Intelligente Landungslichtenteisung mit Fortschrittlichem Transparentem Metallnetzleiter

Details

Veröffentlichungs-Nr.

EP4209420

Aktenzeichen

EP23150170

Anmeldetag

3. Januar 2023

Veröffentlichung

12. Juli 2023

Rechtsraum

EP

IPC

B64D47/04B64D15/12F21S45/60

Abstract

Systems and methods for deicing an aircraft landing light may include a metal mesh (212) conductor coupled to a lens (210) of a landing light (202). The systems and methods may include a power supply (418), a temperature sensor (414), a deicing control unit (416), an aircraft light having a lens (210), and a mesh (212) coupled to the lens (210). The temperature sensor (414) may be a microwave resonator sensor configured to sense the temperature of the landing light (202) and send signals to the deicing control unit (416). The signals may be configured to instruct the deicing control unit (416) to either apply an electric current to the mesh (212), or cease applying an electric current to the mesh (212), depending on the landing light temperatures. The deicing control unit (416) may receive landing pulses from a flight control system. The pulses may indicate that the aircraft is landing or has landed.

Anmelder

Firma

Goodrich Lighting Systems, Inc.

Land

🇺🇸 USA

Fachgebiete