Patent · US Active

Combined aircraft navigation and anti-collision light, and method of determining a state of erosion of a lens cover of a combined aircraft navigation and anti-collision light

US11225336B2 · kind B2 · utility

3Cited by
7References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateOct 22, 2020
Grant dateJan 18, 2022
Priority date
Expiry dateOct 22, 2040

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF21Y2115/10
  • WIPO fieldElectrical machinery, apparatus, energy
  • WIPO sectorElectrical engineering

Abstract

A combined aircraft navigation and anti-collision light, includes: at least one navigation light source and one anti-collision light source; a navigation light sensor, in operation outputting a light detection signal corresponding to an amount of light detected by the navigation light sensor; first and second optical systems, associated with navigation and collision light sources, wherein the first optical system is configured for shaping a navigation light output from light emitted by the at least one navigation light source and is configured for directing stray light from the at least one navigation light source to the navigation light sensor and a second optical system, associated with the at least one anti-collision light source and configured for shaping an anti-collision light output from light emitted by the at least one anti-collision light source; a lens cover, arranged over the light sources and optical systems for passing light therethrough.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.