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    • 41. 发明公开
    • IMPROVED ION MIRROR AND ION-OPTICAL LENS FOR IMAGING
    • EP3381045A1
    • 2018-10-03
    • EP16869126.9
    • 2016-11-21
    • Micromass UK LimitedLeco Corporation
    • HOYES, John BrianVERENCHIKOV, AnatolyYAVOR, MikhailRICHARDSON, Keith
    • H01J49/40
    • H01J49/406H01J49/063H01J49/067H01J49/068H01J49/08
    • An ion mirror is disclosed comprising an ion entrance electrode section (62) at the ion entrance to the ion mirror, an energy focussing electrode section (66) for reflecting ions back along a longitudinal axis towards said ion entrance, and a spatial focussing electrode section (64) arranged between the ion entrance electrode section (62) and the energy focussing electrode section (66) for spatially focussing the ions. One or more DC voltage supply is provided to apply a DC potential to the ion entrance electrode section (62) that is intermediate the DC potential applied to the spatial focussing electrode section (64) and the DC potential applied to the energy focussing electrode section (66). The ion mirror further comprises: (i) at least one first transition electrode (68) arranged between said ion entrance electrode section (62) and said spatial focussing electrode section (64), wherein said one or more DC voltage supply is configured to apply a DC potential to said at least one first transition electrode that is intermediate the DC potential applied to the ion entrance electrode section (62) and the DC potential applied to the spatial focussing electrode section (64); and (ii) at least one second transition electrode (69) arranged between said energy focussing electrode section (66) and said spatial focussing electrode section (64), wherein said one or more DC voltage supply is configured to apply a DC potential to said at least one second transition electrode (69) that is intermediate the DC potential applied to the spatial focussing electrode section (64) and the DC potential applied to the ion entrance electrode section (62).
    • 45. 发明公开
    • ORTHOGONAL ACCELERATION COAXIAL CYLINDER TIME OF FLIGHT MASS ANALYSER
    • KOAXIALZYLINDER-FLUGZEITMASSENANALYSATOR DER ORTHOGONALEN BESCHLEUNIGUNG
    • EP2850647A2
    • 2015-03-25
    • EP13724351.5
    • 2013-05-16
    • Micromass UK Limited
    • HOYES, John BrianLANGRIDGE, David J.WILDGOOSE, Jason Lee
    • H01J49/40
    • A Time of Flight mass analyzer 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。