SYSTEM FOR STRUCTURALLY INTEGRATED THERMAL MANAGEMENT FOR THIN WING AIRCRAFT CONTROL SURFACE ACTUATORS
SYSTEM FOR STRUCTURALLY INTEGRATED THERMAL MANAGEMENT FOR THIN WING AIRCRAFT CONTROL SURFACE ACTUATORS
- Neue Suche nach: WHITE EDWARD V
- Neue Suche nach: WHITE EDWARD V
A thermal management system for transferring heat from a heat load includes a composite structural member that supports a heat load source and a heat transfer member in thermal contact with the composite structural member, and in thermal contact with a heat sink. The system further includes at least one thermally-conductive first fastener that is in thermal contact with the heat transfer member, couples the heat load source to the composite structural member, and conducts heat from the heat load source into the heat transfer member. The heat transfer member conducts heat from the thermally-conductive first fastener to the heat sink.
Dokumentinformationen
SYSTEM FOR STRUCTURALLY INTEGRATED THERMAL MANAGEMENT FOR THIN WING AIRCRAFT CONTROL SURFACE ACTUATORS
2020-10-08
Patent
Elektronische Ressource
Englisch
| IPC: | B64C AEROPLANES , Flugzeuge / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64G Raumfahrt , COSMONAUTICS / F28F Einzelheiten von Wärmetauschern oder Wärmeübertragungsvorrichtungen für allgemeine Verwendung , DETAILS OF HEAT-EXCHANGE OR HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION |
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