Patent · US Expired

Cooling system and method for expelling heat from a heat source located in the interior of an aircraft

US7967249B2 · kind B2 · utility

9Cited by
14References
5Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 30, 2004
Grant dateJun 28, 2011
Priority date
Expiry dateAug 5, 2025

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D2013/0629
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

With a cooling system for expelling heat from a heat source (30) located in the interior of an aircraft to a heat reducer (32), with a piping system (10) sealed against the surrounding atmosphere which is thermally coupled to a heat intake section (14) with the heat source (38) and to a heat output section (22) with the heat reducer (32), and which preferably has an essentially adiabate transport section (21), it is proposed that the piping system (10) is filled with a heat conveyance medium (12) which, when taking in heat from the heat source (38) in the heat intake section (14) undergoes a transition from the liquid phase to the gaseous phase, then flows into the heat output section (22), and here, when discharging heat to the heat reducer (32) condenses once again, and flows back into the heat intake section (14).

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