Abkuppeln eines Rotors

Details

Veröffentlichungs-Nr.

EP2752364

Aktenzeichen

EP13157514

Anmeldetag

1. März 2013

Veröffentlichung

21. Oktober 2015

Erteilung

21. Oktober 2015

Rechtsraum

EP

IPC

B64C27/12B64C27/14B64C27/82B64D35/04

Abstract

According to one embodiment, a clutch (300) may be coupled between a rotor system (110)and a power train of a rotorcraft (100). The clutch may be operable to disengage the rotor system (110) from the power train during operation of the power train. A clutch control system (200) in communication with the clutch (300)and include a rotorcraft condition sensor (240, 250, 260, 270) operable to sense an operating condition of the rotorcraft (100) and a control unit (210) operable to prevent the clutch (300) from disengaging the rotor system (220)from the power train if the operating condition of the rotorcraft (100) fails to satisfy a predetermined criterion.

Anmelder

Firma

Bell Helicopter Textron Inc.

Land

🇺🇸 USA

Fachgebiete