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1. 发明授权

US08747957B2 Component having coating and coating method 有权
标题翻译：具有涂层和涂层方法的组分
公开(公告)号：US08747957B2
公开(公告)日：2014-06-10
申请号：US12906453
申请日：2010-10-18
申请人： Mathias Gruen , Dietmar Voelkle , Benedict Michelis , Florian Hesselbach
发明人： Mathias Gruen , Dietmar Voelkle , Benedict Michelis , Florian Hesselbach
IPC分类号： B05D1/06 , B05D1/34 , B05D3/02
CPC分类号： B05D1/045 , B05D1/06 , B05D5/02 , B05D5/061 , B05D7/52
摘要： A coating method wherein in order to simplify the coating method and increase the flexibility thereof with respect to respective desired coatings, provision is made that a powder lacquer layer (3) is applied to a surface (2) of the component (1), and an imprint (4) is applied to the powder lacquer layer (3), preferably by an inkjet method.
摘要翻译：一种涂布方法，其中为了简化涂布方法并增加其对各个所需涂层的柔性，提供了将粉末涂料层（3）施加到组分（1）的表面（2）上，并且优选通过喷墨法将印模（4）施加到粉末涂料层（3）上。

2. 发明申请

US20110284689A1 AIRCRAFT CABIN PANEL FOR SOUND REDUCTION 审中-公开
标题翻译：用于减速的飞机客舱
公开(公告)号：US20110284689A1
公开(公告)日：2011-11-24
申请号：US13140068
申请日：2009-12-17
申请人： Christian Thomas , Florian Hesselbach , Stephan Hoetzeldt , Wilfried Michaelis , Uwe Schneider , Ralph Sturm , Arno Berger
发明人： Christian Thomas , Florian Hesselbach , Stephan Hoetzeldt , Wilfried Michaelis , Uwe Schneider , Ralph Sturm , Arno Berger
IPC分类号： B64C1/40 , G10K11/16
CPC分类号： G10K11/168 , B64C1/066 , B64C1/40 , Y02T50/46
摘要： 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.
摘要翻译：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。

3. 发明申请

US20110097544A1 COMPONENT HAVING COATING AND COATING METHOD 有权
标题翻译：具有涂料和涂料方法的组分
公开(公告)号：US20110097544A1
公开(公告)日：2011-04-28
申请号：US12906453
申请日：2010-10-18
申请人： Mathias GRÜN , Dietmar VÖLKLE , Benedict MICHELIS , Florian HESSELBACH
发明人： Mathias GRÜN , Dietmar VÖLKLE , Benedict MICHELIS , Florian HESSELBACH
IPC分类号： B32B3/10 , B32B3/00 , B05D1/36 , B05D5/00 , B05D3/06 , B05D3/02
CPC分类号： B05D1/045 , B05D1/06 , B05D5/02 , B05D5/061 , B05D7/52
摘要： A coating method wherein in order to simplify the coating method and increase the flexibility thereof with respect to respective desired coatings, provision is made that a powder lacquer layer (3) is applied to a surface (2) of the component (1), and an imprint (4) is applied to the powder lacquer layer (3), preferably by an inkjet method.
摘要翻译：一种涂布方法，其中为了简化涂布方法并增加其对各个所需涂层的柔性，提供了将粉末涂料层（3）施加到组分（1）的表面（2）上，并且优选通过喷墨法将印模（4）施加到粉末涂料层（3）上。

4. 发明申请

US20120040599A1 SANDWICH BOARD FOR AN INNER WALL CLADDING OF A PASSENGER CABIN 审中-公开
标题翻译：用于客舱的内墙的三明治板
公开(公告)号：US20120040599A1
公开(公告)日：2012-02-16
申请号：US13207953
申请日：2011-08-11
申请人： Florian HESSELBACH , Dietmar VÖLKLE
发明人： Florian HESSELBACH , Dietmar VÖLKLE
IPC分类号： B60H1/26 , B32B3/10 , B32B3/24 , B32B3/26
CPC分类号： B64D11/00 , B64C1/066 , B64D2013/0625 , Y10T428/24008 , Y10T428/24331 , Y10T428/24802
摘要： To implement replenished-air ventilation of a passenger cabin of, for example, an aircraft, an inner wall cladding (12) with integrated replenished-air inlets (18) is proposed. For this purpose, the inner wall cladding (12) has sandwich boards (30) which are constructed from a first top layer (32) facing the passenger cabin (10), a second top layer (34) facing away from the passenger cabin (10) and a sandwich core (36) arranged between the first top layer (32) and the second top layer (34), the sandwich core (36) being designed to be at least partially air-permeable, and the first top layer (32) having at least one air-permeable portion (38).
摘要翻译：为了实现例如飞行器的客舱的补充空气通风，提出了具有集成补充空气入口（18）的内壁包层（12）。为此目的，内壁包层（12）具有夹层板（30），它们由面向客舱（10）的第一顶层（32）构成，第二顶层（34）背向客舱（ 10）和布置在第一顶层（32）和第二顶层（34）之间的夹心芯（36），夹心芯（36）被设计为至少部分透气，并且第一顶层（ 32）具有至少一个透气部分（38）。

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