Taumelscheibenfreies Koaxialdrehflügelflugzeug

Details

Veröffentlichungs-Nr.

EP2829471

Aktenzeichen

EP14177865

Anmeldetag

21. Juli 2014

Veröffentlichung

15. Februar 2017

Erteilung

15. Februar 2017

Rechtsraum

EP

IPC

B64C27/10B64C27/72// B64C27/32B64C27/12B64C27/82

Abstract

A main rotor system 12 of an aircraft 10 is provided including a first rotor 16 coupled to a transmission 25 and configured to rotate about an axis R in a first direction. A second rotor 18 is similarly coupled to the transmission 25 and is configured to rotate about the axis R in a second direction. At least the first rotor 16 includes an individual blade control system (IBCS) 50 configured to adjust a pitch of each of a plurality of blade 54 of the first rotor 16 independently. At least one slip ring 60 is configured to transmit electrical power and/or a control signal to the at least one IBCS 50.

Anmelder

Firma

Sikorsky Aircraft Corporation

Land

🇺🇸 USA

Fachgebiete