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    AIRCRAFT WITH A PROTECTIVE SHIELD AGAINST AN ENGINE BLADE RELEASE
    1.
    发明申请
    AIRCRAFT WITH A PROTECTIVE SHIELD AGAINST AN ENGINE BLADE RELEASE 审中-公开
    具有防护罩的飞机对发动机叶片释放

    公开(公告)号：US20160362167A1

    公开(公告)日：2016-12-15

    申请号：US15182672

    申请日：2016-06-15

    Applicant: Airbus Operations S.L. ,  Airbus Operations S.A.S.

    Inventor： Javier Toral Vazquez ,  Esteban Martino Gonzalez ,  Diego Folch Cortes ,  Pablo Goya Abaurrea ,  Vasilis Votsios ,  Michel Fouinnetau ,  Sylvain Roumegas ,  Wolfgang Brochard

    IPC: B64C1/06 ,  B64D27/10 ,  B64D37/04

    Abstract: An internal shield inside the rear fuselage of an aircraft having a propulsion system formed by two engines mounted on each side of it. The internal shield is located in a suitable place inside the rear fuselage for covering the possible trajectories of fragments detached from one of the engines in a failure event that would impact critical elements of the opposite engine. The internal shield comprises an ensemble of fluid containers belonging to aircraft sub-systems, such as, particularly, the potable water and waste water sub-systems, with enough fluid for providing the energy absorption capability required for stopping the fragments. An aircraft having the internal shield is also disclosed.

    Abstract translation: 飞机后部机身内部有一个内部屏蔽罩，它具有由安装在其两侧的两个发动机构成的推进系统。 内部防护罩位于后机身内部的合适位置，用于覆盖可能影响对方发动机的关键元件的故障事件中与其中一个发动机分离的碎片的可能轨迹。 内部屏蔽件包括属于飞行器子系统的流体容器的集合体，特别是饮用水和废水子系统，具有足够的流体，用于提供停止碎片所需的能量吸收能力。 还公开了具有内部屏蔽的飞机。

    Propeller blade for an aircraft engine
    4.
    发明申请
    Propeller blade for an aircraft engine 审中-公开
    用于飞机发动机的螺旋桨叶片

    公开(公告)号：US20160176509A1

    公开(公告)日：2016-06-23

    申请号：US14757591

    申请日：2015-12-23

    Applicant: Airbus Operations, S.L.

    Inventor： Javier Toral Vazquez ,  Diego Folch Cortes ,  Esteban Martino Gonzalez ,  Pablo Goya Abaurrea ,  Vasilis Votsios ,  Michel Fouinnetau ,  Sylvain Roumegas

    IPC: B64C11/20 ,  B64D45/00

    CPC classification number: B64C11/26 ,  B64D2201/00

    Abstract: The disclosure refers to a propeller blade for an aircraft engine that includes an airbag system contained inside the blade and comprising at least one bag and at least one gas generator, the at least one gas generator in fluid communication with at least one bag for inflating the bag, a detecting system for detecting a rupture of a part of the blade, a trigger for activating the at least one gas generator when the rupture is detected by the detecting system, and the blade skin being configured for allowing the at least one bag to pass through the blade skin for being expanded outside the blade upon the bag inflation by the gas generator.

    Abstract translation: 本发明涉及一种用于飞行器发动机的螺旋桨叶片，其包括包含在叶片内部并包括至少一个袋和至少一个气体发生器的气囊系统，所述至少一个气体发生器与至少一个袋流体连通，用于使 袋，用于检测叶片的一部分破裂的检测系统，用于当由检测系统检测到破裂时启动至少一个气体发生器的触发器，并且叶片皮肤被配置为允许至少一个袋子 穿过叶片皮肤，以在气体发生器的袋子充气时在叶片外部膨胀。

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