Multi-reflecting TOF mass spectrometer

Abstract

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).

Claims

1. A multi-reflecting time-of-flight mass spectrometer comprising: two ion mirrors that are spaced apart from each other in a first dimension (X-dimension) and that are each elongated in a second dimension (Z-dimension) that is orthogonal to the first dimension; an ion introduction mechanism for introducing packets of ions into the space between the mirrors such that they travel along a trajectory that is arranged at an angle to the first and second dimensions such that the ions repeatedly oscillate in the first dimension (X-dimension) between the mirrors as they drift through said space in the second dimension (Z-dimension); wherein the mirrors and ion introduction mechanism are arranged and configured such that the ions also oscillate in a third dimension (Y-dimension), that is orthogonal to both the first and second dimensions, as the ions drift through said space in the second dimension (Z-dimension) such that the ions oscillate in the third dimension (Y-dimension) so as to perform an oscillation between positions of maximum amplitude of the oscillation; wherein the spectrometer comprises an ion receiving mechanism arranged such that all ions, in each of the packets of ions, that are received by the ion receiving mechanism have oscillated the same number of times between the ion mirrors the first dimension (X-dimension); and wherein: (i) at least part of the ion introduction mechanism is arranged between the mirrors, wherein at positions in the first and second dimensions (X- and Z-dimensions) of said at least part of the ion introduction mechanism, the at least part of the ion introduction mechanism extends over only part of the distance in the third dimension (Y-dimension) between said positions of maximum amplitude of the oscillation; and/or (ii) at least part of the ion receiving mechanism is arranged between the mirrors, wherein at positions in the first and second dimensions (X- and Z-dimensions) of said at least part of the ion receiving mechanism, the at least part of the ion receiving mechanism extends over only part of the distance in the third dimension (Y-dimension) between said positions of maximum amplitude of the oscillation.

2. The spectrometer of claim 1, wherein the ion mirrors and ion introduction mechanism are configured so as to cause the ions to travel a distance Z.sub.R in the second dimension (Z-dimension) during each reflection of the ions between the mirrors in the first dimension (X-dimension); and wherein the distance Z.sub.R is smaller than the length in the second dimension (Z-dimension) of said at least part of the ion introduction mechanism and/or of the length in the second dimension (Z-dimension) of said at least part of the ion receiving mechanism.

3. The spectrometer of claim 2, wherein the length in the second dimension (Z-dimension) of said at least part of the ion introduction mechanism and/or of the length in the second dimension (Z-dimension) of said at least part of the ion receiving mechanism is up to four times the distance Z.sub.R.

4. The spectrometer of claim 1, wherein the ion mirrors and ion introduction mechanism are configured so as to cause the ions to oscillate at rates in the first dimension (X-dimension) and third dimension (Y-dimension) such that when the ions have the same position in the first and second dimensions (X- and Z-dimensions) as said at least part of the ion introduction mechanism, the ions have a different position in the third dimension (Y-dimension), such that the trajectories of the ions bypass said ion introduction mechanism at least once as the ions oscillate in the first dimension (X-dimension); and/or wherein the ion mirrors and ion introduction mechanism are configured so as to cause the ions to oscillate at rates in the first dimension (X-dimension) and third dimension (Y-dimension) such that when the ions have the same position in the first and second dimensions (X- and Z-directions) as said at least part of the ion receiving mechanism, the ions have a different position in the third dimension (Y-dimension), such that the trajectories of the ions bypass said ion receiving mechanism least once as they oscillate in the first dimension (X-dimension).

5. The spectrometer of claim 1, configured such that the ions oscillate in the third dimension (Y-dimension) about an axis with a maximum amplitude of oscillation, and wherein said at least part of the ion introduction mechanism, and/or said at least part of the ion receiving mechanism, is spaced apart from the axis in the third dimension (Y-dimension) by a distance that is smaller than the maximum amplitude of oscillation.

6. The spectrometer of claim 1, configured such that the ions oscillate in the third dimension (Y-dimension) about an axis of oscillation, and wherein either: (i) said at least part of the ion introduction mechanism and said at least part of ion receiving mechanism are spaced apart from the axis in the third dimension (Y-dimension); or (ii) either one of said at least part of the ion introduction mechanism and said at least part of ion receiving mechanism is located on the axis, and the other of said at least part of the ion introduction mechanism and said at least part of ion receiving mechanism is spaced apart from the axis in the third dimension (Y-dimension); or (iii) both said at least part of the ion introduction mechanism and said at least part of the ion receiving mechanism are located on the axis.

7. The spectrometer of claim 1, wherein said at least part of the ion receiving mechanism is arranged between the mirrors for receiving ions from the space between the mirrors after the ions have oscillated one or more times in the third dimension (Y-dimension).

8. The spectrometer of claim 1, wherein the ion receiving mechanism comprises an ion guide and said at least part of the ion receiving mechanism is the entrance to the ion guide, further comprising an ion detector arranged outside of the space between the ion mirrors, wherein the ion guide is arranged and configured to receive ions from said space between the ion mirrors and to guide the ions onto the ion detector.

9. The spectrometer of claim 8, wherein the ion guide is an electric or magnetic sector.

10. The spectrometer of claim 1, wherein the ion receiving mechanism is an ion deflector for deflecting ions out of the space between the mirrors onto a detector arranged outside of the space between the ion mirrors.

11. The spectrometer of claim 1, wherein the ion introduction mechanism is a pulsed ion source arranged between the mirrors and configured to eject, or generate and emit, packets of ions so as to perform the step of introducing ions into the space between the mirrors.

12. The spectrometer of claim 11, wherein said pulsed ion source comprises an orthogonal accelerator or ion trap for converting a beam of ions into packets of ions.

13. The spectrometer of claim 1, wherein the ion introduction mechanism comprises an ion guide and said at least part of the ion introduction mechanism is the exit of the ion guide, further comprising an ion source arranged outside of the space between the ion mirrors, wherein the ion guide is arranged and configured to receive ions from said ion source and to guide the ions into said space so as to pass along said trajectory that is arranged at an angle to the first and second dimensions.

14. The spectrometer of claim 13, wherein the ion guide is an electric or magnetic sector.

15. The spectrometer of claim 1, wherein said at least part of the ion introduction mechanism is an ion deflector for deflecting the trajectory of the ions.

16. The spectrometer of claim 1, further comprising one or more beam stops arranged between the ion mirrors and in the ion flight path between the ion introduction mechanism and the ion receiving mechanism, wherein the one or more beam stops is arranged and configured so as to block the passage of ions that are located at the front and/or rear edge of each ion beam packet as determined in the second dimension (Z-dimension); and/or wherein each packet of ions diverges in the second dimension (Z-dimension) as it travels from the ion introduction mechanism to the ion receiving mechanism; and wherein one or more beam stops is arranged and configured to block the passage of ions in the ion packet that diverge from the average ion trajectory by more than a predetermined amount.

17. The spectrometer of claim 16, wherein at least one of the beam stops is an auxiliary ion detector, wherein the spectrometer comprises: a primary ion detector arranged and configured for detecting the ions after they have performed a desired number of oscillations in the first dimension (X-dimension) between the mirrors and said auxiliary ion detector, wherein said auxiliary detector is arranged and configured to detect a portion of the ions in each ion packet; and a control system for performing at least one of: controlling the gain of the primary ion detector based on the intensity detected by the auxiliary detector, or steering the trajectories of the ion packets based on the signal output from the auxiliary ion detector, optionally for optimising ion transmission from the ion introduction mechanism to the primary ion detector.

18. The spectrometer of claim 1, wherein the ion introduction mechanism comprises at least one voltage supply, electronic circuitry and electrodes; wherein the circuitry is configured to control the voltage supply to apply voltages to the electrodes so as to pulse ions into one of the ion mirrors at an angle or position relative to an axis of the mirror such that the ions oscillate in the third dimension (Y-dimension).

19. The spectrometer of claim 1, wherein the ion receiving mechanism is an ion detector and the spectrometer is configured to determine the mass to charge ratios of the ions from their time of flight from the ion introduction mechanism to the ion receiving mechanism.

20. A method of time-of-flight mass spectrometry comprising: providing two ion mirrors that are spaced apart from each other in a first dimension (X-dimension) and that are each elongated in a second dimension (Z-dimension) that is orthogonal to the first dimension; introducing packets of ions into the space between the mirrors using an ion introduction mechanism such that the ions travel along a trajectory that is arranged at an angle to the first and second dimensions such that the ions repeatedly oscillate in the first dimension (X-dimension) between the mirrors as they drift through said space in the second dimension (Z-dimension); oscillating the ions in a third dimension (Y-dimension), that is orthogonal to both the first and second dimensions, as the ions drift through said space in the second dimension (Z-dimension) such that the ions oscillate in the third dimension (Y-dimension) so as to perform an oscillation between positions of maximum amplitude of the oscillation; receiving the ions in or on an ion receiving mechanism after the ions have oscillated multiple times in the first dimension (X-dimension); wherein all ions, in each of the packets of ions, that are received in or on the ion receiving mechanism have oscillated the same number of times between the ion mirrors in the first dimension (X-dimension); and wherein: (i) at least part of the ion introduction mechanism is arranged between the mirrors, wherein at positions in the first and second dimensions (X- and Z-dimensions) of said at least part of the ion introduction mechanism, the at least part of the ion introduction mechanism extends over only part of the distance in the third dimension (Y-dimension) between said positions of maximum amplitude of the oscillation; and/or (ii) at least part of the ion receiving mechanism is arranged between the mirrors, wherein at positions in the first and second dimensions (X- and Z-dimensions) of said at least part of the ion receiving mechanism the at least part of the ion receiving mechanism extends over only part of the distance in the third dimension (Y-dimension) between said positions of maximum amplitude of the oscillation.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Various embodiments of the present invention will now be described, by way of example only, and with reference to the accompanying drawings in which:

(2) FIG. 1 shows an MR-TOF-MS instrument according to the prior art;

(3) FIG. 2 shows a block diagram of the method of multi-reflecting time-of-flight mass spectrometric analysis according to an embodiment of the present invention;

(4) FIGS. 3A-3B show simulated and schematic views of the ion trajectory in the X-Y plane of an MRTOF analyzer according to an embodiment of the present invention;

(5) FIGS. 4A-4D show two and three-dimensional schematic views of an MR-TOF-MS according to an embodiment of the present invention, wherein the ion source and detector are displaced in the Y-direction;

(6) FIGS. 5A-5B show an example of gridless ion mirrors that are optimized for isochronous off-axis ion motion; and FIGS. 5C-5E show projections in the X-Y plane of example ion trajectories in the analyzer that are optimized for reducing flight time aberrations with respect to the spatial and energy spreads;

(7) FIGS. 6A-6C show results of ion optical simulations for the analyzer of FIGS. 5A-5B;

(8) FIGS. 7A-7B show two and three-dimensional schematic views of an MR-TOF-MS according to another embodiment of the present invention, wherein electric sectors are used to inject and extract the ions from the time of flight region;

(9) FIGS. 8A-8B show two and three-dimensional schematic views of MR-TOF-MS instruments according to further embodiments of the present invention, wherein deflectors are used to control the initial trajectory of the ions;

(10) FIGS. 9A-9F show two and three-dimensional schematic views of an MR-TOF-MS according to another embodiment of the present invention, wherein various different types of pulsed converters are used to inject ions into the time of flight region.

DETAILED DESCRIPTION

(11) In order to assist the understanding of the present invention, a prior art instrument will now be described with reference to FIG. 1. FIG. 1 shows a schematic of the folded path planar MR-TOF-MS of SU 1725289, incorporated herein by reference. The planar MR-TOF-MS 11 comprises two gridless electrostatic mirrors 12, each composed of three electrodes that are extended in the drift Z-direction. Each ion mirror forms a two-dimensional electrostatic field in the X-Y plane. An ion source 13 (e.g., pulsed ion converter) and an ion receiver 14 (e.g., detector) are located in the drift space between said ion mirrors 12 and are spaced apart in the Z-direction. Ion packets are produced by the source 13 and are injected into the time of flight region between the mirrors 12 at a small inclination angle to the X-axis. The ions therefore have a velocity in the X-direction and also have a drift velocity in the Z-direction. The ions are reflected between the ion mirrors 12 multiple times as they travel in the Z-direction from the source 13 to the detector 14. The ions thus have jigsaw ion trajectories 15,16,17 through the device.

(12) The ions advance in the drift Z-direction by an average distance Z.sub.RC*sin per mirror reflection, where C is the distance in the X-direction between the ion reflection points. The ion trajectories 15 and 16 represent the spread of ion trajectories caused by the initial ion packet width Z.sub.S in the ion source 13. The trajectories 16 and 17 represent the angular divergence of the ion packet as it travels through the instrument, which increases the ion packet width in the Z-direction by an amount dZ by the time that the ions reach the detector 14. The overall spread of the ion packet by the time that it reaches the detector 14 is represented by Z.sub.D.

(13) The MR-TOF-MS 11 provides no ion focusing in the drift Z-direction, thus limiting the number of reflection cycles between the ion mirrors 12 that can be performed before the ion beam becomes overly dispersed in the Z-direction by the time it reaches the detector 14. This arrangement therefore requires a certain ion trajectory advance per reflection Z.sub.R which must be above a certain value in order to avoid ion trajectories overlapping due to ion dispersion and causing spectral confusion.

(14) As has been described in WO 2014/074822, incorporated herein by reference, the lowest realistic divergence of ion packets is expected to be about +/1 mrad for known orthogonal ion accelerators, radial traps and pulsed ion sources. The combination of initial velocity and spatial spread of the ions in a realistic ion source limits the minimal turnaround time of the ions at maximal energy spread. In order for the MR-TOF-MS instrument to reach mass resolving powers above R=200000, the ion flight path through the time of flight region of the instrument must be extended to at least 16 m. Accordingly, the beam width in the Z-direction at the detector 14 is expected to be Z.sub.D30 mm. Further, in order to avoid ion trajectory and signal overlapping between adjacent mirror reflections in the prior art instrument 11, the ion trajectory advance per mirror reflection Z.sub.R must be at least 50 mm, so as to exceed the ion packet spreading at the detector Z.sub.D. Accordingly, the total advance in the Z-direction for 16 reflections (i.e. the distance between source 13 and detector 14) is Z.sub.A>800 mm. When accounting for Z-edge fringing fields, electrode widths, gaps for electrical isolation and vacuum chamber width, the estimated analyzer size in the X-Z plane would be above 1 m1 m. This is beyond the practical size for a commercial instrument, for example, because the vacuum chamber would be too large and unstable.

(15) Another problem of such planar MR-TOF analyzers 11 is the small duty cycle due to the orthogonal accelerator 13. For example, in order to avoid spectral overlaps for values of ion trajectory advance per mirror reflection Z.sub.R=50 mm and beam width at detector Z.sub.D=40 mm, the width of each injected ion packets is limited to about Z.sub.S=10 mm. The duty cycle of an orthogonal accelerator can be estimated as a ratio Z.sub.S/Z.sub.A, and is therefore about 1% for the example in which Z.sub.A>800 mm. When using smaller analyzers, the duty cycle therefore rapidly diminishes and drops even lower than this.

(16) Embodiments of the present invention provide a planar MR-TOF-MS instrument having an improved duty cycle, high resolution and practical size. For example, the instrument may have an improved duty cycle while reaching a resolution above 200,000 and having a size below 0.5 m1 m.

(17) The inventors have realized that the planar MR-TOF-MS instrument may be substantially improved by oscillating the ions in the X-Y plane such that ions do not collide with the source 13 (e.g., orthogonal accelerator) when they are reflected between the ion mirrors 12. Alternatively, or additionally, the ions may be oscillated in the X-Y plane such that ions do not collide with the receiver 14 (e.g., detector) until the ions have performed at least a predetermined number of ion mirror reflections. The embodiments therefore relate to an instrument that is similar to that shown and described in relation to FIG. 1, except that the ions are oscillated in the X-Y plane.

(18) FIG. 2 shows a flow diagram illustrating a method 21 of multi-reflecting time-of-flight mass spectrometric analysis according to an embodiment of the present invention. The method comprises the following steps: (a) forming ion mirrors having two substantially parallel aligned electrostatic fields, wherein said fields may be two-dimensional in the X-Y plane and substantially extended along the drift Z-direction, and wherein said fields may be arranged for isochronous ion reflection in the X-direction; (b) forming pulsed ion packets in an ion source and injecting each ion packet at a relatively small inclination angle to the X-axis in the X-Z plane, thus forming a mean jigsaw ion trajectory with an advance distance Z.sub.R per ion mirror reflection; (c) receiving said ion packets on an ion receiver displaced downstream in the Z-direction from said ion injection region; (d) providing said ion packets, said ion source, or said ion receiver so as to be elongated with a width above one advance Z.sub.R per ion mirror reflection; and (e) displacing or steering at least a portion of said mean ion trajectory in the Y-direction so as to form periodic ion trajectory oscillations in the X-Y plane so as to bypass said ion source or said ion receiver for at least one ion mirror reflection.

(19) An important feature of the embodiments of the present invention is to cause the ions to bypass the ion source 13 and/or ion detector 14 by causing the ions to periodically oscillate within the analyzer in the X-Y plane together with ion drift in the X-Z plane under a relatively small ion injection angle . This will be described in more detail below.

(20) FIGS. 3A and 3B illustrate the ion trajectories in the X-Y plane 31 of the analyser for four reflections between the ion mirrors. In these embodiments the ion source 33 and the ion detector 34 are displaced from the central axis of the device in the +Y direction by a distance Y.sub.0. FIG. 3A illustrates the ion trajectory during a first of the ion reflections (I), in which the ions are pulsed from the ion source 33 into the upper ion mirror and are then reflected back to the central axis of the device. FIG. 3A also illustrates the ion trajectory during the second of the ion reflections (II), in which the ions continue to travel from the central axis of the device into the lower ion mirror and are then reflected back to the central Y-Z plane at a location that is displaced from the central axis in the Y direction by a distance Y.sub.0. FIG. 3B illustrates the ion trajectory during a third of the ion reflections (III), in which the ions continue to travel back into the upper ion mirror and are then reflected back to the central Y-Z plane at a location on the central axis. FIG. 3B also illustrates the ion trajectory during a fourth of the ion reflections (IV), in which the ions continue to travel from the central axis of the device into the lower ion mirror and are then reflected back to the central Y-Z plane at a location that is displaced from the central axis in the +Y direction by a distance Y.sub.0, at which point the ions impact on the detector 34.

(21) The mean ion trajectories are modeled for a distance between ion mirror reflections (or distance between mirror caps) of C=1 m and for a displacement Y.sub.0=5 mm. In order to more clearly illustrate the embodiments, the ion trajectories in the Y-direction have been exaggerated. As shown in FIG. 3A, the first segment (I) of the mean ion trajectory starts at middle plane X=0, at a Y-displacement of Y.sub.0=5 mm, and the ions initially travel parallel to the X-axis (i.e. angle =0). The ions then travel into the upper ion mirror, which causes the ions to oscillate in the Y-direction. After one mirror reflection, the ions returns to the central axis (X=0; Y=0), though at an angle of =7 mrad. The second segment (II) of the mean ion trajectory continues, and after the mirror reflection returns to the X=0 plane at a Y displacement of 5 mm and parallel to the X-axis (=0). As shown in FIG. 3B, the third segment (III) of the mean ion trajectory continues and after the mirror reflection the ions return to the central axis (X=0; Y=0) at an angle =7 mrad. The fourth segment (IV) of the mean ion trajectory continues and after the mirror reflection the ions returns to the original point in the X-Y plane (i.e. Y=5 mm, =0), thus closing the trajectory loop after four mirror reflections. It will however, be appreciated that the ions continue to move in the Z-direction during the four oscillations.

(22) The analyzer electrostatic field is assumed to be optimized for minimal time per spatial aberrations as described below, so that the repetitive trajectory loop stays at minor spatial diffusion of ion packets for multiple oscillations.

(23) Again referring to FIGS. 3A and 3B, the ion trajectories oscillate in the Y-direction and do not return to their initial Y-direction displacement until every fourth ion mirror reflection. As the ion source 33 is located in the initial Y-direction position, this ensures that it is not possible for the ions to impact on the ion source 33 for the first three out of every four reflections (provided that the ion source and ion packet maintain a moderate width in the Y-direction as compared to the initial Y.sub.0 displacement of the ions). This means that the ions are able to drift along the device in the Z-direction for three out of four reflections without being at a Y-location in which they could impact on the ion source 33. As such, this enables the length of the ion source to be extended in the Z-direction without interfering with the ion trajectories during the first three reflections. The length of the ion source 33 can be extended up to a length of 4Z.sub.R, i.e. four advances per mirror reflection, thus increasing the number of ions that may be injected between the mirrors and enhancing the duty cycle of the instrument. The elongation of ion packets in the Z-direction at the source 33 makes the instrument less sensitive to ion packet spreading in the Z-direction between the source 33 and the detector 34, since such spreading becomes smaller or more comparable to the initial Z-size of ion packet. Ion packet elongation also reduces space-charge effects in the analyzer. It also allows the use of a larger area detector 34, thus extending the dynamic range and lifetime of the detector 34.

(24) Alternatively, rather than the Y-oscillations being used to enable an increase in the ion source length, the Y-oscillations can be used to decrease the distance Z.sub.R that the ions travel per ion mirror reflection whilst preventing the ions from colliding with the ion source 33, thereby reducing the size of the instrument in the Z-direction.

(25) Although the technique of oscillating ions in the Y-direction has been described as being used for preventing the ions from impacting the ion source 33 during the ion reflections, the technique can alternatively, or additionally, be used for preventing ions from impacting on the detector until the desired number of ion mirror reflections (in the X-direction) have been achieved.

(26) Note that different ion mirror fields and ion injection schemes for injecting ions between the mirrors may be employed to form different patterns of looped X-Y oscillations, e.g., an oval trajectory or a pattern with a yet larger number of mirror reflections per full ion path loop may be used. Also, Y-oscillations may be induced by ion packet angular steering.

(27) FIGS. 4A-4C show three different views of an embodiment of a MR-TOF-MS instrument according to the present invention. FIG. 4A shows a view of the embodiment in the X-Y plane, FIG. 4B shows a perspective view, and FIG. 4C shows a view in the Y-Z plane. The embodiment 41 is a planar MR-TOF instrument comprising two parallel gridless ion mirrors 42, an ion source 43 (e.g., a pulsed ion source or orthogonal ion accelerator), an ion receiver 44 (e.g., detector), optional stops 48, and an optional lens 49 for spatially focusing ions in the Z-direction. The ion mirrors 42 are substantially extended in the drift Z-direction, thus forming two dimensional electrostatic fields in the X-Y plane at sufficient distance (about twice the Y-height of the ion mirror window) from the Z-edges of ion mirror electrodes. The ion source 43 and the ion detector 44 are arranged on opposite lateral sides of the middle X-Z plane 46 through the analyser, with each of the ion source 43 and detector 44 being displaced a distance Y.sub.0 from the analyzer middle X-Z plane 46. In this embodiment, both the ion source 43 and ion detector 44 are relatively narrow in the Y-direction. For clarity, it is assumed that the half width (W/2) of each of the ion source 43 and of the detector 44 is less than the Y.sub.0 displacement, that the ion source 43 is symmetric in the Y-direction, and that it emits ion packets from its centre.

(28) An important feature of the embodiments of the present invention is that the ion trajectories 45 are displaced in the Y-direction such that they bypass the ion source 43 as they travel along the Z-direction. As shown in FIG. 4A, the off-axis mean ion trajectory 45 starts at a displacement in the Y-direction of Y.sub.0 and proceeds in the manner described with reference to FIGS. 3A and 3B. FIG. 4A shows the ion trajectory as dashed lines for two mirror reflections, although more than two ion mirror reflections may be performed before the ions arrive at the detector, as will be described with reference to FIGS. 4B and 4C.

(29) All views demonstrate how ion trajectory 45 oscillates in the X-Y plane with a period corresponding to four mirror reflections. The trajectory 45 bypasses the ion source 43 for three ion mirror reflections and returns to the same positive Y-displacement after four reflections.

(30) As shown in FIG. 4B, the ions are pulsed from the ion source 43 with a trajectory 45 that is arranged at an inclination angle to the X-axis. Each ion packet thus advances a distance Z.sub.R in the Z-direction for every ion mirror reflection. The positions of the ion packet at different times is represented by different groups of white circles 47. It can be seen that the ion packet starts at the ion source 43 and is reflected by the upper ion mirror 42 such that when the ion packet arrives at the middle Y-Z plane the ions are not displaced in the Y-direction. The ion packet then continues into the lower ion mirror 42 and is reflected such that when the ion packet arrives at the middle Y-Z plane the ions are displaced to a position Y.sub.0 in the Y-direction. The ion packet then continues into the upper ion mirror 42 for a second time and is reflected such that when the ion packet arrives at the middle Y-Z plane the ions are not displaced in the Y-direction. The ion packet then continues into the lower ion mirror 42 for a second time and is reflected such that when the ion packet arrives at the middle Y-Z plane the ions are displaced to a position Y.sub.0 in the Y-direction. At this stage, the ion packet has performed four reflections in the ion mirrors and the ion packet has the same Y-displacement that it originally had at the ion source 43.

(31) The ion packet then continues into the upper ion mirror 42 for a third time and is reflected such that when the ion packet arrives at the middle Y-Z plane the ions are not displaced in the Y-direction. The ion packet then continues into the lower ion mirror 42 for a third time and is reflected such that when the ion packet arrives at the middle Y-Z plane the ions are displaced to a position Y.sub.0 in the Y-direction. The ion packet then continues into the upper ion mirror 42 for a fourth time and is reflected such that when the ion packet arrives at the middle Y-Z plane the ions are not displaced in the Y-direction. The ion packet then continues into the lower ion mirror 42 for a fourth time and is reflected such that when the ion packet arrives at the middle Y-Z plane the ions are displaced to a position Y.sub.0 in the Y-direction. The ion packet then continues into the upper ion mirror 42 for a fifth time and is reflected such that when the ion packet arrives at the middle Y-Z plane the ions are not displaced in the Y-direction. The ion packet then continues into the lower ion mirror 42 for a fifth time and is reflected such that when the ion packet arrives at the middle Y-Z plane the ions are displaced to a position Y.sub.0 in the Y-direction, at which they impact on the detector 44.

(32) As described above, FIG. 4C shows a view of the embodiment in the Y-Z plane. The positions of the ion packets at different times that are illustrated by the white circles in FIG. 4B are also shown in FIG. 4C. As shown in FIG. 4C, the ion displacement in the Z-direction after each reflection in the ion mirror is Z.sub.R. It can be seen that after the first ion mirror reflection the ion packet has only traveled a distance Z.sub.R is the Z-direction, which is smaller than the length of the ion source 43 in the Z-direction. If the ions had not been displaced in the Y-direction relative to their initial position, then after the first ion mirror reflection the trailing portion (in the Z-direction) of the ion packet would have impacted on the ion source 43. However, as the ions have been moved in the Y-direction relative to their initial position at the ion source 43, they are able to bypass the ion source 43 and continue through the device. The second and third ion reflections also cause the ion packet to have Y-direction positions such that it is impossible for them to impact on the detector. It is only after the fourth ion mirror reflection that the ion packet has returned to its original Y-direction position, i.e. that of the ion source 43. However, at this stage, the ions have traveled a distance 4Z.sub.R in the Z-direction, at which point the ion packet has traveled sufficiently far in the Z-direction that it is impossible for the ions to impact on the ion source 43.

(33) This technique allows for a relationship wherein the length in the Z-direction of the ions source 43 (i.e. a length in the Z-direction of the initial ion packet 47) may be up to approximately 4Z.sub.R without ions hitting the ion source 43 as they travel through the device. Oscillating the ion packets in the Y-direction therefore allows the length of the ion source 43 in the Z-direction to be increased, or the Z-distance traveled by the ions after each reflection Z.sub.R to be decreased, relative to arrangements wherein the ions are not oscillated in the Y-direction. Increasing the length of the ion source 43 or decreasing the length Z.sub.R have the advantages described above.

(34) In a similar manner to that described above, the ion packets 47 may be made to bypass the narrow ion detector 44 for three reflections out of every four. In other words, the detector 44 may be located in the Y-direction such that it is impossible for the ions to impact the detector 44 for three out of four reflections due to the locations of the ions in the Y-direction. This allows the length of the detector 44 in the Z-direction to be increased relative to an arrangement in which ions are not oscillated in the Y-direction.

(35) The ion packet may expand in the Z-direction as it travels through the device, due to its initial angular divergence and inaccuracies in the electric fields. In order to avoid this causing spectral confusion, stops 48 may be provided for blocking the passage of ions that are arranged at the Z-direction edges of the ion packet as it travels through the device. Any ions in the ion packet that diverge in the Z-direction by an undesirable amount may therefore impact on the stops 48 and hence be blocked by the stops 48 and prevented from reaching the detector 44.

(36) It is of importance to note that ion packet expansion in the Z-direction is less critical as compared to in the prior art planar MR-TOF-MS instrument 11 shown in FIG. 1. In the prior art MR-TOF-MS instrument 11, both ion packet width Z.sub.S and packet Z-expansion dZ must be far shorter than the distance traveled in the Z-direction during each reflection Z.sub.R. In contrast, the embodiments of the present invention 41 allows the use of a much longer ion source 43 and detector 44, with the length of the ion source Z.sub.S and the length of the detector Z.sub.D being up to approximately 4Z.sub.R. As such, it is relatively easy to maintain the ion packet expansion dZ relatively short as compared to the ion source and detector length (dZ<Z.sub.SZ.sub.D<4Z.sub.R). Ion losses on ion stops 48 may therefore be kept moderate.

(37) Optionally, at least one of the ion stops 48 may be used as an auxiliary ion detector, for example, to sense the overall intensity of ion packets travelling through the device. This may be used, for example, to adjust the gain of main detector 44, For example, the ion signal from the auxiliary detector may be fed into a control system that controls the gain level of the main detector 44 based on the magnitude of the ion signal. If the ion signal from the auxiliary detector is relatively low then the control system sets the gain of the main detector 44 to be relatively high, and vice versa. Alternatively, the ion signal from the auxiliary detector may be fed into a control system that controls the angle of injection of the ions into the space between the mirrors, or controls a steering system that alters the ion trajectory of ions as they travel between the mirrors. For example, this may be achieved by the control system controlling the magnitude of a voltage applied to an electrode based on the ion signal from the auxiliary detector. These latter methods change the trajectories of ions moving between the mirrors and the control system may use the feedback from the auxiliary detector to ensure that the ion trajectories are along the desired trajectories. For example, the control system may control the ion trajectories until the auxiliary ion detector outputs its minimum ion signal, indicating that most ions are being transmitted between the mirrors, rather than impacting on the auxiliary detector.

(38) Assuming that the ion packet undergoes 16 ion mirror reflections, has an expansion in the Z-direction dZ of 30 mm by the time it reaches the detector 44, that Z.sub.R is 20 mm and that Z.sub.S=Z.sub.D=60 mm; then the MR-TOF-instrument of this embodiment would have a length in the Z-direction of just Z.sub.A=320 mm, and an ion loss on stops 48 of only 20% (as seen in FIG. 4D). This is to be compared with the corresponding prior art example described above in relation to FIG. 1, which had a length in the Z-direction of Z.sub.A=800 mm.

(39) Thus, arranging the ions to oscillate in the Y-direction allows the ion packets to bypass the ion source 43 and ion detector 44 for a number of ion reflections and hence allows extension of the ion packets, ion source 43 and ion detector 44 in the drift Z-direction.

(40) In the particular example of the ion mirror field described above, the Y-direction oscillation loop closes in four ion mirror reflections. However, it is contemplated that the Y-direction oscillation loop may close in a fewer or greater number of ion mirror reflections.

(41) The techniques of the embodiments described above provide multiple improvements as compared to the prior-art planar MR-TOF-MS instrument 11. For example, the embodiments provides a notable reduction (at least two-fold) in the analyzer Z-direction length. This enables the ion path length of 16 m that is required for a resolution R200,000 to be provided in an instrument that is of practical size. The embodiments provide a significant ion source elongation (5-10 fold), thus improving the duty cycle of pulsed ion converters, which are estimated below as 5-20%, depending on the converter type. The embodiments enable ion packets to be elongated in the Z-direction to 30-100 mm, which extends the space-charge limit of the analyzer. The embodiments enable the detector to be elongated to 30-100 mm, which extends the dynamic range and life time of the detector.

(42) The method of oscillating ions in the X-Y plane brings a concern that a Y-direction displacement of the ions could cause either spatial or time of flight spreading of the ion packets, which may limit the resolution of analyzers having high order aberrations. This concern is addressed in the accompanying simulations, showing that analyzer geometries are capable of operating with Y-axis oscillations for realistic ion packets.

(43) FIG. 5A shows the geometry of a planar MR-TOF-MS instrument 51 according to an embodiment of the present invention in the X-Z plane, and 5B shows one of the ion mirrors of this embodiment in the X-Y plane and the various voltages and dimensions that may be applied to the components of the instrument. In the embodiment modeled, the axial distribution of electrostatic potentials in the ion mirror 52 provides for a mean ion kinetic energy in the drift space between the mirrors of 6 keV. The mirrors have four independently tuned electrodes; three of them (the cap and two neighboring electrodes) may be set to retarding voltages and another (the longest in FIG. 5B) to an accelerating voltage. The total cap to cap distance C between opposing ion mirrors is about 1 m and the Y-height of the window within each mirror may be 39 mm. The ion injection angle in the X-Z plane is set to 20 mrad, the initial Y-displacement of the ion trajectories is Y.sub.0=5 mm, and the detector is arranged at a Y-displacement of Y.sub.0=5 mm.

(44) FIG. 5A shows light and dark simulated ion trajectories. The light ion trajectories represent the ions emitted from the rear of the ion source (in the Z-direction), whereas the dark ion trajectories represent the ions emitted from the front of the ion source (in the Z-direction). The technique of oscillating the ions in the Y-direction allows both the ion source and ion detector to have a length of around 50 mm in the Z-direction (e.g., a source length of 50 mm and a detector length of 56 mm). As the ion source has a length in the Z-direction of 50 mm, the light and dark simulated trajectories are offset by almost 50 mm in the Z-direction. The total average distance traveled in the Z-direction during the 16 ion mirror reflections until the ions hit the detector is Z.sub.A=280 mm. Accounting for Z-fringing fields of planar ion mirrors, this provides that the overall ion mirror length in the Z-direction needs to be approximately 420 mm, which is reasonable for commercial instrumentation.

(45) FIGS. 5C-5E show projections in the X-Y plane of example ion trajectories in the analyzer (the Y-scale is exaggerated) that are optimized for reducing flight time aberrations with respect to the spatial and energy spreads.

(46) FIG. 5C shows ion trajectories with different ion energies. The ion mirrors may be tuned so as to eliminate the spatial energy dispersion in the middle of the analyzer after each reflection and thus to provide spatial achromaticity (i.e. the absence of coordinate and angular energy dispersion) after each two reflections. According to the general ion-optical theory (M. Yavor, Optics of Charged Particle Analyzers, Acad. Press, Amsterdam, 2009) such tuning provides for a first order isochronous ion transport with respect to spatial ion spread (i.e. dT/dY=dT/dB=0, where B=dY/dX is the inclination of ion trajectory).

(47) FIG. 5D shows ion trajectories with different initial Y-coordinates. The ion mirrors may be tuned so as to provide a parallel-to-point focusing of the ion trajectories in the middle of the analyzer after one reflection, and consequently parallel-to-parallel focusing after each two reflections.

(48) FIG. 5E shows ion trajectories with different initial B-angles of ion trajectories. The ion mirrors may be tuned so as to provide a point-to-parallel focusing of ion trajectories in the middle of the analyzer after one reflection, and consequently point-to-point focusing after each two reflections and the unity transformation after each four reflections. Overall, after each four reflections the spatial phase space of the ion packet experiences the unity transformation. According to the general ion-optical theory (D. C. Carey, Nucl. Instrum. Meth., v. 189 (1981) p. 365), tuning of the ion mirrors to satisfy only one additional condition d.sup.2Y/dBdK=0, where K is the ion kinetic energy, leads to elimination of all second order flight time aberrations due to spatial (coordinate and angular) variations as well as to mixed spatial and energy variations after 16, 20, 24 . . . etc. reflections. The remaining dependence of the flight time with respect to the energy spread can be eliminated to at least the third aberration order (dT/dK=d.sup.2 T/dK.sup.2=d.sup.3 T/dK.sup.3=0) by a proper choice of electrode lengths and cap-to-cap distance.

(49) FIGS. 6A-6C show results of ion optical simulations for the analyzer shown in FIGS. 5A-5B, for the case of the ion packets produced by a 50 mm long orthogonal accelerator with an accelerating field of 300 V/mm from a continuous ion beam of 1.4 mm diameter with an angular divergence of 1.2 degrees and a beam energy of 18 eV. The resultant ion peak time width at the detector together with the time-energy diagram is shown and is characterized by a FWHM of 1.1 ns at a flight time of about 488 s for ion masses of 1000 a.m.u., i.e. to mass resolving power of 224,000.

(50) It should be understood that other numerical compromises can be used for improved resolution at smaller Y displacements or somewhat compromised resolution for larger Y displacement when meeting challenges at making narrow ion source or narrow detector.

(51) Since MR-TOF-instrument aberrations generally grow with the amplitude of the Y-displacement of the ions during the oscillations, it is desirable to minimize the trajectory Y-offset Y.sub.0. On the other hand, the minimal Y-offset should still be sufficient for differentiating axial trajectories and Y-displaced ion trajectories, defined by ion packet Y-width and Y-divergence. Besides, the minimal Y-offset has to be sufficient to bypass the ion source and/or detector during at least some of the oscillations (e.g., three Y-direction oscillations). In other words, depending on the ion injection scheme, the minimal Y-offset may depend on the physical width of the ion source and/or of the detector. In order to maintain a moderate Y-displacement of the ion packets while bypassing ion packets around the ion source, a number of methods may be used according to the present invention. For example, the ion source may be narrow, e.g., the ion source may be an orthogonal accelerator (OA) having a DC accelerator formed by resistive boards. Alternatively, the ion packets may be injected via a curved isochronous sector interface having a curvature in the X-Y plane. Alternatively, or additionally, there may be employed a pulsed deflector that deflects ions in the Y-direction so as to reduce the displacement of the ion packet compared to half the width of the orthogonal accelerator.

(52) In order to avoid the detector interfering with bypassing ion trajectories the detector may comprise an ion to electron converter, which may have a smaller rim size than standard TOF detectors. The secondary electrons produced by the detector may be focused (for smaller spot in fast detectors) or defocused onto a detector (for longer detector life time) by either non-uniform magnetic or electrostatic fields.

(53) FIGS. 7A and 7B show an embodiment of an MR-TOF-MS instrument that is the same as that shown in FIGS. 4A-4D, except that isochronous electrostatic sectors 75 are used to inject and extract ions from the time of flight region. FIG. 7A shows a view in the X-Y plane and FIG. 7B shows a view in the Y-Z plane. The instrument 71 comprises a planar MR-TOF analyzer 72 comprising a relatively wide ion source 73 of width S arranged outside of the time of flight region, a relatively wide ion detector 74 of width D arranged outside of the time of flight region, and isochronous electrostatic sectors 75 of width W for interfacing the ion source 73 and ion detector 74 with the time of flight region. The curved ion trajectories 78 of the sectors 75 lie within the X-Y plane of the analyzer 72.

(54) In operation, packets of ions 76 are accelerated from the ion source 73 into the entrance sector 75. The entrance sector 75 transfers the ion packets 76 from the ion source 73 into the analyzer 72 along the curved ion trajectory 78 so as to arrange the ion trajectory 77 within the analyzer parallel to the Y-axis at a Y-displacement Y.sub.0 from X-Z middle plane. This arrangement enables the ions to be injected into the analyser 72 having a Y-displacement Y.sub.0 that is more easily controllable than the Y-displacement provided by arranging the ion source in the flight region of the analyser (e.g., as in FIGS. 4A-4B). For example, when using an ion source having a relatively wide width in the Y-direction, it may be difficult to arrange the ion source inside the flight region of the analyser such that the ions have the desired initial Y.sub.0 displacement and such that the ions do not impact on the ion source as they travel along the device. For example, in the embodiment shown in FIG. 4A-4B ions are emitted from the centre of the ion source (in the Y-direction) and so the initial displacement Y.sub.0 cannot be made smaller than the half width (in the Y-direction) of the ion source without the ions later impacting on the ion source. In contrast, it can be seen from FIGS. 7A-7B that the use of sectors 78 enable the initial displacement Y.sub.0 to be notably smaller than the half-width S/2 of the ion source and the half-width of the detector D/2.

(55) In order to avoid the ions impacting on the sectors 75, the half-width in the Y-direction (W/2) of each of the sectors is arranged to smaller than Y.sub.0.

(56) Isochronous properties of sector interfaces 75 have been described in WO 2006/102430, incorporated herein by reference. The use of the sector interfaces 75 decouple the amplitude of Y.sub.0 trajectory displacement from the physical width S and D of the ion source 73 or detector 74 at moderate time dispersion.

(57) FIG. 7B corresponds to FIG. 4C, except that the isochronous electrostatic sectors 75 are used to inject and extract ions from the time of flight region. FIG. 7B shows projections of the ion source 73, ion receiver 74 and of the curved sectors 75. Groups of circles 47 represent the different locations of an ion packet crossing Y-Z middle plane at different times. As described previously, the ion stops 48 may be provided to remove portions of the ion packets that diverge excessively. Also, as described previously, one or more of the stops 48 may be an auxiliary detector for optimizing ion beam transmission through the analyzer 72, or as an auxiliary detector for automatic gain adjustment of the main detector 74.

(58) FIGS. 8A-8B show an embodiment of an MR-TOF-MS instrument that is the same as that shown in FIGS. 4A-4D, except that ion deflectors are used to inject ions along the desired trajectory. FIG. 8A shows a view in the X-Y plane and FIG. 8B shows a view in the Y-Z plane.

(59) The instrument 81 comprises a planar MR-TOF analyzer 82 comprising a relatively wide ion source 83 of width S (S>2Y.sub.0), a relatively narrow detector 84 of width D (D<2Y.sub.0), a deflector 85 of width W.sub.1, and an optional deflector 88. As in the previous embodiments, it is desired to inject the ions so that they initially travel parallel to the X-axis at a displacement from the X-axis of Y.sub.0. As described previously, if the width of the source 83 in the Y-direction is greater than 2Y.sub.0 then the ions will impact on the ion source 83 as they travel through the device. The ion source 83 is therefore offset in the Y-direction so as to avoid interference with ion trajectory 87 after ion mirror reflections. Ions may then be directed from the ion source 83 towards the Y=0 plane and the deflector 85 may be used to deflect the ion trajectory so that the deflector 85 steers the ion packets along trajectory 87, parallel to the X-axis and at an offset of Y.sub.0.

(60) The ion ejection axis of the ion source 83 may be arranged to be parallel to the X-axis and an additional ion deflector 88 may be provided to steers the ion packets along trajectory 86 towards deflector 85, such that the Y-displacement of the ions becomes equal to Y.sub.0 at the center of the deflector 85. The deflector 85 then steers the packets along the trajectory 87. Alternatively, the ejection axis of the ion source 83 may be tilted in the X-Y plane so as to eject the ion packets along trajectory 89 towards deflector 85, such that the Y-displacement of the ions becomes equal to Y.sub.0 at the center of the deflector 85. The deflector 85 then steers the packets along the trajectory 87. Deflector 85 and/or 88 may be either a pulsed or static deflector.

(61) Multiple other arrangements of pulsed or static deflectors are viable to transfer ion packets along the displaced trajectory 87 while avoiding their interference with moderately wide ion sources having a Y-direction width S above 2Y.sub.0.

(62) FIG. 8C shows a view in the Y-Z plane of an alternative embodiment that is the same as that shown in FIGS. 8A-8B, except that deflector 85 is replaced with a deflector 90 having a width that is greater in the Y-direction. The deflector 90 has the same function as deflector 85, except that the width W.sub.2 of the deflector 90 is chosen to be above 2Y.sub.0, thereby providing an alternative way to avoid it interfering with ion trajectory 87 within the analyzer 82. In other words, the deflector comprises electrodes that oppose each other in the Y-direction, wherein the electrodes are arranged on opposing sides of the Y=0 plane, and wherein the distance of each electrode from the Y=0 plane is greater than Y.sub.0. The deflector 90 operates in a pulsed manner so as to avoid ion packet distortions after the first ion mirror reflection.

(63) FIGS. 9A-9B show an embodiment of an MR-TOF-MS instrument that is the same as that shown in FIGS. 4A-4D, except that the ions source may be a pulsed converter 93 that periodically pulses a continuous beam 92, or a pulsed ion beam, into the ion mirrors. For example, the pulsed converter 93 may be an orthogonal acceleration device. FIG. 9A shows a view in the X-Y plane and FIG. 9B shows a view in the Y-Z plane. As with the ion source in the previously described embodiment, the pulsed converter 93 may be oriented substantially along the drift Z-direction with a converter length Z.sub.S being extended up to 4*Z.sub.R. The converter 93 may be gridless and may have a terminating electrostatic lens for providing a low divergence of a few mrad in the Y-direction.

(64) Ion packets are produced by the pulsed converter 93 are injected into the time of flight region at a small inclination angle to the X-axis. It is desired to optimize the angle such that ion trajectories can be separated between groups of four reflections while maintaining a reasonable length of the analyzer in the Z-direction, e.g., Z.sub.A300-400 mm. The angle of ion trajectories 45 may be optimized to 20 mrad. The pulsed converter need not necessarily provide an optimal inclination angle of the ion trajectories and electrodes may be provides to steer the ion packets in order to achieve an optimal inclination angle 20 mrad.

(65) FIG. 9C shows a view in the X-Y plane and a view in the X-Z plane of a pulsed converter 93A comprising a radial ejecting ion trap used in a through mode. As shown in the X-Y view, the pulsed converter 93 comprises a pass-through rectilinear ion trap having top and bottom electrodes and side trap electrodes. A radiofrequency voltage signal is applied to the side trap electrodes in order to confine an ion beam 92. The ion beam is may be a relatively slow ion beam having an energy K.sub.Z=3-5 eV. Periodically, the RF signal is switched off and electrical voltage pulses are applied to the top and bottom electrodes so as to extract an ion packet through a slit in the top electrode. Each ion packet is accelerated within DC accelerating stage 94A to an energy of, for example, K.sub.X=5-10 keV. The ion packet has a natural inclination angle , defined as =sqrt(K.sub.Z/K.sub.X, that is close to the desired inclination angle 20 mrad within the MRTOF analyzer.

(66) As the ion beam 92 has a reduced energy (compared to orthogonal acceleration), the pulsed converter 93A provides an improved duty cycle, but additional ion losses on stops 48 may occur due to the ion packet expanding in the Z-direction. A numerical example will now be described. Let us assume that the continuous ion beam 92 has an average ion energy K.sub.Z=5 eV, the energy spread in the Z-direction is K.sub.Z=1 eV, and the length of the rectilinear trap Zs=80 mm (using notation as FIG. 4). Let us also assume that the MR-TOF analyzer has an acceleration energy K.sub.X=8000 eV and that 16 ion mirror reflections are performed before the ions are detected. In this case, the average inclination angle is =sqrt(K.sub.Z/K.sub.X)=25 mrad, and the ion packet advance per ion mirror reflection is Z.sub.R=25 mm at a cap to cap spacing of 1 m. The inclination angle spread is =*K.sub.Z/2K.sub.Z=2.5 mrad. After 16 ion mirror reflections the ion packet will drift in the Z-direction by a distance of Z.sub.A=16 C*sin =400 mm (using notation of FIG. 1) and will expand in the Z-direction by dZ=16 C*=40 mm (using notation of FIG. 1). The accelerator length Z.sub.S=80 mm (chosen to stay shorter than 4Z.sub.R) provides 20% duty cycle, while transmission TR through stops 48 is TR=0.8, as illustrated in the geometrical example 50 of FIG. 4D. Thus, the overall effective duty cycle is 16%. The trap 93A is an almost ideal converter, except that switching of the RF fields may present some problems with mass accuracy in the MR-TOF spectra.

(67) FIG. 9D shows a view in the X-Y plane and a view in the X-Z plane of a pulsed converter 93B comprising a radial ejecting ion trap used in an accumulating mode. As shown in the X-Y view, the pulsed converter 93 comprises a pass-through rectilinear ion trap having top and bottom electrodes and side trap electrodes. A radiofrequency voltage signal is applied to the side trap electrodes in order to confine a pulse injected ion beam 96 in radial directions. The trap comprises several segments of RF trap (not shown in the schematic view) and voltages are applied to these segments so as to provide a DC well of 1V in the Z-direction of the trap. The injected ions are trapped and dampened in gas collisions, for time T and at gas pressure P, wherein the product of P*T may be approximately 3-5 ms*mTor. Typical pressures P may be 2-3 mTor and typical times T may be 1-2 ms. Periodically, the RF signal is switched off and electrical pulses are applied to the top and bottom electrodes so as to extract ion packets through the slit in the top electrode. The ion packets may be accelerated within a DC accelerating stage 94A to an energy of K.sub.X=5-10 keV, at a natural inclination angle of zero. In order to arrange for the angle 20 mrad without notable time aberrations, the trap and DC accelerator 94B are tilted to an angle /210 mard from the Z-direction and a segmented deflector 95B (arranged in multiple segments for a uniform deflection field at small Y-width of the deflector) is used to deflect ion packets at an angle of /210 mrad.

(68) The product of the trap 93B length Z.sub.S and steering angle /2 should be under 500 mm*mrad to maintain the T|ZK time aberration under a FWHM of 1 ns at a relative energy spread of ion packets matching the energy tolerance of the MRTOF analyzer K.sub.X/K.sub.X=6%. Thus, the trap length Z.sub.S may be kept at 50 mm at an angle /2=10 mrad.

(69) Although the accumulating trap converter provides unity duty cycle, the trap may rapidly overfill as an ion cloud of 1E+6 ions may be accumulated during a 1 ms accumulation period when using realistic modern ion sources, which have a productivity of 1E+9 to 1E+10 ions per second. This problem may be partially solved by using controlled or alternating ion injection times. The elongated ion trap 93B having a length Z.sub.S50 mm still provides a much larger space-charge capacity than prior art axial ejecting traps that have a characteristic ion cloud size of 1 mm.

(70) FIG. 9E shows a pulsed converter 93C comprising a conventional orthogonal accelerator with DC accelerating stage 94C aligned with the Z-axis and a multi-deflector 95C. The multi-deflector 95C comprises multiple deflection cells formed of thin (e.g., under 0.1 mm) and close lying deflection plates, optionally arranged on double sided printed circuit boards. Optionally, the Z-width of each deflection cell is about Z.sub.C=1 mm. The orthogonal acceleration operation is known to be stable at ion beam 92 energies above 15 to 20 eV. The ion beam 92 may be set to have an energy of K.sub.Z=20 eV, producing ion packets having an inclination angle 50 mrad for K.sub.X=8 keV. In order to arrange sixteen ion mirror reflections within a reasonable analyzer length in the Z-direction of up to 400 mm, the inclination angle is reduced to approximately 20 mrad. The multi-deflector 95C alters the angle of the ion packets by =30 mrad angle. At a cell width of Z.sub.C=1 mm, the time fronts are tilted for an angle of which expands the ion packets in the X-direction to X=Z.sub.C*sin() 30 m. At a flight path length of 16 m, the steering step imposes a limit of R<L/2X250,000 onto base peak mass resolution, i.e. approximately 500,000 resolution at FWHM. Thus, steering in a 1 mm cell multi-deflector is still able to obtain an overall resolving power of R200,000. The overall duty cycle is estimated as 5-7%, depending on the accelerator length (accelerator length is limited to Z.sub.S<60-70 mm for Z.sub.R=20 mm) and on geometrical transmission of the multi-deflector.

(71) FIG. 9F shows a pulsed converter 93D comprising a conventional orthogonal accelerator 94D tilted at angle 30 mrad to the Z-axis and a segmented deflector 95D. Several segments of the deflector 95D are arranged to provide a uniform deflection field at moderate Y-width of the deflector. A safe ion beam energy is chosen to be about 15-20 eV, resulting in a natural inclination angle of 50 mrad. The deflector steering angle = is adjusted to equal to the tilting angle of the orthogonal accelerator in order to compensate for the first order time front inclinations (mutual compensation of tilting and steering time aberrations). The next notable time aberration T|ZK.sub.X appears since the steering angle depends on ion packet energy K.sub.X. However, the second order aberration still allows a product of z.sub.S* up to 500 mm*mrad for a relative energy spread of the ion packet of K.sub.X/K.sub.X=6% for keeping the FWHM of additional time spread under 1 ns, i.e. limits the resolution to R200,000 at an orthogonal accelerator length up to 20-30 mm. The overall duty cycle is estimated to be 3-5%, which is still about 10 times better than in the prior art MR-TOF instruments.

(72) FIG. 10 a view in the Y-Z plane of an embodiment that is the same as that shown in FIG. 4C, except wherein the detector 44 is arranged so that the ions impact on the detector 44 after only four ion mirror reflections. This arrangement provides a relatively high duty cycle with a moderate resolution. By way of example, the cap to cap spacing in this arrangement may be C=1 m and the effective flight path may be 4 m (which is 1.6 times greater than in the current Q-TOF of Xevo XS). If the ion beam has a physical extent in the pusher, in the direction of push, of 1.2-1.4 mm, and the gradient in the pusher is 300 V/mm, then the energy spread k seen by the ions is approximately 420 eV for singly charged ions. The energy acceptance of such a device is given by k/k, where k is the acceleration voltage (e.g., 6000 V). This gives an energy acceptance of 6-7% whilst maintaining RA=100 K. Accordingly, a 1.2-1.4 mm beam may be used with a pusher gradient of 300 V/mm.

(73) The present invention allows significant elongation of the ion accelerator in the Z-direction, for example, to 30-80 mm as compared to a length of 5-6 mm in prior art MR-TOF-MS instruments. The present invention therefore substantially improves the mass range and sensitivity the instruments with orthogonal accelerators.

(74) Although the present invention has been described with reference to various embodiments, it will be understood by those skilled in the art that various changes in form and detail may be made without departing from the scope of the invention as set forth in the accompanying claims.