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14 条记录 (耗时 0.038 秒)

    Gas turbine exhaust case
    4.
    发明授权
    Gas turbine exhaust case 有权
    燃气轮机排气箱

    公开(公告)号：US08826669B2

    公开(公告)日：2014-09-09

    申请号：US13292289

    申请日：2011-11-09

    申请人： Richard Bouchard ,  John Pietrobon ,  Eric Durocher

    发明人： Richard Bouchard ,  John Pietrobon ,  Eric Durocher

    IPC分类号： F02C7/08 ,  F03G1/00 ,  F02G3/00 ,  F02K1/82 ,  F02C7/24

    CPC分类号： F02C7/24 ,  F02K1/04 ,  F02K1/78 ,  F02K1/80 ,  F02K1/827

    摘要： A turbine exhaust case for a turbofan engine comprises a plurality of arcuate acoustic panels assembled into a circumferentially extending inner shroud with circumferential gaps between adjacent acoustic panels. An outer shroud extends circumferentially about the inner shroud. The inner shroud and the outer shroud define an annular gaspath therebetween. A plurality of circumferentially spaced-apart exhaust struts extends radially across the annular gaspath and structurally connects the individual acoustic panels forming the inner shroud to the outer shroud.

    摘要翻译： 用于涡轮风扇发动机的涡轮机排气箱包括组装成周向延伸的内护罩的多个弓形声波面板，在相邻的声学面板之间具有圆周间隙。 外护罩围绕内护罩周向延伸。 内护罩和外护罩在其间限定了环形气路。 多个周向间隔开的排气支柱径向延伸穿过环形气体路径，并将构成内护罩的各个隔音板结构连接到外护罩上。

    Seal arrangement for segmented gas turbine engine components
    6.
    发明授权
    Seal arrangement for segmented gas turbine engine components 有权
    分段燃气涡轮发动机部件的密封装置

    公开(公告)号：US09534500B2

    公开(公告)日：2017-01-03

    申请号：US13094916

    申请日：2011-04-27

    申请人： Richard Bouchard ,  John Pietrobon

    发明人： Richard Bouchard ,  John Pietrobon

    IPC分类号： F16J15/02 ,  F01D9/04 ,  F01D11/00 ,  F16J15/06 ,  F16J15/08

    CPC分类号： F01D9/04 ,  F01D11/003 ,  F05D2240/11 ,  F05D2250/75 ,  F16J15/065 ,  F16J15/0812 ,  F16J15/0881

    摘要： A seal arrangement for segmented turbine components comprises a sealing strip and a resilient cord element compressed against the strip to provide positive loading of the strip against the segment sealing faces. The sealing strip and the resilient cord element are engaged in confronting cavities defined in the end faces of adjacent segments. The resilient cord element is commonly held by both segments in a compressed state against the sealing strip.

    摘要翻译： 用于分段涡轮机部件的密封装置包括密封条和压缩在条带上的弹性绳索元件，以提供条带抵靠部分密封面的正负载。 密封条和弹性绳索元件接合在相邻段的端面中限定的相对的空腔中。 弹性绳索元件通常由压缩状态的两个段保持抵靠密封条。

    Strut mounting arrangement for gas turbine exhaust case
    7.
    发明授权
    Strut mounting arrangement for gas turbine exhaust case 有权
    燃气轮机排气箱支柱安装

    公开(公告)号：US08944753B2

    公开(公告)日：2015-02-03

    申请号：US13292295

    申请日：2011-11-09

    申请人： Richard Bouchard ,  Daniel Trottier ,  Gaetan Girard

    发明人： Richard Bouchard ,  Daniel Trottier ,  Gaetan Girard

    IPC分类号： F01D25/28 ,  F01D9/06

    CPC分类号： F01D25/28 ,  F01D9/06 ,  F05D2240/62 ,  F05D2300/5021

    摘要： A turbine exhaust case comprises inner and outer annular shrouds defining therebetween an annular hot gaspath. A circumferential array of exhaust struts extends across the gaspath. The exhaust struts are mounted at one radial end thereof on a flexible strut mounting structure. The flexible strut mounting structure is radially deflectable relative to the outer and inner shrouds to accommodate thermal expansion of the exhaust struts during engine operation.

    摘要翻译： 涡轮机排气箱包括在其间限定环形热气路径的内环和外环。 排气支柱的圆周阵列延伸穿过气路。 排气支柱在其一个径向端部安装在柔性支柱安装结构上。 柔性支柱安装结构相对于外护罩和内护罩可径向偏转，以适应发动机运行期间排气支柱的热膨胀。

    Gas turbine engine exhaust mixer
    8.
    发明授权
    Gas turbine engine exhaust mixer 有权
    燃气轮机发动机排气混合机

    公开(公告)号：US08739513B2

    公开(公告)日：2014-06-03

    申请号：US12858313

    申请日：2010-08-17

    申请人： Guy Lefebvre ,  Nicolas Grivas ,  Richard Bouchard ,  Denis Leclair ,  Eric Durocher

    发明人： Guy Lefebvre ,  Nicolas Grivas ,  Richard Bouchard ,  Denis Leclair ,  Eric Durocher

    IPC分类号： F02C7/08 ,  F02G1/00 ,  F02G3/00 ,  F02C7/20

    CPC分类号： F02K1/386 ,  F01D9/04 ,  F02K1/48 ,  F02K1/80 ,  F05D2220/32 ,  F05D2230/642 ,  F05D2240/10 ,  F05D2240/127 ,  Y02T50/671

    摘要： An exhaust mixer for a gas turbine engine includes an annular wall having upstream end adapted to be fastened to an engine case and a downstream end forming a plurality of inner and outer mixer lobes. A support member interconnects at least a number of the inner lobes, and includes a circumferentially extending stiffener ring located radially inwardly from the inner lobes and a series of circumferentially spaced apart mixer struts radially extending from the inner lobes to the stiffener ring. The mixer struts have a radial length at least equal to a width of a main gas path defined between the inner lobes and the exhaust cone such that the mixer struts extend entirely through the main gas path. The stiffener ring being fixed solely to the mixer struts such as to float with respect to the exhaust cone and permit relative movement therebetween.

    摘要翻译： 用于燃气涡轮发动机的排气混合器包括具有适于紧固到发动机壳体的上游端的环形壁和形成多个内部和外部混合器凸角的下游端。 支撑构件互连至少多个内裂片，并且包括从内裂片径向向内定位的周向延伸的加强环，以及一系列周向间隔开的从内裂纹到加强环径向延伸的混合器支柱。 混合器支柱具有至少等于限定在内部叶片和排气锥体之间的主气体通道的宽度的径向长度，使得混合器支柱完全延伸穿过主气体路径。 加强环仅被固定到混合器支柱上，以便相对于排气锥体浮动并允许它们之间的相对运动。

    SYSTEM FOR MONITORING, DETERMINING, AND REPORTING DIRECTIONAL SPECTRA OF OCEAN SURFACE WAVES IN NEAR REAL-TIME FROM A MOORED BUOY
    9.
    发明申请
    SYSTEM FOR MONITORING, DETERMINING, AND REPORTING DIRECTIONAL SPECTRA OF OCEAN SURFACE WAVES IN NEAR REAL-TIME FROM A MOORED BUOY 有权
    近海实时监测，确定和报告海洋表面波的方向谱的系统

    公开(公告)号：US20110060525A1

    公开(公告)日：2011-03-10

    申请号：US12554910

    申请日：2009-09-06

    申请人： Chung-Chu Teng ,  Rodney Riley ,  Richard Bouchard

    发明人： Chung-Chu Teng ,  Rodney Riley ,  Richard Bouchard

    IPC分类号： G06F19/00 ,  B63B22/24

    CPC分类号： B63B22/00 ,  B63B2022/006 ,  B63B2211/02 ,  G01C13/002

    摘要： A moored buoy floating at the ocean surface and anchored to the seafloor precisely measures acceleration, pitch, roll, and Earth's magnetic flux field of the buoy over a limited sampling period. The system includes: 1) A buoy, 2) A mooring system, 3) An electronic data logger controlling communications between the system and the on-board remote telecommunications system, 4) an embedded computer for data input/output, temporary or permanent data storage, and algorithms to convert the measured time series data into surface ocean wave spectra and quality assurance statistics and encode the results for transfer to the data logger, 5) Sensors include one or three acceleration sensors, three orthogonal angular rate sensors, and three orthogonal magnetometers to measure the Earth's magnetic flux field, 6) A telecommunications system that links the buoy data logger and a shoreside processing system, and 7) A shoreside processing system that decodes the transmitted data, performs, quality control, and computes derived wave parameters.

    摘要翻译： 漂浮在海洋表面并锚定到海底的系泊浮标在有限的采样周期内精确测量浮标的加速度，俯仰，滚动和地球的磁通场。 该系统包括：1）浮标，2）系泊系统; 3）控制系统与车载远程通信系统之间通信的电子数据记录器; 4）嵌入式计算机，用于数据输入/输出，临时或永久数据 存储和算法将测量的时间序列数据转换为表面海洋波谱和质量保证统计信息，并将结果编码以传输到数据记录器; 5）传感器包括一个或三个加速度传感器，三个正交角速率传感器和三个正交 测量地球磁通场的磁力计，6）连接浮标数据记录器和岸边处理系统的电信系统，以及7）解码传输数据的后台处理系统，执行质量控制和计算派生波参数。

    Gas turbine exhaust case with acoustic panels
    10.
    发明授权
    Gas turbine exhaust case with acoustic panels 有权
    带声学面板的燃气轮机排气箱

    公开(公告)号：US09200537B2

    公开(公告)日：2015-12-01

    申请号：US13292277

    申请日：2011-11-09

    申请人： Richard Bouchard ,  Gaetan Girard ,  Christian Pronovost

    发明人： Richard Bouchard ,  Gaetan Girard ,  Christian Pronovost

    IPC分类号： F01D25/06 ,  F01D25/04 ,  F02C7/20 ,  F02C7/045 ,  F01D25/16 ,  F02K1/82

    CPC分类号： F01D25/162 ,  F02C7/20 ,  F02K1/827 ,  Y10T29/49323

    摘要： A turbine exhaust case for a gas turbine engine has an outer shroud and an inner shroud concentrically defining therebetween an annular gaspath for channelling hot gases. A plurality of circumferentially spaced-apart turbine exhaust struts extends radially across the hot gaspath. The inner shroud may be provided in the form of an acoustic panel. The acoustic panel has a radially outwardly facing surface defining the radially inner flow boundary surface of the gaspath. The acoustic panel is mechanically fastened to the radially inner end of the struts.

    摘要翻译： 用于燃气涡轮发动机的涡轮机排气箱具有外护罩和内护套，同心地在其间限定用于引导热气体的环形气路。 多个周向间隔开的涡轮排气支柱径向延伸穿过热气路径。 内护罩可以以声学板的形式设置。 声学面板具有限定气体路径的径向内部流动边界表面的径向向外表面。 声学面板机械地紧固到支柱的径向内端。