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1. 发明公开

EP1467065A2 Turbine blade 有权转让
标题翻译： Turbinenschaufel
公开(公告)号：EP1467065A2
公开(公告)日：2004-10-13
申请号：EP04252073.4
申请日：2004-04-07
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： Cunha, Frank J. , Dahmer, Matthew T.
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , B22C9/103 , F01D5/186 , F05D2230/21 , F05D2260/2212 , F05D2260/22141
摘要： A turbine element airfoil (22) has a cooling passageway network with a slot extending from a trailing passageway toward the trailing edge (32). A number of discrete posts arranged in rows (130-146) span the slot between pressure and suction sidewall portions.
摘要翻译：涡轮机构翼型件（22）具有冷却通道网络，其具有从后部通道朝向后缘（32）延伸的狭槽。排列成行（130-146）的多个离散柱跨越压力和抽吸侧壁部分之间的槽。

2. 发明授权

EP1467065B1 Turbine blade 有权转让
标题翻译：涡轮叶片
公开(公告)号：EP1467065B1
公开(公告)日：2012-05-23
申请号：EP04252073.4
申请日：2004-04-07
申请人： United Technologies Corporation
发明人： Cunha, Frank J. , Dahmer, Matthew T.
IPC分类号： F01D5/18 , B22C9/10 , B22C21/14
CPC分类号： F01D5/187 , B22C9/103 , F01D5/186 , F05D2230/21 , F05D2260/2212 , F05D2260/22141

3. 发明授权

EP2471614B1 Microcircuit cooling for vanes 有权转让
标题翻译： KühlungmitMikrokanälenfürLeitschaufeln
公开(公告)号：EP2471614B1
公开(公告)日：2017-04-05
申请号：EP12162248.4
申请日：2006-11-22
申请人： United Technologies Corporation
发明人： Cunha, Francisco J. , Dahmer, Matthew T.
IPC分类号： B22C9/10 , F01D5/18 , B22C9/06 , B22D29/00
CPC分类号： F01D5/186 , B22C9/06 , B22C9/108 , B22D29/002 , F05D2230/21 , F05D2260/202 , F05D2300/13 , Y10T29/49341

4. 发明授权

EP1790823B1 Microcircuit cooling for turbine vanes 有权转让
标题翻译：具有微通道冷却的涡轮叶片
公开(公告)号：EP1790823B1
公开(公告)日：2013-05-15
申请号：EP06255986.9
申请日：2006-11-22
申请人： United Technologies Corporation
发明人： Cunha, Francisco J. , Dahmer, Matthew T.
IPC分类号： B22C9/10 , B22C9/06 , B22D29/00 , F01D5/18
CPC分类号： F01D5/186 , B22C9/06 , B22C9/108 , B22D29/002 , F05D2230/21 , F05D2260/202 , F05D2300/13 , Y10T29/49341

5. 发明授权

EP1900905B1 Airfoil thermal management with microcircuit cooling 有权转让
标题翻译：与微通道冷却翼型热控制
公开(公告)号：EP1900905B1
公开(公告)日：2012-12-05
申请号：EP07253638.6
申请日：2007-09-13
申请人： United Technologies Corporation
发明人： Cunha, Francisco J. , Dahmer, Matthew T.
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F05D2260/2214

6. 发明公开

EP2471614A3 Microcircuit cooling for vanes 有权转让
标题翻译：与微型槽，用来冷却叶片
公开(公告)号：EP2471614A3
公开(公告)日：2012-09-05
申请号：EP12162248.4
申请日：2006-11-22
申请人： United Technologies Corporation
发明人： Cunha, Francisco J. , Dahmer, Matthew T.
IPC分类号： B22C9/10 , F01D5/18 , B22C9/06 , B22D29/00
CPC分类号： F01D5/186 , B22C9/06 , B22C9/108 , B22D29/002 , F05D2230/21 , F05D2260/202 , F05D2300/13 , Y10T29/49341
摘要： A turbine engine component (12) has an airfoil portion (10) with a suction side (14). The component (12) includes a cooling microcircuit (32) embedded within a wall structure forming the suction side (14). The cooling microcircuit (32) has at least one cooling film hole (36) positioned ahead of a gage point (38) for creating a flow of cooling fluid over an exterior surface of the suction side (14) which travels past the gage point (38).

7. 发明公开

EP2388438A1 Turbine element-forming core assembly and method of manufacturing a turbine blade 失效转让
标题翻译： Kern eines Turbinenelements und Verfahren zur Herstellung einer Turbinenschaufel
公开(公告)号：EP2388438A1
公开(公告)日：2011-11-23
申请号：EP11178096.1
申请日：2004-04-07
申请人： United Technologies Corporation
发明人： Cunha, Frank J. , Dahmer, Matthew T.
IPC分类号： F01D5/18 , B22C9/10 , B22C21/14
CPC分类号： F01D5/187 , B22C9/103 , F01D5/186 , F05D2230/21 , F05D2260/2212 , F05D2260/22141
摘要： A turbine element airfoil (22) has a cooling passageway network with a slot extending from a trailing passageway toward the trailing edge (32). A number of discrete posts arranged in rows (130-146) span the slot between pressure and suction sidewall portions.
摘要翻译：涡轮机构翼型件（22）具有冷却通道网络，其具有从后部通道朝向后缘（32）延伸的狭槽。排列成行（130-146）的多个离散柱跨越压力和抽吸侧壁部分之间的槽。

8. 发明授权

EP1900904B1 Multi-peripheral serpentine microcircuits for high aspect ratio blades 有权
标题翻译： Multiperipherisch蛇形微课程具有高性能比铲
公开(公告)号：EP1900904B1
公开(公告)日：2013-01-02
申请号：EP07253511.5
申请日：2007-09-05
申请人： United Technologies Corporation
发明人： Cunha, Francisco J. , Dahmer, Matthew T.
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F05D2250/185

9. 发明公开

EP1900905A3 Airfoil thermal management with microcircuit cooling 有权转让
标题翻译：与微通道冷却翼热控制
公开(公告)号：EP1900905A3
公开(公告)日：2011-06-22
申请号：EP07253638.6
申请日：2007-09-13
申请人： United Technologies Corporation
发明人： Cunha, Francisco J. , Dahmer, Matthew T.
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F05D2260/2214
摘要： A turbine engine component (100), such as a turbine engine blade, has an airfoil portion (104) with a pressure side wall (106) and a suction side wall (108), a plurality of ribs (110) extending between the pressure side wall (106) and the suction side wall (108), and a plurality of supply cavities (120, 144, 150, 164) located between the ribs (110). The component further has an arrangement for cooling the airfoil portion (104). The cooling arrangement comprises a first cooling circuit (114, 117) embedded within the suction side wall (108) for convectively cooling the suction side wall (108), a second cooling circuit (124, 130) embedded within the pressure side wall (106) for cooling the pressure side wall (106), and a third passageway (122, 128) for increasing a temperature of at least one of the ribs (110) by conduction.

10. 发明公开

EP1900905A2 Airfoil thermal management with microcircuit cooling 有权转让
标题翻译： SchaufelblattwärmeregelungmitMikrokanalkühlung
公开(公告)号：EP1900905A2
公开(公告)日：2008-03-19
申请号：EP07253638.6
申请日：2007-09-13
申请人： United Technologies Corporation
发明人： Cunha, Francisco J. , Dahmer, Matthew T.
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F05D2260/2214
摘要： A turbine engine component (100), such as a turbine engine blade, has an airfoil portion (104) with a pressure side wall (106) and a suction side wall (108), a plurality of ribs (110) extending between the pressure side wall (106) and the suction side wall (108), and a plurality of supply cavities (120, 144, 150, 164) located between the ribs (110). The component further has an arrangement for cooling the airfoil portion (104). The cooling arrangement comprises a first cooling circuit (114, 117) embedded within the suction side wall (108) for convectively cooling the suction side wall (108), a second cooling circuit (124, 130) embedded within the pressure side wall (106) for cooling the pressure side wall (106), and a third passageway (122, 128) for increasing a temperature of at least one of the ribs (110) by conduction.
摘要翻译：诸如涡轮发动机叶片的涡轮发动机部件（100）具有带有压力侧壁（106）和吸力侧壁（108）的翼型部分（104），多个肋（110）在压力侧壁（106）和吸力侧壁（108）以及位于肋（110）之间的多个供应腔（120,144,150,164）。该部件还具有用于冷却翼型件部分（104）的布置。冷却装置包括嵌入在吸入侧壁（108）内的用于对流冷却吸入侧壁（108）的第一冷却回路（114,117），嵌入压力侧壁（106）内的第二冷却回路（124,130））和用于通过传导增加至少一个肋（110）的温度的第三通道（122,128）。

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