Patent · US Active

Aircraft electronics cooling apparatus for an aircraft having a liquid cooling system

US9167720B2 · kind B2 · utility

3Cited by
20References
7Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 18, 2013
Grant dateOct 20, 2015
Priority date
Expiry dateJan 21, 2034

Classification

  • Technology area (CPC H)Electricity
  • CPC primaryH05K7/20681
  • WIPO fieldAudio-visual technology
  • WIPO sectorElectrical engineering

Abstract

The invention relates to an improved aircraft electronics cooling system for an aircraft having a liquid cooling system, the aircraft electronics cooling system providing a thermal coupling between an electronic device to be cooled and the liquid cooling system of the aircraft. A coolant delivered by the liquid cooling system may flow through a board of the electronic device, through a heat sink on which the electronic device is arranged and/or through a housing in which the electronic device is arranged. The coolant may be permanently in the liquid state in a cooling circuit. The coolant may vaporize at least partially while cooling the electronic device.

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