Patent · US Active

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

US8315053B2 · kind B2 · utility

1Cited by
8References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 28, 2011
Grant dateNov 20, 2012
Priority date
Expiry dateFeb 28, 2031

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 (2), the aircraft electronics cooling system providing a thermal coupling between an electronic device (40a, 40b, 40c, 40d, 42, 44) to be cooled and the liquid cooling system (2) of the aircraft. A coolant delivered by the liquid cooling system (2) may flow through a board of the electronic device (40a, 40b, 40c, 40d), through a heat sink on which the electronic device (42) is arranged and/or through a housing in which the electronic device (44) 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.