公开(公告)号：US08541065B2

公开(公告)日：2013-09-24

申请号：US12602331

申请日：2008-05-31

申请人： Gerold Lukowski ,  Karsten Schroeder ,  Wolf-Dieter Juelich ,  Ruediger Foest ,  Klaus-Dieter Weltmann ,  Joerg Ehlbeck

发明人： Gerold Lukowski ,  Karsten Schroeder ,  Wolf-Dieter Juelich ,  Ruediger Foest ,  Klaus-Dieter Weltmann ,  Joerg Ehlbeck

IPC分类号： H05H1/00 ,  B05D3/00 ,  B05D1/12

CPC分类号： B05D3/141 ,  A61K9/5123 ,  A61L2/14 ,  A61L27/34 ,  A61L27/50 ,  A61L27/54 ,  A61L2300/22 ,  A61L2300/404 ,  A61L2300/602 ,  A61L2300/606 ,  A61L2400/12 ,  B05D3/142 ,  B05D3/145 ,  B05D7/02 ,  B05D2201/00 ,  B05D2401/32 ,  Y10T428/25

摘要： The invention relates to a method for coating surfaces with micro- and nanoparticles, the micro- and nanoparticles being chemically bonded to the surface, comprising the steps of pre-treatment of the surface with a plasma method, simultaneous or subsequent application of the micro- and nanoparticles to the surface, and subsequent fixation of the micro and nanoparticles on the surface using a plasma method, characterized in that the fixation of the micro- and nanoparticles takes place with the aid of anisothermal plasmas, the median electrical energy of which lies in the range of the bond dissociation energy of the micro- and nanoparticles, thus allowing the strength of the chemical bond between the surface and the micro- and nanoparticles to be variably set.

摘要翻译： 本发明涉及一种用微孔和纳米颗粒涂覆表面的方法，微米和纳米颗粒化学键合到表面，包括以等离子体方法预处理表面的步骤， 和纳米颗粒到表面，以及随后使用等离子体方法将微粒和纳米颗粒固定在表面上，其特征在于，借助于等温等离子体，其中的中等电能位于 微米和纳米颗粒的键解离能的范围，从而允许表面和微米级和纳米颗粒之间的化学键的强度可变地设定。

公开(公告)号：US20110159273A1

公开(公告)日：2011-06-30

申请号：US12602331

申请日：2008-05-31

申请人： Gerold Lukowski ,  Karsten Schroeder ,  Wolf-Dieter Juelich ,  Ruediger Foest ,  Klaus-Dieter Weltmann ,  Joerg Ehlbeck

发明人： Gerold Lukowski ,  Karsten Schroeder ,  Wolf-Dieter Juelich ,  Ruediger Foest ,  Klaus-Dieter Weltmann ,  Joerg Ehlbeck

IPC分类号： B32B5/16 ,  B05D3/10 ,  B05D1/12 ,  B05D1/18 ,  B05D1/00 ,  B05D5/00 ,  B82Y40/00 ,  B82Y5/00 ,  B82Y99/00

CPC分类号： B05D3/141 ,  A61K9/5123 ,  A61L2/14 ,  A61L27/34 ,  A61L27/50 ,  A61L27/54 ,  A61L2300/22 ,  A61L2300/404 ,  A61L2300/602 ,  A61L2300/606 ,  A61L2400/12 ,  B05D3/142 ,  B05D3/145 ,  B05D7/02 ,  B05D2201/00 ,  B05D2401/32 ,  Y10T428/25

摘要： The invention relates to a method for coating surfaces with micro- and nanoparticles, the micro- and nanoparticles being chemically bonded to the surface, comprising the steps of pre-treatment of the surface with a plasma method, simultaneous or subsequent application of the micro- and nanoparticles to the surface, and subsequent fixation of the micro and nanoparticles on the surface using a plasma method, characterized in that the fixation of the micro- and nanoparticles takes place with the aid of anisothermal plasmas, the median electrical energy of which lies in the range of the bond dissociation energy of the micro- and nanoparticles, thus allowing the strength of the chemical bond between the surface and the micro- and nanoparticles to be variably set.

摘要翻译： 本发明涉及一种用微孔和纳米颗粒涂覆表面的方法，微米和纳米颗粒化学键合到表面，包括以等离子体方法预处理表面的步骤， 和纳米颗粒到表面，以及随后使用等离子体方法将微粒和纳米颗粒固定在表面上，其特征在于，借助于等温等离子体，其中的中等电能位于 微米和纳米颗粒的键解离能的范围，从而允许表面和微米级和纳米颗粒之间的化学键的强度可变地设定。

公开(公告)号：US08596586B2

公开(公告)日：2013-12-03

申请号：US13490009

申请日：2012-06-06

申请人： Karsten Schroeder

发明人： Karsten Schroeder

IPC分类号： B64C3/50

CPC分类号： B64C9/24 ,  B64C2009/143 ,  Y02T50/32

摘要： A high lift system is provided for an aircraft. The high lift system includes, but is not limited to a lift flap arranged on a wing and coupled to the wing so as to be movable relative to the wing, between a retracted position and at least one extended position. In the retracted position the lift flap rests against the wing, and in an extended position forms an air gap to the wing. The lift flap directed towards its trailing edge comprises at least one region of variable curvature, which region in an extended position of the lift flap extends towards the wing.

摘要翻译： 飞机提供了高升程系统。 高升降系统包括但不限于设置在机翼上并联接到机翼上以便在缩回位置和至少一个延伸位置之间相对于机翼移动的升降挡板。 在缩回位置，提升翼片靠在机翼上，并且在延伸位置形成与机翼的气隙。 指向其后缘的升降翼包括至少一个可变曲率的区域，该提升翼的延伸位置中的该区域向翼延伸。

公开(公告)号：US20090164002A1

公开(公告)日：2009-06-25

申请号：US12339965

申请日：2008-12-19

申请人： Baerbel Becher ,  Carsten Momma ,  Daniel Lootz ,  Antje Quade ,  Andreas Ohl ,  Karsten Schroeder

发明人： Baerbel Becher ,  Carsten Momma ,  Daniel Lootz ,  Antje Quade ,  Andreas Ohl ,  Karsten Schroeder

IPC分类号： A61F2/06 ,  A61B19/00

CPC分类号： A61L31/022 ,  A61L31/082 ,  A61L31/148

摘要： An implant having a base body, comprised either entirely or in part of a biocorrodible metallic material wherein at least the parts of the base body having the biocorrodible metallic material are at least partially covered with a coating of a crosslinked CFx layer with an F/C ratio in the range of 0.5 to 1.5.

摘要翻译： 具有基体的植入体，其全部或部分由生物可腐蚀的金属材料组成，其中至少部分具有生物可腐蚀金属材料的基体部分至少部分地覆盖有具有F / C的交联CFx层的涂层 比例在0.5至1.5的范围内。

公开(公告)号：US08474763B2

公开(公告)日：2013-07-02

申请号：US13529855

申请日：2012-06-21

申请人： Karsten Schroeder

发明人： Karsten Schroeder

IPC分类号： B64C3/58

CPC分类号： B64C3/50 ,  B64C7/00 ,  B64C2003/145

摘要： A wing arrangement includes, but is not limited to an adjustable flap, which is adjustable between a retracted position and at least one extended position, has at least one fairing element for covering a flap adjustment mechanism and at least one cover element. The fairing element extends downstream at least as far as the flap and has, in a surface facing the flap, a cutout which correlates with an intended adjustment movement of the flap. The cover element is movably arranged with respect to the fairing element and adapted such to cover the cutout in the fairing element in the retracted position of the flap and expose at least part of said cutout in an extended position.

摘要翻译： 机翼装置包括但不限于在缩回位置和至少一个延伸位置之间可调整的可调节翼片，具有用于覆盖翼片调节机构和至少一个盖元件的至少一个整流罩元件。 整流罩元件至少延伸到翼片的下游，并且在面向翼片的表面中具有与翼片的预期调节运动相关的切口。 盖元件相对于整流罩元件可移动地布置，并且适于在折翼的缩回位置覆盖整流元件中的切口，并将所述切口的至少一部分暴露在延伸位置。