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165 条记录 (耗时 0.034 秒)

    Mechanical coupling for a rotor shaft assembly of dissimilar materials
    2.
    发明申请
    Mechanical coupling for a rotor shaft assembly of dissimilar materials 失效
    用于不同材料的转子轴组件的机械联轴器

    公开(公告)号：US20070237646A1

    公开(公告)日：2007-10-11

    申请号：US11221440

    申请日：2005-09-08

    申请人： Jun Shi ,  David Bombara ,  Kevin Green ,  Connic Bird ,  John Holowczak

    发明人： Jun Shi ,  David Bombara ,  Kevin Green ,  Connic Bird ,  John Holowczak

    IPC分类号： F04D29/00

    CPC分类号： F01D5/025 ,  F05B2260/301 ,  F05D2250/131 ,  F05D2250/232 ,  F05D2250/292

    摘要： A mechanical coupling for coupling a ceramic disc member to a metallic shaft includes a first wedge clamp and a second wedge clamp. A fastener engages a threaded end of a tie-bolt to sandwich the ceramic disc between the wedge clamps. An axial spring is positioned between the fastener and the second wedge clamp to apply an axial preload along the longitudinal axis. Another coupling utilizes a rotor shaft end of a metallic rotor shaft as one wedge clamp. Still another coupling includes a solid ceramic rotor disc with a multiple of tie-bolts radially displaced from the longitudinal axis to exert the preload on the solid ceramic rotor disc.

    摘要翻译： 用于将陶瓷盘构件耦合到金属轴的机械联接器包括第一楔形夹具和第二楔形夹具。 紧固件与衔铁螺栓的螺纹端接合以将陶瓷盘夹在楔形夹具之间。 轴向弹簧定位在紧固件和第二楔形夹具之间以沿着纵向轴线施加轴向预载荷。 另一个联轴器使用金属转子轴的转子轴端作为一个楔形夹。 另一个联接器包括固体陶瓷转子盘，其具有从纵向轴线径向偏移的多个连接螺栓，以将固体载荷施加在固体陶瓷转子盘上。

    CERAMIC MATRIX COMPOSITE SEAL SEGMENT FOR A GAS TURBINE ENGINE
    4.
    发明申请
    CERAMIC MATRIX COMPOSITE SEAL SEGMENT FOR A GAS TURBINE ENGINE 有权
    陶瓷基体复合材料密封段用于气体涡轮发动机

    公开(公告)号：US20160348528A1

    公开(公告)日：2016-12-01

    申请号：US14721705

    申请日：2015-05-26

    申请人： Daniel Kent Vetters ,  David J. Thomas ,  Ted Freeman ,  Douglas David Dierksmeier ,  Jun Shi ,  Todd Engel

    发明人： Daniel Kent Vetters ,  David J. Thomas ,  Ted Freeman ,  Douglas David Dierksmeier ,  Jun Shi ,  Todd Engel

    IPC分类号： F01D11/08 ,  F01D25/24

    CPC分类号： F01D11/08 ,  F01D9/04 ,  F01D25/24 ,  F01D25/246 ,  F05D2220/32 ,  F05D2240/24 ,  F05D2300/6033

    摘要： A ceramic matrix composite (CMC) seal segment for use in a segmented turbine shroud for radially encasing a turbine in a gas turbine engine. The CMC seal segment comprises an arcuate flange having a surface facing the turbine and a portion defining a bore for receiving an elongated pin, with the bore having a length that is at least 70% of the length of the elongated pin received therein. The CMC seal segment is carried by the carrier by at least one of the elongated pins being received within the bore. The CMC seal segment portion defining a pin-receiving bore is radially spaced from the arcuate flange by a spacing flange extending radially outward from the arcuate flange.

    摘要翻译： 一种陶瓷基体复合材料（CMC）密封段，用于分段涡轮机罩，用于在燃气涡轮发动机中径向包围涡轮机。 CMC密封段包括具有面向涡轮的表面的弧形凸缘和限定用于接收细长销的孔的部分，孔的长度为其中接收的细长销的长度的至少70％。 CMC密封段由载体承载，其中至少一个细长销被接收在孔内。 限定销接收孔的CMC密封段部分通过从弧形凸缘径向向外延伸的间隔凸缘与弓形凸缘径向间隔开。

    Method and apparatus for establishing communications in low signal to noise ratio environments
    8.
    发明授权
    Method and apparatus for establishing communications in low signal to noise ratio environments 有权
    用于在低信噪比环境下建立通信的方法和装置

    公开(公告)号：US08571494B2

    公开(公告)日：2013-10-29

    申请号：US12692099

    申请日：2010-01-22

    申请人： Petru Christian Budianu ,  Amal Ekbal ,  David Jonathan Julian ,  Jun Shi

    发明人： Petru Christian Budianu ,  Amal Ekbal ,  David Jonathan Julian ,  Jun Shi

    IPC分类号： H04B1/66

    CPC分类号： H04W76/10 ,  H04W8/005 ,  H04W84/18

    摘要： An apparatus is disclosed having a receiver configured to communicate, by a first apparatus, with a second apparatus in a first mode; determine side information by the first apparatus based on the communication during the first mode; and store the side information by the first apparatus for communication in a second mode with the second apparatus, wherein the first and second modes of communication have different date rates. A method for wireless communications is also disclosed.

    摘要翻译： 公开了一种装置，其具有被配置为以第一模式与第二装置通信的第一装置的接收器; 基于第一模式期间的通信确定第一装置的侧信息; 并且利用第二装置以第二模式存储第一装置进行通信的侧信息，其中第一和第二通信模式具有不同的日期速率。 还公开了一种用于无线通信的方法。

    Segmented ceramic matrix composite turbine airfoil component
    9.
    发明授权
    Segmented ceramic matrix composite turbine airfoil component 有权
    分段陶瓷基体复合涡轮机翼型件

    公开(公告)号：US08511980B2

    公开(公告)日：2013-08-20

    申请号：US13555877

    申请日：2012-07-23

    申请人： Tracy A. Propheter-Hinckley ,  Jun Shi

    发明人： Tracy A. Propheter-Hinckley ,  Jun Shi

    IPC分类号： F01D9/02

    CPC分类号： F01D5/284 ,  F01D5/3015 ,  F05D2240/80 ,  Y02T50/672 ,  Y02T50/673

    摘要： A segmented component for use with a gas turbine engine comprises a radially extending gas path portion. The gas path portion is for interacting with gas flow from the gas turbine engine. The gas path portion comprises a forward portion forming a leading edge of a stationary vane, an aft portion forming a trailing edge of the stationary vane, and a plurality of middle portions forming a pressure side and a suction side of the stationary vane. The component is divided into axially aligned segments comprising a forward segment, an aft segment, and a plurality of middle segments disposed between the forward segment and the aft segment. The middle segments comprise radially elongate ceramic matrix composite material plates.

    摘要翻译： 用于燃气涡轮发动机的分段部件包括径向延伸的气体路径部分。 气体路径部分用于与来自燃气涡轮发动机的气体流相互作用。 气体路径部包括形成静止叶片的前缘的前部，形成静止叶片的后缘的后部，以及形成静止叶片的压力侧和吸力侧的多个中间部。 该部件被分成轴向对准的段，其包括前段，后段和设置在前段和后段之间的多个中段。 中间段包括径向细长的陶瓷基复合材料板。