公开(公告)号：US20070084050A1

公开(公告)日：2007-04-19

申请号：US11591908

申请日：2006-11-02

申请人： Jefferson Davis ,  Martin Gosling ,  Yong Kang

发明人： Jefferson Davis ,  Martin Gosling ,  Yong Kang

IPC分类号： B21K21/16 ,  B23P19/04

CPC分类号： F01D5/005 ,  B23P6/002 ,  F05D2230/80 ,  Y10T29/49316 ,  Y10T29/49318 ,  Y10T29/4932 ,  Y10T29/49325 ,  Y10T29/49336 ,  Y10T29/49716 ,  Y10T29/49721

摘要： A method for reconfiguring an airfoil of a turbine vane segment. In at least one embodiment, the method may be used to straighten an airfoil of a turbine vane segment to remove lean, twist, or racking, or any combination thereof. The airfoil may be straightened by heating the airfoil to no more than 750 degrees F. while applying a load to an inner shroud in a direction that is generally tangential to an outer shroud of the turbine vane segment. The load is up to 6000 lbf. Orifices may be cut into the airfoil suction side, inboard of the outer shroud, to facilitate the straightening process. The orifices may be sealed upon completion of the process.

摘要翻译： 一种用于重新配置涡轮叶片段的翼型的方法。 在至少一个实施例中，该方法可以用于矫直涡轮叶片段的翼型以去除倾斜，扭转或翻倒，或其任何组合。 通过将翼型件加热至不超过750华氏度，同时在与涡轮叶片段的外护罩大致相切的方向上向内护罩施加负载的情况下，翼型件可被矫直。 负载高达6000 lbf。 孔可以被切入机翼吸入侧，在外护罩的内侧，以便矫直过程。 在完成该过程之后，可以密封孔。

公开(公告)号：US20070084048A1

公开(公告)日：2007-04-19

申请号：US11249791

申请日：2005-10-13

申请人： Martin Gosling ,  Jefferson Davis ,  Yong Kang

发明人： Martin Gosling ,  Jefferson Davis ,  Yong Kang

IPC分类号： B21K21/16 ,  B23P6/00

CPC分类号： B23P6/002 ,  F01D5/005 ,  F05D2230/80 ,  Y10T29/37 ,  Y10T29/49316 ,  Y10T29/49318 ,  Y10T29/49325 ,  Y10T29/49336 ,  Y10T29/49716 ,  Y10T29/49718 ,  Y10T29/53

摘要： A system and method for reconfiguring an airfoil of a turbine vane segment. In at least one embodiment, the system may be used to straighten an airfoil of a turbine vane segment to remove lean, twist, or racking, or any combination thereof. The airfoil may be straightened by applying a load to an inner shroud in a direction that is generally tangential to an outer shroud of the turbine vane segment. Orifices may be cut into the airfoil suction side, inboard of the outer shroud, to facilitate the straightening process. The orifices may be sealed upon completion of the process.

摘要翻译： 一种用于重新配置涡轮叶片段的翼型的系统和方法。 在至少一个实施例中，该系统可以用于矫直涡轮叶片段的翼型件以去除倾斜，扭转或翻倒，或其任何组合。 可以通过沿与涡轮叶片段的外护罩大致相切的方向向内护罩施加负载来使翼型矫直。 孔可以被切入机翼吸入侧，在外护罩的内侧，以便矫直过程。 在完成该过程之后，可以密封孔。

公开(公告)号：US07503113B2

公开(公告)日：2009-03-17

申请号：US11249791

申请日：2005-10-13

申请人： Martin C. Gosling ,  Jefferson Davis ,  Yong Kang

发明人： Martin C. Gosling ,  Jefferson Davis ,  Yong Kang

IPC分类号： B21D53/78

CPC分类号： B23P6/002 ,  F01D5/005 ,  F05D2230/80 ,  Y10T29/37 ,  Y10T29/49316 ,  Y10T29/49318 ,  Y10T29/49325 ,  Y10T29/49336 ,  Y10T29/49716 ,  Y10T29/49718 ,  Y10T29/53

摘要： A system and method for reconfiguring an airfoil of a turbine vane segment. In at least one embodiment, the system may be used to straighten an airfoil of a turbine vane segment to remove lean, twist, or racking, or any combination thereof. The airfoil may be straightened by applying a load to an inner shroud in a direction that is generally tangential to an outer shroud of the turbine vane segment. Orifices may be cut into the airfoil suction side, inboard of the outer shroud, to facilitate the straightening process. The orifices may be sealed upon completion of the process.

摘要翻译： 一种用于重新配置涡轮叶片段的翼型的系统和方法。 在至少一个实施例中，该系统可以用于矫直涡轮叶片段的翼型件以去除倾斜，扭转或翻倒，或其任何组合。 可以通过沿与涡轮叶片段的外护罩大致相切的方向向内护罩施加负载来使翼型矫直。 孔可以被切入机翼吸入侧，在外护罩的内侧，以便矫直过程。 在完成该过程之后，可以密封孔。

公开(公告)号：US20090260206A1

公开(公告)日：2009-10-22

申请号：US12372168

申请日：2009-02-17

申请人： Martin C. Gosling ,  Jefferson Davis ,  Yong Kang

发明人： Martin C. Gosling ,  Jefferson Davis ,  Yong Kang

IPC分类号： B23P6/00

CPC分类号： B23P6/002 ,  F01D5/005 ,  F05D2230/80 ,  Y10T29/37 ,  Y10T29/49316 ,  Y10T29/49318 ,  Y10T29/49325 ,  Y10T29/49336 ,  Y10T29/49716 ,  Y10T29/49718 ,  Y10T29/53

摘要： A system and method for reconfiguring an airfoil of a turbine vane segment. In at least one embodiment, the system may be used to straighten an airfoil of a turbine vane segment to remove lean, twist, or racking, or any combination thereof. The airfoil may be straightened by applying a load to an inner shroud in a direction that is generally tangential to an outer shroud of the turbine vane segment. Orifices may be cut into the airfoil suction side, inboard of the outer shroud, to facilitate the straightening process. The orifices may be sealed upon completion of the process.

摘要翻译： 一种用于重新配置涡轮叶片段的翼型的系统和方法。 在至少一个实施例中，该系统可以用于矫直涡轮叶片段的翼型件以去除倾斜，扭转或翻倒，或其任何组合。 可以通过沿与涡轮叶片段的外护罩大致相切的方向向内护罩施加负载来使翼型矫直。 孔可以被切入机翼吸入侧，在外护罩的内侧，以便矫直过程。 在完成该过程之后，可以密封孔。

公开(公告)号：US07536783B2

公开(公告)日：2009-05-26

申请号：US11591908

申请日：2006-11-02

申请人： Jefferson Davis ,  Martin C. Gosling ,  Yong Kang

发明人： Jefferson Davis ,  Martin C. Gosling ,  Yong Kang

IPC分类号： B21D53/78 ,  B23P6/00

CPC分类号： F01D5/005 ,  B23P6/002 ,  F05D2230/80 ,  Y10T29/49316 ,  Y10T29/49318 ,  Y10T29/4932 ,  Y10T29/49325 ,  Y10T29/49336 ,  Y10T29/49716 ,  Y10T29/49721

摘要： A method for reconfiguring an airfoil of a turbine vane segment. In at least one embodiment, the method may be used to straighten an airfoil of a turbine vane segment to remove lean, twist, or racking, or any combination thereof. The airfoil may be straightened by heating the airfoil to no more than 750 degrees F. while applying a load to an inner shroud in a direction that is generally tangential to an outer shroud of the turbine vane segment. The load is up to 6000 lbf. Orifices may be cut into the airfoil suction side, inboard of the outer shroud, to facilitate the straightening process. The orifices may be sealed upon completion of the process.

摘要翻译： 一种用于重新配置涡轮叶片段的翼型的方法。 在至少一个实施例中，该方法可以用于矫直涡轮叶片段的翼型以去除倾斜，扭转或翻倒，或其任何组合。 通过将翼型件加热至不超过750华氏度，同时在与涡轮叶片段的外护罩大致相切的方向上向内护罩施加负载的情况下，翼型件可被矫直。 负载高达6000 lbf。 孔可以被切入机翼吸入侧，在外护罩的内侧，以便矫直过程。 在完成该过程之后，可以密封孔。

公开(公告)号：US07730756B2

公开(公告)日：2010-06-08

申请号：US12372168

申请日：2009-02-17

申请人： Martin C. Gosling ,  Jefferson Davis ,  Yong Kang

发明人： Martin C. Gosling ,  Jefferson Davis ,  Yong Kang

IPC分类号： B21D53/78 ,  B21D3/16 ,  B23P6/00

CPC分类号： B23P6/002 ,  F01D5/005 ,  F05D2230/80 ,  Y10T29/37 ,  Y10T29/49316 ,  Y10T29/49318 ,  Y10T29/49325 ,  Y10T29/49336 ,  Y10T29/49716 ,  Y10T29/49718 ,  Y10T29/53

摘要： A system and method for reconfiguring an airfoil of a turbine vane segment. In at least one embodiment, the system may be used to straighten an airfoil of a turbine vane segment to remove lean, twist, or racking, or any combination thereof. The airfoil may be straightened by applying a load to an inner shroud in a direction that is generally tangential to an outer shroud of the turbine vane segment. Orifices may be cut into the airfoil suction side, inboard of the outer shroud, to facilitate the straightening process. The orifices may be sealed upon completion of the process.

摘要翻译： 一种用于重新配置涡轮叶片段的翼型的系统和方法。 在至少一个实施例中，该系统可以用于矫直涡轮叶片段的翼型件以去除倾斜，扭转或翻倒，或其任何组合。 可以通过沿与涡轮叶片段的外护罩大致相切的方向向内护罩施加负载来使翼型矫直。 孔可以被切入机翼吸入侧，在外护罩的内侧，以便矫直过程。 在完成该过程之后，可以密封孔。

公开(公告)号：US08614989B2

公开(公告)日：2013-12-24

申请号：US13452437

申请日：2012-04-20

申请人： Changming Liu ,  Yong Kang ,  Jianlin Zeng ,  Sreekanth Reddy

发明人： Changming Liu ,  Yong Kang ,  Jianlin Zeng ,  Sreekanth Reddy

IPC分类号： H04W4/00

CPC分类号： H04W36/0011 ,  H04L12/4633 ,  H04L63/0876 ,  H04W8/005 ,  H04W8/02 ,  H04W8/087 ,  H04W8/18 ,  H04W8/26 ,  H04W12/04 ,  H04W28/08 ,  H04W36/0016 ,  H04W36/0061 ,  H04W36/0066 ,  H04W36/08 ,  H04W36/245 ,  H04W48/16 ,  H04W76/12 ,  H04W76/22 ,  H04W84/12 ,  H04W88/08

摘要： A network device of a subnet determines predictive roaming information for a wireless client. Predictive roaming information can identify the wireless client and a home network subnet of the wireless client. The network device provides predictive roaming information associated with a wireless client to neighboring subnets. Neighboring subnets store received predictive roaming information, and use the predictive roaming information if the wireless client roams to them.

公开(公告)号：US20070083836A1

公开(公告)日：2007-04-12

申请号：US11491073

申请日：2006-07-24

申请人： Yong Kang

发明人： Yong Kang

IPC分类号： G06F17/50

CPC分类号： H05K1/181 ,  G06F17/5077 ,  H05K2201/09227 ,  H05K2201/10159 ,  H05K2201/10689 ,  Y02P70/611

摘要： A method of wiring data transmission lines between a CPU including CPU data pins identified by a set of pin numbers and a DRAM including DRAM data pins also identified by the set of pin numbers, the method including connecting the CPU data pins to the DRAM data pins with data transmission lines including unit-bit data transmission lines so that the unit-bit data transmission lines do not cross each other and without matching the pin numbers of the CPU data pins to the pin numbers of the DRAM data pins.

摘要翻译： 一种在包括由一组引脚号码识别的CPU数据引脚的CPU与包含DRAM数据引脚的DRAM之间布线数据传输线的方法，该引脚也由该组引脚号标识，该方法包括将CPU数据引脚连接到DRAM数据引脚 数据传输线包括单位数据传输线，使得单位数据传输线不互相交叉，而不将CPU数据引脚的引脚号与DRAM数据引脚的引脚号进行匹配。

公开(公告)号：US20060105757A1

公开(公告)日：2006-05-18

申请号：US11257919

申请日：2005-10-25

申请人： Yong Kang ,  Ji Jung ,  Myung Lee ,  In Kim ,  Kwang Choi

发明人： Yong Kang ,  Ji Jung ,  Myung Lee ,  In Kim ,  Kwang Choi

IPC分类号： H04M3/00

CPC分类号： H04M1/0235 ,  G06F1/1624 ,  G06F1/1677 ,  G06F1/1684 ,  H04M1/0245 ,  H04M1/72519 ,  H04M2250/12

摘要： A wireless communication terminal with an opening/closing function using a plurality of magnetic pole sensors and method therefor is provided. The invention activates or inactivates a display unit via a switch by sensing an opening/closing of a sub-body using the magnetic pole sensors, to thereby prevent a malfunctioning due to a magnetic pole caused by an external magnetic pole generator. The inventive wireless communication terminal comprises a first magnetic pole generator for generating a north (N) magnetic pole, a second magnetic pole generator for generating a south (S) magnetic pole, a first magnetic pole sensor for sensing the N magnetic pole from the first magnetic pole generator, a second magnetic pole sensor for sensing the S magnetic pole from the second magnetic pole generator, a controller for controlling an operation of a switch to activate or inactivate an output unit based on the sense result from the first and the second magnetic pole sensors, the switch performing a switching operation in response to a control signal from the controller, and the output unit activated or inactivated in accordance with the switching operation of the switch.

摘要翻译： 提供一种具有使用多个磁极传感器的打开/关闭功能的无线通信终端及其方法。 本发明通过使用磁极传感器感测子体的开/关来通过开关来激活或灭活显示单元，从而防止由外部磁极发生器引起的磁极引起的故障。 本发明的无线通信终端包括用于产生北（N）磁极的第一磁极发生器，用于产生南（S）磁极的第二磁极发生器，用于从第一磁极感测N磁极的第一磁极传感器 磁极发生器，用于感测来自第二磁极发生器的S磁极的第二磁极传感器，用于基于来自第一和第二磁极的感测结果来控制开关的操作以激活或失活输出单​​元的控制器 所述开关响应于来自所述控制器的控制信号执行切换操作，并且所述输出单元根据所述开关的切换操作而被激活或非激活。

公开(公告)号：US20050253295A1

公开(公告)日：2005-11-17

申请号：US11117644

申请日：2005-04-29

申请人： Jin-Hua Song ,  Yong Kang ,  Karnik Tarverdi ,  Bruce Yeo

发明人： Jin-Hua Song ,  Yong Kang ,  Karnik Tarverdi ,  Bruce Yeo

IPC分类号： B29C44/46 ,  B29C47/88 ,  B29C47/90 ,  B29C65/48 ,  B29C69/02 ,  B29C47/00

CPC分类号： B29C44/468 ,  B29C44/20 ,  B29C44/3402 ,  B29C48/001 ,  B29C48/0012 ,  B29C48/06 ,  B29C48/15 ,  B29C48/90 ,  B29C48/91 ,  B29C65/48 ,  B29C65/4895 ,  B29C66/0222 ,  B29C66/1122 ,  B29C66/43 ,  B29C66/435 ,  B29C66/526 ,  B29C66/727 ,  B29K2003/00 ,  B29K2105/0005 ,  B29K2105/0038 ,  B29K2105/0097 ,  B29K2105/04 ,  B29K2995/006 ,  B29L2031/712 ,  B29C65/00

摘要： An apparatus and a method for making a biodegradable material are disclosed. The apparatus comprises an extruder for forming a foamed starch rod and a heated die for modifying the rod. The rod is fed through the heated die by feeding rollers. A bonding agent application station is located downstream of the heated die and upstream of a packing unit. The method comprises forming a foamed starch rod by extrusion and passing the rod through a heated die. The rods may be formed into sheets or blocks by cutting, the application of bonding agent and adhering the cut rods together.

摘要翻译： 公开了一种用于制造可生物降解材料的装置和方法。 该装置包括用于形成发泡淀粉棒的挤出机和用于改变棒的加热模具。 通过进给辊将杆送入加热模具。 粘合剂施用站位于加热模具的下游和包装单元的上游。 该方法包括通过挤压成型发泡淀粉棒并使棒穿过加热的模头。 杆可以通过切割，施加粘合剂并将切割杆粘合在一起而形成片或块。