Wärmeabführeinrichtung mit doppelter Leitung für Raumfahrzeug

Wärmeabführeinrichtung mit doppelter Leitung für Raumfahrzeug

The device has a radiating panel (PR) installed parallel to traveling wave tubes (T) and thermally coupled with a body (B) of the tubes. A radiating receptacle (RR) has walls (P1-P3) defining a housing to accommodate collectors (C) of the tubes. The receptacle is thermally coupled with the collector...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: JAUBERT, PIERRE, FOUCHER, JEAN-LUC, COMBES, CHARLES
Format: Patent
Sprache:ger
Schlagworte:
AIRCRAFT
AVIATION
BASIC ELECTRIC ELEMENTS
COSMONAUTICS
ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
ELECTRICITY
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
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Beschreibung
Zusammenfassung:The device has a radiating panel (PR) installed parallel to traveling wave tubes (T) and thermally coupled with a body (B) of the tubes. A radiating receptacle (RR) has walls (P1-P3) defining a housing to accommodate collectors (C) of the tubes. The receptacle is thermally coupled with the collectors by one of the walls so that the heat is distributed on the wall and between the collectors. An independent claim is also included for a space vehicle.