MEMBER

• Main Authors: KAMIHARA, NOBUYUKI, ABE, TOSHIO
• Format: Patent
• Language: English; French; Japanese
• Published: 09.06.2016
• Subjects: AEROPLANES; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F,C08G; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING; AIRCRAFT; AVIATION; BLASTING; CHEMISTRY; COMPOSITIONS BASED THEREON; COSMONAUTICS; DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION; GENERAL PROCESSES OF COMPOUNDING; HEAT EXCHANGE IN GENERAL; HEATING; HELICOPTERS; LIGHTING; MECHANICAL ENGINEERING; METALLURGY; ORGANIC MACROMOLECULAR COMPOUNDS; PERFORMING OPERATIONS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR; SHAPING OR JOINING OF PLASTICS; THEIR PREPARATION OR CHEMICAL WORKING-UP; TRANSPORTING; WEAPONS; WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL; WORKING-UP

A member is provided with a first composite member (11) which is made from a plastic that is reinforced with heat-conductive carbon fibers comprising metal-coated carbon fibers and/or pitch-based carbon fibers, wherein one end of the heat-conductive carbon fibers is arranged at a heat-generating section and the other end of the heat-conductive carbon fibers is arranged at a heat-dissipating section as observed in the fiber direction. Cette invention concerne un élément comprenant un premier élément composite (11) à base d'une matière plastique qui est renforcée par des fibres de carbone thermoconductrices comprenant des fibres de carbone revêtues de métal et/ou des fibres de carbone à base de poix, une des extrémités des fibres de carbone thermoconductrices étant agencée dans une section génératrice de chaleur et l'autre, dans une section dissipatrice de chaleur, selon une observation dans le sens des fibres. 　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（１１）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。