利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

10 条记录 (耗时 0.009 秒)

    INTEGRATED BEARING ASSEMBLIES FOR GUIDED ATTACK ROCKETS
    2.
    发明申请
    INTEGRATED BEARING ASSEMBLIES FOR GUIDED ATTACK ROCKETS 有权
    集成轴承组件用于引导攻击轴

    公开(公告)号：US20160010685A1

    公开(公告)日：2016-01-14

    申请号：US14468677

    申请日：2014-08-26

    申请人： ROLLER BEARING COMPANY OF AMERICA, INC.

    发明人： Alex Habibvand

    IPC分类号： F16C25/06 ,  F42B15/01 ,  F16C19/54

    CPC分类号： F16C25/06 ,  F16C19/163 ,  F16C19/548 ,  F16C2226/60 ,  F16C2240/14 ,  F42B15/01 ,  F42B15/36

    摘要： A guide mechanism, configured for use with a guided attack rocket, includes an inner housing partially disposed in an outer housing. The inner and outer housings each define a forward end and an aft end. A first angular contact bearing is positioned between the outer housing forward end and the inner housing forward end. A second angular contact bearing is positioned between the outer housing aft end and the inner housing aft end. A retaining nut is received over the inner housing forward end. The retaining nut preloads the first and second angular contact bearings. Each of the angular contact bearings includes an inner member disposed within an outer member. The outer member defines an outer raceway and the inner member defines an inner raceway. A plurality of rolling elements is disposed between the outer raceway and the inner raceway.

    摘要翻译： 构造成与引导式攻击火箭一起使用的引导机构包括部分地设置在外壳中的内壳。 内壳体和外壳体每个限定前端和后端。 第一角接触轴承定位在外壳前端和内壳前端之间。 第二角接触轴承位于外壳体后端和内壳体后端之间。 保持螺母容纳在内壳前端上。 保持螺母预加载第一和第二角接触轴承。 每个角接触轴承包括设置在外部构件内部的内部构件。 外部构件限定外部滚道，并且内部构件限定内部滚道。 多个滚动元件设置在外滚道和内滚道之间。

    Integrated bearing assemblies for guided attack rockets
    5.
    发明授权
    Integrated bearing assemblies for guided attack rockets 有权
    导向攻击火箭的集成轴承组件

    公开(公告)号：US09453531B2

    公开(公告)日：2016-09-27

    申请号：US14468677

    申请日：2014-08-26

    申请人： Roller Bearing Company of America, Inc.

    发明人： Alex Habibvand

    IPC分类号： F16C19/54 ,  F16C25/06 ,  F42B15/01 ,  F42B15/36 ,  F16C19/16

    CPC分类号： F16C25/06 ,  F16C19/163 ,  F16C19/548 ,  F16C2226/60 ,  F16C2240/14 ,  F42B15/01 ,  F42B15/36

    摘要： A guide mechanism, configured for use with a guided attack rocket, includes an inner housing partially disposed in an outer housing. The inner and outer housings each define a forward end and an aft end. A first angular contact bearing is positioned between the outer housing forward end and the inner housing forward end. A second angular contact bearing is positioned between the outer housing aft end and the inner housing aft end. A retaining nut is received over the inner housing forward end. The retaining nut preloads the first and second angular contact bearings. Each of the angular contact bearings includes an inner member disposed within an outer member. The outer member defines an outer raceway and the inner member defines an inner raceway. A plurality of rolling elements is disposed between the outer raceway and the inner raceway.

    摘要翻译： 构造成与引导式攻击火箭一起使用的引导机构包括部分地设置在外壳中的内壳。 内壳体和外壳体每个限定前端和后端。 第一角接触轴承定位在外壳前端和内壳前端之间。 第二角接触轴承位于外壳体后端和内壳体后端之间。 保持螺母容纳在内壳前端上。 保持螺母预加载第一和第二角接触轴承。 每个角接触轴承包括设置在外部构件内部的内部构件。 外部构件限定外部滚道，并且内部构件限定内部滚道。 多个滚动元件设置在外滚道和内滚道之间。

    BEARING ARRANGEMENT OF A WIND TURBINE AND METHOD FOR ADJUSTING THE PRELOAD OF A BEARING ARRANGEMENT
    7.
    发明申请
    BEARING ARRANGEMENT OF A WIND TURBINE AND METHOD FOR ADJUSTING THE PRELOAD OF A BEARING ARRANGEMENT 有权
    风力涡轮机的轴承装配和调整轴承装置的推进方法

    公开(公告)号：US20150030277A1

    公开(公告)日：2015-01-29

    申请号：US14513531

    申请日：2014-10-14

    申请人： Eolotec GmbH

    发明人： Mathias PICK ,  Wolfgang LOSERT

    IPC分类号： F03D11/00 ,  F16C41/02 ,  F16C19/38

    CPC分类号： F03D11/0008 ,  F03D80/70 ,  F05B2240/50 ,  F16C19/364 ,  F16C19/38 ,  F16C19/548 ,  F16C25/06 ,  F16C37/007 ,  F16C41/02 ,  F16C2229/00 ,  F16C2240/14 ,  F16C2300/14 ,  F16C2360/31 ,  Y02E10/722 ,  Y02P70/523

    摘要： To facilitate adjusting a bearing arrangement, particularly in a wind turbine, for different operating situations, the bearing arrangement has an adjusting device with which the bearing preload can be adjusted starting from a base preload. This can allow, for example signs of wear to be compensated, manufacturing tolerances or design inaccuracies to be corrected and in particular current loading states to be addressed. This design avoids the otherwise usual overdimensioning of the bearing arrangement, thereby increasing the efficiency of the wind turbine as well as the service life of the bearing arrangement.

    摘要翻译： 为了便于调整轴承装置，特别是在风力涡轮机中，为了不同的运行情况，轴承装置具有调节装置，通过该调节装置可以从基础预载荷开始调节轴承预载荷。 这可以允许例如要补偿的磨损迹象，制造公差或要校正的设计不准确度，特别是要解决的当前负载状态。 这种设计避免了通常的轴承装置的超大尺寸，从而提高了风力涡轮机的效率以及轴承装置的使用寿命。

    BEARING PRELOADING DEVICE
    9.
    发明申请
    BEARING PRELOADING DEVICE 有权
    轴承推进装置

    公开(公告)号：US20160290394A1

    公开(公告)日：2016-10-06

    申请号：US15035562

    申请日：2014-10-31

    申请人： NTN CORPORATION

    发明人： Yasuhiro SHIMIZU

    IPC分类号： F16C25/08 ,  F16C33/60 ,  F16C19/38

    CPC分类号： F16C25/083 ,  F16C19/385 ,  F16C33/586 ,  F16C33/60 ,  F16C33/783 ,  F16C33/7886 ,  F16C2226/60 ,  F16C2229/00 ,  F16C2240/14 ,  F16C2322/12

    摘要： In a bearing preloading device in which a compression coil spring is used, a hole is formed in a bearing race or in a separate member from the bearing race, the separate member being axially opposed to the bearing race. The hole has an inner periphery constituted by a threaded portion connected to the bottom surface of the hole, and a shallow hole portion connected to the edge of the hole, and having an inner diameter larger than that of the threaded portion. By axially screwing the compression coil spring into the threaded portion so as to be threadedly engaged in the threaded portion, it is possible to easily prevent the compression coil spring from being pulled out.

    摘要翻译： 在使用压缩螺旋弹簧的轴承预加载装置中，在轴承座圈或与轴承座圈分开的构件中形成有孔，该分离构件与轴承座轴向相对。 所述孔具有由与所述孔的底面连接的螺纹部构成的内周面和与所述孔的边缘连接并且具有比所述螺纹部的内径大的内径的浅孔部。 通过将压缩螺旋弹簧轴向旋入到螺纹部分中以与螺纹部分螺纹接合，可以容易地防止压缩螺旋弹簧被拉出。

    METHOD FOR MEASURING A PRELOADING FORCE AND BEARING ASSEMBLY FOR PERFORMING THE METHOD
    10.
    发明申请
    METHOD FOR MEASURING A PRELOADING FORCE AND BEARING ASSEMBLY FOR PERFORMING THE METHOD 有权
    用于测量推进力的方法和用于执行该方法的轴承组件

    公开(公告)号：US20160215816A1

    公开(公告)日：2016-07-28

    申请号：US14913535

    申请日：2014-08-20

    申请人： SCHAEFFLER TECHNOLOGIES AG & CO. KG

    发明人： Alexander Hofmann ,  Rainer Gebauer

    IPC分类号： F16C19/52 ,  F16C41/00

    CPC分类号： F16C19/522 ,  F16C33/585 ,  F16C41/00 ,  F16C41/007 ,  F16C41/008 ,  F16C2208/34 ,  F16C2229/00 ,  F16C2240/14

    摘要： A method for determining at least one preloading force (K) acting between a carrying body (7) and a rolling-element bearing (2) of a bearing assembly (1), which rolling-element bearing is mounted on the carrying body, and the bearing assembly includes the rolling-element bearing and the at least one sensor device (3). The sensor device is arranged in or on the rolling-element bearing in an installation position (E1) and is coupled to an evaluating device (10) in a signaling manner. The sensor device senses the preloading force, produces at least one signal (S) in accordance with the preloading force, and transmits the signal to the evaluating device, and the evaluating device evaluates the signal in order to measure the preloading force and the sensor device is permanently decoupled from the evaluating device after the evaluation of the signal.

    摘要翻译： 一种用于确定作用在轴承组件（1）的承载体（7）和滚动体轴承（2）之间的至少一个预加载力（K）的方法，该滚动元件轴承安装在承载体上，以及 轴承组件包括滚动元件轴承和至少一个传感器装置（3）。 传感器装置布置在安装位置（E1）中的滚动元件轴承中或其上，并且以信令方式耦合到评估装置（10）。 传感器装置感测预加载力，根据预加载力产生至少一个信号（S），并将该信号发送到评估装置，并且评估装置评估信号以便测量预加载力和传感器装置 在评估信号后，与评估装置永久解耦。