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1. 发明授权

US06984106B2 Resilent seal on leading edge of turbine inner shroud 有权
标题翻译：涡轮机内护罩前缘的安全密封
公开(公告)号：US06984106B2
公开(公告)日：2006-01-10
申请号：US10752572
申请日：2004-01-08
申请人： Jeff Brian Thompson
发明人： Jeff Brian Thompson
IPC分类号： F01D11/08
CPC分类号： F01D11/08 , F05D2240/11 , F05D2240/55
摘要： A sealing arrangement for a stator shroud segment is provided that includes a resilient seal to reduce air leakage and improve turbine engine efficiency. The stator shroud segment includes an outer shroud having a leading edge groove and a trailing edge groove, and a plurality of inner shrouds each having a leading edge hook and a trailing edge hook. The leading and trailing hooks of each of the inner shrouds are respectively engaged with the leading and trailing edge grooves of the outer shroud so as to connect the inner shrouds to the outer shroud. A resilient shaped seal is located on a leading edge hook of the inner shroud so as to be between the leading hook and a retaining ring that contributes to holding the inner shroud in place.
摘要翻译：提供了一种用于定子护罩段的密封装置，其包括弹性密封件以减少空气泄漏并提高涡轮发动机效率。定子护罩段包括具有前缘槽和后缘槽的外护罩，以及多个内护罩，每个内护罩具有前缘钩和后缘钩。每个内护罩的前钩和尾钩分别与外护罩的前缘和后缘槽接合，以将内护罩连接到外护罩。弹性形状的密封件位于内护罩的前缘钩上，以便位于引导钩和保持环之间，该保持环有助于将内护罩保持在适当的位置。

2. 发明授权

US06739838B1 Airfoil shape for a turbine bucket 有权
标题翻译：涡轮叶片的翼型
公开(公告)号：US06739838B1
公开(公告)日：2004-05-25
申请号：US10388476
申请日：2003-03-17
申请人： Craig Allen Bielek , Robert Alan Brittingham , Jeff Brian Thompson , Benjamin Arnette Lagrange , Robert Walter Coign
发明人： Craig Allen Bielek , Robert Alan Brittingham , Jeff Brian Thompson , Benjamin Arnette Lagrange , Robert Walter Coign
IPC分类号： F01D514
CPC分类号： F01D5/141 , F01D5/225 , F05D2240/301 , F05D2240/80 , Y10S416/05
摘要： Third stage turbine buckets have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth Table I wherein X and Y values are in inches and the Z values are non-dimensional values from 0 to 1 convertible to Z distances in inches by multiplying the Z values by the height of the airfoil in inches. The X and Y values are distances which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z. The profile sections at each distance Z are joined smoothly to one another to form a complete airfoil shape. The X, Y and Z distances may be scalable as a function of the same constant or number to provide a scaled up or scaled down airfoil section for the bucket. The nominal airfoil given by the X, Y and Z distances lies within an envelop of ±0.060 inches in directions normal to the surface of the airfoil.
摘要翻译：第三级涡轮机叶片具有基本上符合X，Y和Z的笛卡尔坐标值的机翼型材，其中X和Y值为英寸，Z值为从0到1的可转换为Z距离的无量纲值将Z值乘以翼型件的高度（英寸）。 X和Y值是通过平滑连续弧连接时定义每个距离Z处的翼型轮廓部分的距离。每个距离Z处的轮廓部分彼此平滑地连接以形成完整的翼型形状。 X，Y和Z距离可以作为相同常数或数字的函数来缩放，以提供用于铲斗的放大或缩小的翼型部分。由X，Y和Z距离给出的额定翼型在垂直于翼面表面的方向上处于±0.060英寸的包络内。

3. 发明授权

US07494327B2 Portable air compressor having storage compartment 有权
标题翻译：带储物箱的便携式空气压缩机
公开(公告)号：US07494327B2
公开(公告)日：2009-02-24
申请号：US10812235
申请日：2004-03-29
申请人： Mark A. Etter , J. Cody Stilwell , Jeff Brian Thompson , Gary D. White
发明人： Mark A. Etter , J. Cody Stilwell , Jeff Brian Thompson , Gary D. White
IPC分类号： F04B53/00
CPC分类号： F04B41/02
摘要： The present invention is directed to a portable air compressor having a storage compartment, which may be used to store air compressor accessories. A shroud which encloses a portable air compressor has a recess. The recess is at least partially covered with a cover member, which is mounted to the shroud. The recess and the cover member together define a storage compartment for storing air compressor accessories such as fittings, nozzles, and the like, and/or tools such as a wrench, or the like.
摘要翻译：本发明涉及一种便携式空气压缩机，其具有可用于存储空气压缩机附件的储藏室。封闭便携式空气压缩机的护罩具有凹部。凹部至少部分地覆盖有盖构件，盖构件安装到护罩上。凹部和盖构件一起限定用于存储诸如配件，喷嘴等的空气压缩机附件的存储隔室和/或诸如扳手等的工具。

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