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1. 发明授权

US07416389B2 Methods and apparatus for assembling rotatable machines 有权
标题翻译：用于组装可旋转机器的方法和装置
公开(公告)号：US07416389B2
公开(公告)日：2008-08-26
申请号：US11270091
申请日：2005-11-09
申请人： Thomas Richard Henning , John Douglas Mickol , Daniel Edward Mollmann
发明人： Thomas Richard Henning , John Douglas Mickol , Daniel Edward Mollmann
IPC分类号： F01D5/10 , B21K25/00
CPC分类号： F01D5/3007 , F01D5/027 , F01D5/30 , F05D2230/60 , F05D2240/30 , F05D2240/40 , Y02T50/672 , Y02T50/673 , Y10T29/49323
摘要： Methods and systems for ordering blades in a rotatable machine is provided. The method includes receiving at least one geometric parameter measurement of each blade in a row of blades, determining a root sum squared value of a difference of a selected one of the received geometric parameter measurements between adjacent blades in the row of blades, determining a vector sum of a selected other one of the received geometric parameter measurements, determining a moment weight vector sum of each blade to be positioned on the rotor, and determining, using a computer, a sequence map of each blade using the root sum squared value of the difference of the geometric parameter measurement between adjacent blades in the row of blades, the vector sum of a selected other one of the received geometric parameter measurements, and the moment weight vector sum.
摘要翻译：提供了用于在可旋转机器中订购叶片的方法和系统。该方法包括：接收一行叶片中的每个叶片的至少一个几何参数测量，确定叶片行中相邻叶片之间接收到的几何参数测量值中所选择的一个的差的根和平方值，确定矢量确定所接收的几何参数测量中所选择的另一个的总和，确定要定位在转子上的每个叶片的力矩加权矢量和，以及使用计算机，使用计算机确定每个叶片的序列图，刀片行中相邻刀片之间的几何参数测量的差异，所接收的几何参数测量中所选择的另一个的矢量和和力矩权重向量和。

2. 发明授权

US08180596B2 Methods and apparatus for assembling rotatable machines 有权
标题翻译：用于组装可旋转机器的方法和装置
公开(公告)号：US08180596B2
公开(公告)日：2012-05-15
申请号：US10889742
申请日：2004-07-13
申请人： Thomas Richard Henning , John Douglas Mickol , Daniel Edward Mollmann , Michael Harvey Schneider
发明人： Thomas Richard Henning , John Douglas Mickol , Daniel Edward Mollmann , Michael Harvey Schneider
IPC分类号： G06F17/50
CPC分类号： F04D27/001 , F04D15/0088 , F04D29/666 , Y10T29/49316
摘要： A processor-implemented method of assembling a rotatable machine is provided. The machine includes a plurality of blades that extend radially outwardly from a rotor. The method includes determining a geometric parameter for each blade in a row of blades that is relative to a ratio, R of an inlet area and an outlet area of a predetermined volume defined between each pair of blades, determining an initial sequence map for the row of blades that facilitates minimizing a difference of R between circumferentially adjacent pairs of blades, and iteratively remapping the sequence of the blades to facilitate reducing a moment weight vector sum of the rotor to a value that is less than a predetermined value.
摘要翻译：提供了一种组装可旋转机器的处理器实现方法。机器包括从转子径向向外延伸的多个叶片。该方法包括确定一排叶片中每个叶片的几何参数，其相对于在每对叶片之间限定的预定体积的入口面积和出口面积的比率R，确定该行的初始序列图的叶片，其有助于最小化周向相邻的叶片对之间的R的差异，并且迭代地重新映射叶片的序列，以便于将转子的力矩加权矢量和减小到小于预定值的值。

3. 发明授权

US07090464B2 Methods and apparatus for assembling rotatable machines 有权
标题翻译：用于组装可旋转机器的方法和装置
公开(公告)号：US07090464B2
公开(公告)日：2006-08-15
申请号：US10889945
申请日：2004-07-13
申请人： Thomas Richard Henning , John Douglas Mickol , Daniel Edward Mollmann , Michael Harvey Schneider , Andrew Breeze-Stringfellow , Max Farson
发明人： Thomas Richard Henning , John Douglas Mickol , Daniel Edward Mollmann , Michael Harvey Schneider , Andrew Breeze-Stringfellow , Max Farson
IPC分类号： F01D5/10 , B21K25/00
CPC分类号： F01D5/3007 , F01D5/027 , F01D5/30 , F05D2230/60 , F05D2240/30 , F05D2240/40 , Y02T50/672 , Y02T50/673 , Y10T29/49323
摘要： A method and apparatus for ordering blades in a rotatable machine is provided. The machine includes a plurality of blades that extend radially outwardly from a rotor. The method includes determining a moment weight of each blade in a row of blades, determining a geometric parameter of each blade in the same row of blades, and determining a mapping order of each blade using the moment weight and the geometric parameter. The apparatus includes a computer system that includes a software product code segment for minimizing imbalance in a bladed rotor wherein the segment is configured to receive a moment weight value for each blade to be installed in said rotor, receive a geometric parameter value for each blade to be installed in said rotor, calculate a blade location on the rotor based on the received values, and generate a blade map based on the calculated location.
摘要翻译：提供了一种用于在可旋转机器中订购刀片的方法和装置。机器包括从转子径向向外延伸的多个叶片。该方法包括确定一行叶片中的每个叶片的力矩重量，确定同一行叶片中每个叶片的几何参数，以及使用力矩和几何参数确定每个叶片的映射顺序。该装置包括计算机系统，该计算机系统包括用于最小化叶片式转子中的不平衡的软件产品代码段，其中该段被配置为接收要安装在所述转子中的每个叶片的力矩权值，接收每个叶片的几何参数值安装在所述转子中，基于所接收的值计算转子上的叶片位置，并且基于所计算的位置生成叶片图。

4. 发明授权

US06908285B2 Methods and apparatus for assembling rotatable machines 失效
标题翻译：用于组装可旋转机器的方法和装置
公开(公告)号：US06908285B2
公开(公告)日：2005-06-21
申请号：US10409392
申请日：2003-04-08
申请人： Thomas Richard Henning , Gert J. van der Merwe , William Carl Ruehr , Daniel Edward Mollmann
发明人： Thomas Richard Henning , Gert J. van der Merwe , William Carl Ruehr , Daniel Edward Mollmann
IPC分类号： F01D5/10 , F01D5/02 , F01D5/30 , F02C7/00 , F04D29/32 , F04D29/34 , F04D29/66 , B63H1/00
CPC分类号： F01D5/027 , F01D5/30 , F01D5/3007 , F04D29/662 , F05D2230/60 , Y02T50/671 , Y02T50/673 , Y10S416/50 , Y10T29/49321
摘要： A method and apparatus for assembling a rotatable machine is provided. The machine includes a plurality of blades that extend radially outwardly from a rotor. The method includes determining a moment weight of each blade in a row of blades, determining a geometric parameter of each blade in the same row of blades, and determining a mapping order of each blade using the moment weight and the geometric parameter. The apparatus includes a computer system that includes a software product code segment for minimizing imbalance in a bladed rotor wherein the segment is configured to receive a moment weight value for each blade to be installed in said rotor, receive a geometric parameter value for each blade to be installed in said rotor, calculate a blade location on the rotor based on the received values, and generate a blade map based on the calculated location.
摘要翻译：提供了一种用于组装可旋转机器的方法和装置。机器包括从转子径向向外延伸的多个叶片。该方法包括确定一行叶片中的每个叶片的力矩重量，确定同一行叶片中每个叶片的几何参数，以及使用力矩和几何参数确定每个叶片的映射顺序。该装置包括计算机系统，其包括用于最小化叶片式转子中的不平衡的软件产品代码段，其中所述段被配置为接收要安装在所述转子中的每个叶片的力矩权重值，接收每个叶片的几何参数值安装在所述转子中，基于所接收的值计算转子上的叶片位置，并且基于所计算的位置生成叶片图。

5. 发明申请

US20130156592A1 FAN BLADE WITH COMPOSITE CORE AND WAVY WALL TRAILING EDGE CLADDING 有权
标题翻译：风扇叶片与复合核心和波纹墙拖车边缘
公开(公告)号：US20130156592A1
公开(公告)日：2013-06-20
申请号：US13331301
申请日：2011-12-20
申请人： Nicholas Joseph Kray , Daniel Edward Mollmann , Dong-Jin Shim , Trevor Howard Wood
发明人： Nicholas Joseph Kray , Daniel Edward Mollmann , Dong-Jin Shim , Trevor Howard Wood
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。

6. 发明授权

US09121294B2 Fan blade with composite core and wavy wall trailing edge cladding 有权
标题翻译：风扇叶片与复合芯和波浪形墙后缘包层
公开(公告)号：US09121294B2
公开(公告)日：2015-09-01
申请号：US13331301
申请日：2011-12-20
申请人： Nicholas Joseph Kray , Daniel Edward Mollmann , Dong-Jin Shim , Trevor Howard Wood
发明人： Nicholas Joseph Kray , Daniel Edward Mollmann , Dong-Jin Shim , Trevor Howard Wood
IPC分类号： F01D5/28 , 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。

7. 发明授权

US08313279B2 Dual rotor vibration monitoring 有权
标题翻译：双转子振动监测
公开(公告)号：US08313279B2
公开(公告)日：2012-11-20
申请号：US12106491
申请日：2008-04-21
申请人： Daniel Edward Mollmann
发明人： Daniel Edward Mollmann
IPC分类号： F01D25/04
CPC分类号： F01D21/003 , F01D25/04 , F05D2260/96 , G01H1/006
摘要： Vibration is monitored in a dual rotor engine. A first total vibration of the engine is measured during operation. Relative phase of the two rotors is then clocked, and a second total vibration of the engine is then measured during operation. First and second total unbalances are then resolved at a common response frequency from the measured total vibrations. First and second rotor unbalances are then resolved for the corresponding rotors from the first and second total unbalances. In a further method, corresponding corrective balance weights may be determined for offsetting the resolved rotor unbalances.
摘要翻译：在双转子发动机中监测振动。在运行期间测量发动机的第一次总振动。然后对两个转子的相对相位进行计时，然后在运行期间测量发动机的第二个总振动。然后从测量的总振动以相同的响应频率解决第一和第二不平衡。然后从第一和第二总不平衡中分离出相应转子的第一和第二转子不平衡。在另一种方法中，可以确定相应的校正平衡重量以抵消分辨的转子不平衡。

8. 发明授权

US07780410B2 Method and apparatus for gas turbine engines 有权
标题翻译：燃气轮机发动机的方法和装置
公开(公告)号：US07780410B2
公开(公告)日：2010-08-24
申请号：US11616607
申请日：2006-12-27
申请人： Nicholas Joseph Kray , David William Crall , Daniel Edward Mollmann
发明人： Nicholas Joseph Kray , David William Crall , Daniel Edward Mollmann
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。

9. 发明申请

US20080159854A1 Methods and apparatus for fabricating a fan assembly for use with turbine engines 有权
标题翻译：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。

10. 发明申请

US20080152498A1 METHODS AND SYSTEMS FOR BALANCING A ROTATABLE MEMBER 失效
标题翻译：用于平衡可旋转构件的方法和系统
公开(公告)号：US20080152498A1
公开(公告)日：2008-06-26
申请号：US11613782
申请日：2006-12-20
申请人： Daniel Edward Mollmann , Steven Alan Ross , Stephen Wade Faw , Enzo Luigi Morabito , Jeffrey Scott Allen
发明人： Daniel Edward Mollmann , Steven Alan Ross , Stephen Wade Faw , Enzo Luigi Morabito , Jeffrey Scott Allen
IPC分类号： F01D25/04
CPC分类号： F01D5/027 , F01D21/003 , G01M1/36 , Y02T50/671
摘要： Methods and systems of balancing a rotatable member are provided. A method includes separately balancing a first portion and a second portion of the rotatable member wherein the second portion mateable to said first portion, coupling the first and second portions to each other, measuring a physical dimension of the coupled first and second portions, and determining a balance weight magnitude and position based on the measured physical dimension.
摘要翻译：提供了平衡可旋转构件的方法和系统。一种方法包括单独地平衡可旋转构件的第一部分和第二部分，其中第二部分可配合到所述第一部分，将第一和第二部分彼此耦合，测量耦合的第一和第二部分的物理尺寸，以及确定基于测量的物理尺寸的平衡重量幅度和位置。

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