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1. 发明申请

US20050079061A1 AIRFOIL SHAPE FOR A TURBINE BUCKET 有权
标题翻译：用于涡轮马桶的气翼形状
公开(公告)号：US20050079061A1
公开(公告)日：2005-04-14
申请号：US10681144
申请日：2003-10-09
申请人： Thomas Beddard , David Pesetsky
发明人： Thomas Beddard , David Pesetsky
IPC分类号： F01D5/06 , F01D5/14 , B63H1/26
CPC分类号： F01D5/141 , F05D2240/301 , F05D2250/50 , Y10S416/02 , Y10S416/05
摘要： Second 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 0.05 to 0.95 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 and Y 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 ±0.160 inches in directions normal to the surface of the airfoil.
摘要翻译：第二级涡轮机叶片具有基本上符合X，Y和Z的笛卡尔坐标值的翼型轮廓，其中X和Y值为英寸，Z值为0.05至0.95，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。作为相同常数或数字的函数，X和Y距离可以是可缩放的，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在±0.160英寸的范围内。

2. 发明申请

US20070116572A1 Method and apparatus for wind turbine braking 有权
标题翻译：风力发电机制动的方法和装置
公开(公告)号：US20070116572A1
公开(公告)日：2007-05-24
申请号：US11282127
申请日：2005-11-18
申请人： Corneliu Barbu , Ralph Teichmann , Aaron Avagliano , Leonardo Kammer , Kirk Pierce , David Pesetsky , Peter Gauchel
发明人： Corneliu Barbu , Ralph Teichmann , Aaron Avagliano , Leonardo Kammer , Kirk Pierce , David Pesetsky , Peter Gauchel
IPC分类号： B63H1/06
CPC分类号： F03D7/024 , F03D7/0224 , F03D7/0244 , F03D7/0252 , F03D7/0264 , F03D7/042 , F05B2260/901 , F05B2270/1071 , Y02E10/723
摘要： A method for braking a wind turbine including at least one rotor blade coupled to a rotor. The method includes selectively controlling an angle of pitch of the at least one rotor blade with respect to a wind direction based on a design parameter of a component of the wind turbine to facilitate reducing a force induced into the wind turbine component as a result of braking.
摘要翻译：一种用于制动风力涡轮机的方法，包括联接到转子的至少一个转子叶片。该方法包括基于风力涡轮机的部件的设计参数来选择性地控制至少一个转子叶片相对于风向的俯仰角，以便有助于减少由于制动而导致的风力涡轮机部件的力。

3. 发明授权

US06804612B2 Methods and systems for performing integrated analyzes, such as integrated analyzes for gas turbine power plants 有权
标题翻译：执行综合分析的方法和系统，如燃气轮机发电厂的综合分析
公开(公告)号：US06804612B2
公开(公告)日：2004-10-12
申请号：US10020588
申请日：2001-10-30
申请人： Cedric Chow , Kelly Crotty , John Drohan , James Fehlberg , Arlie Russell Martin , Thad Morton , Todd Nemec , David Pesetsky , Robert Russell Priestley , Ming Zhou
发明人： Cedric Chow , Kelly Crotty , John Drohan , James Fehlberg , Arlie Russell Martin , Thad Morton , Todd Nemec , David Pesetsky , Robert Russell Priestley , Ming Zhou
IPC分类号： G06F1900
CPC分类号： F02C9/52 , F05D2260/81
摘要： Automated systems for performing integrated analyses. In one embodiment, an integrated analysis system can be used to comprehensively evaluate the effects of changes in hardware configuration or operating conditions on gas turbine power plant performance and economics. The system evaluates these changes by concurrently analyzing a number of different aspects of the power plant while ensuring that the data used in each of the different analyses is consistent. These analyses can include turbine and compressor aerodynamic analysis, cooling and leakage flow analysis, heat transfer analysis, part life analysis, heat balance analysis, cost analysis and overall power plant performance and economic analysis.
摘要翻译：用于执行集成分析的自动化系统。在一个实施例中，可以使用集成分析系统来全面评估硬件配置或操作条件变化对燃气轮机发电厂性能和经济性的影响。系统通过同时分析发电厂的不同方面来评估这些变化，同时确保每个不同分析中使用的数据是一致的。这些分析可以包括涡轮机和压缩机的空气动力学分析，冷却和泄漏流量分析，热传递分析，零件寿命分析，热平衡分析，成本分析和总体发电厂性能以及经济分析。

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