Title:
航空機の内部に位置する熱源から熱を排出させる冷却システム及び方法
Document Type and Number:
Japanese Patent JP4673856
Kind Code:
B2
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).
Inventors:
Georg Mussallah
Michael Markwald
Andreas Edom
Michael Markwald
Andreas Edom
Application Number:
JP2006546123A
Publication Date:
April 20, 2011
Filing Date:
December 30, 2004
Export Citation:
Assignee:
Airbus Opera Zion Gesellschaft Mitt Beschlenktel Haftung
International Classes:
B64D13/08; B64D11/04; F25D9/00; F28D15/02; F28D15/06
Domestic Patent References:
| JP1311999A |
Foreign References:
| US20030159808 | ||||
| US5966951 | ||||
| US2499736 | ||||
| GB1595961A | ||||
| GB1526160A |
Attorney, Agent or Firm:
Kenji Sugimura
Tatsuya Sawada
Kosaku Sugimura
Shiro Fujitani
Kiyoshi Kuruma
Yoshiyuki Iwasa
Tatsuya Sawada
Kosaku Sugimura
Shiro Fujitani
Kiyoshi Kuruma
Yoshiyuki Iwasa