BIOMARKER FOR ASSESSING RESPONSE TO CHYMASE TREATMENT
    3.
    发明申请
    BIOMARKER FOR ASSESSING RESPONSE TO CHYMASE TREATMENT 审中-公开
    生物标记评估对CHYMASE治疗的反应

    公开(公告)号:US20100003712A1

    公开(公告)日:2010-01-07

    申请号:US12474413

    申请日:2009-05-29

    IPC分类号: C12Q1/02 C07K14/715

    摘要: A biomarker that correlates to treatment with drugs that inhibit chymase is disclosed. This biomarker has been shown to have utility in assessing response to chymase inhibitor compounds. The immunoreactivity or levels of the biomarker is increased upon treatment with chymase inhibitor compounds, thus indicating that this biomarker is involved in chymase activity.

    摘要翻译: 公开了与用抑制胃促胰酶的药物治疗相关的生物标志物。 该生物标志物已被证明可用于评估对胃促胰酶抑制剂化合物的反应。 在用糜酶抑制剂化合物治疗时,生物标志物的免疫反应性或水平增加,因此表明该生物标志物参与糜酶活性。

    Processing of SLPI by chymase
    4.
    发明申请
    Processing of SLPI by chymase 有权
    通过胃肠酶处理SLPI

    公开(公告)号:US20070166779A1

    公开(公告)日:2007-07-19

    申请号:US11652753

    申请日:2007-01-12

    IPC分类号: C12Q1/37

    CPC分类号: C12Q1/37 G01N2333/811

    摘要: It is now discovered that human chymase cleaves human SLPI at a specific site and that this cleavage can be used as an indicator of chymase activity. The present invention provides methods of diagnosing a chymase-associated disease or evaluating the efficiency of a treatment of a chymase-associated disease in a human subject by measuring SLPI processing, as well as other related methods and compositions.

    摘要翻译: 现在发现人糜酶在特定位点切割人SLPI,并且该切割可以用作糜酶活性的指示剂。 本发明提供了通过测量SLPI处理以及其它相关方法和组合物来诊断糜酶相关疾病或通过测量人受试者中糜酶相关疾病的治疗效率的方法。

    Centrifugal compressor forward thrust and turbine cooling apparatus
    7.
    发明授权
    Centrifugal compressor forward thrust and turbine cooling apparatus 有权
    离心式压缩机前推和涡轮冷却装置

    公开(公告)号:US08147178B2

    公开(公告)日:2012-04-03

    申请号:US12342972

    申请日:2008-12-23

    IPC分类号: F01D3/04

    摘要: A gas turbine engine centrifugal compressor axial forward thrust apparatus bleeds impeller tip aft bleed flow from between an annular centrifugal compressor impeller of a high pressure rotor and a diffuser directly downstream of the impeller. The apparatus then uses the aft bleed flow to pressurize an annular cavity extending radially between an inner combustor casing and the rotor and extending axially between forward and aft thrust balance seals. Forward and aft thrust balance lands are in sealing engagement with the forward and aft thrust balance seals on the high pressure rotor respectively. An annular stator plenum in fluid communication with the annular cavity is bounded in part by a forward end wall having conical diffusion holes therethrough which may be axially or circumferentially or axially and circumferentially angled. The forward thrust balance seal may be on an aft conical arm of the impeller.

    摘要翻译: 燃气涡轮发动机离心式压缩机轴向前推推力装置使叶轮尖端从高压转子的环形离心式压缩机叶轮与直接在叶轮下游的扩散器之间流出。 然后,该装置使用尾部流出流对在内部燃烧器壳体和转子之间径向延伸并在前后推力平衡密封件之间轴向延伸的环形空腔加压。 前后推力平衡台分别与高压转子上的前后推力平衡密封件密封接合。 与环形空腔流体连通的环形定子增压室部分地由具有锥形扩散孔的前端壁限定,其可以在轴向或周向或轴向和周向上成角度。 前推力平衡密封件可以在叶轮的后圆锥形臂上。

    CENTRIFUGAL COMPRESSOR FORWARD THRUST AND TURBINE COOLING APPARATUS
    8.
    发明申请
    CENTRIFUGAL COMPRESSOR FORWARD THRUST AND TURBINE COOLING APPARATUS 有权
    离心式压缩机前进式和涡轮冷却装置

    公开(公告)号:US20100158668A1

    公开(公告)日:2010-06-24

    申请号:US12342972

    申请日:2008-12-23

    IPC分类号: F01D3/04

    摘要: A gas turbine engine centrifugal compressor axial forward thrust apparatus bleeds impeller tip aft bleed flow from between an annular centrifugal compressor impeller of a high pressure rotor and a diffuser directly downstream of the impeller. The apparatus then uses the aft bleed flow to pressurize an annular cavity extending radially between an inner combustor casing and the rotor and extending axially between forward and aft thrust balance seals. Forward and aft thrust balance lands are in sealing engagement with the forward and aft thrust balance seals on the high pressure rotor respectively. An annular stator plenum in fluid communication with the annular cavity is bounded in part by a forward end wall having conical diffusion holes therethrough which may be axially or circumferentially or axially and circumferentially angled. The forward thrust balance seal may be on an aft conical arm of the impeller.

    摘要翻译: 燃气涡轮发动机离心式压缩机轴向前推推力装置使叶轮尖端从高压转子的环形离心式压缩机叶轮与直接在叶轮下游的扩散器之间流出。 然后,该装置使用尾部流出流对在内部燃烧器壳体和转子之间径向延伸并在前后推力平衡密封件之间轴向延伸的环形空腔加压。 前后推力平衡台分别与高压转子上的前后推力平衡密封件密封接合。 与环形空腔流体连通的环形定子增压室部分地由具有锥形扩散孔的前端壁限定,所述锥形扩散孔可沿轴向或周向或轴向和周向成角度。 前推力平衡密封件可以在叶轮的后圆锥形臂上。