PROBLEM TO BE SOLVED: To provide a component which can efficiently release the heat generated by a heat generating part of an aircraft.SOLUTION: A component has a first composite component having plastic reinforced with thermally conductive carbon fiber including one or both of metal coated carbon fiber and pitch-based carbon fiber, where with respect to fiber direction, one end of the thermally conductive carbon fiber is disposed at a heat generating part, and the other end of the thermally conductive carbon fiber is disposed at a heat radiation part.SELECTED DRAWING: Figure 2
【課題】航空機の発熱部で発生した熱を効率良く放出できる部材を提供する。【解決手段】部材は、金属コート炭素繊維及びピッチ系炭素繊維の一方又は両方を含む熱伝導性炭素繊維で強化されたプラスチックを有する第1複合部材を備え、繊維方向に関して熱伝導性炭素繊維の一端部が発熱部に配置され、熱伝導性炭素繊維の他端部が放熱部に配置される。【選択図】図2
COMPONENT
部材
2016-06-20
Patent
Electronic Resource
Japanese
IPC: | C08J Verarbeitung , WORKING-UP / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / 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 / B64C AEROPLANES , Flugzeuge / F28F Einzelheiten von Wärmetauschern oder Wärmeübertragungsvorrichtungen für allgemeine Verwendung , DETAILS OF HEAT-EXCHANGE OR HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION |
European Patent Office | 2018
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