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公开(公告)号：US20160214701A1
公开(公告)日：2016-07-28
申请号：US15005265
申请日：2016-01-25
发明人： Stefan PROBST , Wolfgang HUENECKE , Frank LOESER , Johannes FRESE , Sebastian MORES , Michael MATT
CPC分类号： B64C1/1415 , B64C1/24 , B64D11/00
摘要： An aircraft comprising a rear opening and a rear door to close such rear opening, wherein the rear door is attached to the fuselage of the aircraft by means of an arrangement having two links due to which the rear door can be displaced longitudinally and in elevation up to a position at the interior of the fuselage.
摘要翻译： 一种飞机，包括后开口和后门以关闭这种后开口，其中后门通过具有两个连杆的装置附接到飞机的机身上，由此可以使后门纵向移动并且向上升高 到机身内部的位置。
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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
摘要： 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.
摘要翻译： 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。
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