公开(公告)号：US20100064656A1

公开(公告)日：2010-03-18

申请号：US12233368

申请日：2008-09-18

申请人： David Andrew Lopez ,  Tom Elliott ,  Kendall Keith Dalton ,  Craig E. Thompson ,  Dale Mukavetz ,  Joseph S. Howard, III ,  John Harvell ,  Dana Metz ,  Leonard J. Meyer ,  Michael Tate

发明人： David Andrew Lopez ,  Tom Elliott ,  Kendall Keith Dalton ,  Craig E. Thompson ,  Dale Mukavetz ,  Joseph S. Howard, III ,  John Harvell ,  Dana Metz ,  Leonard J. Meyer ,  Michael Tate

IPC分类号： F02C9/20 ,  F01D9/02 ,  F02C9/00

CPC分类号： F01D9/02 ,  F02C9/16 ,  F05D2270/021 ,  F05D2270/304

摘要： Engines and methods for operating the engines are provided. The engine includes a means for limiting overspeed in flow communication with a turbine section flowpath, wherein the means for limiting overspeed is adapted to block a first portion of an airflow received along a first direction vector from flowing into an exhaust section flowpath and to redirect a second portion of the airflow received along the first direction vector or a portion of the blocked first portion of the airflow to flow along another direction vector that is closer to parallel with a longitudinal axis than the first direction vector.

摘要翻译： 提供用于操作发动机的发动机和方法。 发动机包括用于限制与涡轮部分流动路径的流动连通的超速的装置，其中用于限制超速的装置适于阻挡沿着第一方向矢量接收的气流的第一部分流入排气部分流动路径并且重定向 沿着第一方向矢量接收的气流的第二部分或气流的阻塞的第一部分的一部分沿着比与第一方向矢量更靠近平行于纵轴的另一方向矢量流动。

公开(公告)号：US08955072B2

公开(公告)日：2015-02-10

申请号：US12939817

申请日：2010-11-04

申请人： Anthony Wilkinson ,  Per Olav Larsson ,  Ashley Nuttall ,  Hans Christenson ,  Tom Elliott ,  Steven Sigel ,  Adam G. Gross

发明人： Anthony Wilkinson ,  Per Olav Larsson ,  Ashley Nuttall ,  Hans Christenson ,  Tom Elliott ,  Steven Sigel ,  Adam G. Gross

IPC分类号： H04L9/32 ,  G06F21/33 ,  G06F21/34 ,  G06F21/41

CPC分类号： H04L63/0815 ,  G06F21/335 ,  G06F21/34 ,  G06F21/41 ,  G06F21/445 ,  G06F2009/45587 ,  H04L9/3226 ,  H04L9/3234 ,  H04L9/3263 ,  H04L9/3273 ,  H04L63/0428 ,  H04L63/0807 ,  H04L63/0823 ,  H04L63/083 ,  H04L63/0853 ,  H04L63/0884 ,  H04L63/10 ,  H04L2209/56

摘要： A user accesses a remote session, the connection to which is managed by a connection broker, according to a single sign-on (SSO) process. The SSO process includes the user entering his or her credentials and being authenticated to the connection broker. In addition to user authentication, the SSO process includes connection broker authentication to confirm that the connection broker is trustworthy. When the connection broker is authenticated, the user credentials are transmitted to the connection broker in a secure manner and the connection broker forwards them onto a machine hosting the remote session so that the user can be logged into the remote session without entering his or her credentials again.

摘要翻译： 根据单点登录（SSO）进程，用户访问远程会话，由连接代理管理的连接。 SSO进程包括用户输入他或她的凭据并被认证给连接代理。 除了用户身份验证之外，SSO进程还包括连接代理身份验证，以确认连接代理是值得信赖的。 当连接代理被认证时，用户凭证以安全的方式传送到连接代理，并且连接代理将它们转发到托管远程会话的机器上，以便用户可以登录远程会话而不输入他或她的凭证 再次。

公开(公告)号：US20140258157A1

公开(公告)日：2014-09-11

申请号：US13787617

申请日：2013-03-06

申请人： Keenan Pridmore ,  Philip John MacGregor, IV ,  Robert Newlan ,  Tom Elliott

发明人： Keenan Pridmore ,  Philip John MacGregor, IV ,  Robert Newlan ,  Tom Elliott

IPC分类号： G06Q40/00 ,  G06Q50/00

CPC分类号： G06Q40/00 ,  G06Q50/01

摘要： Exemplary methods, apparatuses, and systems display selectable partners to facilitate a financial contribution from a user, receive user selection of one of the partners and an amount of the financial contribution, receive partner feedback to demonstrate an impact of the financial contribution, and display the feedback to the user. The feedback includes a photograph taken of a beneficiary of the financial contribution upon receiving benefit of the financial contribution. The partner submits the feedback to an organizer for review and the organizer approves and provides the feedback to the user.

摘要翻译： 示例性方法，装置和系统显示可选择的伙伴以促进来自用户的财务贡献，接收用户对合作伙伴之一的选择和一定数量的财务贡献，接收合作伙伴反馈以显示财务贡献的影响，并且显示 反馈给用户。 反馈包括在收到财务捐款的利益时拍摄的财政捐助受益人的照片。 合作伙伴将反馈提交给组织者进行审核，组织者批准并向用户提供反馈。

公开(公告)号：US08167557B2

公开(公告)日：2012-05-01

申请号：US12187791

申请日：2008-08-07

申请人： Tom Elliott ,  Greg Heitland ,  Jeff Howe ,  Mark C. Morris

发明人： Tom Elliott ,  Greg Heitland ,  Jeff Howe ,  Mark C. Morris

IPC分类号： F01D5/18

CPC分类号： F01D5/186 ,  F05D2240/127 ,  F05D2240/81 ,  F05D2260/2212 ,  Y02T50/673 ,  Y02T50/676

摘要： A gas turbine engine assembly has combustion gases flowing through a gas flow path. The gas turbine engine assembly includes a stator assembly comprising a stator vane that extends into the gas flow path; and a turbine rotor assembly downstream of the stator assembly and comprising a turbine platform and a turbine rotor blade extending from the turbine platform into the mainstream combustion gases flow path. The turbine rotor blade includes a pressure side and a suction side opposing the pressure side that extend from a leading edge to a trailing edge. The combustion gases form horseshoe vortices at a formation area adjacent the leading edge of the turbine rotor blade, and the turbine rotor assembly further includes a first set of holes in the turbine platform for directing first jets into the formation area of the horseshoe vortices.

摘要翻译： 燃气涡轮发动机组件具有流过气体流路的燃烧气体。 燃气涡轮发动机组件包括定子组件，该定子组件包括延伸到气体流路中的定子叶片; 以及在定子组件下游的涡轮机转子组件，并且包括涡轮机平台和从涡轮机平台延伸到主流燃烧气体流动路径中的涡轮机转子叶片。 涡轮转子叶片包括压力侧和与从前缘延伸到后缘的压力侧相对的吸力侧。 燃烧气体在与涡轮机转子叶片的前缘相邻的形成区域形成马蹄形旋涡，并且涡轮机转子组件还包括涡轮机平台中的第一组孔，用于将第一射流引导到马蹄形旋涡的形成区域中。

公开(公告)号：US20100034663A1

公开(公告)日：2010-02-11

申请号：US12187791

申请日：2008-08-07

申请人： Tom Elliott ,  Greg Heitland ,  Jeff Howe ,  Mark C. Morris

发明人： Tom Elliott ,  Greg Heitland ,  Jeff Howe ,  Mark C. Morris

IPC分类号： F01D5/18

CPC分类号： F01D5/186 ,  F05D2240/127 ,  F05D2240/81 ,  F05D2260/2212 ,  Y02T50/673 ,  Y02T50/676

摘要： A gas turbine engine assembly has combustion gases flowing through a gas flow path. The gas turbine engine assembly includes a stator assembly comprising a stator vane that extends into the gas flow path; and a turbine rotor assembly downstream of the stator assembly and comprising a turbine platform and a turbine rotor blade extending from the turbine platform into the mainstream combustion gases flow path. The turbine rotor blade includes a pressure side and a suction side opposing the pressure side that extend from a leading edge to a trailing edge. The combustion gases form horseshoe vortices at a formation area adjacent the leading edge of the turbine rotor blade, and the turbine rotor assembly further includes a first set of holes in the turbine platform for directing first jets into the formation area of the horseshoe vortices.

摘要翻译： 燃气涡轮发动机组件具有流过气体流路的燃烧气体。 燃气涡轮发动机组件包括定子组件，该定子组件包括延伸到气体流路中的定子叶片; 以及在定子组件下游的涡轮机转子组件，并且包括涡轮机平台和从涡轮机平台延伸到主流燃烧气体流动路径中的涡轮机转子叶片。 涡轮转子叶片包括压力侧和与从前缘延伸到后缘的压力侧相对的吸力侧。 燃烧气体在与涡轮机转子叶片的前缘相邻的形成区域形成马蹄形旋涡，并且涡轮机转子组件还包括涡轮机平台中的第一组孔，用于将第一射流引导到马蹄形旋涡的形成区域中。