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1. 发明授权

US07086829B2 Film cooling for the trailing edge of a steam cooled nozzle 有权
标题翻译：蒸汽冷却喷嘴后缘的薄膜冷却
公开(公告)号：US07086829B2
公开(公告)日：2006-08-08
申请号：US10771195
申请日：2004-02-03
申请人： Jason Fuller , Gary Itzel , Cathy Chiurato , Matthew Findlay
发明人： Jason Fuller , Gary Itzel , Cathy Chiurato , Matthew Findlay
IPC分类号： F04D29/58 , F01D5/18
CPC分类号： F01D5/186 , F01D9/02 , F01D25/12 , F05D2240/122 , F05D2240/304 , F05D2260/202 , F05D2260/205 , F05D2260/2322
摘要： A nozzle assembly (10) for a turbine engine includes an inner band (16) and an outer band (14) spaced apart from each other. An airfoil (12) installed between the bands has a leading edge (18) and a trailing edge (20). The airfoil has cavities formed in it for fluid flow through the nozzle assembly. A plurality of film cooling holes (1A–6H) are formed in a sidewall of the airfoil on a concave side of the assembly, and a plurality of film cooling holes (1J–1R) are formed in a sidewall of the nozzle on a convex side thereof. The holes are formed on each side of the airfoil, adjacent the trailing edge of the nozzle, in a plurality of rows of holes including at least a forward row (C, J), an aft row (A, L), and an intermediate row (B, K). The spacing between the intermediate row and aft row is substantially closer than the spacing between the forward row and the intermediate row.
摘要翻译：用于涡轮发动机的喷嘴组件（10）包括彼此间隔开的内带（16）和外带（14）。安装在带之间的翼型件（12）具有前缘（18）和后缘（20）。机翼具有形成在其中的空腔，用于流过喷嘴组件的流体。在组件的凹面上的翼型件的侧壁上形成有多个薄膜冷却孔（1A-6H），并且在该侧壁中形成多个薄膜冷却孔（1J-1R）喷嘴在其凸面上。所述孔形成在所述翼型件的与所述喷嘴的后缘相邻的每一侧上，所述多排排孔至少包括前排（C，J），后排（A，L）和中间体行（B，K）。中间行和后排之间的间隔基本上比前排和中间行之间的间距更近。

2. 发明申请

US20100105956A1 Internal Loop Reactor And OXO Process Using Same 有权
标题翻译：内循环反应器和OXO过程使用相同
公开(公告)号：US20100105956A1
公开(公告)日：2010-04-29
申请号：US12652171
申请日：2010-01-05
申请人： Ronald Dean Garton , Matthew Findlay , Krishnan Sankaranarayanan , Arie Van Vliet
发明人： Ronald Dean Garton , Matthew Findlay , Krishnan Sankaranarayanan , Arie Van Vliet
IPC分类号： C07C45/00 , B01J19/00
CPC分类号： C07C45/50 , B01J8/226 , B01J2208/00061 , B01J2208/00088 , B01J2208/00132 , B01J2219/00081 , C07C47/02
摘要： The invention relates to improvements in internal loop reactors. The reactor of the invention is characterized by a plurality of cooling tubes which form the annulus between the riser and the downcomer path of said internal loop reactor. The reactor also provides improvements in hydroformylation reactions using the improved reactor.
摘要翻译：本发明涉及内循环反应器的改进。本发明的反应器的特征在于多个冷却管，其在所述内循环反应器的提升管和降液管路径之间形成环形空间。反应器还使用改进的反应器提供加氢甲酰化反应的改进。

3. 发明申请

US20080009554A1 Internal loop reactor and Oxo process using same 有权
标题翻译：内循环反应器和使用相同的Oxo工艺
公开(公告)号：US20080009554A1
公开(公告)日：2008-01-10
申请号：US11484178
申请日：2006-07-10
申请人： Ronald Dean Garton , Matthew Findlay , Krishnan Sankaranarayanan , Arie Van Vliet
发明人： Ronald Dean Garton , Matthew Findlay , Krishnan Sankaranarayanan , Arie Van Vliet
IPC分类号： B01J19/00 , C07C27/26
CPC分类号： C07C45/50 , B01J8/226 , B01J2208/00061 , B01J2208/00088 , B01J2208/00132 , B01J2219/00081 , C07C47/02
摘要： The invention relates to improvements in internal loop reactors. The reactor of the invention is characterized by a plurality of cooling tubes which form the annulus between the riser and the downcomer path of said internal loop reactor. The reactor also provides improvements in hydroformylation reactions using the improved reactor.
摘要翻译：本发明涉及内循环反应器的改进。本发明的反应器的特征在于多个冷却管，其在所述内循环反应器的提升管和降液管路径之间形成环形空间。反应器还使用改进的反应器提供加氢甲酰化反应的改进。

4. 发明申请

US20060257256A1 Turbulator on the underside of a turbine blade tip turn and related method 有权
公开(公告)号：US20060257256A1
公开(公告)日：2006-11-16
申请号：US11491957
申请日：2006-07-25
申请人： John Eastman , Matthew Findlay , Jon Ebacher
发明人： John Eastman , Matthew Findlay , Jon Ebacher
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F05D2250/185 , F05D2260/2212 , F05D2260/2214 , F05D2260/22141 , Y02T50/67 , Y02T50/676
摘要： A turbine blade includes a shank portion and an airfoil portion with leading and trailing edges and a radially outer tip. An internal closed-loop cooling circuit is formed within the airfoil portion and includes at least one radial outflow passage and at least one radial inflow passage connected by at least one respective tip turn at the radially outer end of the airfoil portion. At least one tip turn is provided with a single turbulence-enhancement device on an underside of the radially outer tip, projecting into the tip turn.

5. 发明申请

US20050169746A1 Film cooling for the trailing edge of a steam cooled nozzle 有权
标题翻译：蒸汽冷却喷嘴后缘的薄膜冷却
公开(公告)号：US20050169746A1
公开(公告)日：2005-08-04
申请号：US10771195
申请日：2004-02-03
申请人： Jason Fuller , Gary Itzel , Cathy Chiurato , Matthew Findlay
发明人： Jason Fuller , Gary Itzel , Cathy Chiurato , Matthew Findlay
IPC分类号： F01D5/18 , F01D9/02 , F01D25/12 , F03D11/00
CPC分类号： F01D5/186 , F01D9/02 , F01D25/12 , F05D2240/122 , F05D2240/304 , F05D2260/202 , F05D2260/205 , F05D2260/2322
摘要： A nozzle assembly (10) for a turbine engine includes an inner band (16) and an outer band (14) spaced apart from each other. An airfoil (12) installed between the bands has a leading edge (18) and a trailing edge (20). The airfoil has cavities formed in it for fluid flow through the nozzle assembly. A plurality of film cooling holes (1A-6H) are formed in a sidewall of the airfoil on a concave side of the assembly, and a plurality of film cooling holes (1J-1R) are formed in a sidewall of the nozzle on a convex side thereof. The holes are formed on each side of the airfoil, adjacent the trailing edge of the nozzle, in a plurality of rows of holes including at least a forward row (C, J), an aft row (A, L), and an intermediate row (B, K). The spacing between the intermediate row and aft row is substantially closer than the spacing between the forward row and the intermediate row.
摘要翻译：用于涡轮发动机的喷嘴组件（10）包括彼此间隔开的内带（16）和外带（14）。安装在带之间的翼型件（12）具有前缘（18）和后缘（20）。机翼具有形成在其中的空腔，用于流过喷嘴组件的流体。在组件的凹面上的翼型件的侧壁上形成有多个薄膜冷却孔（1A-6H），并且在该侧壁中形成多个薄膜冷却孔（1J-1R）喷嘴在其凸面上。所述孔形成在所述翼型件的与所述喷嘴的后缘相邻的每一侧上，所述多排排孔至少包括前排（C，J），后排（A，L）和中间体行（B，K）。中间行和后排之间的间隔基本上比前排和中间行之间的间距更近。

6. 发明授权

US07666366B2 Internal loop reactor and Oxo process using same 有权
标题翻译：内循环反应器和使用相同的Oxo工艺
公开(公告)号：US07666366B2
公开(公告)日：2010-02-23
申请号：US11484178
申请日：2006-07-10
申请人： Ronald Dean Garton , Matthew Findlay , Krishnan Sankaranarayanan , Arie Van Vliet
发明人： Ronald Dean Garton , Matthew Findlay , Krishnan Sankaranarayanan , Arie Van Vliet
IPC分类号： F28D7/00 , B01J19/18
CPC分类号： C07C45/50 , B01J8/226 , B01J2208/00061 , B01J2208/00088 , B01J2208/00132 , B01J2219/00081 , C07C47/02
摘要： The invention relates to improvements in internal loop reactors. The reactor of the invention is characterized by a plurality of cooling tubes which form the annulus between the riser and the downcomer path of said internal loop reactor. The reactor also provides improvements in hydroformylation reactions using the improved reactor.
摘要翻译：本发明涉及内循环反应器的改进。本发明的反应器的特征在于多个冷却管，其在所述内循环反应器的提升管和降液管路径之间形成环形空间。反应器还使用改进的反应器提供加氢甲酰化反应的改进。

7. 发明申请

US20050238488A1 Turbulator on the underside of a turbine blade tip turn and related method 失效
标题翻译：涡轮机叶片下侧的涡轮机转动及相关方法
公开(公告)号：US20050238488A1
公开(公告)日：2005-10-27
申请号：US10832252
申请日：2004-04-27
申请人： John Alan Eastman , Matthew Findlay , Jon Ebacher
发明人： John Alan Eastman , Matthew Findlay , Jon Ebacher
IPC分类号： F01D5/18 , B63H1/14 , F02C7/18 , F15D1/02
CPC分类号： F01D5/187 , F05D2250/185 , F05D2260/2212 , F05D2260/2214 , F05D2260/22141 , Y02T50/67 , Y02T50/676
摘要： A turbine blade includes a shank portion and an airfoil portion with leading and trailing edges and a radially outer tip. An internal closed-loop cooling circuit is formed within the airfoil portion and includes at least one radial outflow passage and at least one radial inflow passage connected by at least one respective tip turn at the radially outer end of the airfoil portion. At least one tip turn is provided with a single turbulence-enhancement device on an underside of the radially outer tip, projecting into the tip turn.
摘要翻译：涡轮机叶片包括柄部和具有前缘和后缘以及径向外端的翼型部分。内部闭环冷却回路形成在翼型部分内，并且包括至少一个径向流出通道和至少一个径向流入通道，其通过在翼型部分的径向外端处的至少一个相应的尖端匝连接。至少一个尖端转向在径向外部尖端的下侧上设置有单个湍流增强装置，突出到尖端匝中。

8. 发明授权

US07875254B2 Internal loop reactor and Oxo process using same 有权
标题翻译：内循环反应器和使用相同的Oxo工艺
公开(公告)号：US07875254B2
公开(公告)日：2011-01-25
申请号：US12652171
申请日：2010-01-05
申请人： Ronald Dean Garton , Matthew Findlay , Krishnan Sankaranarayanan , Arie Van Vliet
发明人： Ronald Dean Garton , Matthew Findlay , Krishnan Sankaranarayanan , Arie Van Vliet
IPC分类号： B01J19/18 , F28D7/00
CPC分类号： C07C45/50 , B01J8/226 , B01J2208/00061 , B01J2208/00088 , B01J2208/00132 , B01J2219/00081 , C07C47/02
摘要： The invention relates to improvements in internal loop reactors. The reactor of the invention is characterized by a plurality of cooling tubes which form the annulus between the riser and the downcomer path of said internal loop reactor. The reactor also provides improvements in hydroformylation reactions using the improved reactor.
摘要翻译：本发明涉及内循环反应器的改进。本发明的反应器的特征在于多个冷却管，其在所述内循环反应器的提升管和降液管路径之间形成环形空间。反应器还使用改进的反应器提供加氢甲酰化反应的改进。

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