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    • 15. 发明申请
    • ORTHOGONAL ACCELERATION COAXIAL CYLINDER TIME OF FLIGHT MASS ANALYSER
    • 飞行质量分析仪的正交加速同轴气缸时间
    • WO2013171499A2
    • 2013-11-21
    • PCT/GB2013/051269
    • 2013-05-16
    • MICROMASS UK LIMITED
    • HOYES, John BrianLANGRIDGE, David J.WILDGOOSE, Jason Lee
    • H01J49/40
    • H01J49/401G01N2223/506H01J49/0031H01J49/405H01J49/406H01J49/408
    • A Time of Flight mass analyser is disclosed comprising an annular ion guide having a longitudinal axis and comprising a first annular ion guide section and a second annular ion guide section. Ions are introduced into the first annular ion guide section so that the ions form substantially stable circular orbits within the first annular ion guide section about the longitudinal axis. An ion detector is disposed within the annular ion guide. Ions are orthogonally accelerated in a first axial direction from the first annular ion guide section into the second annular ion guide section. An axial DC potential is maintained along at least a portion of the second annular ion guide section so that the ions are reflected in a second axial direction which is substantially opposed to the first axial direction. The ions undergo multiple axial passes through the second annular ion guide section before being detected by the ion detector.
    • 公开了一种飞行时间质量分析器,其包括具有纵向轴线的环形离子引导件,并且包括第一环形离子引导部分和第二环形离子引导部分。 离子被引入到第一环形离子引导部分中,使得离子在第一环形离子引导部分内围绕纵向轴线形成基本上稳定的圆周轨道。 离子检测器设置在环形离子导向器内。 离子在从第一环形离子引导部分到第二环形离子引导部分的第一轴向方向上正交加速。 沿着第二环形离子引导部分的至少一部分保持轴向DC电位,使得离子在基本上与第一轴向方向相对的第二轴向反射。 在被离子检测器检测到之前,离子经过多个轴向通过第二环形离子引导部分。
    • 19. 发明申请
    • MULTI-REFLECTING TOF MASS SPECTROMETER
    • 多反射TOF质谱仪
    • WO2016174462A1
    • 2016-11-03
    • PCT/GB2016/051238
    • 2016-04-29
    • MICROMASS UK LIMITEDLECO CORPORATION
    • HOYES, John BrianRICHARDSON, KeithVERENCHIKOV, AnatolyYAVOR, Mikhail
    • H01J49/40H01J49/06
    • H01J49/405H01J49/061H01J49/406H01J49/426
    • A method of time-of-flight mass spectrometry is disclosed comprising: providing two ion mirrors (42) that are spaced apart in a first dimension (X-dimension) and that are each elongated in a second dimension (Z-dimension) orthogonal to the first dimension; introducing packets of ions (47) into the space between the mirrors using an ion introduction mechanism (43) such that the ions repeatedly oscillate in the first dimension (X-dimension) between the mirrors (42) as they drift through said space in the second dimension (Z-dimension); oscillating the ions in a third dimension (Y-dimension) orthogonal to both the first and second dimensions as the ions drift through said space in the second dimension (Z-dimension); and receiving the ions in or on an ion receiving mechanism (44) after the ions have oscillated multiple times in the first dimension (X-dimension); wherein at least part of the ion introduction mechanism (43) and/or at least part of the ion receiving mechanism (44) is arranged between the mirrors (42).
    • 公开了一种飞行时间质谱法的方法,其包括:提供在第一维度(X维)上间隔开的两个离子镜(42),并且每个离子镜在与第二维度(X维)正交的第二维度 第一维度 使用离子引入机构(43)将离子束(47)引入到反射镜之间的空间中,使得当它们漂移通过所述空间中的所述空间时,离子在反射镜(42)之间的第一维度(X维)中重复地振荡 第二维(Z维); 当离子漂移通过第二维度(Z维)中的所述空间时,使垂直于第一和第二维度的第三维(Y-维)中的离子振荡; 以及在所述离子在所述第一维度(X维度)中多次振荡之后,接收离子接收机构(44)中或其上的离子; 其中所述离子引入机构(43)的至少一部分和/或所述离子接收机构(44)的至少一部分配置在所述反射镜(42)之间。