-
公开(公告)号：US08662444B2
公开(公告)日：2014-03-04
申请号：US13355976
申请日：2012-01-23
Applicant: Jürgen Tappe , Christian Holst , Ralph Sturm , Gregor Behlau , Michael Waller , Frank Trautmann , Arne Terstal
Inventor： Jürgen Tappe , Christian Holst , Ralph Sturm , Gregor Behlau , Michael Waller , Frank Trautmann , Arne Terstal
IPC: B64D11/00
CPC classification number: B64D11/02 , B64D2011/0046
Abstract: An area-expandable monument is provided for a cabin of a vehicle that includes, but is not limited to two housing parts that are displaceable relative to each other and can be fastened. A gap between the housing parts in an expanded state can be covered by a covering element. In the monument, a first sanitary fixture could be arranged whose position adapts to the spatial state of the monument. Optionally, there is also a pivotable second sanitary fixture that can be activated with the monument in its pushed-out state.
Abstract translation: 为车辆舱提供区域可扩展的纪念碑，其包括但不限于相对于彼此可移动并且可以被紧固的两个壳体部件。 处于膨胀状态的壳体部件之间的间隙可以被覆盖元件覆盖。 在纪念碑中，可以安排第一个卫生设备，其位置适应于纪念碑的空间状态。 可选地，还有可枢转的第二卫生设备，其能够在其被推出状态下被纪念碑启动。
-
公开(公告)号：USD723447S1
公开(公告)日：2015-03-03
申请号：US29387647
申请日：2011-03-16
Applicant: Jan Lesemann , Michael Meyer , Bernd Trahmer , Ralph Sturm
Designer： Jan Lesemann , Michael Meyer , Bernd Trahmer , Ralph Sturm
CPC classification number: B64C1/068 , B64C1/00 , B64C2001/0045
-
公开(公告)号：US20120068014A1
公开(公告)日：2012-03-22
申请号：US13233336
申请日：2011-09-15
Applicant: Jan Lesemann , Michael Meyer , Bernd Trahmer , Ralph Sturm
Inventor： Jan Lesemann , Michael Meyer , Bernd Trahmer , Ralph Sturm
IPC: B64C1/00
CPC classification number: B64C1/068 , B64C1/00 , B64C2001/0045
Abstract: According to an exemplary embodiment of the invention a fuselage segment of an aircraft fuselage is provided, which aircraft fuselage comprises four different radii of curvature, wherein two radii of curvature comprise centre points that are not situated on a vertical symmetry axis of the fuselage segment.
Abstract translation: 根据本发明的示例性实施例，提供了一种机身机身的机身段，该机身机身包括四个不同的曲率半径，其中两个曲率半径包括不位于机身段的垂直对称轴上的中心点。
-
公开(公告)号：US20110284689A1
公开(公告)日：2011-11-24
申请号：US13140068
申请日：2009-12-17
Applicant: Christian Thomas , Florian Hesselbach , Stephan Hoetzeldt , Wilfried Michaelis , Uwe Schneider , Ralph Sturm , Arno Berger
Inventor： Christian Thomas , Florian Hesselbach , Stephan Hoetzeldt , Wilfried Michaelis , Uwe Schneider , Ralph Sturm , Arno Berger
CPC classification number: G10K11/168 , B64C1/066 , B64C1/40 , Y02T50/46
Abstract: The present invention relates to an aircraft cabin panel for sound reduction in an interior space. The invention in particular also relates to an aircraft comprising an interior lining with sound-absorbing and sound-reducing panels. In order to provide a panel that is optimized in terms of the design space required by it and in terms of its weight, for use in aircraft, which panel provides improved sound reduction and sound absorption characteristics, an aircraft cabin panel for sound reduction in an interior space is provided, which aircraft cabin panel in at least one region comprises a sandwich construction with a core layer, a first covering layer and a second covering layer. The core layer comprises sound absorbing open-pore core material. The first and the second covering layer are connected to the core layer in a planar fashion. The first covering layer is arranged towards the sound waves to be absorbed and the second covering layer is arranged opposite the first covering layer. The first covering layer is designed so as to be acoustically transparent.
Abstract translation: 本发明涉及一种用于内部空间中的减声的飞机机舱面板。 本发明特别涉及一种包括具有吸声和减声面板的内衬的飞行器。 为了提供在其所需的设计空间和其重量方面优化的面板，在飞机上使用，该面板提供改进的减声和吸声特性，用于减少噪音的飞机机舱面板 提供内部空间，至少一个区域中的飞机机舱面板包括具有芯层的夹层结构，第一覆盖层和第二覆盖层。 芯层包括吸声开孔芯材。 第一和第二覆盖层以平面方式连接到芯层。 第一覆盖层被布置成朝向被吸收的声波，并且第二覆盖层被布置成与第一覆盖层相对。 第一覆盖层被设计成声透明。
-
公开(公告)号：US08757545B2
公开(公告)日：2014-06-24
申请号：US13233336
申请日：2011-09-15
Applicant: Jan Lesemann , Michael Meyer , Bernd Trahmer , Ralph Sturm
Inventor： Jan Lesemann , Michael Meyer , Bernd Trahmer , Ralph Sturm
CPC classification number: B64C1/068 , B64C1/00 , B64C2001/0045
Abstract: According to an exemplary embodiment of the invention a fuselage segment of an aircraft fuselage is provided, which aircraft fuselage comprises four different radii of curvature, wherein two radii of curvature comprise center points that are not situated on a vertical symmetry axis of the fuselage segment.
Abstract translation: 根据本发明的示例性实施例，提供了一种机身机身的机身段，该机身机身包括四个不同的曲率半径，其中两个曲率半径包括不位于机身段的垂直对称轴上的中心点。
-
Patent Agency Ranking
公开(公告)号：US20120119029A1
公开(公告)日：2012-05-17
申请号：US13355976
申请日：2012-01-23
Applicant: Jürgen Tappe , Christian Holst , Ralph Sturm , Gregor Behlau , Michael Waller , Frank Trautmann , Arne Terstal
Inventor： Jürgen Tappe , Christian Holst , Ralph Sturm , Gregor Behlau , Michael Waller , Frank Trautmann , Arne Terstal
CPC classification number: B64D11/02 , B64D2011/0046
Abstract: An area-expandable monument is provided for a cabin of a vehicle that includes, but is not limited to two housing parts that are displaceable relative to each other and can be fastened. A gap between the housing parts in an expanded state can be covered by a covering element. In the monument, a first sanitary fixture could be arranged whose position adapts to the spatial state of the monument. Optionally, there is also a pivotable second sanitary fixture that can be activated with the monument in its pushed-out state.
Abstract translation: 为车辆舱提供区域可扩展的纪念碑，其包括但不限于相对于彼此可移动并且可以被紧固的两个壳体部件。 处于膨胀状态的壳体部件之间的间隙可以被覆盖元件覆盖。 在纪念碑中，可以安排第一个卫生设备，其位置适应于纪念碑的空间状态。 可选地，还有可枢转的第二卫生设备，其能够在其被推出状态下被纪念碑启动。
-
7.发明授权公开(公告)号：US07520468B2
公开(公告)日：2009-04-21
申请号：US11220251
申请日：2005-09-06
Applicant: Oliver Döebertin , Wilfried Sprenger , Ralph Sturm
Inventor： Oliver Döebertin , Wilfried Sprenger , Ralph Sturm
IPC: B64D11/06
CPC classification number: B64D11/0015 , A63B2009/006 , A63B2208/12 , A63B2210/50 , A63H33/008 , B64D11/0691
Abstract: A children's play container in the cabin area on the level of the passenger deck, which when folded away has dimensions compatible with aircraft fixtures. In its assembled state, at least one side wall may be folded outwards along the lower horizontal edge onto the floor to form part of a play area. The inside of the children's play container incorporates playing equipment and fixtures for child care, which are accessible by opening at least one side wall.
Abstract translation: 在乘客甲板水平的客舱区域内的儿童游乐容器，折叠后的尺寸与飞机夹具相匹配。 在其组装状态下，至少一个侧壁可以沿着下水平边缘向外折叠到地板上以形成游戏区域的一部分。 儿童游乐用品容器的内部装有用于幼儿保育的演奏设备和固定装置，通过打开至少一个侧壁可以进入。
-
8.发明申请公开(公告)号：US20060058107A1
公开(公告)日：2006-03-16
申请号：US11220251
申请日：2005-09-06
Applicant: Oliver Dobertin , Wilfried Sprenger , Ralph Sturm
Inventor： Oliver Dobertin , Wilfried Sprenger , Ralph Sturm
CPC classification number: B64D11/0015 , A63B2009/006 , A63B2208/12 , A63B2210/50 , A63H33/008 , B64D11/0691
Abstract: A children's play container in the cabin area on the level of the passenger deck, which when folded away has dimensions compatible with aircraft fixtures. In its assembled state, at least one side wall may be folded outwards along the lower horizontal edge onto the floor to form part of a play area. The inside of the children's play container incorporates playing equipment and fixtures for child care, which are accessible by opening at least one side wall.
-
公开(公告)号：US08919695B2
公开(公告)日：2014-12-30
申请号：US12747237
申请日：2008-12-11
Applicant: Thomas Bock , Martin Dehn , Ian Scoley , Ralph Sturm
Inventor： Thomas Bock , Martin Dehn , Ian Scoley , Ralph Sturm
CPC classification number: B64D11/003
Abstract: A storage compartment configuration and an aircraft having a storage compartment configuration according to the invention are proposed. The storage compartment configuration has a storage compartment having a storage space and a suspension. The storage space is designed to receive pieces of luggage. The suspension is used for the attaching the storage compartment to a load-bearing structure of the aircraft. The suspension is designed in such a manner that the storage compartment can be pivoted essentially around a geometrical center point of the storage space.
Abstract translation: 提出了一种储藏室结构和具有根据本发明的储藏室结构的飞行器。 储藏室配置具有具有储存空间和悬浮液的储藏室。 存储空间设计用于接收行李。 悬架用于将储藏室连接到飞机的承载结构。 悬挂装置被设计成使得储物室可以基本围绕存储空间的几何中心点枢转。
-
公开(公告)号：US20100288879A1
公开(公告)日：2010-11-18
申请号：US12747237
申请日：2008-12-11
Applicant: Thomas Bock , Martin Dehn , Ian Scoley , Ralph Sturm
Inventor： Thomas Bock , Martin Dehn , Ian Scoley , Ralph Sturm
IPC: B64D11/00
CPC classification number: B64D11/003
Abstract: A storage compartment configuration and an aircraft having a storage compartment configuration according to the invention are proposed. The storage compartment configuration has a storage compartment having a storage space and a suspension. The storage space is designed to receive pieces of luggage. The suspension is used for the attaching the storage compartment to a load-bearing structure of the aircraft. The suspension is designed in such a manner that the storage compartment can be pivoted essentially around a geometrical center point of the storage space.
Abstract translation: 提出了一种储藏室结构和具有根据本发明的储藏室结构的飞行器。 储藏室配置具有具有储存空间和悬浮液的储藏室。 存储空间设计用于接收行李。 悬架用于将储藏室连接到飞机的承载结构。 悬挂装置被设计成使得储物室可以基本围绕存储空间的几何中心点枢转。
-
-
-
-
-
-
-
-
-
Search Results
10
records
(took 0.012 seconds)
