利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

20 条记录 (耗时 0.024 秒)

    Handrail guide assembly for escalator newel
    1.
    发明授权
    Handrail guide assembly for escalator newel 失效
    扶手扶手导轨组件

    公开(公告)号：US5366061A

    公开(公告)日：1994-11-22

    申请号：US998098

    申请日：1992-12-30

    申请人： Michael Kruse ,  Hans-Dietrich Riedel

    发明人： Michael Kruse ,  Hans-Dietrich Riedel

    IPC分类号： B66B23/24 ,  B66B23/22 ,  B65G15/00

    CPC分类号： B66B23/22

    摘要： The moving handrail of an escalator or moving walkway is guided around the curved newel of the escalator balustrade by a plastic guide system. A metal base member is frictionally fitted onto the outer edge of the glass balustrade. An extruded aluminum profile is mounted in the upper and outer surface of the base. A series of spaced pads formed from a low coefficient of friction plastic are fixed to the profile to form the contact sliding surface for the handrail.

    摘要翻译： 自动扶梯或移动式走道的移动扶手通过塑料引导系统引导到自动扶梯栏杆的弧形底板周围。 金属底座摩擦配合在玻璃栏杆的外边缘上。 挤压铝型材安装在基座的上表面和外表面上。 由低摩擦系数塑料形成的一系列间隔垫片固定在轮廓上，以形成扶手的接触滑动面。

    Escalator/people mover bearing
    2.
    发明授权
    Escalator/people mover bearing 失效
    自动扶梯/人移动轴承

    公开(公告)号：US5072821A

    公开(公告)日：1991-12-17

    申请号：US624006

    申请日：1990-12-07

    申请人： Michael Kruse ,  Hans-Dietrich Riedel

    发明人： Michael Kruse ,  Hans-Dietrich Riedel

    IPC分类号： B66B23/02 ,  B66B23/12

    CPC分类号： F16C33/04 ,  B66B23/02 ,  B66B23/12

    摘要： An escalator or people mover having steps or pallets which are supported by axles that are driven by a step chain, utilize a split bearing disposed between the axle and the step or pallet. The split bearing allows for rapid replacement of a worn bearing. The split bearing has a shaped outer portion for cooperating with the step or pallet to prevent rotation of the bearing relative to the step.

    OSTEOINDUCTIVE MATERIALS
    3.
    发明申请
    OSTEOINDUCTIVE MATERIALS 有权
    机械材料

    公开(公告)号：US20090155366A1

    公开(公告)日：2009-06-18

    申请号：US12336895

    申请日：2008-12-17

    申请人： Jens POHL ,  Rolf Bechtold ,  Michael Kruse

    发明人： Jens POHL ,  Rolf Bechtold ,  Michael Kruse

    IPC分类号： A61K38/00 ,  A61K9/00 ,  A61P17/02 ,  A61K38/18

    CPC分类号： C07K14/51 ,  A61L27/34 ,  A61L27/56 ,  A61L2430/02 ,  C07K14/475 ,  C07K14/495 ,  C08L89/00

    摘要： The present invention concerns improved osteoinductive materials comprising matrix materials and morphogenetic roteins, wherein depending on the subject matter the proteins may be dimeric or monomeric proteins. The osteoinductive materials according to the present invention have improved properties. The invention further concerns methods for producing the respective improved osteoinductive materials.

    摘要翻译： 本发明涉及包含基质材料和形态发生蛋白质的改进的骨诱导材料，其中取决于主题，蛋白质可以是二聚体或单体蛋白质。 根据本发明的骨诱导材料具有改善的性质。 本发明还涉及生产各种改进的骨诱导材料的方法。

    Combplate with a wear resistant coating
    4.
    发明授权
    Combplate with a wear resistant coating 失效
    搭配耐磨涂层

    公开(公告)号：US5370213A

    公开(公告)日：1994-12-06

    申请号：US92175

    申请日：1993-07-15

    申请人： Hermann W. Ahls ,  Michael Kruse

    发明人： Hermann W. Ahls ,  Michael Kruse

    IPC分类号： B66B29/00 ,  B66B29/06

    CPC分类号： B66B29/06

    摘要： A combplate for a people moving device is provided having a body with a top surface and a bottom surface, a comb having a plurality of fingers, and a wear resistant polymeric coating, having a color, bonded to the combplate and made of a thermal setting plasticized polyvinylchloride plastic.

    摘要翻译： 提供了一种用于人员移动装置的梳板，具有具有顶表面和底表面的主体，具有多个指状物的梳子和具有粘合到梳板上并由热定形制成的具有颜色的耐磨聚合物涂层 塑化聚氯乙烯塑料。

    LOAD INTRODUCTION STRUCTURE, IN PARTICULAR A LINING FRAME, FOR AN AIRCRAFT
    6.
    发明申请
    LOAD INTRODUCTION STRUCTURE, IN PARTICULAR A LINING FRAME, FOR AN AIRCRAFT 有权
    负载引言结构，特别是一个内置的框架，用于飞机

    公开(公告)号：US20100038486A1

    公开(公告)日：2010-02-18

    申请号：US12512477

    申请日：2009-07-30

    申请人： Hermann Benthien ,  Michael Kruse

    发明人： Hermann Benthien ,  Michael Kruse

    IPC分类号： B64C1/00 ,  B64C1/06

    CPC分类号： B64C1/061 ,  B64C1/066

    摘要： The invention relates to a load introduction structure for an aircraft, comprising two lateral frames which are arranged opposite one another in the two lateral regions of a fuselage airframe structure of the aircraft and adjoin a continuous floor surface which rests on a floor frame. The two lateral frames are connected via the top thereof by a ceiling frame, the ceiling frame being suspended from a ceiling region of the fuselage airframe structure. Each lateral frame is divided into at least two lateral frame segments. At least three track portions which extend parallel to a longitudinal axis of the aircraft are arranged on each lateral frame segment. The lateral frames are connected to the fuselage airframe structure, the ring frames in particular, by a plurality of x-rods, y-rods and y-cardan rods. The load introduction structure is largely uncoupled according to the invention from the fuselage airframe structure of the aircraft inter alia by a plurality of coupling members arranged between the track portions to form gaps in order to compensate for load-induced and/or thermally-induced deformations, in particular changes in length, of the fuselage airframe structure.

    摘要翻译： 本发明涉及一种用于飞行器的载荷引入结构，包括两个横向框架，它们在机身的机身机身结构的两个横向区域中彼此相对布置并且邻接在搁置在地板框架上的连续地板表面上。 两个横向框架通过其顶部通过天花板框架连接，天花板框架从机身机身结构的天花板区域悬挂。 每个横向框架被分成至少两个横向框架段。 至少三个平行于飞行器的纵向轴线延伸的轨道部分布置在每个横向框架段上。 横向框架通过多个x杆，Y杆和y-万向棒连接到机身机身结构，特别是环形框架。 根据本发明，负载引入结构根据本发明从飞机的机身机身结构中大体上脱离，尤其是通过布置在轨道部分之间的多个联接构件形成间隙，以便补偿负载引起的和/或热诱导的变形 ，特别是长度的变化，机身机身结构。

    Roll stand arrangement for a single wire rolling mill train
    9.
    发明授权
    Roll stand arrangement for a single wire rolling mill train 失效
    轧机机架单列轧机列车

    公开(公告)号：US06216515B1

    公开(公告)日：2001-04-17

    申请号：US09533474

    申请日：2000-03-23

    申请人： Rüdiger Grimmel ,  Michael Kruse

    发明人： Rüdiger Grimmel ,  Michael Kruse

    IPC分类号： B21B4104

    CPC分类号： B21B39/18 ,  B21B1/18 ,  B21B2201/06

    摘要： A roll stand arrangement for a single wire rolling mill train, and including arranged along a main pitch line, a multi-stand finishing block, a multi-stand post finishing block located downstream of the finishing block, and a pitch line change-over unit arranged between the finishing block and the post finishing block for advancing a wire strand from the finishing block to the post finishing block directly or through a looping pitch line in which there are provided a cooling zone, a wire looper, and a looping table.

    摘要翻译： 一种用于单丝轧机机组的轧机机架装置，并且包括沿主间距线布置的多机架精加工机组，位于精加工机组下游的多机架后精加工机组，以及变桨线转换单元 布置在精加工块和后整理块之间，用于将线材从精加工块直接或通过环形节距线直接提供到后端整理块，其中设置有冷却区，导线器和环形台。

    Load introduction structure, in particular a lining frame, for an aircraft
    10.
    发明授权
    Load introduction structure, in particular a lining frame, for an aircraft 有权
    负载引导结构，特别是用于飞行器的衬里框架

    公开(公告)号：US08376276B2

    公开(公告)日：2013-02-19

    申请号：US12512477

    申请日：2009-07-30

    申请人： Hermann Benthien ,  Michael Kruse

    发明人： Hermann Benthien ,  Michael Kruse

    IPC分类号： B64C1/00

    CPC分类号： B64C1/061 ,  B64C1/066

    摘要： The invention relates to a load introduction structure for an aircraft, comprising two lateral frames which are arranged opposite one another in the two lateral regions of a fuselage airframe structure of the aircraft and adjoin a continuous floor surface which rests on a floor frame. The two lateral frames are connected via the top thereof by a ceiling frame, the ceiling frame being suspended from a ceiling region of the fuselage airframe structure. Each lateral frame is divided into at least two lateral frame segments. At least three track portions which extend parallel to a longitudinal axis of the aircraft are arranged on each lateral frame segment. The lateral frames are connected to the fuselage airframe structure, the ring frames in particular, by a plurality of x-rods, y-rods and y-cardan rods. The load introduction structure is largely uncoupled according to the invention from the fuselage airframe structure of the aircraft inter alia by a plurality of coupling members arranged between the track portions to form gaps in order to compensate for load-induced and/or thermally-induced deformations, in particular changes in length, of the fuselage airframe structure.

    摘要翻译： 本发明涉及一种用于飞行器的载荷引入结构，包括两个横向框架，它们在机身的机身机身结构的两个横向区域中彼此相对布置并且邻接在搁置在地板框架上的连续地板表面上。 两个横向框架通过其顶部通过天花板框架连接，天花板框架从机身机身结构的天花板区域悬挂。 每个横向框架被分成至少两个横向框架段。 至少三个平行于飞行器的纵向轴线延伸的轨道部分布置在每个横向框架段上。 横向框架通过多个x杆，y杆和y-万向棒连接到机身机身结构，特别是环形框架。 根据本发明，负载引入结构根据本发明从飞机的机身机身结构中大体上脱离，尤其是通过布置在轨道部分之间的多个联接构件形成间隙，以便补偿负载引起的和/或热诱导的变形 ，特别是长度的变化，机身机身结构。