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1. 发明申请

US20080267784A1 Van Wheel of Turbine Comprising a Vane and at Least One Cooling Channel 有权
标题翻译：包括叶片和至少一个冷却通道的涡轮风轮
公开(公告)号：US20080267784A1
公开(公告)日：2008-10-30
申请号：US11632013
申请日：2005-06-13
申请人： Han-Thomas Bolms , Andreas Heselhaus , Roland Habel , Torsten Koch , Ralf Musgen
发明人： Han-Thomas Bolms , Andreas Heselhaus , Roland Habel , Torsten Koch , Ralf Musgen
IPC分类号： F01D5/18
CPC分类号： F01D5/30 , F01D5/081 , F01D25/12 , F05D2230/12 , F05D2240/127 , F05D2240/81 , F05D2250/291 , F05D2260/2212 , F05D2260/22141
摘要： There is described a vane wheel of a turbine comprising at least one vane, the footing thereof being held on a wheel disk. At least one cooling channel is arranged between the wheel disk and the vane footing. Said vane wheel having a plurality of turbulators is embodied on at least one of the walls of the cooling channel, said turbulators being configured in such a way that the turbulence and thus the heat transfer of a cooling fluid flowing through the cooling channel are increased.
摘要翻译：描述了一种涡轮机的叶轮，包括至少一个叶片，其叶片保持在轮盘上。至少一个冷却通道设置在轮盘和叶片基脚之间。具有多个紊流器的所述叶轮被实施在冷却通道的至少一个壁上，所述湍流器被构造成使得流过冷却通道的冷却流体的紊流和热传递增加。

2. 发明授权

US07758309B2 Vane wheel of turbine comprising a vane and at least one cooling channel 有权
标题翻译：涡轮的叶轮包括叶片和至少一个冷却通道
公开(公告)号：US07758309B2
公开(公告)日：2010-07-20
申请号：US11632013
申请日：2005-06-13
申请人： Hans-Thomas Bolms , Andreas Heselhaus , Roland Häbel , Torsten Koch , Ralf Müsgen
发明人： Hans-Thomas Bolms , Andreas Heselhaus , Roland Häbel , Torsten Koch , Ralf Müsgen
IPC分类号： F01D5/18
CPC分类号： F01D5/30 , F01D5/081 , F01D25/12 , F05D2230/12 , F05D2240/127 , F05D2240/81 , F05D2250/291 , F05D2260/2212 , F05D2260/22141
摘要： There is described a vane wheel of a turbine comprising at least one vane, the footing thereof being held on a wheel disk. At least one cooling channel is arranged between the wheel disk and the vane footing. The vane wheel having a plurality of turbulators is embodied on at least one of the walls of the cooling channel, the turbulators being configured in such a way that the turbulence and thus the heat transfer of a cooling fluid flowing through the cooling channel are increased.
摘要翻译：描述了一种涡轮机的叶轮，包括至少一个叶片，其叶片保持在轮盘上。至少一个冷却通道设置在轮盘和叶片基脚之间。具有多个紊流器的叶轮被实施在冷却通道的壁中的至少一个壁上，所述湍流器被构造成使得流过冷却通道的冷却流体的紊流以及热传递增加。

3. 发明申请

US20110262695A1 Discreetly Defined Porous Wall Structure for Transpirational Cooling 有权
标题翻译：用于旋转冷却的谨慎定义的多孔壁结构
公开(公告)号：US20110262695A1
公开(公告)日：2011-10-27
申请号：US12765004
申请日：2010-04-22
申请人： Ching-Pang Lee , Chander Prakash , Gary B. Merrill , Andreas Heselhaus , Andrew J. Burns
发明人： Ching-Pang Lee , Chander Prakash , Gary B. Merrill , Andreas Heselhaus , Andrew J. Burns
IPC分类号： B32B3/10
CPC分类号： F01D5/182 , B33Y80/00 , F01D5/183 , F01D5/184 , F05D2230/22 , F05D2230/90 , F05D2250/18 , F05D2250/185 , F05D2250/28 , F05D2250/30 , F05D2260/203 , F05D2260/221 , Y10T428/24273
摘要： A wall structure (32, 42, 68, 70, 80) with layers (A, B, C, D, E) of non-random voids (26A, 26B, 28B, 30B) that interconnect to form discretely defined tortuous passages between an interior (21) and an exterior surface (23) of the wall for transpiration cooling of the wall. A coolant flow (38) through the wall may be metered by restrictions in coolant outlets (31) and/or within the passages to minimize the coolant requirement. Pockets (44) may be formed on the exterior surface of the wall for thermal Insulation (46). The layers may be formed by lamination, additive manufacturing, or casting. Layer geometries include alternating layers (A, B, C) with different overlapping void patterns (42), 3-D lattice structures (70), and offset waffle structures (80).
摘要翻译：具有非随机空隙（26A，26B，28B，30B）的层（A，B，C，D，E）的壁结构（32,42,68,70,80），其互连以在所述壁的内部（21）和外表面（23）用于所述壁的蒸发冷却。通过壁的冷却剂流（38）可以通过冷却剂出口（31）和/或通道内的限制来计量，以使冷却剂需求最小化。口袋（44）可以形成在隔热壁的外表面上（46）。层可以通过层压，添加剂制造或铸造形成。层几何形状包括具有不同重叠空白图案（42），3-D网格结构（70）和偏置华夫饼结构（80）的交替层（A，B，C）。

4. 发明授权

US07670675B2 High-temperature layered system for dissipating heat and method for producing said system 有权
标题翻译：用于散热的高温分层系统和用于生产所述系统的方法
公开(公告)号：US07670675B2
公开(公告)日：2010-03-02
申请号：US10578425
申请日：2004-10-12
申请人： Andreas Heselhaus
发明人： Andreas Heselhaus
IPC分类号： B32B5/14 , B32B15/00 , F01D5/14 , F23R3/00 , F01D5/28 , B32B18/00
CPC分类号： F28F13/185 , B33Y80/00 , F01D5/288 , F01D11/122 , F05D2300/612 , F23R3/002 , F23R3/007 , F28F13/003 , Y02T50/67 , Y10T428/24149 , Y10T428/249953 , Y10T428/249961 , Y10T428/249975 , Y10T428/249981 , Y10T428/249987
摘要： Layered systems in prior art are inefficient at cooling an external hot gas. The inventive layered system comprises an external porous layer, in which the pore walls of the pores have differing thicknesses. This improves the cooling action by preventing too much heat from entering the layered system.
摘要翻译：现有技术中的分层系统在冷却外部热气时效率低下。本发明的分层系统包括外部多孔层，其中孔的孔壁具有不同的厚度。这通过防止太多的热量进入层状体系来改善冷却作用。

5. 发明申请

US20070275210A1 High-Temperature Layered System for Dissipating Heat and Method for Producing Said System 有权
标题翻译：用于散热的高温分层系统和生产所述系统的方法
公开(公告)号：US20070275210A1
公开(公告)日：2007-11-29
申请号：US10578425
申请日：2004-10-12
申请人： Andreas Heselhaus
发明人： Andreas Heselhaus
IPC分类号： B32B5/14 , B32B15/00 , F01D5/14 , F23R3/00 , F01D5/28 , B32B18/00
CPC分类号： F28F13/185 , B33Y80/00 , F01D5/288 , F01D11/122 , F05D2300/612 , F23R3/002 , F23R3/007 , F28F13/003 , Y02T50/67 , Y10T428/24149 , Y10T428/249953 , Y10T428/249961 , Y10T428/249975 , Y10T428/249981 , Y10T428/249987
摘要： Layered systems in prior art are inefficient at cooling an external hot gas. The inventive layered system comprises an external porous layer, in which the pore walls of the pores have differing thicknesses. This improves the cooling action by preventing too much heat from entering the layered system.
摘要翻译：现有技术中的分层系统在冷却外部热气体时效率低下。本发明的分层系统包括外部多孔层，其中孔的孔壁具有不同的厚度。这通过防止太多的热量进入层状体系来改善冷却作用。

6. 发明申请

US20060153685A1 Layer structure and method for producing such a layer structure 失效
标题翻译：用于制造这种层结构的层结构和方法
公开(公告)号：US20060153685A1
公开(公告)日：2006-07-13
申请号：US10563948
申请日：2004-06-17
申请人： Hans-Thomas Bolms , Andreas Heselhaus
发明人： Hans-Thomas Bolms , Andreas Heselhaus
IPC分类号： B64C27/46
CPC分类号： C23C28/3215 , C23C28/042 , C23C28/322 , C23C28/345 , C23C28/3455 , C23C30/00 , F01D5/183 , F01D5/288 , Y10T428/249954 , Y10T428/249955 , Y10T428/249956 , Y10T428/249961 , Y10T428/249967 , Y10T428/24997 , Y10T428/24999
摘要： The invention relates to a temperature resistant layered structure comprising a substrate and a porous layer arranged on the substrate having a pore defined by a wall, and a ceramic coating on an interior surface of the wall. The invention also relates to a layered turbine component arrangement comprising a substrate having a cooling passage adapted to allow a cooling gas medium to pass through the substrate and a porous layer arranged on the substrate, the porous layer having cooling passages formed by gas-permeable inter-connections between pores in the porous layer.
摘要翻译：本发明涉及一种耐温分层结构，其包括基板和布置在基板上的多孔层，其具有由壁限定的孔，以及在该壁的内表面上的陶瓷涂层。本发明还涉及一种层状涡轮机部件装置，其包括具有适于允许冷却气体介质通过基板的冷却通道的基板和布置在基板上的多孔层，多孔层具有通过气体可渗透相互间形成的冷却通道 - 多孔层中的孔之间的连接。

7. 发明授权

US09334741B2 Discreetly defined porous wall structure for transpirational cooling 有权
标题翻译：用于蒸发冷却的谨慎定义的多孔壁结构
公开(公告)号：US09334741B2
公开(公告)日：2016-05-10
申请号：US12765004
申请日：2010-04-22
申请人： Ching-Pang Lee , Chander Prakash , Gary B. Merrill , Andreas Heselhaus , Andrew J. Burns
发明人： Ching-Pang Lee , Chander Prakash , Gary B. Merrill , Andreas Heselhaus , Andrew J. Burns
IPC分类号： B32B3/10 , B32B3/12 , F01D5/18
CPC分类号： F01D5/182 , B33Y80/00 , F01D5/183 , F01D5/184 , F05D2230/22 , F05D2230/90 , F05D2250/18 , F05D2250/185 , F05D2250/28 , F05D2250/30 , F05D2260/203 , F05D2260/221 , Y10T428/24273
摘要： A wall structure (32, 42, 68, 70, 80) with layers (A, B, C, D, E) of non-random voids (26A, 26B, 28B, 30B) that interconnect to form discretely defined tortuous passages between an interior (21) and an exterior surface (23) of the wall for transpiration cooling of the wall. A coolant flow (38) through the wall may be metered by restrictions in coolant outlets (31) and/or within the passages to minimize the coolant requirement. Pockets (44) may be formed on the exterior surface of the wall for thermal Insulation (46). The layers may be formed by lamination, additive manufacturing, or casting. Layer geometries include alternating layers (A, B, C) with different overlapping void patterns (42), 3-D lattice structures (70), and offset waffle structures (80).
摘要翻译：具有非随机空隙（26A，26B，28B，30B）的层（A，B，C，D，E）的壁结构（32,42,68,70,80），其互连以在所述壁的内部（21）和外表面（23）用于所述壁的蒸发冷却。通过壁的冷却剂流（38）可以通过冷却剂出口（31）和/或通道内的限制来计量，以使冷却剂需求最小化。口袋（44）可以形成在隔热壁的外表面上（46）。层可以通过层压，添加剂制造或铸造形成。层几何形状包括具有不同重叠空白图案（42），3-D网格结构（70）和偏置华夫饼结构（80）的交替层（A，B，C）。

8. 发明申请

US20140193241A1 INTERNALLY COOLABLE COMPONENT FOR A GAS TURBINE WITH AT LEAST ONE COOLING DUCT 有权
标题翻译：用于具有至少一个冷却导管的气体涡轮机的内部可冷却部件
公开(公告)号：US20140193241A1
公开(公告)日：2014-07-10
申请号：US14237871
申请日：2012-08-02
申请人： Marcel Eifel , Daniel Gloss , Andreas Heselhaus , Stephan Klumpp , Marco Link , Uwe Sieber , Stefan Volker , Michael Wagner
发明人： Marcel Eifel , Daniel Gloss , Andreas Heselhaus , Stephan Klumpp , Marco Link , Uwe Sieber , Stefan Volker , Michael Wagner
IPC分类号： F02C7/12
CPC分类号： F01D5/187 , F02C7/12 , F05D2260/22141
摘要： An internally coolable component for a gas turbine with at least one cooling duct, on the inner surface of which swirl elements are arranged in the form of turbulators which extend transversely with respect to the main flow direction of a coolant is provided. In order to reduce pressure losses for the coolant in the cooling duct, pins with different heights are set up between the turbulators.
摘要翻译：提供了一种用于具有至少一个冷却管道的燃气轮机的内部可冷却部件，其内表面上设置有相对于冷却剂的主流动方向横向延伸的涡流体形式的涡流元件。为了减少冷却管道中的冷却剂的压力损失，在湍流器之间建立具有不同高度的销。

9. 发明申请

US20140219814A1 FILM-COOLED TURBINE BLADE FOR A TURBOMACHINE 有权
标题翻译：用于涡轮机的薄膜冷却涡轮叶片
公开(公告)号：US20140219814A1
公开(公告)日：2014-08-07
申请号：US13756653
申请日：2013-02-01
申请人： Andreas Heselhaus
发明人： Andreas Heselhaus
IPC分类号： F01D25/12
CPC分类号： F01D5/186 , F05D2260/209 , F05D2260/2212
摘要： A turbine blade for a turbomachine has an outer wall which delimits an inner cavity. Cooling fluid flows in the inner cavity. A through duct is arranged in the outer wall through which the cooling fluid flows from the inner cavity to an outside of the turbine blade. The through duct is inclined with respect to a trailing edge of the turbine blade, wherein a marginal portion of an entrance of the through duct is designed on an upstream side to be sharp-edged in relation to other marginal portions of the entrance such that a separation zone of a cooling fluid flow is formed in the through duct. A pair of swirls builds up in the through duct, wherein velocity vectors of the cooling fluid flow between the swirl centers point toward a downstream side of the through duct.
摘要翻译：用于涡轮机的涡轮机叶片具有限定内腔的外壁。冷却液在内腔中流动。通气管布置在外壁中，冷却流体通过该外壁从内腔流到涡轮叶片的外部。贯通管道相对于涡轮机叶片的后缘倾斜，其中贯通管道入口的边缘部分被设计在相对于入口的其它边缘部分被锐化的上游侧，使得在通气管中形成冷却流体流的分离区。在通气管中形成一对漩涡，其中冷却流体在涡流中心之间流动的速度矢量指向通过管道的下游侧。

10. 发明授权

US07402335B2 Layer structure and method for producing such a layer structure 失效
标题翻译：用于制造这种层结构的层结构和方法
公开(公告)号：US07402335B2
公开(公告)日：2008-07-22
申请号：US10563948
申请日：2004-06-17
申请人： Hans-Thomas Bolms , Andreas Heselhaus
发明人： Hans-Thomas Bolms , Andreas Heselhaus
IPC分类号： B32B5/14
CPC分类号： C23C28/3215 , C23C28/042 , C23C28/322 , C23C28/345 , C23C28/3455 , C23C30/00 , F01D5/183 , F01D5/288 , Y10T428/249954 , Y10T428/249955 , Y10T428/249956 , Y10T428/249961 , Y10T428/249967 , Y10T428/24997 , Y10T428/24999
摘要： The invention relates to a temperature resistant layered structure comprising a substrate and a porous layer arranged on the substrate having a pore defined by a wall, and a ceramic coating on an interior surface of the wall. The invention also relates to a layered turbine component arrangement comprising a substrate having a cooling passage adapted to allow a cooling gas medium to pass through the substrate and a porous layer arranged on the substrate, the porous layer having cooling passages formed by gas-permeable inter-connections between pores in the porous layer.
摘要翻译：本发明涉及一种耐温分层结构，其包括基板和布置在基板上的多孔层，其具有由壁限定的孔，以及在该壁的内表面上的陶瓷涂层。本发明还涉及一种层状涡轮机部件装置，其包括具有适于允许冷却气体介质通过基板的冷却通道的基板和布置在基板上的多孔层，多孔层具有由透气相互隔开的冷却通道 - 多孔层中的孔之间的连接。

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