公开(公告)号：US20070128033A1

公开(公告)日：2007-06-07

申请号：US11294210

申请日：2005-12-05

申请人： Ching-Pang Lee ,  Aspi Wadia ,  John Brauer

发明人： Ching-Pang Lee ,  Aspi Wadia ,  John Brauer

IPC分类号： F01D5/18

CPC分类号： F01D5/20 ,  F05D2250/29 ,  F05D2250/292 ,  Y02T50/673

摘要： A turbine airfoil includes opposite pressure and suction sidewalls, and extends in chord between opposite leading and trailing edges and in span from a root to an outer tip cap. The tip cap bridges the sidewalls, and a flute extends chordally along the pressure sidewall and below the tip cap.

公开(公告)号：US20060005546A1

公开(公告)日：2006-01-12

申请号：US10885147

申请日：2004-07-06

申请人： Robert Orlando ,  Thomas Moniz ,  John Brauer ,  Ian Prentice ,  Erich Krammer ,  James Dolan ,  Robert Frederick

发明人： Robert Orlando ,  Thomas Moniz ,  John Brauer ,  Ian Prentice ,  Erich Krammer ,  James Dolan ,  Robert Frederick

IPC分类号： F02C7/12

CPC分类号： F01D9/065 ,  F02C6/08

摘要： A gas turbine engine includes a compressor powered by a turbine. The turbine includes a nozzle having vanes extending between outer and inner bands. Each vane includes an internal cooling plenum and a bypass tube extending through the bands. First and second manifolds surround the outer band and are disposed in flow communication with the plenums and bypass tubes, respectively. A bleed circuit joins the compressor to the manifolds for providing pressurized air thereto. A control valve modulates airflow to the first manifold and in turn through the cooling plenums of the vanes.

摘要翻译： 燃气涡轮发动机包括由涡轮机供电的压缩机。 涡轮机包括具有在外带和内带之间延伸的叶片的喷嘴。 每个叶片包括一个内部冷却通风室和一个延伸穿过该带的旁通管。 第一和第二歧管围绕外部带并分别设置成与集气室和旁通管流动连通。 泄放回路将压缩机连接到歧管，以向其提供加压空气。 控制阀调节到第一歧管的气流，并依次通过叶片的冷却增压室。

公开(公告)号：US20050252194A1

公开(公告)日：2005-11-17

申请号：US10845032

申请日：2004-05-13

申请人： Robert Orlando ,  Thomas Moniz ,  John Brauer ,  John Henry ,  Raymond Patt ,  Randy Vondrell ,  James Dolan ,  Erich Krammer ,  David Kirk

发明人： Robert Orlando ,  Thomas Moniz ,  John Brauer ,  John Henry ,  Raymond Patt ,  Randy Vondrell ,  James Dolan ,  Erich Krammer ,  David Kirk

IPC分类号： F02C3/04 ,  F02C3/13 ,  F02C7/00 ,  F02C9/18

CPC分类号： F02C3/13 ,  F02C3/04 ,  F05D2230/60

摘要： A method facilitates assembling a gas turbine engine including a compressor and a rotor assembly coupled in axial flow communication downstream from the compressor. The method comprises coupling a bypass system in flow communication with the compressor to channel a portion of flow discharged from the compressor towards the rotor assembly is channeled through the bypass system, and coupling a downstream end of the bypass system within the gas turbine engine such that the flow entering the bypass system flows past the rotor assembly and is discharged downstream from the rotor assembly.

摘要翻译： 一种方法有利于组装燃气涡轮发动机，该燃气涡轮发动机包括压缩机和在压缩机下游的轴向流动连通中联接的转子组件。 该方法包括将与压缩机流体连通的旁路系统联接以将从压缩机排出的一部分流向转子组件引导通过旁路系统，并将旁路系统的下游端连接在燃气涡轮发动机内，使得 进入旁路系统的流量流过转子组件，并从转子组件的下游排出。

公开(公告)号：US06848247B2

公开(公告)日：2005-02-01

申请号：US10341586

申请日：2003-01-14

申请人： Wayne A. Rozen ,  Philip A. March, Sr. ,  John Brauer

发明人： Wayne A. Rozen ,  Philip A. March, Sr. ,  John Brauer

IPC分类号： A01D7/06 ,  A01F7/06

CPC分类号： A01D7/06

摘要： A golf bunker rake has a coupling member adapted to receive a support. First teeth are connected to the support and have substantially round first tips. Second teeth are connected to the support and have substantially round second tips. The first teeth are longer than the second teeth. The rounded tips of the first teeth prevent damage to the golf bunker liner during use.

摘要翻译： 高尔夫球仓耙具有适于接收支撑件的联接构件。 第一齿连接到支撑件并具有大致圆形的第一尖端。 第二齿连接到支撑件并且具有大致圆形的第二尖端。 第一个牙齿比第二个牙齿长。 第一颗牙齿的圆形尖端防止在使用过程中损坏高尔夫球舱衬垫。

公开(公告)号：USD1034203S1

公开(公告)日：2024-07-09

申请号：US29819282

申请日：2021-12-14

申请人： John Brauer ApS

设计人： John Brauer

摘要： FIG. 1 is a front perspective view of a bottle according to the present invention; and,
FIG. 2 is a front perspective view of the bottle according to the present invention with the lid removed.
The broken lines and the lower opacity areas within the broken lines show portions of the bottle that form no part of the claimed design.

公开(公告)号：US20070157618A1

公开(公告)日：2007-07-12

申请号：US11329783

申请日：2006-01-11

申请人： John Manteiga ,  Duane Thomsen ,  Daniel Brown ,  John Brauer

发明人： John Manteiga ,  Duane Thomsen ,  Daniel Brown ,  John Brauer

IPC分类号： F23R3/00

CPC分类号： F23R3/60 ,  F02C3/14 ,  F23R3/50

摘要： A method for assembling a gas turbine engine is provided. The method includes providing a combustor liner support including a first portion formed with a plurality of circumferentially-spaced recessed areas, and a second portion extending from the first portion. The method also includes coupling the combustor liner support within a combustor such that during engine operations cooling air is channeled through the plurality of recessed areas to facilitate cooling the combustor liner support.

摘要翻译： 提供一种用于组装燃气涡轮发动机的方法。 该方法包括提供包括形成有多个周向间隔开的凹陷区域的第一部分和从第一部分延伸的第二部分的燃烧器衬套支撑件。 该方法还包括将燃烧器衬套支撑件联接在燃烧器内，使得在发动机操作期间，冷却空气被引导通过多个凹陷区域以便于冷却燃烧器衬套支撑件。