Damping of helicopter blades

Data di pubblicazione

21-10-2021

Codice

DAER.21.079.A

Stato

Disponibile

Data di priorità

08-07-2021

Fase

Italian Patent Application process

Titolare

Politecnico di Milano

Dipartimento

Department of Aerospace Science and Technology

Autori

Masarati Pierangelo, Frison Leonardo Antonio

Descrizione

The invention consists of a novel method of introducing damping in relation with the lead-lag motion of the blades of a helicopter rotor, maximizing it for motions that require it, and minimizing or making it vanish for those that do not need damping.

Stadio di sviluppo

Simulations

Contatto

licensing.tto@polimi.it