专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

WO2015184294A1 FASTBACK TURBULATOR 审中-公开
公开(公告)号：WO2015184294A1
公开(公告)日：2015-12-03
申请号：PCT/US2015/033240
申请日：2015-05-29
申请人： GENERAL ELECTRIC COMPANY
发明人： BUNKER, Ronald, Scott , BRIGGS, Robert, David , PEARSON, Shawn, Michael
IPC分类号： F01D5/14 , F01D5/18 , F01D25/12 , F23R3/00 , F28F13/12
CPC分类号： F01D5/145 , F01D5/141 , F01D5/187 , F01D9/04 , F01D25/12 , F05D2220/30 , F05D2240/127 , F05D2260/2212 , F23R3/005 , F23R2900/03045 , Y02T50/673 , Y02T50/676
摘要： A structure for disrupting the flow of a fluid, the structure comprising: (a) a first lateral wall and a second lateral wall spaced apart from one another a distance across an X-axis; (b) a turbulator extending between the first lateral wall and the second lateral wall, the turbulator extending away from the floor, the turbulator comprising: (i) a first front surface extending between the first lateral wall and the second lateral wall, the first front surface extending from the floor and being transverse with respect to a Z-axis extending longitudinally along the floor, (ii) a second front surface extending between the first lateral wall and the second lateral wall, the second front surface extending from the floor and being transverse with respect to the Z-axis, the second front surface not in parallel with the first front surface, (iii) a first rear surface extending between the first lateral wall and the second lateral wall, the first rear surface extending between the first front surface and the floor, the first rear surface having an inclining section that is angled between ninety and ten degrees with respect to a Y-axis extending perpendicular to the floor, the Y-axis being perpendicular to the Z-axis, and (iv) a second rear surface adjoining the first rear surface and extending between the first lateral wall and the second lateral wall, the second rear surface extending between the second front surface and the floor, the second rear surface having an inclining section that is angled between ninety and ten degrees with respect to the Y-axis, where the X-axis is perpendicular to both the Y-axis and the Z-axis.
摘要翻译：一种用于破坏流体流动的结构，所述结构包括：（a）第一侧壁和第二侧壁，所述第一侧壁和第二侧壁彼此间隔开跨越X轴的距离; （b）在所述第一侧壁和所述第二侧壁之间延伸的湍流器，所述湍流器远离所述地板延伸，所述湍流器包括：（i）在所述第一侧壁和所述第二侧壁之间延伸的第一前表面，前表面从地板延伸并相对于沿着地板纵向延伸的Z轴横向;（ii）在第一侧壁和第二侧壁之间延伸的第二前表面，第二前表面从地板延伸，相对于Z轴横向，第二前表面不与第一前表面平行，（iii）在第一侧壁和第二侧壁之间延伸的第一后表面，第一后表面在第一前表面和地板，第一后表面具有倾斜部分，该倾斜部分相对于垂直于地板延伸的Y轴成90度到10度之间，th e轴垂直于Z轴，和（iv）邻接第一后表面并在第一侧壁和第二侧壁之间延伸的第二后表面，第二后表面在第二前表面和第二侧表面之间延伸所述第二后表面具有相对于所述Y轴倾斜90度到10度的倾斜部分，所述X轴垂直于所述Y轴和Z轴。

2. 发明申请

WO2016099662A2 ENGINE COMPONENT ASSEMBLY 审中-公开
标题翻译：发动机组件组件
公开(公告)号：WO2016099662A2
公开(公告)日：2016-06-23
申请号：PCT/US2015/057708
申请日：2015-10-28
申请人： GENERAL ELECTRIC COMPANY
发明人： BERGHOLZ, Robert, Frederick , ALLEN, Jason, Randolph , BRIGGS, Robert, David , FELDMANN, Kevin, Robert , STOVER, Curtis, Walton , WEBSTER, Zachary, Daniel , REITER, Fernando
IPC分类号： F01D5/18
CPC分类号： F01D25/12 , F01D5/187 , F01D5/188 , F01D9/041 , F01D11/08 , F02C3/04 , F02C7/18 , F05D2220/32 , F05D2240/127 , F05D2240/128 , F05D2240/24 , F05D2240/35 , F05D2250/38 , F05D2250/712 , F05D2260/201 , F05D2260/202 , F05D2260/2212 , F05D2260/22141 , F05D2260/607 , F23R3/002 , F23R3/005 , F23R3/04 , F23R3/06 , F23R2900/03042 , F23R2900/03044 , F23R2900/03045 , Y02T50/672 , Y02T50/673 , Y02T50/676
摘要： An engine component assembly includes a first engine component having a hot surface in thermal communication with a hot combustion gas flow and a cooling surface with at least one cavity. A second engine component is spaced from the cooling surface, and includes at least one cooling aperture. The cooling aperture is arranged such that cooling fluid impinges on the cooling surface at an angle.
摘要翻译：发动机部件组件包括具有热表面与热燃烧气流热连通的第一发动机部件和具有至少一个空腔的冷却表面。第二发动机部件与冷却表面间隔开，并且包括至少一个冷却孔。冷却孔被布置成使得冷却流体以一定角度撞击在冷却表面上。

3. 发明申请

WO2016025054A2 ENGINE COMPONENTS WITH COOLING FEATURES 审中-公开
标题翻译：发动机组件与冷却功能
公开(公告)号：WO2016025054A2
公开(公告)日：2016-02-18
申请号：PCT/US2015/032597
申请日：2015-05-27
申请人： GENERAL ELECTRIC COMPANY
发明人： STOVER, Curtis, Walton , RAUSCH, Jonathan, Michael , ATSUCHI, Satoshi , BRAINCH, Gulcharan, Singh , BRIGGS, Robert, David , BUNKER, Ronald, Scott , KULKARNI, Ambarish, Jayant , MEADE, Michael, Alan , PRITCHARD, Byron, Andrew , PROCTOR, Robert
CPC分类号： F02C7/18 , F01D5/189 , F01D9/041 , F01D11/08 , F01D25/12 , F05D2240/81 , F05D2250/38 , F05D2260/201 , F05D2260/202 , F05D2260/22141 , F05D2260/607 , F23R3/002 , F23R3/005 , F23R2900/03042 , F23R2900/03043 , F23R2900/03044 , F23R2900/03045 , Y02T50/673 , Y02T50/676
摘要： Gas turbine engine components are provided which utilize an insert to provide cooling air along a cooled surface of an engine component. The insert provides an array of cooling holes or apertures which are facing the cool side surface of the engine component and direct cooling air onto that cool side surface. The apertures may be formed in arrays and are directed at an oblique angle or a non-orthogonal angle to the surface of the insert and further may be at an angle to the surface of the engine component being cooled. An engine component assembly is provided with counterflow impingement cooling. The engine component comprises an engine component cooling surface having a cooling fluid flow path on one side thereof and a second component adjacent to the first component. The second component, for example an insert, may have a plurality of openings forming an array wherein the openings extend through the second component at a non-orthogonal angle to the surface of the second component. The array of openings create counterflows in substantially opposite directions along the engine component cooling surface.
摘要翻译：提供燃气涡轮发动机部件，其利用插入件沿发动机部件的冷却表面提供冷却空气。插入件提供了一组面向发动机部件的冷却侧表面的冷却孔或孔，并将冷却空气直接冷却到该冷却侧表面上。孔可以形成为阵列并且以与插入件的表面成倾斜的角度或非正交的角度定向，并且还可以与被冷却的发动机部件的表面成一角度。发动机部件组件设有逆流冲击冷却。发动机部件包括在其一侧具有冷却流体流动路径的发动机部件冷却表面和与第一部件相邻的第二部件。第二部件，例如插入件，可以具有形成阵列的多个开口，其中开口以与第二部件的表面成非正交角延伸穿过第二部件。开口阵列沿着发动机部件冷却表面沿基本上相反的方向产生逆流。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式