ふくごうざいこうくうきこうぞうの英語

孔付き繊維強化複合体の製造方法、及びその複合体からなる航空機構造用部材例文帳に追加

METHOD FOR PRODUCING FIBER-REINFORCED PERFORATED COMPOSITE MEMBER, AND STRUCTURAL MEMBER FOR AIRCRAFT CONSTITUTED BY SUCH COMPOSITE MEMBERS - 特許庁

航空機構造体の複合材料用のそれらの電磁特性を改善するためのエポキシ樹脂のナノファイバーの製造方法例文帳に追加

METHOD FOR PRODUCING NANOFIBER OF EPOXY RESIN FOR COMPOSITE MATERIAL OF AERONAUTICAL STRUCTURE TO IMPROVE THEIR ELECTROMAGNETIC CHARACTERISTICS - 特許庁

同一配向の連続積層を有する繊維強化複合材料部材において、圧縮強度などの力学的特性に優れ、航空機構造などとして好適に用いられる部材を、樹脂注入法により生産性よく得る。例文帳に追加

To provide a fiber reinforced composite material member having a continuous laminated layer with a same orientation and being superior in dynamic characteristics such as a compressive strength or the like, suitably used as an aircraft structure member or the like and produced in a good productivity by a resin injection method. - 特許庁

高空隙率水硬性複合物内に内包された空隙に、鱗状黒鉛や土状黒鉛の天然黒鉛又は人造黒鉛微粉末を含む前記高熱伝導率粉状体を含む充填材を所定形状の型枠内に充填してコンクリート成型体を製造する。例文帳に追加

A packing material comprising a powdery body having high thermal conductivity including natural graphite such as flake graphite and earthy graphite or artificial graphite fine powder in gaps involved within a hydraulic composite having a high porosity is packed into a frame with a prescribed shape, so as to produce a concrete molded body. - 特許庁