Methods to facilitate extending gas turbine engine useful life
    1.
    发明授权
    Methods to facilitate extending gas turbine engine useful life 有权
    方便扩大燃气轮机发动机的使用寿命

    公开(公告)号:US08327538B2

    公开(公告)日:2012-12-11

    申请号:US11251679

    申请日:2005-10-17

    IPC分类号: B23P6/00

    摘要: A method facilitates extending the useful life of a turbine engine including a combustor and a turbine downstream from and in flow communication with the combustor. The method comprises identifying at least a portion of the combustor that is at least one of distressed, worn, deteriorated, satisfied pre-determined threshold data, and beyond serviceable limits, identifying at least one enhancement kit for installation within the combustor, and removing at least two portions of the combustor including at least two of a combustor dome assembly, a swirler/cowl assembly, and the combustor inner and outer liners. The method also comprises installing the enhancement kit within the turbine engine such that a useful life of the turbine engine is facilitated to be increased.

    摘要翻译: 一种方法有助于延长涡轮发动机的使用寿命,该涡轮发动机包括燃烧器和从燃烧器流动连通的下游的涡轮。 该方法包括识别至少一部分燃烧器,该燃烧器的至少一部分是处于不利的,磨损的,恶化的,满足的预定阈值数据中的至少一个,并且超出可操作的极限,识别用于安装在燃烧器内的至少一个增强套件, 燃烧器的至少两部分包括燃烧器顶盖组件,旋流器/整流罩组件和燃烧器内衬和外衬中的至少两个。 该方法还包括将增强套件安装在涡轮发动机内,从而有助于提高涡轮发动机的使用寿命。

    Methods to facilitate extending gas turbine engine useful life
    2.
    发明申请
    Methods to facilitate extending gas turbine engine useful life 有权
    方便扩大燃气轮机发动机的使用寿命

    公开(公告)号:US20070084049A1

    公开(公告)日:2007-04-19

    申请号:US11251679

    申请日:2005-10-17

    IPC分类号: B23P19/04 B23P6/00

    摘要: A method facilitates extending the useful life of a turbine engine including a combustor and a turbine downstream from and in flow communication with the combustor. The method comprises identifying at least a portion of the combustor that is at least one of distressed, worn, deteriorated, satisfied pre-determined threshold data, and beyond serviceable limits, identifying at least one enhancement kit for installation within the combustor, and removing at least two portions of the combustor including at least two of a combustor dome assembly, a swirler/cowl assembly, and the combustor inner and outer liners. The method also comprises installing the enhancement kit within the turbine engine such that a useful life of the turbine engine is facilitated to be increased.

    摘要翻译: 一种方法有助于延长涡轮发动机的使用寿命,该涡轮发动机包括燃烧器和从燃烧器流动连通的下游的涡轮。 该方法包括识别至少一部分燃烧器,该燃烧器的至少一部分是处于不利的,磨损的,恶化的,满足的预定阈值数据中的至少一个,并且超出可操作的极限,识别用于安装在燃烧器内的至少一个增强组件, 燃烧器的至少两部分包括燃烧器顶盖组件,旋流器/整流罩组件和燃烧器内衬和外衬中的至少两个。 该方法还包括将增强套件安装在涡轮发动机内,从而有助于提高涡轮发动机的使用寿命。

    Load balancing by spatial partitioning of interaction centers
    3.
    发明申请
    Load balancing by spatial partitioning of interaction centers 审中-公开
    通过交互中心的空间划分进行负载平衡

    公开(公告)号:US20060241928A1

    公开(公告)日:2006-10-26

    申请号:US11113939

    申请日:2005-04-25

    IPC分类号: G06F9/45

    CPC分类号: G16B15/00

    摘要: A method for creating a load balanced spatial partitioning of a structured, diffusing system of particles with pairwise interactions, comprises steps of: assigning a weight corresponding to a computational cost for a pair interaction of particles to a simulation space distance between the particles; performing a spatial partitioning of the simulation space; and assigning computation of pair interaction to any node that has the positions of both particles. The method can also be implemented as machine executable instructions executed by a programmable information processing system or as hard coded logic in a specialized computing apparatus such as an application-specific integrated circuit (ASIC).

    摘要翻译: 用于创建具有成对相互作用的结构化,扩散系统的负载平衡空间划分的方法包括以下步骤:将与粒子的相互作用的计算成本对应的权重分配给所述粒子之间的模拟空间距离; 执行模拟空间的空间划分; 并且将对交互的计算分配给具有两个粒子的位置的任何节点。 该方法还可以被实现为由可编程信息处理系统执行的机器可执行指令,或者作为诸如专用集成电路(ASIC)的专业计算装置中的硬编码逻辑。