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1. 发明授权

US09243502B2 Airfoil cooling enhancement and method of making the same 有权
标题翻译：翼型冷却增强及其制作方法
公开(公告)号：US09243502B2
公开(公告)日：2016-01-26
申请号：US13454180
申请日：2012-04-24
申请人： JinQuan Xu
发明人： JinQuan Xu
IPC分类号： B22F5/00 , F01D5/18 , B22F3/105 , B23P15/02
CPC分类号： F01D5/187 , B22C9/10 , B22C9/18 , B22F3/1055 , B22F5/009 , B22F7/08 , B22F2005/005 , B23P15/02 , B28B1/001 , B28B7/342 , C04B2235/6026 , C04B2235/665 , C30B1/02 , C30B29/52 , F05D2230/22 , F05D2230/31 , F05D2230/40 , F05D2250/241 , F05D2260/2212 , F05D2260/2214 , Y02P10/292 , Y02P10/295 , Y10T29/49336 , Y10T29/49341
摘要： An airfoil includes a body that includes leading and trailing edges joined by spaced apart pressure and suction sides to provide an exterior airfoil surface. A cooling passage is arranged interiorly of the exterior airfoil surface and provides an interior surface. The interior cooling surface includes micro-bumps that protrude from the interior cooling surface into the cooling passage. The micro-bumps are discrete from and noncontiguous relative to one another in multiple directions along the interior cooling surface. The micro-bumps may be provided while forming the airfoil or using correspondingly shaped micro-depressions on an airfoil core.
摘要翻译：翼型件包括主体，其包括通过间隔开的压力和吸力侧连接的前缘和后缘，以提供外部翼面表面。冷却通道设置在外部翼面表面的内部并提供内表面。内部冷却表面包括从内部冷却表面突出到冷却通道中的微小凸起。微型凸块沿着内部冷却表面在多个方向上相对于彼此离散并且不连续。可以在形成翼型件或在翼型件芯上使用相应形状的微凹陷时提供微型凸块。

2. 发明申请

US20130280092A1 AIRFOIL COOLING ENHANCEMENT AND METHOD OF MAKING THE SAME 有权
标题翻译：气流冷却增强及其制造方法
公开(公告)号：US20130280092A1
公开(公告)日：2013-10-24
申请号：US13454180
申请日：2012-04-24
申请人： JinQuan Xu
发明人： JinQuan Xu
IPC分类号： F01D5/18 , B23P17/00 , B23P15/02
CPC分类号： F01D5/187 , B22C9/10 , B22C9/18 , B22F3/1055 , B22F5/009 , B22F7/08 , B22F2005/005 , B23P15/02 , B28B1/001 , B28B7/342 , C04B2235/6026 , C04B2235/665 , C30B1/02 , C30B29/52 , F05D2230/22 , F05D2230/31 , F05D2230/40 , F05D2250/241 , F05D2260/2212 , F05D2260/2214 , Y02P10/292 , Y02P10/295 , Y10T29/49336 , Y10T29/49341
摘要： An airfoil includes a body that includes leading and trailing edges joined by spaced apart pressure and suction sides to provide an exterior airfoil surface. A cooling passage is arranged interiorly of the exterior airfoil surface and provides an interior surface. The interior cooling surface includes micro-bumps that protrude from the interior cooling surface into the cooling passage. The micro-bumps are discrete from and noncontiguous relative to one another in multiple directions along the interior cooling surface. The micro-bumps may be provided while forming the airfoil or using correspondingly shaped micro-depressions on an airfoil core.
摘要翻译：翼型件包括主体，其包括通过间隔开的压力和吸力侧连接的前缘和后缘，以提供外部翼面表面。冷却通道设置在外部翼面表面的内部并提供内表面。内部冷却表面包括从内部冷却表面突出到冷却通道中的微小凸起。微型凸块沿着内部冷却表面在多个方向上相对于彼此离散并且不连续。可以在形成翼型件或在翼型件芯上使用相应形状的微凹陷时提供微型凸块。

3. 发明授权

US08522558B1 Multi-lobed cooling hole array 有权
标题翻译：多叶冷却孔阵列
公开(公告)号：US08522558B1
公开(公告)日：2013-09-03
申请号：US13544112
申请日：2012-07-09
申请人： JinQuan Xu
发明人： JinQuan Xu
IPC分类号： F23R3/00
CPC分类号： F01D5/186 , F05D2250/324 , F05D2250/52 , F05D2260/202 , F05D2260/221 , Y02T50/676 , Y10T29/49323
摘要： A gas turbine engine component includes a wall having first and second wall surfaces and first and second cooling holes extending through the wall. The first and second cooling holes each include an inlet located at the first wall surface, an outlet located at the second wall surface, a metering section extending downstream from the inlet and a diffusing section extending from the metering section to the outlet. Each diffusing section includes first and second lobes, each lobe diverging longitudinally and laterally from the metering section. The outlets of each cooling hole include first and second lateral ends and a trailing edge. One of the lateral ends of the outlet of the first cooling hole and one of the lateral ends of the outlet of the second cooling hole meet upstream of the trailing edge of the first cooling hole and the trailing edge of the second cooling hole.
摘要翻译：燃气涡轮发动机部件包括具有第一和第二壁表面的壁和延伸穿过壁的第一和第二冷却孔。第一和第二冷却孔各自包括位于第一壁表面处的入口，位于第二壁表面处的出口，从入口下游延伸的计量部分和从计量部分延伸到出口的扩散部分。每个漫射部分包括第一和第二瓣，每个瓣从计量部分纵向和横向发散。每个冷却孔的出口包括第一和第二侧端和后缘。第一冷却孔的出口的横向端部和第二冷却孔的出口的一个横向端部与第一冷却孔的后缘和第二冷却孔的后缘相连。

4. 发明申请

US20130205794A1 GAS TURBINE ENGINE COMPONENT WITH IMPINGEMENT AND LOBED COOLING HOLE 有权
标题翻译：气动涡轮发动机组件与冲击和滚动冷却孔
公开(公告)号：US20130205794A1
公开(公告)日：2013-08-15
申请号：US13544257
申请日：2012-07-09
申请人： JinQuan Xu
发明人： JinQuan Xu
IPC分类号： F23R3/02 , F02C7/12
CPC分类号： F01D5/186 , F01D9/065 , F05D2240/81 , F05D2260/201 , F05D2260/202 , F23R3/06 , F23R2900/03042 , Y02T50/673 , Y02T50/676
摘要： A gas turbine engine component includes a gas path wall having a first and second opposing surfaces and a baffle positioned along the gas path wall. The baffle has impingement holes for directing cooling fluid onto the first surface of the gas path wall. A cooling hole is formed in the gas path wall and extends from a metering section having an inlet in the first surface through a transition to a diffusing section having an outlet in the second surface. A longitudinal ridge extends along the cooling hole between the transition and the outlet. The longitudinal ridge divides the diffusing section of the cooling hole into first and second lobes.
摘要翻译：燃气涡轮发动机部件包括具有第一和第二相对表面的气体通道壁和沿着气体路径壁定位的挡板。挡板具有用于将冷却流体引导到气体通道壁的第一表面上的冲击孔。在气体通道壁中形成冷却孔，并且从具有第一表面中的入口的计量部分延伸通过在第二表面中具有出口的扩散部分的过渡。纵向脊沿着过渡段和出口之间的冷却孔延伸。纵向脊将冷却孔的扩散部分分成第一和第二凸角。

5. 发明申请

US20130050348A1 PRINTHEAD SUPPORT STRUCTURE INCLUDING THERMAL INSULATOR 有权
标题翻译： PRINTHEAD支撑结构，包括热绝缘体
公开(公告)号：US20130050348A1
公开(公告)日：2013-02-28
申请号：US13217715
申请日：2011-08-25
申请人： Mikhail Fishkin , Andrew Ciaschi , Jinquan Xu
发明人： Mikhail Fishkin , Andrew Ciaschi , Jinquan Xu
IPC分类号： B41J2/05
CPC分类号： B41J2/1433 , B41J2/1606
摘要： A printing system includes a plurality of inkjet printheads for printing on a print media that is moved relative to the plurality of printheads and a support structure for locating the plurality of printheads relative to the print media. The support structure includes a face adjacent to the print media. The face of the support structure includes a thermal insulator.
摘要翻译：打印系统包括用于在相对于多个打印头移动的打印介质上打印的多个喷墨打印头和用于相对于打印介质定位多个打印头的支撑结构。支撑结构包括与打印介质相邻的面。支撑结构的表面包括热绝缘体。

6. 发明申请

US20100295911A1 ROTATING COANDA CATCHER 有权
标题翻译：旋转COANDA CATCHER
公开(公告)号：US20100295911A1
公开(公告)日：2010-11-25
申请号：US12468077
申请日：2009-05-19
申请人： Jinquan Xu
发明人： Jinquan Xu
IPC分类号： B41J2/185
CPC分类号： B41J2/185
摘要： A catcher includes a housing and a drop contact structure. The housing defines a liquid removal conduit. The drop contact structure includes a moveable surface that delivers collected liquid drops to the liquid removal conduit of the housing.
摘要翻译：抓地器包括壳体和液滴接触结构。壳体限定了液体移除导管。液滴接触结构包括将收集的液滴输送到壳体的液体移除导管的可移动表面。

7. 发明授权

US07824019B2 Continuous printing apparatus having improved deflector mechanism 有权
标题翻译：连续打印设备具有改进的导流器机构
公开(公告)号：US07824019B2
公开(公告)日：2010-11-02
申请号：US11744987
申请日：2007-05-07
申请人： Zhanjun Gao , Jinquan Xu
发明人： Zhanjun Gao , Jinquan Xu
IPC分类号： B41J2/09
CPC分类号： B41J2/09 , B41J2002/031 , B41J2002/033
摘要： A printing system includes a liquid drop ejector, a fluid flow device, and a fluid flow source. The liquid drop ejector is operable to eject liquid drops having a plurality of volumes along a first path. The fluid flow device includes a first section comprising a plurality of sub-channels created by a partition and a second section comprising a plurality of sub-channels created by a partition. Each partition has a height as viewed from a wall of the fluid flow device. The height of the partition of the second section is less than the height of the partition of the first section. The fluid flow source is operable to produce a fluid flow through the fluid flow device. The fluid flow interacts with the liquid drops to cause liquids drops having one of the plurality of volumes to begin moving along a second path.
摘要翻译：打印系统包括液滴喷射器，流体流动装置和流体流动源。液滴喷射器可操作以沿着第一路径排出具有多个体积的液滴。流体流动装置包括第一部分，其包括由分区产生的多个子通道和包括由分区产生的多个子通道的第二部分。每个隔板具有从流体流动装置的壁观察的高度。第二部分的隔板的高度小于第一部分的隔板的高度。流体流动源可操作以产生流过流体流动装置的流体流。流体流与液滴相互作用以引起具有多个体积中的一个体积的液滴开始沿第二路径移动。

8. 发明申请

US20080088680A1 CONTINUOUS DROP EMITTER WITH REDUCED STIMULATION CROSSTALK 有权
标题翻译：具有减少刺激性CROSSTALK的连续喷射发射器
公开(公告)号：US20080088680A1
公开(公告)日：2008-04-17
申请号：US11548709
申请日：2006-10-12
申请人： Jinquan Xu , Randolph C. Brost , Qing Yang , Fernando Lopes , Stephen F. Pond
发明人： Jinquan Xu , Randolph C. Brost , Qing Yang , Fernando Lopes , Stephen F. Pond
IPC分类号： B41J2/02
CPC分类号： B41J2/03 , B41J2002/022 , B41J2002/033 , B41J2202/13 , B41J2202/16
摘要： A continuous drop emitter comprising a liquid supply chamber containing a liquid held at a positive pressure; first and second nozzles in fluid communication with the liquid supply chamber nozzles emitting first and second continuous streams of a liquid; first and second stream break-up transducers adapted to independently synchronize the break up of the first and second continuous streams of the liquid into first and second streams of drops of predetermined volumes, respectively; and an acoustic damping material located adjacent to or within the liquid supply chamber for damping sound waves generated within the liquid chamber by the first and second stream break-up transducer. The continuous drop emitter may also configured with a Helmholtz resonant chamber tuned to a critical stimulation frequency having an acoustic damping material therein for absorbing acoustic stimulation energy. The Helmholtz resonant chamber may serve as a portion of the common liquid supply for the first and second jets in which case the acoustic damping material may be porous to allow the liquid to pass through. The acoustic damping materials may acoustically lossy materials that transmute energy into heat via molecular motions. The acoustic damping materials may be porous materials that absorb acoustic energy by forcing the liquid through small passages causing viscous flow energy losses. In addition the acoustic damping materials may include components that cause the disruption of acoustic waves by reflection from materials that are impedance mismatched to the liquid, either very dense materials or gas filled voids.
摘要翻译：一种连续液滴发射器，包括一个含有保持在正压力下的液体的液体供应室; 第一和第二喷嘴与液体供应室喷嘴流体连通，发射第一和第二连续的液体流; 第一和第二流分解换能器，其适于独立地将所述液体的所述第一和第二连续流的分解独立地同步到预定体积的第一和第二液滴流中; 以及声音阻尼材料，其位于液体供应室附近或内部，用于阻止由第一和第二流断裂传感器在液体室内产生的声波。连续液滴发射器还可以配置有调谐到临界刺激频率的亥姆霍兹谐振腔，其中具有用于吸收声学刺激能量的声阻尼材料。亥姆霍兹共振腔可以用作第一和第二射流的公共液体供应的一部分，在这种情况下，声阻尼材料可以是多孔的以允许液体通过。声阻尼材料可以通过分子运动将能量转变成热量的声学损耗材料。声阻尼材料可以是通过迫使液体通过小通道而引起粘性流动能量损失来吸收声能的多孔材料。此外，声阻尼材料可以包括通过来自与液体阻抗不匹配的材料（非常致密的材料或气体填充的空隙）的反射导致声波破坏的组件。

9. 发明授权

US09422815B2 Gas turbine engine component with compound cusp cooling configuration 有权
标题翻译：燃气轮机组件具有复合尖端冷却配置
公开(公告)号：US09422815B2
公开(公告)日：2016-08-23
申请号：US13544227
申请日：2012-07-09
申请人： JinQuan Xu
发明人： JinQuan Xu
IPC分类号： F01D5/18 , F01D9/06
CPC分类号： F01D5/187 , F01D5/186 , F01D9/041 , F01D9/065 , F01D25/12 , F01D25/24 , F01D25/30 , F02C3/04 , F04D29/324 , F04D29/522 , F04D29/542 , F04D29/582 , F05D2220/32 , F05D2240/35 , F05D2240/81 , F05D2250/70 , F05D2250/71 , F05D2260/202 , F23R3/002 , F23R2900/03042 , Y02T50/676
摘要： A component for a gas turbine engine including a gas path wall having a first surface and a second surface. A cooling hole extends through the gas path wall from an inlet in the first surface through a transition to an outlet in the second surface. Cusps are formed on the transition.
摘要翻译：一种用于燃气涡轮发动机的部件，其包括具有第一表面和第二表面的气体通道壁。冷却孔从第一表面中的入口穿过气体通道壁延伸穿过第二表面中的出口。尖峰形成在过渡处。

10. 发明授权

US09416665B2 Cooling hole with enhanced flow attachment 有权
标题翻译：冷却孔具有增强的流动附件
公开(公告)号：US09416665B2
公开(公告)日：2016-08-16
申请号：US13544074
申请日：2012-07-09
申请人： JinQuan Xu , Glenn Levasseur
发明人： JinQuan Xu , Glenn Levasseur
IPC分类号： F01D5/18 , F01D9/06
CPC分类号： F01D5/186 , F01D9/065 , F05D2240/81 , F05D2260/202 , F23R2900/03042 , Y02T50/676
摘要： A gas turbine engine component includes a wall having first and second wall surfaces, a cooling hole extending through the wall and a convexity. The cooling hole includes an inlet located at the first wall surface, an outlet located at the second wall surface, a metering section extending downstream from the inlet and a diffusing section extending from the metering section to the outlet. The diffusing section includes a first lobe diverging longitudinally and laterally from the metering section and a second lobe adjacent the first lobe and diverging longitudinally and laterally from the metering section. The convexity is located near the outlet.
摘要翻译：燃气涡轮发动机部件包括具有第一和第二壁表面的壁，延伸穿过壁的冷却孔和凸起。冷却孔包括位于第一壁表面的入口，位于第二壁表面处的出口，从入口下游延伸的计量部分和从计量部分延伸到出口的扩散部分。扩散部分包括从计量部分纵向和横向分叉的第一凸角和邻近第一凸角并从计量部分纵向和横向发散的第二凸角。凸起位于出口附近。

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