公开(公告)号：US09713437B2

公开(公告)日：2017-07-25

申请号：US14165253

申请日：2014-01-27

申请人： Larry W. Fullerton ,  John E. Greene ,  Tommy G. Nguyen ,  Eduardo Chi Sing

发明人： Larry W. Fullerton ,  John E. Greene ,  Tommy G. Nguyen ,  Eduardo Chi Sing

IPC分类号： A61B5/06 ,  A61B90/98 ,  A61B5/00 ,  A61B5/05 ,  A61B34/20 ,  A61B90/00

CPC分类号： A61B5/064 ,  A61B5/0507 ,  A61B5/4312 ,  A61B5/6847 ,  A61B90/39 ,  A61B2034/2048 ,  A61B2090/3908 ,  A61B2090/3925 ,  A61B2090/3966 ,  A61B2090/3975 ,  A61B2090/3987 ,  A61B2090/3991

摘要： Apparatus, systems, and methods are provided for localizing lesions within a patient's body, e.g., within a breast. The system includes a microwave antenna probe for transmitting and receiving electromagnetic signals to detect one or more markers that are implanted within or around the target tissue region. During use, the marker(s) are implanted into a target tissue region, and the microwave antenna probe is placed against the patient's skin to transmit a signal to the marker(s) and to receive the reflected signal from the marker(s) in order to determine the location of the marker(s). A tissue specimen, including the lesion and the marker(s), is then removed from the target tissue region based at least in part on the location information from the microwave antenna probe.

公开(公告)号：US20140309522A1

公开(公告)日：2014-10-16

申请号：US14165253

申请日：2014-01-27

申请人： Larry W. Fullerton ,  John E. Greene ,  Tommy G. Nguyen ,  Eduardo Chi Sing

发明人： Larry W. Fullerton ,  John E. Greene ,  Tommy G. Nguyen ,  Eduardo Chi Sing

IPC分类号： A61B5/06 ,  A61B19/00

CPC分类号： A61B5/064 ,  A61B5/0507 ,  A61B5/4312 ,  A61B5/6847 ,  A61B90/39 ,  A61B2034/2048 ,  A61B2090/3908 ,  A61B2090/3925 ,  A61B2090/3966 ,  A61B2090/3975 ,  A61B2090/3987 ,  A61B2090/3991

摘要： Apparatus, systems, and methods are provided for localizing lesions within a patient's body, e.g., within a breast. The system includes a microwave antenna probe for transmitting and receiving electromagnetic signals to detect one or more markers that are implanted within or around the target tissue region. During use, the marker(s) are implanted into a target tissue region, and the microwave antenna probe is placed against the patient's skin to transmit a signal to the marker(s) and to receive the reflected signal from the marker(s) in order to determine the location of the marker(s). A tissue specimen, including the lesion and the marker(s), is then removed from the target tissue region based at least in part on the location information from the microwave antenna probe.

摘要翻译： 提供了设备，系统和方法，用于定位患者身体内的损伤，例如在乳房内。 该系统包括用于发送和接收电磁信号的微波天线探针，以检测植入在靶组织区域内或周围的一个或多个标记。 在使用期间，将标记植入目标组织区域中，并且将微波天线探针放置在患者皮肤上以将信号传送到标记物并且从一个或多个标记物接收反射信号 以确定标记的位置。 至少部分地基于来自微波天线探针的位置信息，从目标组织区域中去除包括病变和标记物的组织标本。

公开(公告)号：US20110311353A1

公开(公告)日：2011-12-22

申请号：US13216347

申请日：2011-08-24

申请人： Brian P. Arness ,  John E. Greene ,  Sze Bun B. Chan

发明人： Brian P. Arness ,  John E. Greene ,  Sze Bun B. Chan

IPC分类号： F01D11/08

CPC分类号： F01D9/041 ,  F01D11/005 ,  F01D25/246 ,  F05D2220/3212 ,  F05D2230/64 ,  F05D2240/57 ,  F05D2250/182 ,  F05D2260/30 ,  F05D2300/505

摘要： A method for assembling a turbine nozzle assembly with respect to a combustor of a gas turbine engine is provided. The method includes coupling a radial outer retaining ring to an aft end of the combustor. A plurality of turbine nozzles is provided. Each turbine nozzle includes an inner band, a radially opposing outer band, and at least one vane extending between the inner band and the outer band. The outer band of each turbine nozzle is coupled to the outer retaining ring to define the turbine nozzle assembly. An inner retaining ring is positioned about an axis of the gas turbine engine and coupled to the inner band of each turbine nozzle.

摘要翻译： 提供了一种用于组装相对于燃气涡轮发动机的燃烧器的涡轮喷嘴组件的方法。 该方法包括将径向外保持环联接到燃烧器的后端。 提供多个涡轮喷嘴。 每个涡轮喷嘴包括内带，径向相对的外带，以及在内带和外带之间延伸的至少一个叶片。 每个涡轮喷嘴的外带连接到外保持环以限定涡轮喷嘴组件。 内部保持环围绕燃气涡轮发动机的轴线定位并且联接到每个涡轮喷嘴的内部带。

公开(公告)号：US08403634B2

公开(公告)日：2013-03-26

申请号：US13216347

申请日：2011-08-24

申请人： Brian P. Arness ,  John E. Greene ,  Sze Bun B. Chan

发明人： Brian P. Arness ,  John E. Greene ,  Sze Bun B. Chan

IPC分类号： F01D9/04

CPC分类号： F01D9/041 ,  F01D11/005 ,  F01D25/246 ,  F05D2220/3212 ,  F05D2230/64 ,  F05D2240/57 ,  F05D2250/182 ,  F05D2260/30 ,  F05D2300/505

摘要： A retaining seal assembly for use in a gas turbine engine is provided. The retaining seal assembly comprises an outer retaining ring coupled to an aft end of a gas turbine engine combustor. A turbine nozzle is coupled to the outer retaining ring and comprises an outer band. The outer band comprises a leading edge and an opposing trailing edge that defines a slot. A retention seal comprises a first end positioned within the slot, a generally opposing second end that contacts the outer retaining ring, and a body extending between the first end and the second end. The body further comprises an insertion portion positioned within a passage formed in the outer band. The retention seal is fabricated from a resilient material and is configured to facilitate coupling the turbine nozzle to the outer retaining ring.

摘要翻译： 提供了一种用于燃气轮机的保持密封组件。 保持密封组件包括联接到燃气涡轮发动机燃烧器的后端的外保持环。 涡轮喷嘴连接到外保持环并且包括外带。 外带包括前缘和限定槽的相对的后缘。 保持密封件包括定位在槽内的第一端，与外保持环接触的大致相对的第二端，以及在第一端和第二端之间延伸的本体。 主体还包括位于形成在外带中的通道内的插入部分。 保持密封件由弹性材料制成并且构造成便于将涡轮喷嘴连接到外保持环。

公开(公告)号：US07329093B2

公开(公告)日：2008-02-12

申请号：US11340577

申请日：2006-01-27

申请人： Thomas W. Vandeputte ,  John E. Greene ,  Peter C. Selent ,  Linda J. Farral ,  Sze Bun Brian Chan ,  Brian P. Arness

发明人： Thomas W. Vandeputte ,  John E. Greene ,  Peter C. Selent ,  Linda J. Farral ,  Sze Bun Brian Chan ,  Brian P. Arness

IPC分类号： F01D9/00

CPC分类号： F01D5/141 ,  F05D2240/128 ,  F05D2250/74 ,  Y10S416/02

摘要： First stage stator vanes for a turbine comprised airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in inches in Table I, which define a plurality of radially spaced profile sections forming the nominal profile. The Z coordinate values for each profile section are radial distances from the turbine axis to a portion of the surface of revolution about the axis containing the profile section. The X and Y values for each profile section are coordinate values which, when connected by smooth continuing arcs define the airfoil profile section along the surface of revolution portion. The radially spaced profile sections are joined smoothly with one another to form the nominal airfoil profile.

摘要翻译： 用于涡轮机的第一级定子叶片包括基本上按照表I中以英寸为单位的X，Y和Z的笛卡尔坐标值的翼型分布，其定义了形成标称轮廓的多个径向间隔的轮廓部分。 每个轮廓截面的Z坐标值是从涡轮机轴线到围绕围绕轮廓部分的轴线的旋转表面的一部分的径向距离。 每个轮廓截面的X和Y值是坐标值，当通过平滑的连续弧连接时，沿着旋转部分的表面限定翼型轮廓部分。 径向隔开的轮廓部分彼此平滑地连接以形成标称翼型轮廓。

公开(公告)号：US08038389B2

公开(公告)日：2011-10-18

申请号：US11325185

申请日：2006-01-04

申请人： Brian P. Arness ,  John E. Greene ,  Sze Bun B. Chan

发明人： Brian P. Arness ,  John E. Greene ,  Sze Bun B. Chan

IPC分类号： F01D9/04

CPC分类号： F01D9/041 ,  F01D11/005 ,  F01D25/246 ,  F05D2220/3212 ,  F05D2230/64 ,  F05D2240/57 ,  F05D2250/182 ,  F05D2260/30 ,  F05D2300/505

摘要： A turbine nozzle assembly and a method for assembling the turbine nozzle assembly with respect to a combustor of a gas turbine engine are provided. The method includes coupling a radial outer retaining ring to an aft end of the combustor. A plurality of turbine nozzles are provided. Each turbine nozzle includes an inner band, a radially opposing outer band, and at least one vane extending between the inner band and the outer band. The outer band of each turbine nozzle is coupled to the outer retaining ring to define the turbine nozzle assembly. An inner retaining ring is positioned about an axis of the gas turbine engine and coupled to the inner band of each turbine nozzle.

摘要翻译： 提供了一种涡轮喷嘴组件和用于将涡轮喷嘴组件相对于燃气涡轮发动机的燃烧器组装的方法。 该方法包括将径向外保持环联接到燃烧器的后端。 提供多个涡轮喷嘴。 每个涡轮喷嘴包括内带，径向相对的外带，以及在内带和外带之间延伸的至少一个叶片。 每个涡轮喷嘴的外带连接到外保持环以限定涡轮喷嘴组件。 内部保持环围绕燃气涡轮发动机的轴线定位并且联接到每个涡轮喷嘴的内部带。