Method and system for managing changes to a contact database
    5.
    发明申请
    Method and system for managing changes to a contact database 有权
    管理联系人数据库更改的方法和系统

    公开(公告)号:US20050208971A1

    公开(公告)日:2005-09-22

    申请号:US11115590

    申请日:2005-04-26

    摘要: Described is a system and method for updating a contact and adding a new contact from a call log in a communications device. The system includes a contact manager that is directed towards creating and updating call contact cards in a contact database with information retrieved from call logs of phone calls made to or from the communications device. In one embodiment, information is pre-populated into a predetermined data field of the contact card, thereby reducing workload to a user. The method includes determining if a request is for updating an existing contact card or for adding a new contact card to the contact database. The update or addition is made with information retrieved from call logs. Call information is pre-populated into a predetermined data field of the contact card, when it is determined that the request is to add a new contact card to the contact database.

    摘要翻译: 描述了一种用于更新联系人并从通信设备中的呼叫日志添加新联系人的系统和方法。 该系统包括一个联系人管理器,该联系人管理器旨在通过从通信设备进行的电话呼叫的呼叫记录中检索到的信息来创建和更新联系人数据库中的呼叫接触卡。 在一个实施例中,将信息预先填充到联系人卡片的预定数据字段中,从而减少用户的工作量。 该方法包括确定请求是否用于更新现有的联系人卡片或者将新的联系人卡片添加到联系人数据库。 更新或添加使用从呼叫记录检索的信息。 当确定请求将新的联系人卡片添加到联系人数据库时,呼叫信息被预先填充到联系人卡片的预定数据字段中。

    Film cooling for the trailing edge of a steam cooled nozzle
    7.
    发明授权
    Film cooling for the trailing edge of a steam cooled nozzle 有权
    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

    IPC分类号: F04D29/58 F01D5/18

    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。

    Film cooling for the trailing edge of a steam cooled nozzle
    8.
    发明申请
    Film cooling for the trailing edge of a steam cooled nozzle 有权
    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

    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。