam
LM Bottasso, G Ghrinighelli, A Perazzolo, E Fosco, M Ricciardi, ...
2017
Active Control of Helicopter Gearbox Supports and Effects on Cabin Acoustic Field
W Corbetta, A Toso, E Vigoni, G Ghiringhelli, L Dozio, F Cenedese
23rd International Conference on Noise and Vibration Engineering 2008, ISMA …, 2008
2008
Active Gearbox Isolation Systems for Helicopter Quieter Cabin Environment
A Toso, W Corbetta, E Vigoni, L Dozio, G Ghiringhelli
2007
Sisifo: a Flexible System for Control of Multiple Fatigue Tests
E Vigoni, L Dozio, G Ghiringhelli, P Mantegazza
2005
Flexible Digital Control System for Multiple Fatigue Tests
E Vigoni, GL Ghiringhelli, L Dozio, P Mantegazza
2003
El sistema no puede realizar la operación en estos momentos. Inténtalo de nuevo más tarde.
Artículos 1–18