Mass spectrometers comprising accelerator devices

Patent metadata

Field	Value
Publication number	US-9318309-B2
Application number	US-201214355884-A
Country	US
Kind code	B2
Filing date	Nov 5, 2012
Priority date	Nov 4, 2011
Publication date	Apr 19, 2016
Grant date	Apr 19, 2016

Abstract

A method of mass spectrometry is disclosed comprising providing a flight region for ions to travel through and a detector or fragmentation device. A potential profile is maintained along the flight region such that ions travel towards the detector or fragmentation device. The potential at which a first length of the flight region is maintained is then changed from a first potential to a second potential while at least some ions are travelling within the first length of flight region. The changed potential provides a first potential difference at an exit of the length of flight region, through which the ions are accelerated as they leave the length of flight region. This increases the kinetic energy of the ions prior to them reaching the detector or fragmentation cell.

First claim

The invention claimed is:

1. A method of mass spectrometry comprising:
providing a flight region for ions to travel through between an acceleration electrode and an ion detector, wherein ions are accelerated into the flight region by applying a voltage pulse to the acceleration electrode;
maintaining a potential profile along the flight region such that ions travel towards the detector, wherein ions having a range of different mass to charge ratios are passed into the flight region and separate spatially according to mass to charge ratio as the ions travel towards the detector; and
changing the potential at which a first length of the flight region is maintained from a first potential to a second potential whilst at least some ions are travelling within said first length of the flight region, the changed potential providing a first potential difference at an exit of said length of the flight region, whereby said at least some ions are accelerated through the potential difference as the ions leave said length of the flight region so as to arrive at the detector with increased kinetic energy so as to increase ion detection efficiency of these ions.

2. The method of claim 1 , wherein the potential at which the first length of the flight region is maintained is changed relative to the potential at which the detector is maintained so as to provide said potential difference between said first length and said detector.

3. The method of claim 1 , wherein the potential at which the first length of the flight region is maintained is changed relative to the potential at which a second downstream length of said flight region is maintained so as to provide said potential difference between said first and second lengths of the flight region.

4. The method of claim 1 , wherein the potential of the first length of the flight region is varied with time such that the potential difference is set to be relatively small or no potential difference whilst ions of relatively low mass to charge ratio pass through and exit the first length of the flight region, and such that the potential difference is set to be relatively high when ions of relatively high mass to charge ratio pass through and exit the first length of the flight region.

5. The method of claim 1 , comprising changing the potential at which the first length of the flight region is maintained from the second potential to a third potential whilst ions are travelling within said first length of the flight region, the changed potential providing a second potential difference at an exit of said first length of the flight region, whereby ions are accelerated through the second potential difference as the ions leave the first length of the flight region.

6. The method of claim 1 , comprising providing an ion mirror in the flight region such that ions travel in a first direction through the first length of the flight region and to a first end of the first length of the flight region as the ions travel towards the ion mirror, and wherein the ions travel through the first length of the flight region in a second direction and to a second end of the first length of the flight region after having been reflected by the mirror as the ions travel the detector; wherein said step of changing the potential at which the first length of the flight region is maintained provides the first potential difference at the second end of said first length of the flight region, wherein the ions are reflected by the ion mirror so that the ions travel through the first length of the flight region in the second direction, and wherein the ions are then accelerated through the first potential difference as the ions leave said first length of the flight region through the second end and travel towards the detector.

7. The method of claim 1 , comprising changing the potential at which a further length of the flight region is maintained whilst at least some ions are travelling within said further length of the flight region, the further length being in a different axial position of the flight region to the first length of the flight region, the changed potential resulting in a further potential difference being arranged at the exit of said further length of flight region, whereby at least some ions are accelerated through the further potential difference as the ions leave said further length of flight region.

8. The method of claim 1 , wherein axially spaced electrodes are arranged along an axial length of the flight region and DC potentials are applied to these electrodes so as to create a DC axial field that exerts a force on ions in an axial direction that is opposite to the direction in which the ions are accelerated by the potential difference(s); wherein the potential of the first length of the flight region or the potential of a further length of the flight region is varied with time so as to accelerate ions of a selected range of mass to charge ratios through the first or further potential difference in one direction, and wherein ions having other mass to charge ratios are driven in another direction by the DC axial field.

9. The method of claim 8 , wherein the first or further length of flight region is a field free region, and wherein the step of changing the potential at which the first or further length of the flight region is maintained comprises maintaining the length as a field free region.

10. The method of claim 8 , wherein an axial voltage gradient is arranged along the first or further length of flight region, and wherein changing the potential at which the first or further length of the flight region is maintained comprises changing the magnitudes of the voltages forming a voltage gradient whilst maintaining the voltage gradient constant.

11. The method of claim 8 , wherein changing the potential of said first or further length of flight region whilst ions travel therethrough increases the potential energy of the ions without increasing their kinetic energy as the ions travel therethrough.

12. The method of claim 8 , wherein the ion detector is maintained at a constant potential whilst the potential applied to the first or further length of the flight region is changed.

13. A time of flight mass spectrometer comprising:
an acceleration electrode;
a detector;
a flight region for ions to travel through between the acceleration electrode and the detector; and
control means arranged and adapted to:
accelerate ions into the flight region by applying a voltage pulse to the acceleration electrode;
maintain a potential profile along the flight region such that, in use, ions travel towards the detector, wherein ions having a range of different mass to charge ratios are passed into the flight region and separate spatially according to mass to charge ratio as the ions travel towards the detector; and
change the potential at which a first length of the flight region is maintained from a first potential to a second potential whilst at least some ions are travelling within said first length of the flight region, the changed potential providing a first potential difference at an exit of said length of the flight region, whereby said at least some ions are accelerated through the potential difference as the ions leave said length of the flight region so as to arrive at the detector with increased kinetic energy so as to increase an ion detection efficiency of these ions.

Assignees

• Micromass Ltd

Inventors

• Brown Jeffery Mark
• Green Martin Raymond
• Langridge David J

Classifications

• H01J49/06 Primary

  Electron- or ion-optical arrangements · CPC title

• H01J49/403

  characterised by the acceleration optics and/or the extraction fields · CPC title

• H01J49/40 Primary

  Time-of-flight spectrometers (H01J49/36 takes precedence) · CPC title

• H01J49/062

  Ion guides (linear ion traps performing mass selection H01J49/4225, mass filters H01J49/421) · CPC title

• H01J49/0031 Primary

  Step by step routines describing the use of the apparatus (H01J49/0081 takes precedence) · CPC title