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1. 发明申请

WO2014186006A3 COOLING HOLE FOR A GAS TURBINE ENGINE COMPONENT 审中-公开
标题翻译：用于气体涡轮发动机部件的冷却孔
公开(公告)号：WO2014186006A3
公开(公告)日：2015-02-26
申请号：PCT/US2014015198
申请日：2014-02-07
申请人： UNITED TECHNOLOGIES CORP
发明人： XU JINQUAN
IPC分类号： F01D25/12 , F01D5/18 , F01D9/02 , F02C7/18 , F04D29/58
CPC分类号： F01D5/186 , F01D5/288 , F01D9/023 , F01D9/065 , F01D11/08 , F05D2240/81 , F05D2260/202 , F23R3/002 , F23R3/02 , F23R2900/03042
摘要： A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a wall having an internal surface, an outer skin and a cooling hole having an inlet extending from the internal surface and merging into a metering section, and a diffusion section downstream of the metering section that extends to an outlet located at the outer skin. At least two lobes are embedded within the diffusion section of the cooling hole. At least one surface of each of the at least two lobes is at least partially cylindrical.
摘要翻译：根据本公开的示例性方面的用于燃气涡轮发动机的部件尤其包括具有内表面，外表皮和冷却孔的壁，所述壁具有从内表面延伸并且合并到计量部分中的入口以及在计量部分下游延伸到位于外皮的出口的扩散部分。至少两个叶片嵌入在冷却孔的扩散部分内。至少两个裂片中的每一个的至少一个表面至少部分是圆柱形的。

2. 发明申请

WO2015017095A3 PLATED POLYMER NOSECONE 审中-公开
公开(公告)号：WO2015017095A3
公开(公告)日：2015-04-09
申请号：PCT/US2014045985
申请日：2014-07-09
申请人： UNITED TECHNOLOGIES CORP
发明人： ROACH JAMES T , KLING COLIN J , COOK GRANT O III , MCPHAIL JAMES J , BUGAJ SHARI L , O'BRIEN JAMES F , DEHLAVI MAJIDULLAH , SMITH SCOTT A , RADER MATTHEW R , TURNER MATTHEW A , XU JINQUAN
IPC分类号： F01D25/00 , B29D22/00 , F01D25/24 , F02C7/20
CPC分类号： B64D29/00 , B29D22/00 , F01D5/02 , F01D25/28 , F02K3/04 , F05D2220/32 , F05D2230/30 , F05D2230/90 , F05D2300/10 , F05D2300/43 , F05D2300/603 , Y02T50/672
摘要： Plated polymeric gas turbine engine parts and methods for fabricating lightweight plated polymeric gas turbine engine parts are disclosed. The parts include a polymeric substrate plated with one or more metal layers. The polymeric material of the polymeric substrate may be structurally reinforced with materials that may include carbon, metal, or glass. The polymeric substrate may also include a plurality of layers to form a composite layup structure.
摘要翻译：公开了用于制造轻质电镀聚合物燃气涡轮发动机部件的电镀聚合物燃气涡轮发动机部件和方法。部件包括镀有一个或多个金属层的聚合物基底。聚合物基材的聚合物材料可以用可包含碳，金属或玻璃的材料在结构上增强。聚合物基材还可以包括多个层以形成复合叠层结构。

3. 发明申请

WO2013123008A8 GAS TURBINE ENGINE COMPONENT WITH CONVERGING/DIVERGING COOLING PASSAGE 审中-公开
标题翻译：具有混合/分流式冷却通气的气体涡轮发动机部件
公开(公告)号：WO2013123008A8
公开(公告)日：2014-09-04
申请号：PCT/US2013025881
申请日：2013-02-13
申请人： UNITED TECHNOLOGIES CORP
发明人： XU JINQUAN , LEVASSEUR GLENN
IPC分类号： F02C7/00 , F01D25/08 , F02C7/12 , F02C9/00
CPC分类号： F01D5/186 , F01D9/041 , F01D25/12 , F05D2220/32 , F05D2250/14 , F05D2250/20 , F05D2250/52 , F05D2250/70 , F05D2260/202 , F05D2260/2212 , Y02T50/676
摘要： A component for a gas turbine engine includes a gas path wall having a first surface and a second surface and a cooling hole extending through the gas path wall from the first surface to the second surface. The cooling hole includes an inlet portion having an inlet at the first surface, an outlet portion having an outlet at the second surface, and a transition defined between the inlet and the outlet. The inlet portion converges in a first direction from the inlet to the transition and diverges in a second direction from the inlet to the transition. The outlet portion diverges at least in one of the first and second directions from the transition to the outlet.
摘要翻译：用于燃气涡轮发动机的部件包括具有第一表面和第二表面的气体通道壁和从第一表面延伸穿过气体通道壁到第二表面的冷却孔。冷却孔包括在第一表面具有入口的入口部分，在第二表面具有出口的出口部分和在入口和出口之间限定的过渡。入口部分在从入口到过渡部的第一方向上会聚，并且在从入口到过渡的第二方向上发散。出口部分至少在第一和第二方向中的一个方向上从过渡到出口发散。

4. 发明申请

WO2014081490A2 FILM COOLING CHANNEL ARRAY WITH MULTIPLE METERING PORTIONS 审中-公开
标题翻译：薄膜冷却通道阵列与多个测量部分
公开(公告)号：WO2014081490A2
公开(公告)日：2014-05-30
申请号：PCT/US2013057040
申请日：2013-08-28
申请人： UNITED TECHNOLOGIES CORP
发明人： XU JINQUAN , LEVASSEUR GLENN
IPC分类号： F01D5/18
CPC分类号： F01D5/186 , F01D9/065 , F05D2240/81 , F05D2250/312 , F05D2260/202 , F23R2900/03042 , Y02T50/676
摘要： A cooling channel array for a gas turbine engine is provided. The cooling channel array is carried by a component wall having an inner surface and an outer surface and comprises at least two metering portions that communicate with a diffusion cavity.
摘要翻译：提供了一种用于燃气涡轮发动机的冷却通道阵列。冷却通道阵列由具有内表面和外表面的部件壁承载，并且包括与扩散腔连通的至少两个计量部分。

5. 发明申请

WO2014081489A2 FILM COOLING CHANNEL ARRAY HAVING ANTI-VORTEX PROPERTIES 审中-公开
标题翻译：电影冷却通道阵列具有反VORTEX属性
公开(公告)号：WO2014081489A2
公开(公告)日：2014-05-30
申请号：PCT/US2013057034
申请日：2013-08-28
申请人： UNITED TECHNOLOGIES CORP
发明人： XU JINQUAN
IPC分类号： F28F3/12
CPC分类号： F01D5/186 , F01D9/065 , F05D2240/81 , F05D2260/202 , F23R3/002 , F23R2900/03042 , Y02T50/676
摘要： A cooling channel array carried by a component wall of a gas turbine engine is provided. The cooling channel array comprises a diffusion cavity and a metering section. The metering section comprises a main hole and two or more side holes. The side holes may be separate from the main hole or may branch off of the main hole. The diffusion cavity may incorporate a lobed configuration to help diffuse cooling fluid as it exits the cooling channel array.
摘要翻译：提供了由燃气涡轮发动机的部件壁承载的冷却通道阵列。冷却通道阵列包括扩散腔和计量部。计量部分包括主孔和两个或更多个侧孔。侧孔可以与主孔分离，或者可以从主孔分支。扩散腔可以包括叶形结构，以帮助冷却流体在离开冷却通道阵列时扩散。

6. 发明申请

WO2013165508A3 MULTI-LOBED COOLING HOLE ARRAY 审中-公开
标题翻译：多孔冷却孔阵列
公开(公告)号：WO2013165508A3
公开(公告)日：2013-12-27
申请号：PCT/US2013025710
申请日：2013-02-12
申请人： UNITED TECHNOLOGIES CORP
发明人： XU JINQUAN
IPC分类号： F02C7/18 , F01D5/08 , F01D25/12 , F02K3/00
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。

7. 发明申请

WO2013165503A2 COOLING HOLE WITH ENHANCED FLOW ATTACHMENT 审中-公开
标题翻译：冷却孔与增强的流量附件
公开(公告)号：WO2013165503A2
公开(公告)日：2013-11-07
申请号：PCT/US2013025684
申请日：2013-02-12
申请人： UNITED TECHNOLOGIES CORP
发明人： XU JINQUAN , LEVASSEUR GLENN
IPC分类号： F02C7/18 , F01D5/08 , F01D25/12 , F02K3/00
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。

8. 发明申请

WO2014204570A3 REGENERATING AN ADDITIVELY MANUFACTURED COMPONENT 审中-公开
标题翻译：重新制造附加的制造部件
公开(公告)号：WO2014204570A3
公开(公告)日：2015-03-05
申请号：PCT/US2014034455
申请日：2014-04-17
申请人： UNITED TECHNOLOGIES CORP
发明人： MCBRIEN JOHN , CASTLE LEA KENNARD , SPANGLER BRANDON W , XU JINQUAN
IPC分类号： B23K26/342 , B22F3/105 , C22C19/00
CPC分类号： F01D5/28 , B22C7/02 , B22C9/02 , B22C9/043 , B22C9/061 , B22C9/10 , B22C9/101 , B22C9/108 , B22C9/22 , B22C9/24 , B22D23/06 , B22D25/02 , B22D27/04 , B22D27/045 , B22F3/1055 , B22F3/11 , B22F3/24 , B22F5/04 , B22F2003/248 , B22F2998/00 , B22F2998/10 , B23K15/0006 , B23K15/0086 , B23K26/342 , B32B1/08 , B32B3/08 , B32B3/26 , B32B5/16 , B32B9/005 , B32B2250/03 , B32B2264/105 , B32B2603/00 , B33Y10/00 , B33Y80/00 , C30B11/00 , C30B29/52 , F01D5/147 , F01D5/18 , F01D5/187 , F01D5/282 , F01D9/02 , F01D9/041 , F01D9/065 , F01D25/12 , F05D2220/32 , F05D2230/31 , F05D2300/175 , F05D2300/211 , F05D2300/607 , F23R3/28 , Y02P10/292 , Y02P10/295 , B22F2003/242 , C30B11/14
摘要： One embodiment includes a method to regenerate a component (10). The method includes additively manufacturing a component (10) to have voids greater than 0 percent but less than approximately 15 percent in a near finished shape. The component (10) is encased in a shell mold (22). The shell mold (22) is cured. The encased component (10) is placed in a furnace and the component (10) is melted. The component (10) is solidified in the shell mold (22). The shell mold (22) is removed from the solidified component (10).
摘要翻译：一个实施例包括重新生成组件（10）的方法。该方法包括在接近完成的形状中相加地制造具有大于0％但小于约15％的空隙的部件（10）。组件（10）被封装在壳模（22）中。壳模（22）固化。被封装的部件（10）被放置在炉中并且部件（10）熔化。组分（10）在壳模（22）中固化。从凝固组分（10）中除去壳模（22）。

9. 发明申请

WO2014197043A3 MULTI-LOBED COOLING HOLE 审中-公开
标题翻译：多孔冷却孔
公开(公告)号：WO2014197043A3
公开(公告)日：2015-02-26
申请号：PCT/US2014023346
申请日：2014-03-11
申请人： UNITED TECHNOLOGIES CORP
发明人： XU JINQUAN
IPC分类号： F02C7/12 , F01D5/18 , F01D25/12 , F02C7/18 , F04D29/58
CPC分类号： F01D5/186 , F01D9/065 , F05D2240/11 , F05D2240/81 , F05D2250/73 , F05D2260/202 , F23R2900/03042 , Y02T50/676
摘要： A gas turbine engine component subjected to a flow of high temperature gas includes a wall having first and second surfaces and a cooling hole extending through the wall. The cooling hole includes an inlet located at the first surface, an outlet located at the second 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 having a first downstream end adjacent the outlet and spaced from the inlet by a first distance, a second lobe diverging longitudinally from the metering section and having a second downstream end adjacent the outlet and spaced from the inlet by a second distance different from the first, and a transition region positioned between the lobes, the transition region having a third downstream end adjacent the outlet.
摘要翻译：经受高温气体流动的燃气涡轮发动机部件包括具有第一和第二表面的壁和延伸穿过壁的冷却孔。冷却孔包括位于第一表面处的入口，位于第二表面处的出口，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开的第一凸角，并且具有邻近出口并与入口间隔第一距离的第一下游端，与计量部分纵向分开的第二凸角，并且具有相邻的第二下游端出口并且与入口间隔开不同于第一距离的第二距离，以及位于叶片之间的过渡区域，过渡区域具有邻近出口的第三下游端。

10. 发明申请

WO2015006433A2 PLATED POLYMER FAN 审中-公开
标题翻译：镀聚合物粉末
公开(公告)号：WO2015006433A2
公开(公告)日：2015-01-15
申请号：PCT/US2014045928
申请日：2014-07-09
申请人： UNITED TECHNOLOGIES CORP
发明人： ROACH JAMES T , BARNETT BARRY , COOK III GRANT O , WATSON CHARLES R , BUGAJ SHARI L , LEVASSEUR GLENN , TWELVES WENDELL V JR , HERTEL CHRISTOPHER J , KLING COLIN J , TURNER MATTHEW A , XU JINQUAN , CLARKSON STEVEN , CAULFIELD MICHAEL
CPC分类号： F04D19/002 , B32B1/00 , B32B1/08 , B32B27/281 , B32B27/285 , B32B27/34 , B32B27/36 , B32B2255/10 , B32B2255/205 , B32B2262/101 , B32B2262/103 , B32B2262/106 , B32B2270/00 , B32B2307/554 , F01D5/147 , F01D5/26 , F01D5/282 , F01D5/286 , F01D9/041 , F01D25/02 , F01D25/24 , F04D29/388 , F04D29/541 , F05D2220/32 , F05D2230/90 , F05D2240/00 , F05D2240/12 , F05D2240/30 , F05D2260/96 , F05D2300/10 , F05D2300/43 , F05D2300/603 , Y02T50/672 , Y02T50/673
摘要： Plated polymeric gas turbine engine parts and methods for fabricating lightweight plated polymeric gas turbine engine parts are disclosed. The parts include a polymeric substrate plated with one or more metal layers. The polymeric material of the polymeric substrate may be structurally reinforced with materials that may include carbon, metal, or glass. The polymeric substrate may also include a plurality of layers to form a composite layup structure.
摘要翻译：公开了用于制造轻质电镀聚合物燃气涡轮发动机部件的电镀聚合物燃气涡轮发动机部件和方法。这些部件包括镀有一个或多个金属层的聚合物基材。聚合物基材的聚合材料可以用可以包括碳，金属或玻璃的材料在结构上加强。聚合物基底还可以包括多个层以形成复合铺层结构。

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