Methods and compositions for assessing CpG methylation
    106.
    发明申请
    Methods and compositions for assessing CpG methylation 审中-公开
    用于评估CpG甲基化的方法和组合物

    公开(公告)号:US20050233340A1

    公开(公告)日:2005-10-20

    申请号:US10828986

    申请日:2004-04-20

    IPC分类号: C12Q1/68 C07H21/04 C12M1/34

    摘要: Methods and compositions for assessing CpG island methylation are provided. Specifically, the invention provides an unstructured nucleic acid (UNA) oligonucleotide that base pairs with, i.e., hybridizes to, CpG islands. The subject oligonucleotide may be present in an array, and find use in methods for evaluating methylation of CpG islands in cells. Kits and computer programming for use in practicing the subject methods are also provided.

    摘要翻译: 提供了用于评估CpG岛甲基化的方法和组合物。 具体地,本发明提供了与CpG岛碱基配对,即杂交的非结构化核酸(UNA)寡核苷酸。 受试寡核苷酸可以以阵列存在,并且可用于评估细胞中CpG岛的甲基化的方法。 还提供了用于实践主题方法的套件和计算机程序设计。

    Methods and compositions for assessing chromosome copy number
    107.
    发明申请
    Methods and compositions for assessing chromosome copy number 审中-公开
    用于评估染色体拷贝数的方法和组合物

    公开(公告)号:US20050233338A1

    公开(公告)日:2005-10-20

    申请号:US10828892

    申请日:2004-04-20

    IPC分类号: C12M1/34 C12Q1/68

    摘要: Methods and compositions for assessing chromosome copy number are provided. Specifically, the invention provides an array containing a plurality of features including at least one feature that contains oligonucleotides that are complementary to a structural region of a chromosome. The subject methods and compositions may be used to detect chromosome copy number in a cell, and, as such, may be employed in a variety of diagnostic and research applications. Kits and computer programming for use in practicing the subject methods are also provided.

    摘要翻译: 提供了评估染色体拷贝数的方法和组合物。 具体而言,本发明提供一种包含多个特征的阵列,其包括至少一个特征,其包含与染色体的结构区域互补的寡核苷酸。 本发明的方法和组合物可用于检测细胞中的染色体拷贝数,因此可用于多种诊断和研究应用。 还提供了用于实践主题方法的套件和计算机程序设计。

    Turbine blade airfoil having improved creep capability
    108.
    发明授权
    Turbine blade airfoil having improved creep capability 有权
    涡轮叶片翼型具有改善的蠕变能力

    公开(公告)号:US06932577B2

    公开(公告)日:2005-08-23

    申请号:US10719927

    申请日:2003-11-21

    IPC分类号: B63H1/14 F01D5/14 F01D5/18

    CPC分类号: F01D5/187 F01D5/141

    摘要: A turbine blade including an airfoil having a profile in accordance with Table 1 is disclosed. The turbine blade has a plurality of cooling passages extending radially outward through the airfoil. The aerodynamic profile of the airfoil has been reconfigured to reduce airfoil stress for a given operating temperature, thereby resulting in increased creep rupture life of the airfoil.

    摘要翻译: 公开了一种包括具有根据表1的轮廓的翼型的涡轮叶片。 涡轮机叶片具有径向向外延伸穿过翼型的多个冷却通道。 已经重构了翼型件的空气动力学特性,以减少给定工作温度下的翼型应力,从而导致翼型件的蠕变断裂寿命增加。