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1.发明授权Methods and apparatus for fabricating a fan assembly for use with turbine engines 有权用于制造与涡轮发动机一起使用的风扇组件的方法和装置公开(公告)号：US07972109B2
公开(公告)日：2011-07-05
申请号：US11646826
申请日：2006-12-28
申请人： David William Crall , Frank Worthoff , Daniel Edward Mollmann , Nicholas Joseph Kray , Max Farson
发明人： David William Crall , Frank Worthoff , Daniel Edward Mollmann , Nicholas Joseph Kray , Max Farson
IPC分类号： F01D11/12
CPC分类号： F01D21/045 , F01D5/20 , F01D11/122 , F02K3/06 , F04D29/522 , F05D2220/36 , F05D2300/603 , F05D2300/615 , Y02T50/672 , Y10T29/49316
摘要： A method for fabricating a fan assembly is provided, wherein the method includes providing a rotor having a plurality of rotor blades. At least one rotor blade is fabricated from a frangible material. The method also includes coupling a casing substantially circumferentially about the rotor, and positioning the casing a distance from the plurality of rotor blades. The distance is selected to facilitate increasing an amount of initial resistance created between the casing and the plurality of rotor blades after a bladeout.
摘要翻译： 提供了一种用于制造风扇组件的方法，其中所述方法包括提供具有多个转子叶片的转子。 至少一个转子叶片由易碎材料制成。 该方法还包括基本上围绕转子周向地联接壳体，以及将壳体定位成距离多个转子叶片的距离。 选择该距离以便于在刮除之后增加壳体与多个转子叶片之间产生的初始阻力的量。
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公开(公告)号：US07780410B2
公开(公告)日：2010-08-24
申请号：US11616607
申请日：2006-12-27
IPC分类号： B64C27/46
CPC分类号： F01D5/147 , B23P15/04 , F04D29/324 , F05D2230/23 , F05D2230/232 , F05D2230/237 , F05D2240/30 , F05D2240/303 , F05D2300/133 , Y02T50/672
摘要： A method of assembling a gas turbine engine includes providing at least one blade assembly. The method also includes forming at least one blade tip fuse within at least a portion of the at least one blade assembly. The method further includes coupling the at least one blade assembly into the gas turbine engine. The blade assembly includes an airfoil and a metal leading edge (MLE) coupled to at least a portion of the airfoil. The MLE includes the at least one blade tip fuse.
摘要翻译： 一种组装燃气涡轮发动机的方法包括提供至少一个叶片组件。 该方法还包括在至少一个叶片组件的至少一部分内形成至少一个叶片顶端保险丝。 该方法还包括将至少一个叶片组件联接到燃气涡轮发动机中。 叶片组件包括翼型件和联接到翼型件的至少一部分的金属前缘（MLE）。 MLE包括至少一个叶片顶端保险丝。
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3.发明申请Methods and apparatus for fabricating a fan assembly for use with turbine engines 有权用于制造与涡轮发动机一起使用的风扇组件的方法和装置公开(公告)号：US20080159854A1
公开(公告)日：2008-07-03
申请号：US11646826
申请日：2006-12-28
申请人： David William Crall , Frank Worthoff , Daniel Edward Mollmann , Nicholas Joseph Kray , Max Farson
发明人： David William Crall , Frank Worthoff , Daniel Edward Mollmann , Nicholas Joseph Kray , Max Farson
IPC分类号： F01D1/00
CPC分类号： F01D21/045 , F01D5/20 , F01D11/122 , F02K3/06 , F04D29/522 , F05D2220/36 , F05D2300/603 , F05D2300/615 , Y02T50/672 , Y10T29/49316
摘要： A method for fabricating a fan assembly is provided, wherein the method includes providing a rotor having a plurality of rotor blades. At least one rotor blade is fabricated from a frangible material. The method also includes coupling a casing substantially circumferentially about the rotor, and positioning the casing a distance from the plurality of rotor blades. The distance is selected to facilitate increasing an amount of initial resistance created between the casing and the plurality of rotor blades after a bladeout.
摘要翻译： 提供了一种用于制造风扇组件的方法，其中所述方法包括提供具有多个转子叶片的转子。 至少一个转子叶片由易碎材料制成。 该方法还包括基本上围绕转子周向地联接壳体，以及将壳体定位成距离多个转子叶片的距离。 选择该距离以便于在刮除之后增加壳体与多个转子叶片之间产生的初始阻力的量。
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公开(公告)号：US20080159868A1
公开(公告)日：2008-07-03
申请号：US11616607
申请日：2006-12-27
IPC分类号： B64C27/46
CPC分类号： F01D5/147 , B23P15/04 , F04D29/324 , F05D2230/23 , F05D2230/232 , F05D2230/237 , F05D2240/30 , F05D2240/303 , F05D2300/133 , Y02T50/672
摘要： A method of assembling a gas turbine engine includes providing at least one blade assembly. The method also includes forming at least one blade tip fuse within at least a portion of the at least one blade assembly. The method further includes coupling the at least one blade assembly into the gas turbine engine. The blade assembly includes an airfoil and a metal leading edge (MLE) coupled to at least a portion of the airfoil. The MLE includes the at least one blade tip fuse.
摘要翻译： 一种组装燃气涡轮发动机的方法包括提供至少一个叶片组件。 该方法还包括在至少一个叶片组件的至少一部分内形成至少一个叶片顶端保险丝。 该方法还包括将至少一个叶片组件联接到燃气涡轮发动机中。 叶片组件包括翼型件和联接到翼型件的至少一部分的金属前缘（MLE）。 MLE包括至少一个叶片顶端保险丝。
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公开(公告)号：US20130156592A1
公开(公告)日：2013-06-20
申请号：US13331301
申请日：2011-12-20
IPC分类号： F01D5/14
CPC分类号： F01D5/282 , F01D5/141 , F05D2220/36 , F05D2240/304 , F05D2250/184 , Y02T50/672 , Y02T50/673
摘要： A gas turbine engine airfoil includes leading and trailing edges, pressure and suction sides extending from airfoil base to airfoil tip, trailing edge cladding made of cladding material bonded to composite core made of composite material, cladding material less brittle than composite material, composite core including central core portion extending downstream from leading edge portion to trailing edge portion of composite core, and trailing edge cladding including wavy wall and trailing edge. Pressure and suction side flanks of trailing edge cladding may be bonded to pressure and suction side surfaces of trailing edge portion. Waves of wavy wall may extend normal to and away from the pressure and suction side surfaces. Trailing edge cladding may include wavy pressure and suction side trailing edge guards including waves of wavy wall. Airfoil may extend outwardly from platform of a blade. Root may include integral dovetail.
摘要翻译： 燃气涡轮发动机翼型包括前缘和后缘，压力和吸力侧从翼型基部延伸到翼面，由复合材料复合芯结合的包层材料制成的后缘包层，比复合材料脆的包层材料，复合芯包括 中心芯部分延伸到复合芯的前缘部分到后缘部分的下游，以及包括波浪壁和后缘的后缘包层。 后缘包层的压力和吸力侧面可以结合到后缘部分的压力和吸力侧表面。 波浪形波浪的波浪可以垂直于和远离压力和吸力侧表面延伸。 后缘包层可能包括波浪压力和吸力侧后缘护罩，包括波浪形波浪。 翼型件可以从叶片的平台向外延伸。 根可以包括整体的燕尾。
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公开(公告)号：US09121294B2
公开(公告)日：2015-09-01
申请号：US13331301
申请日：2011-12-20
CPC分类号： F01D5/282 , F01D5/141 , F05D2220/36 , F05D2240/304 , F05D2250/184 , Y02T50/672 , Y02T50/673
摘要： A gas turbine engine airfoil includes leading and trailing edges, pressure and suction sides extending from airfoil base to airfoil tip, trailing edge cladding made of cladding material bonded to composite core made of composite material, cladding material less brittle than composite material, composite core including central core portion extending downstream from leading edge portion to trailing edge portion of composite core, and trailing edge cladding including wavy wall and trailing edge. Pressure and suction side flanks of trailing edge cladding may be bonded to pressure and suction side surfaces of trailing edge portion. Waves of wavy wall may extend normal to and away from the pressure and suction side surfaces. Trailing edge cladding may include wavy pressure and suction side trailing edge guards including waves of wavy wall. Airfoil may extend outwardly from platform of a blade. Root may include integral dovetail.
摘要翻译： 燃气涡轮发动机翼型包括前缘和后缘，压力和吸力侧从翼型基部延伸到翼面，由复合材料复合芯结合的包层材料制成的后缘包层，比复合材料脆的包层材料，复合芯包括 中心芯部分延伸到复合芯的前缘部分到后缘部分的下游，以及包括波浪壁和后缘的后缘包层。 后缘包层的压力和吸力侧面可以结合到后缘部分的压力和吸力侧表面。 波浪形波浪的波浪可以垂直于和远离压力和吸力侧表面延伸。 后缘包层可能包括波浪压力和吸力侧后缘护罩，包括波浪形波浪。 翼型件可以从叶片的平台向外延伸。 根可以包括整体的燕尾。
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公开(公告)号：US09239062B2
公开(公告)日：2016-01-19
申请号：US13608754
申请日：2012-09-10
申请人： Jorge Orlando Lamboy , Nicholas Joseph Kray , Gerald Alexander Pauley , Qiang Li , Daniel Allen Wilkin, II , Tod Winton Davis
发明人： Jorge Orlando Lamboy , Nicholas Joseph Kray , Gerald Alexander Pauley , Qiang Li , Daniel Allen Wilkin, II , Tod Winton Davis
CPC分类号： F04D29/324 , F01D5/147 , F01D5/3007 , F01D11/008 , F04D29/329 , F05D2220/3217 , F05D2240/80 , F05D2300/603 , Y02T50/672 , Y02T50/673
摘要： A fan blade for a gas turbine engine includes: a straight axial dovetail, an airfoil, and a transition section disposed between the dovetail and the airfoil, the fan blade having opposed pressure and suction sides, and further including at least one shoulder protruding from a nominal surface of a selected one of the pressure and suction sides, wherein the at least one shoulder includes a boss defining a side face, and an upper section extending radially outward from the boss and tapering inward to join a nominal surface of the selected side.
摘要翻译： 一种用于燃气涡轮发动机的风扇叶片，包括：直的轴向燕尾榫，翼型件和设置在燕尾榫和翼型件之间的过渡部分，风扇叶片具有相对的压力和吸力侧，并且还包括至少一个从一个 其中所述至少一个肩部包括限定侧面的凸台和从所述凸起径向向外延伸并向内逐渐变细以连接所选侧面的标称表面的上部部分。
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8.发明授权公开(公告)号：US07976694B2
公开(公告)日：2011-07-12
申请号：US11779066
申请日：2007-07-17
申请人： Andrew Lee Trimmer , Nicholas Joseph Kray , Joshua Leigh Miller , Michael Scott Lamphere , Bin Wei
发明人： Andrew Lee Trimmer , Nicholas Joseph Kray , Joshua Leigh Miller , Michael Scott Lamphere , Bin Wei
CPC分类号： B23H5/02 , B23H5/04 , B23H5/06 , B23H5/10 , B23H5/12 , B23H5/14 , B23H9/10 , Y10T409/30756 , Y10T409/30868
摘要： An apparatus and method for hybrid machining a workpiece is disclosed. The workpiece is powered as an anode, a cutter is powered as a cathode and a cutting fluid or coolant is circulated therebetween. The cutter is made of a conductive material and a non-conductive abrasive material. The hybrid machine performs a roughing pass machining operation in which material is removed from the workpiece at a relatively high rate using a high-speed electro-erosion (HSEE) process. Then, the hybrid machine performs a finish pass machining operation in which material is removed from the workpiece using precision electro-grinding (PEG) process at a different differential electrical potential and/or flushing rate than the roughing pass machining operation to provide a smooth finish without thermal effects on the workpiece.
摘要翻译： 公开了一种用于混合加工工件的装置和方法。 工件作为阳极供电，切割器作为阴极供电，切割流体或冷却剂在其间循环。 切割器由导电材料和非导电研磨材料制成。 混合机械进行粗加工加工操作，其中使用高速电蚀（HSEE）工艺以相对高的速率从工件去除材料。 然后，混合机械进行精加工加工操作，其中以与粗加工加工操作不同的差异电位和/或冲洗速率的精密电磨（PEG）工艺从工件去除材料，以提供平滑的光洁度 对工件无热影响。
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9.发明申请公开(公告)号：US20100305876A1
公开(公告)日：2010-12-02
申请号：US12475101
申请日：2009-05-29
申请人： Byungwoo Lee , Yanyan Wu , Nicholas Joseph Kray
发明人： Byungwoo Lee , Yanyan Wu , Nicholas Joseph Kray
CPC分类号： G01B21/20 , G01N21/9515
摘要： An inspection system comprises a sensor configured to acquire inspection data of the object, a motion control device, a joint assembly coupled to the motion control device, and a probe housing coupled to the joint assembly and configured to hold the sensor. The inspection system further comprises a compliant element coupled to the probe housing and configured to cooperate with the joint assembly and the motion control device to position the sensor relative to the object. A self-aligning probe assembly is also presented.
摘要翻译： 检查系统包括被配置为获取对象的检查数据的传感器，运动控制装置，耦合到运动控制装置的联合组件以及耦合到关节组件并被配置为保持传感器的探针壳体。 检查系统还包括耦合到探针壳体并被配置为与接头组件和运动控制装置协作以将传感器相对于物体定位的柔性元件。 还提出了自对准探针组件。
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10.发明申请METHOD AND SYSTEM FOR INTEGRATING EDDY CURRENT INSPECTION WITH A COORDINATE MEASURING DEVICE 有权用辅助测量装置集成EDDY电流检测的方法和系统公开(公告)号：US20100207619A1
公开(公告)日：2010-08-19
申请号：US12372881
申请日：2009-02-18
申请人： Yanyan Wu , Thomas James Batzinger , Nicholas Joseph Kray , Changting Wang , Haiyan Sun , Francis Howard Little , David Paul Lappas , David Michael Dombrowski
发明人： Yanyan Wu , Thomas James Batzinger , Nicholas Joseph Kray , Changting Wang , Haiyan Sun , Francis Howard Little , David Paul Lappas , David Michael Dombrowski
CPC分类号： G01B7/008 , G01B7/28 , G01N27/90 , G01N27/9046
摘要： A method for integrating a measurement device for use in measuring a machine component includes providing a coordinate measuring machine (CMM) and combining eddy current (EC) capabilities and CMM capabilities to form an inspection probe. The method further includes installing the inspection probe on the CMM so that the inspection probe measures external boundaries of the machine component with the CMM capabilities and substantially simultaneously measures at least one of internal boundaries, internal defects, surface defects, and material properties of the machine component with the EC capabilities, which are directly linked to actual component dimensional information provided by CMM. The inspection data can be simultaneously linked to and/or displayed with a CAD model to enable a direct comparison between the inspection data and the nominal requirements specified on the CAD model.
摘要翻译： 用于集成用于测量机器部件的测量装置的方法包括提供坐标测量机（CMM）并组合涡流（EC）能力和CMM能力以形成检查探针。 该方法还包括将检查探针安装在CMM上，使得检查探针以CMM能力测量机器部件的外部边界，并且基本上同时测量机器的内部边界，内部缺陷，表面缺陷和材料特性中的至少一个 具有EC功能的组件，其直接与CMM提供的实际组件尺寸信息相关联。 检查数据可以与CAD模型同时链接和/或显示，以便能够直接比较检验数据和CAD模型上规定的标称要求。
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