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    MODULAR SUBFLOOR ARRANGEMENT FOR AN AIRCRAFT
    1.
    发明申请
    MODULAR SUBFLOOR ARRANGEMENT FOR AN AIRCRAFT 审中-公开

    公开(公告)号：US20190389592A1

    公开(公告)日：2019-12-26

    申请号：US16443960

    申请日：2019-06-18

    Applicant: AIRBUS HELICOPTERS DEUTSCHLAND GMBH

    Inventor： Gottfried HUEBNER ,  Stefan PROBST ,  Frank LOESER ,  Robert SEILER

    IPC: B64D37/04 ,  B64C1/06 ,  B64C1/18 ,  B64D37/06 ,  B64D37/16

    Abstract: A modular subfloor system comprises first longitudinal structural frames, lateral regions, and a modular tank system that is connected to the first longitudinal structural frames. The modular tank system comprises a bottom shell, an upper panel, second longitudinal structural frames arranged between the bottom shell and the upper panel and transversal structural frames that are arranged between the bottom shell and the upper panel. The transversal structural frames and the second longitudinal structural frames form compartments. The modular tank system further comprises tank bladders arranged in at least some of the compartments and sealing elements that seal the upper panel, the bottom shell, and the at least some of the compartments of the modular tank system.

    AIRCRAFT WITH A FUSELAGE THAT DEFINES AT LEAST AN INTERIOR REGION AND A DRIVE SYSTEM ACCOMMODATING REGION
    2.
    发明申请
    AIRCRAFT WITH A FUSELAGE THAT DEFINES AT LEAST AN INTERIOR REGION AND A DRIVE SYSTEM ACCOMMODATING REGION 审中-公开
    具有定义至少一个内部区域和一个驱动系统的飞机的飞机存储区域

    公开(公告)号：US20160236767A1

    公开(公告)日：2016-08-18

    申请号：US15043758

    申请日：2016-02-15

    Applicant: AIRBUS HELICOPTERS DEUTSCHLAND GMBH

    Inventor： Sebastian MORES ,  Frank LOESER ,  Johannes FRESE ,  Ralf BRAEUTIGAM ,  Christian WEHLE

    IPC: B64C1/40 ,  B64C27/82 ,  B64D33/04 ,  B64C1/16

    CPC classification number: B64C1/40 ,  B64C1/10 ,  B64C1/16 ,  B64C27/82 ,  B64D33/04 ,  B64D33/08 ,  B64D41/00

    Abstract: An aircraft with a fuselage that defines at least an interior region and a drive system accommodating region, the drive system accommodating region being arranged inside the fuselage and comprising at least one fire protection zone that is defined by at least one associated firewall arrangement, the at least one fire protection zone accommodating at least one engine within the at least one associated firewall arrangement such that the associated firewall arrangement defines a fire-resistant separation between the at least one engine and the interior region of the fuselage, wherein the at least one associated firewall arrangement comprises at least one air duct for ducting a hot air flow that is generated in operation of the aircraft independent from heat generation of the at least one engine.

    Abstract translation: 具有至少限定内部区域和驱动系统容纳区域的机身的飞行器，所述驱动系统容纳区域布置在所述机身内部，并且包括由至少一个相关联的防火墙布置限定的至少一个防火区域，所述防火墙装置 至少一个防火区域，其容纳至少一个相关联的防火墙装置内的至少一个发动机，使得所述相关联的防火墙装置限定所述至少一个发动机与所述机身的内部区域之间的耐火间隔，其中，所述至少一个相关联的防火墙装置 防火墙装置包括至少一个空气管道，用于在独立于至少一个发动机的发热的情况下运送在飞机运行中产生的热空气流。

    AIRCRAFT WITH A SUBFLOOR REGION THAT ACCOMMODATES AN AUXILIARY COMPARTMENT
    3.
    发明申请
    AIRCRAFT WITH A SUBFLOOR REGION THAT ACCOMMODATES AN AUXILIARY COMPARTMENT 有权
    具有辅助辅助舱的辅助区域的飞机

    公开(公告)号：US20160229516A1

    公开(公告)日：2016-08-11

    申请号：US15014090

    申请日：2016-02-03

    Applicant: AIRBUS HELICOPTERS DEUTSCHLAND GMBH

    Inventor： Michael BEHRENS ,  Markus WAHNFRIED ,  Frank LOESER ,  Sebastian MORES

    IPC: B64C1/18 ,  B64D45/00 ,  B64D9/00

    CPC classification number: B64C1/18 ,  B64C1/062 ,  B64D1/22 ,  B64D9/00 ,  B64D37/04 ,  B64D45/00

    Abstract: An aircraft with a fuselage and a floor structure that is arranged inside the fuselage, the floor structure and the fuselage defining a subfloor region between the floor structure and a fuselage underside of the fuselage, the subfloor region accommodating at least one auxiliary compartment, wherein an equipment bay with at least one auxiliary equipment is arranged within the subfloor region, the at least one auxiliary equipment being at least essentially stowable in the equipment bay in a stow mode and the at least one auxiliary compartment being at least partly arranged in a region between the equipment bay and the floor structure such that the at least one auxiliary compartment separates the equipment bay from the floor structure.

    Abstract translation: 一种具有机身和地板结构的飞行器，其布置在机身内部，地板结构和机身中，在机身的底板结构和机身底面之间限定底板地板，底板地板容纳至少一个辅助隔间，其中， 具有至少一个辅助设备的设备舱布置在底层地板区域内，所述至少一个辅助设备至少基本上以收起模式存储在所述设备舱中，并且所述至少一个辅助隔室至少部分地布置在 所述设备托架和所述地板结构使得所述至少一个辅助隔室将所述设备托架与所述地板结构分离。

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