PROBLEM TO BE SOLVED: To provide an insulation panel and design that is easier to fabricate and reduces generation of powder, for sidewall trim panels of commercial passenger aircraft.SOLUTION: There are disclosed methods and apparatus for manufacturing a foam insulation panel 36 to include a panel feature 54, 58, 62, 66 conforming to a first feature 50, 56, 60, 64 of an aircraft sidewall assembly. A method for manufacturing the insulation panel 36 includes: compressing opposed first and second surfaces of a foam block; advancing a cutter transversely through the foam block to separate the foam block into an excess layer and the foam insulation panel; and translating the foam block by an offset distance determined from the aircraft sidewall assembly first feature 50, 56, 60, 64 to form the panel feature 54, 58, 62, 66.

    【課題】商用旅客機の側壁トリムパネルについて、製作するのが容易で、粉末の発生を減少させる断熱パネルとデザインの提供。【解決手段】航空機側壁アセンブリの第一の特徴50、56、60、64に一致するパネル特徴54、58、62、66を含むように発ぽう断熱パネル36を製造する方法及び装置。発ぽうブロックの向かい合う第一の表面と第二の表面を圧縮すること、発ぽうブロックを通って横方向にカッターを進ませ、発ぽうブロックを余分な層と発ぽう断熱パネルに分離すること、及び航空機側壁アセンブリの第一の特徴50、56、60、64から決定されるオフセット距離だけ発ぽうブロックを移動させ、パネル特徴54、58、62、66を形成することを含む断熱パネル36の製造方法。【選択図】図1


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    Title :

    AIRCRAFT FOAM INSULATION METHOD AND APPARATUS


    Additional title:

    航空機の発ぽう断熱方法及び装置


    Contributors:

    Publication date :

    2015-12-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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