Aeronautics and astronautics – Aircraft structure – Passenger or crew accommodation
Reexamination Certificate
2011-06-28
2011-06-28
Dinh, Tien (Department: 3644)
Aeronautics and astronautics
Aircraft structure
Passenger or crew accommodation
C244S057000, C244S11700R
Reexamination Certificate
active
07967249
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).
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Edom Andreas
Markwart Michael
Mühlthaler Georg
Airbus Deutschland GmbH
Dinh Tien
Green Richard R
Wood Herron & Evans L.L.P.
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