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1. 发明申请

US20080052214A1 System and method for securities borrowing and lending 有权
标题翻译：证券借贷的制度和方法
公开(公告)号：US20080052214A1
公开(公告)日：2008-02-28
申请号：US10461866
申请日：2003-06-16
申请人： John Martinez , Judith Robertson , Brian Lamb , Jamie Solomon , Jeff Mehlman , Michael A. Vardas , Sandra Linn , Bill O'Meara , Pat Cestaro , Kurtis Kreider , Ramaz Ashurov , Gary Klahr , Andrew Monkhouse , Igor Modlin , Keith Babitt , George Payne , Anthony Strazza , Chris Doria , John McKenzie , Anthony Schiavo , Michael Robertson , Brian McCloone , Graham Sida , Leigh A. Weston , Marcus Butt , Ian Strafford-Taylor , Andy Kollegger , Dick Pruis
发明人： John Martinez , Judith Robertson , Brian Lamb , Jamie Solomon , Jeff Mehlman , Michael A. Vardas , Sandra Linn , Bill O'Meara , Pat Cestaro , Kurtis Kreider , Ramaz Ashurov , Gary Klahr , Andrew Monkhouse , Igor Modlin , Keith Babitt , George Payne , Anthony Strazza , Chris Doria , John McKenzie , Anthony Schiavo , Michael Robertson , Brian McCloone , Graham Sida , Leigh A. Weston , Marcus Butt , Ian Strafford-Taylor , Andy Kollegger , Dick Pruis
IPC分类号： G06Q40/00
CPC分类号： G06Q40/00 , G06Q40/04
摘要： Disclosed is a an electronic system for equities securities lending and financing. In particular, the disclosed system provides a hub for electronic financial transactions such as securities borrowing and lending and facilitates the ability of borrowers and lenders to locate suitable counterparties and engage in direct negotiations in a securities lending transaction.
摘要翻译：披露的是证券借贷融资的电子系统。特别是，所披露的系统提供了电子金融交易中心，例如证券借贷和贷款，并有助于借款人和贷方找到合适的交易对手的能力，并进行证券借贷交易的直接谈判。

2. 发明授权

US08185466B2 System and method for securities borrowing and lending 有权
标题翻译：证券借贷的制度和方法
公开(公告)号：US08185466B2
公开(公告)日：2012-05-22
申请号：US10461866
申请日：2003-06-16
申请人： John Martinez , Judith Robertson , Brian Lamb , Jamie Solomon , Jeff Mehlman , Michael A. Vardas , Sandra Linn , Bill O'Meara , Pat Cestaro , Kurtis Kreider , Ramaz Ashurov , Gary Klahr , Andrew Monkhouse , Igor Modlin , Keith Babitt , George Payne , Anthony Strazza , Christine Doria , John McKenzie , Anthony Schiavo , Michael Robertson , Brian McLoone , Graham Sida , Leigh A. Weston , Marcus Butt , Ian Strafford-Taylor , Andy Kollegger , Dirk Pruis
发明人： John Martinez , Judith Robertson , Brian Lamb , Jamie Solomon , Jeff Mehlman , Michael A. Vardas , Sandra Linn , Bill O'Meara , Pat Cestaro , Kurtis Kreider , Ramaz Ashurov , Gary Klahr , Andrew Monkhouse , Igor Modlin , Keith Babitt , George Payne , Anthony Strazza , Christine Doria , John McKenzie , Anthony Schiavo , Michael Robertson , Brian McLoone , Graham Sida , Leigh A. Weston , Marcus Butt , Ian Strafford-Taylor , Andy Kollegger , Dirk Pruis
IPC分类号： G06Q40/00
CPC分类号： G06Q40/00 , G06Q40/04
摘要： Disclosed is a an electronic system for equities securities lending and financing. In particular, the disclosed system provides a hub for electronic financial transactions such as securities borrowing and lending and facilitates the ability of borrowers and lenders to locate suitable counterparties and engage in direct negotiations in a securities lending transaction.
摘要翻译：披露的是证券借贷融资的电子系统。特别是，所披露的系统提供了电子金融交易中心，例如证券借贷和贷款，并有助于借款人和贷方找到合适的交易对手的能力，并进行证券借贷交易的直接谈判。

3. 发明申请

US20050013686A1 Turbine vane plate assembly 失效
标题翻译：涡轮叶片组件
公开(公告)号：US20050013686A1
公开(公告)日：2005-01-20
申请号：US10619343
申请日：2003-07-14
申请人： Anthony Schiavo
发明人： Anthony Schiavo
IPC分类号： F01D5/18 , F01D5/14
CPC分类号： F01D5/187 , F05D2240/12
摘要： A turbine vane assembly includes a turbine vane having first and second shrouds with an elongated airfoil extending between. Each end of the airfoil transitions into a shroud at a respective junction. Each of the shrouds has a plurality of cooling passages, and the airfoil has a plurality of cooling passages extending between the first and second shrouds. A substantially flat inner plate and an outer plate are coupled to each of the first and second shrouds so as to form inner and outer plenums. Each inner plenum is defined between at least the junction and the substantially flat inner plate; each outer plenum is defined between at least the substantially flat inner plate and the outer plate. Each inner plenum is in fluid communication with a respective outer plenum through at least one of the cooling passages in the respective shroud.
摘要翻译：涡轮叶片组件包括具有第一和第二护罩的涡轮叶片，其具有在其之间延伸的细长翼型件。翼型件的每一端在相应的连接处转变成护罩。每个护罩具有多个冷却通道，翼型件具有在第一和第二护罩之间延伸的多个冷却通道。基本平坦的内板和外板联接到第一和第二护罩中的每一个，以便形成内部和外部增压室。每个内部增压室至少限定在接合部和基本平坦的内板之间; 每个外部增压室至少限定在大致平坦的内板和外板之间。每个内部增压室通过相应护罩中的至少一个冷却通道与相应的外部通气室流体连通。

4. 发明申请

US20070258809A1 Multi-layer ring seal 有权
标题翻译：多层环密封
公开(公告)号：US20070258809A1
公开(公告)日：2007-11-08
申请号：US11418863
申请日：2006-05-05
申请人： Stefan Mazzola , Douglas Keller , Anthony Schiavo , David Radonovich
发明人： Stefan Mazzola , Douglas Keller , Anthony Schiavo , David Radonovich
IPC分类号： F01D11/08
CPC分类号： F01D11/08 , F05D2250/70 , F05D2250/712 , F05D2300/21 , F05D2300/603 , F16J15/104
摘要： Aspects of the invention are directed to a multi-layer ring seal segment that can incorporate a plurality of material systems. The ring seal segment can include an inner layer, a central layer and an outer layer. The inner layer can be attached to one side of the central layer, and the outer layer can be attached to an opposite side of the central layer. The inner and outer layers can be made of a ceramic matrix composite, such as a hybrid oxide ceramic matrix composite or an oxide-oxide ceramic matrix composite. The central layer can be made of a material that has high shear strength relative to the inner and outer layers. The ring seal segment according to aspects of the invention can take advantage of the benefits of the different materials so as to better withstand the operational loads of the turbine.
摘要翻译：本发明的方面涉及可以结合多个材料系统的多层环密封段。环形密封段可以包括内层，中心层和外层。内层可以附接到中心层的一侧，并且外层可以附接到中心层的相对侧。内层和外层可以由陶瓷基复合材料制成，例如杂化氧化物陶瓷基复合材料或氧化物 - 氧化物陶瓷基复合材料。中心层可以由相对于内层和外层具有高剪切强度的材料制成。根据本发明的方面的环形密封段可以利用不同材料的优点，以便更好地承受涡轮机的操作负载。

5. 发明申请

US20070237630A1 Vane shroud through-flow platform cover 失效
标题翻译：叶片护罩通流平台盖
公开(公告)号：US20070237630A1
公开(公告)日：2007-10-11
申请号：US11401987
申请日：2006-04-11
申请人： Anthony Schiavo , Bonnie Marini
发明人： Anthony Schiavo , Bonnie Marini
IPC分类号： F04D29/58
CPC分类号： F01D5/225 , F01D11/008 , F05D2240/80
摘要： A turbine vane array (10) for a combustion assembly (8) in a combustion turbine engine. The vane array (10) includes a plurality of stationary vane assemblies (12), each vane assembly (12) including at least one airfoil (24) and inner and outer shroud segments (26, 28) attached to opposing ends of the airfoil (24). The inner and outer shroud segments (26, 28) each include an inner face (34, 36) facing toward a gas path (13) extending through the vane array (10). A removable cover structure may be provided on the inner faces (34, 36) of the inner and outer shroud segments (26, 28). The cover structure may include removably attached insert elements (72, 72′) that are positioned on the inner faces (34, 36) extending between upstream edges (44) and downstream edges (46) of the shroud segments (26, 28) and extending between adjacent airfoils (24).
摘要翻译：一种用于燃气涡轮发动机中的燃烧组件（8）的涡轮叶片阵列（10）。叶片阵列（10）包括多个静止叶片组件（12），每个叶片组件（12）包括至少一个翼型件（24）以及附接到翼型件的相对端部的内部和外侧护罩段（26,28） 24）。内部和外部护罩段（26,28）各自包括面向延伸穿过叶片阵列（10）的气体路径（13）的内表面（34,36）。可拆卸的盖结构可以设置在内护罩段和外护罩段（26,28）的内表面（34,36）上。盖结构可以包括可移除地附接的插入元件（72,72'），其位于在护罩段（26,28）的上游边缘（44）和下游边缘（46）之间延伸的内表面（34,36）上，以及在相邻翼型件（24）之间延伸。

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