Politecnico Di Milano

Leonardo Corporation

Rösler Italiana S.r.l.

Steven Chatterton

Massimo Brunetti

Enrico Bellussi

Giovanni Facchini

Nicola Ostuni

Francesco Castelli Dezza

Nicola Toscani

Marco Mauri

Paolo Emilio Lino Maria Pennacchi

Alessandro Giussani

Nora Lecis

A rotor for an aircraft is described having: a support angularly fixed with respect to an axis and housing a power source; a unit rotatable about axis and housing an electrical load of the resistive type; and a power supply system for the electrical load () and comprising: a first transformer electrically interposed between the power source and the load; the first transformer comprises: a first winding arranged on the support and a second winding arranged on the unit, a stator carried by the support, rotationally fixed with respect to axis and to which the first winding is fixed; and a rotor operatively connected to the unit and to which the second winding is fixed; the power supply system comprises a capacitive circuit electrically connected to the first transformer, so as to reduce the reactive power absorbed by the rotary transformer.

Rotor for a hover-capable aircraft

Growing community of inventors

Samarate, Italy

Steven Chatterton