PROBLEM TO BE SOLVED: To provide a system for sound insulation and impact protection from an open rotor engine.SOLUTION: An aircraft (100) includes: a fuselage (102) including a nose (104), a tail (106), a hollow, and an elongate body (108) extending therebetween; a wing (110) extending laterally away from the fuselage, the wing including a leading edge (114) in a direction (116) of motion of the aircraft during normal flight and a trailing edge (118) on an opposing edge of the wing, and an engine (120) configured to drive a bladed rotatable member (122), the engine coupled to at least one of the wing and the fuselage. The aircraft further includes at least one of a forward chine member (123), which extends from the fuselage at a point (124) forward of the engine aftward to a point (128) aft of the bladed rotatable member, and an aft chine member (132), which extends from a point (134) to a point (138).SELECTED DRAWING: Figure 1

    【課題】オープンロータエンジンからの防音、衝撃防護システムを提供する。【解決手段】飛行機(100)は、機首(104)と、機尾(106)と、中空部と、それらの間に延びる細長本体(108)とを含む胴体(102)と、胴体から横方向に延びる翼(110)で、通常飛行中は飛行機の動く方向(116)に前縁(114)と、翼の反対縁に後縁(118)を含む翼と、動翼付回転可能部材(122)を駆動するよう構成されたエンジン(120)で、翼及び胴体のうち少なくともひとつに結合する前記エンジンと、を含む。飛行機はさらに、エンジンの前方の点(124)で胴体から後方に、前記動翼付回転可能部材の後方の点(128)まで延びる、前方尾根部(123)及び点(134)から点(138)まで延びる後方尾根部(132)の少なくともひとつを含む。【選択図】図1


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    Titel :

    METHOD AND SYSTEM FOR OPEN ROTOR ENGINE FUSELAGE PROTECTION


    Weitere Titelangaben:

    オープンローターエンジン胴体保護方法及びシステム



    Erscheinungsdatum :

    2017-07-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / G10K Tonerzeugungsvorrichtungen , SOUND-PRODUCING DEVICES



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