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1. 发明申请

US20050129499A1 Gas turbine high temperature turbine blade outer air seal assembly 失效
标题翻译：燃气轮机高温涡轮机叶片外部空气密封组件
公开(公告)号：US20050129499A1
公开(公告)日：2005-06-16
申请号：US10734922
申请日：2003-12-11
申请人： Mark Morris , Steve Halfmann , Craig Wilson , Shawn Pollock , Carl Larson
发明人： Mark Morris , Steve Halfmann , Craig Wilson , Shawn Pollock , Carl Larson
IPC分类号： F01D9/04 , F01D11/00 , F01D25/12 , F01D1/00
CPC分类号： F01D9/042 , F01D9/04 , F01D11/005 , F01D25/12 , F05D2230/90 , F05D2260/201 , F05D2300/2283 , Y02T50/67 , Y02T50/671 , Y02T50/676
摘要： A turbine shroud assembly includes forward and aft hangers, an axisymmetric plenum assembly, ceramic shroud segments, ceramic spacers, and forward and aft rope seals. The plenum assembly supplies impingement cooling to the shroud and the hangers. The impingement cooling to the forward and aft hangers is controlled independently to improve blade tip clearance. The rope seals are radially inward from the hangers and reduce cooling flow leakage. The turbine shroud assembly can operate in a higher temperature environment using less cooling flow than the prior art.
摘要翻译：涡轮机罩组件包括前后悬挂架，轴对称增压组件，陶瓷护罩段，陶瓷间隔件和前后绳密封件。增压组件为护罩和衣架提供冲击冷却。对前后吊架的冲击冷却是独立控制的，以提高叶片顶端间隙。绳索密封件从吊架向内径向减小，从而减少冷却流量泄漏。涡轮机罩组件可以在比现有技术更少的冷却流动的较高温度环境中操作。

2. 发明申请

US20060078422A1 Method for modifying gas turbine nozzle area 失效
标题翻译：燃气轮机喷嘴面积修改方法
公开(公告)号：US20060078422A1
公开(公告)日：2006-04-13
申请号：US10963185
申请日：2004-10-12
申请人： Mark Morris , Thomas Strangman , Craig Wilson , George Wolfmeyer , Steve Halfmann , David Jan
发明人： Mark Morris , Thomas Strangman , Craig Wilson , George Wolfmeyer , Steve Halfmann , David Jan
IPC分类号： F01D9/00
CPC分类号： F01D5/005 , F01D5/141 , F01D9/041 , F05D2230/10 , F05D2230/90 , Y10T29/49323
摘要： A method of modifying a turbine nozzle area comprises depositing a thermal barrier coating (TBC) on the nozzle endwalls to provide a minimum nozzle area, evaluating an airflow through the nozzle, and machining the TBC to increase the nozzle area. Adjacent segment area variation may be minimized, improving engine reliability by reducing the aerodynamic excitation to the down stream blade.
摘要翻译：改进涡轮喷嘴区域的方法包括在喷嘴端壁上沉积热障涂层（TBC）以提供最小喷嘴面积，评估通过喷嘴的气流，以及加工TBC以增加喷嘴面积。相邻段区域变化可以被最小化，通过减小对下游叶片的空气动力学激励来提高发动机的可靠性。

3. 发明申请

US20080000082A1 Method to modify an airfoil internal cooling circuit 失效
标题翻译：修改机翼内部冷却回路的方法
公开(公告)号：US20080000082A1
公开(公告)日：2008-01-03
申请号：US11238528
申请日：2005-09-28
申请人： Mark Morris , Jason Smoke , William Weidner , Craig Wilson , Edward Mayer
发明人： Mark Morris , Jason Smoke , William Weidner , Craig Wilson , Edward Mayer
IPC分类号： B23P15/02 , B21K3/04
CPC分类号： F01D5/147 , F01D5/187 , F05D2230/10 , F05D2230/23 , F05D2260/221 , Y02T50/676 , Y10T29/49336 , Y10T29/49339 , Y10T29/49341 , Y10T29/49343 , Y10T29/49771
摘要： Methods are provided for modifying an airfoil internal cooling circuit that include a flow path configured to direct air through the airfoil in a direction and the airfoil having a leading edge, a trailing edge, and a first and a second wall therebetween, each wall having an inner and an outer surface, the inner surfaces defining a cavity and having features forming at least a portion of the internal cooling circuit. The methods may include the steps of forming a pilot hole through the airfoil first and second walls at a predetermined location, forming an insert hole based on the predetermined location, the insert hole enveloping the pilot hole and configured to receive at least a portion of an insert configured to modify the internal cooling circuit flow path, placing the insert into the insert hole, and bonding the insert to the airfoil first and second walls.
摘要翻译：提供了用于修改翼型件内部冷却回路的方法，所述翼型件内部冷却回路包括被构造成沿着一个方向引导空气通过翼型的流动路径，并且所述翼型件具有前缘，后缘以及其间的第一和第二壁，每个壁具有内表面和外表面，内表面限定空腔并且具有形成内部冷却回路的至少一部分的特征。所述方法可以包括以下步骤：在预定位置处通过翼型件形成导向孔，形成基于预定位置的插入孔，所述插入孔包围导向孔并且构造成容纳至少一部分插入件被配置为修改内部冷却回路流动路径，将插入件放入插入孔中，并将插入件接合到翼型件第一和第二壁。

4. 发明申请

US20070201980A1 Method to augment heat transfer using chamfered cylindrical depressions in cast internal cooling passages 审中-公开
标题翻译：在铸造内部冷却通道中使用倒角圆柱形凹陷来增加传热的方法
公开(公告)号：US20070201980A1
公开(公告)日：2007-08-30
申请号：US11390616
申请日：2006-03-27
申请人： Mark Morris , Vivek Agarwal , Jason Smoke , William Baker , Luis Tapia
发明人： Mark Morris , Vivek Agarwal , Jason Smoke , William Baker , Luis Tapia
IPC分类号： F01D5/18
CPC分类号： B22C9/10 , B22C9/04 , B22C9/103 , F01D5/187 , F05D2230/12 , F05D2230/21 , F05D2230/211 , F05D2250/192 , F05D2250/292 , F05D2260/2212 , F05D2260/2214 , F05D2260/22141 , Y02T50/676
摘要： An air-cooled turbine blade is provided having an airfoil shape defined by a convex suction side wall, a concave pressure side wall, a leading edge, a trailing edge, a root and a tip, each wall including an interior surface that defines an interior with the edges, root and tip. The blade includes a plurality of independent cooling circuit flow paths within the blade interior and a roughened surface. The roughened surface is formed on an interior surface of at least one of the convex suction side wall and the concave pressure side wall, the roughened surface comprising a plurality of cylindrical depressions. Each depression includes a cylindrical wall coupled to a bottom wall by a chamfered edge formed therebetween, and the roughened surface defines at least a portion of one of the flow paths of the plurality of independent cooling circuit flow paths. Methods for forming the blade are also provided.
摘要翻译：提供一种风冷式涡轮叶片，其具有由凸形吸入侧壁，凹形压力侧壁，前缘，后缘，根部和尖端限定的翼型，每个壁包括限定内部的内表面边缘，根部和尖端。叶片包括在叶片内部和粗糙表面内的多个独立的冷却回路流动路径。粗糙表面形成在凸吸入侧壁和凹压侧壁中的至少一个的内表面上，粗糙表面包括多个圆柱形凹陷。每个凹陷包括通过其间形成的倒角边缘连接到底壁的圆柱形壁，粗糙表面限定多个独立冷却回路流动路径中的一个流路的至少一部分。还提供了形成叶片的方法。

5. 发明申请

US20060083851A1 Method for making filled epoxy resin compositions 失效
标题翻译：填充环氧树脂组合物的制备方法
公开(公告)号：US20060083851A1
公开(公告)日：2006-04-20
申请号：US10967646
申请日：2004-10-14
申请人： Yongan Yan , Douglas Meyers , Mark Morris , D. Meixner , Satyabrata Raychaudhuri
发明人： Yongan Yan , Douglas Meyers , Mark Morris , D. Meixner , Satyabrata Raychaudhuri
IPC分类号： H05K3/00 , B05D5/12
CPC分类号： C08G59/24 , C08G59/4215 , C08G59/688 , C08K9/06 , C08L63/00 , Y10T428/31511
摘要： An encapsulant is described for an optoelectronic device or optical component, which provides a coefficient of thermal expansion of less than 50 ppm/° C., with a variation of less than ±30%, and further provides an optical transmittance of at least 20% at a wavelength in the range of 400 to 900 nm, at an encapsulant thickness of about 1 mm. The encapsulant includes a filler consisting essentially of glass particles having diameters smaller than 500 μm, being essentially free of titania and lead oxide, and having a refractive index in the range of 1.48 to 1.60, with a variance of less than about 0.001. A method for making the encapsulant also is described, the method including steps of (1) processing the glass to form particles having diameters between 1 and 500 μm, (2) preparing an epoxy resin composition having at a cured stage a refractive index close to that of the glass filler particles, (3) mixing the epoxy resin composition with the filler particles to form a filled epoxy resin composition, (4) encapsulating an optoelectronic device with the filled epoxy resin composition, and (5) curing the filled epoxy resin composition.
摘要翻译：对于光电器件或光学部件描述了一种密封剂，其提供小于50ppm /℃的热膨胀系数，其变化小于±30％，并进一步提供至少20％的光透射率，在400至900nm范围内的波长处，密封剂厚度约为1mm。密封剂包括基本上由直径小于500μm的玻璃颗粒组成的填料，其基本上不含二氧化钛和氧化铅，并且折射率在1.48至1.60范围内，其变化小于约0.001。还描述了制造密封剂的方法，该方法包括以下步骤：（1）处理玻璃以形成直径在1至500μm之间的颗粒;（2）制备环氧树脂组合物，其在固化阶段的折射率接近（3）将环氧树脂组合物与填料颗粒混合以形成填充的环氧树脂组合物，（4）用填充的环氧树脂组合物封装光电器件，和（5）固化填充的环氧树脂组成。

6. 发明申请

US20050123389A1 GAS TURBINE COOLED SHROUD ASSEMBLY WITH HOT GAS INGESTION SUPPRESSION 有权
标题翻译：燃气涡轮机冷却风冷却装置采用高温气体抑制
公开(公告)号：US20050123389A1
公开(公告)日：2005-06-09
申请号：US10729695
申请日：2003-12-04
申请人： Mark Morris , William Howe , George Zurmehly , Alan Tiltman , George Wolfmeyer , John Sciacca
发明人： Mark Morris , William Howe , George Zurmehly , Alan Tiltman , George Wolfmeyer , John Sciacca
IPC分类号： F01D1/00 , F01D9/04 , F01D11/00 , F01D11/08 , F01D11/10 , F01D25/12
CPC分类号： F01D25/12 , F01D9/04 , F01D11/005 , F01D11/10 , F05D2230/12 , F05D2240/11 , F05D2240/81 , F05D2250/29 , F05D2260/202 , Y02T50/67 , Y02T50/676
摘要： A cooled shroud assembly includes an angled slot and a plurality of dilution jet openings. The shroud forward cavity is modified such that at least one recirculation zone is produced. The angled slot forces an axial change in momentum of the hot gas flow and increases radial and axial pressure variation attenuation. The cooled shroud assembly isolates the shroud structure and seals from the hot flow path and a cooling flow from the dilution jet openings dilutes the hot gas flow. A series of recirculation zones shields the shroud carrier and high pressure seals from the hot gas flow.
摘要翻译：冷却的护罩组件包括成角度的槽和多个稀释喷射开口。护罩前腔被修改为使得至少一个再循环区被产生。倾斜的狭槽迫使热气流动力的轴向变化，并增加径向和轴向的压力变化衰减。冷却的护罩组件将护罩结构和密封件与热流路隔离，并且来自稀释喷射口的冷却流量稀释热气流。一系列再循环区域将护罩载体和高压密封件与热气流屏蔽。

7. 植物专利

USPP14450P2 Mint plant named ‘Clackamas’ 有权
标题翻译：薄荷厂名为“Clackamas”
公开(公告)号：USPP14450P2
公开(公告)日：2004-01-06
申请号：US10193213
申请日：2002-07-12
申请人： Mark Morris
发明人： Mark Morris
IPC分类号： A01H500
CPC分类号： A01H5/12
摘要： A new and distinct peppermint plant ‘Clackamas’ characterized by its resistance to Mint rust (Puccinia menthe Pers), Mint wilt (Ferticillium dahliae and Verticillium albo-atrum), and Spider mites as well as a more upright growth habit and a lighter green color the Black Mitcham peppermint plant.
摘要翻译：一种新的和独特的薄荷植物“Clackamas”，其特征在于它对薄荷锈病（Puccinia menthe Pers），薄荷苔藓（大戟属和大戟属）和蜘蛛螨的抗性以及更直立的生长习性和较浅的绿色黑Mitcham薄荷植物。

8. 发明申请

US20110172238A1 BENZIMIDAZOLE ANALOGUES FOR THE TREATMENT OR PREVENTION OF FLAVIVIRUS INFECTIONS 失效
标题翻译：用于治疗或预防感染病毒的苯唑咪唑类似物
公开(公告)号：US20110172238A1
公开(公告)日：2011-07-14
申请号：US12838350
申请日：2010-07-16
申请人： James A. Henderson , John Maxwell , Louis Vaillancourt , Mark Morris , Ronald Grey, JR. , Simon Giroux , Laval Chan Chun Kong , Sanjoy Kumar Das , Bingcan Liu , Carl Poisson , Caroline Cadilhac , Monica Bubenik , T. Jagadeeswar Reddy , Guy Falardeau , Constantin Yannopoulos , Jian Wang , Oswy Z. Pereira , Youssef L. Bennani , Albert C. Pierce , Govinda Rao Bhisetti , Kevin M. Cottrell , Valerie Marone
发明人： James A. Henderson , John Maxwell , Louis Vaillancourt , Mark Morris , Ronald Grey, JR. , Simon Giroux , Laval Chan Chun Kong , Sanjoy Kumar Das , Bingcan Liu , Carl Poisson , Caroline Cadilhac , Monica Bubenik , T. Jagadeeswar Reddy , Guy Falardeau , Constantin Yannopoulos , Jian Wang , Oswy Z. Pereira , Youssef L. Bennani , Albert C. Pierce , Govinda Rao Bhisetti , Kevin M. Cottrell , Valerie Marone
IPC分类号： A61K31/496 , C07D403/14 , A61K31/4184 , C07D401/14 , A61K31/4545 , A61K31/506 , A61K31/4439 , A61P31/14
CPC分类号： C07K5/06052 , C07D401/14 , C07D403/14 , C07D405/14 , C07D407/14 , C07D409/14 , C07D413/14 , C07D417/14 , C07D495/04
摘要： Compounds represented by formula I: or pharmaceutically acceptable salts and solvates thereof, wherein A, B, B′, X, Y, R1, R1′, R2, R2′, R3, R3′, R5, R5′, R6, m, n, or p are as defined herein, are useful for treating flaviviridae viral infections.
摘要翻译：其中A，B，B'，X，Y，R1，R1'，R2，R2'，R3，R3'，R5，R5'，R6，m， n或p如本文所定义，可用于治疗黄病毒科病毒感染。

9. 发明申请

US20070235373A1 Diffuser particle separator 失效
标题翻译：扩散器粒子分离器
公开(公告)号：US20070235373A1
公开(公告)日：2007-10-11
申请号：US11213125
申请日：2005-08-26
申请人： Thomas Strangman , Mark Morris , William Baker , Harry Kington
发明人： Thomas Strangman , Mark Morris , William Baker , Harry Kington
IPC分类号： B07C5/342
CPC分类号： F04D29/441 , F04D29/701 , F05B2260/63
摘要： A diffuser particle separator may be integrated into a gas turbine engine to remove corrosive dust and salt particles from the engine's core air flow. The air flow may pass over a series of particle accumulator entrance orifices, trapping particles in a particle accumulator while allowing the air flow to continue unimpeded. Since dust deposits may become molten at high temperatures, removal of dust from the core and secondary airflow may be critical for long-life superalloy and ceramic components, particularly those with small diameter air-cooling holes and thermal barrier coatings.
摘要翻译：扩散器颗粒分离器可以集成到燃气涡轮发动机中以从发动机的核心空气流中去除腐蚀性灰尘和盐颗粒。空气流可以通过一系列颗粒蓄能器入口，将颗粒捕获在颗粒蓄积器中，同时允许气流继续畅通无阻。由于灰尘沉积物可能在高温下变得熔融，因此从长期使用的超级合金和陶瓷部件，特别是具有小直径空气冷却孔和热障涂层的那些部件中，从芯部和二次气流中除去灰尘可能是至关重要的。

10. 外观设计

USD468252S1 Sleeper shock absorber cover 失效
标题翻译：睡眠减震器盖
公开(公告)号：USD468252S1
公开(公告)日：2003-01-07
申请号：US29146798
申请日：2001-08-17
申请人： Mark Morris
设计人： Mark Morris

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