An electronics system for an aircraft includes a mounting structure and a plate element mounted to the mounting structure with opposing face surfaces, a central region and side edge regions. A serpentine passage in the plate element contains alternating liquid slugs and vapor plugs along its length. The plate element is configured for gathering heat proximate the central region and moving the heat to the side edge regions. An electronic system is mounted on a face surface of the plate element and a heat dissipating structure is thermally coupled with the plate element and positioned along the side edge regions thereof for dissipating heat moved to the side edge regions. A cover structure covers the plate element and electronic system.
MOUNTING SYSTEM FOR MOUNTING AN ELEMENT TO AN AIRCRAFT SURFACE
MONTAGESYSTEM ZUM MONTIEREN EINES ELEMENTES AN EINER FLUGZEUGOBERFLÄCHE
SYSTÈME DE MONTAGE POUR LE MONTAGE D'UN ÉLÉMENT SUR UNE SURFACE D'AÉRONEF
2022-07-13
Patent
Elektronische Ressource
Englisch
Mounting System For Mounting An Element To An Aircraft Surface
Europäisches Patentamt | 2022
|Mounting System For Mounting An Element To An Aircraft Surface
Europäisches Patentamt | 2019
|MOUNTING SYSTEM FOR MOUNTING AN ELEMENT TO AN AIRCRAFT SURFACE
Europäisches Patentamt | 2021
|MOUNTING SYSTEMS FOR MOUNTING AN ELEMENT TO AN AIRCRAFT SURFACE
Europäisches Patentamt | 2019
|MOUNTING SYSTEMS FOR MOUNTING AN ELEMENT TO AN AIRCRAFT SURFACE
Europäisches Patentamt | 2019
|