Patent · US Active

Aircraft light

US8956021B2 · kind B2 · utility

2Cited by
3References
8Claims
0Family size

Assignee

Inventor

Key dates

Filing dateSep 25, 2012
Grant dateFeb 17, 2015
Priority date
Expiry dateFeb 12, 2033

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF28F2013/008
  • WIPO fieldElectrical machinery, apparatus, energy
  • WIPO sectorElectrical engineering

Abstract

An aircraft light consists of a housing containing a light source, a heat sink element forming at least part of the exterior surface of the housing and an auxiliary thermal capacitor that is thermally decoupled from the heat sink element. A thermally expandable medium is coupled to the heat sink element and operates to thermally decouple the light source from the heat sink element and thermally couple the light source to the auxiliary thermal capacitor and vice versa, depending on the actual temperature of the heat sink element.

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