Time-of-flight mass spectrometer
11101127 · 2021-08-24
Assignee
Inventors
Cpc classification
H01J49/022
ELECTRICITY
H01J49/401
ELECTRICITY
International classification
Abstract
An acceleration voltage generator (7) generates a high-voltage pulse to be applied to an electrode in an orthogonal accelerator by turning on/off a high DC voltage generated by a high-voltage power source through MOSFETs (741) in a switch circuit (74). A controller (6) sends driving pulse signals to the switch circuit (74) through a primary-side driver section (71), transformer (72) and secondary driver section (73). An adjustment circuit (742) formed by a gate resistor (742a) and gate capacitor (742b) is provided between the secondary-side driver section (73) and the MOSFET (741). The resistance value of the resistor (742a) and the capacitance value of the capacitor (742b) are determined so as to suppress an overshoot of the gate voltage due to the resonance while preventing a decrease in steepness of the waveform in its rising and falling phases.
Claims
1. A time-of-flight mass spectrometer including an ion ejector configured to eject a measurement-target ion into a flight space by imparting acceleration energy by an effect of an electric field created by a voltage applied to an electrode, and a high-voltage pulse generator configured to apply a high-voltage pulse for ion ejection to the electrode, wherein: the high-voltage pulse generator includes: a) a DC power source configured to generate a high DC voltage; b) a switch circuit configured to generate the high-voltage pulse by switching the high DC voltage generated by the DC power source, and to output the high-voltage pulse to a voltage-output end, the switch circuit including one or more plus-side switching elements and one or more minus-side switching elements connected in series, where each of the plus-side switching elements is configured to output a plus-side voltage generated by the DC power source to the voltage-output end when in an ON state, and each of the minus-side switching elements is configured to output a minus-side voltage generated by the DC power source to the voltage-output end when in an ON state; c) a switching element driver configured to turn on/off the switching elements according to a pulse signal for ejecting ions, the switching element driver including a first switching element driver configured to respond to a first pulse signal and electrically charge a control terminal to a voltage which turns on the plus-side switching element or a voltage which maintains the plus-side switching element in the ON state, as well as a second switching element driver configured to respond to a second pulse signal and electrically charge the control terminal to a voltage which turns on the minus-side switching element or a voltage which maintains the minus-side switching element in the ON state; d) an adjustment circuit including a resistor inserted in series with the control terminal on a signal path extending from the switching element driver to the control terminal, the adjustment circuit configured to make the voltage at the control terminal be a voltage having a predetermined transient characteristic; and e) a controller configured to generate the first pulse signal and the second pulse signal in addition to the pulse signal for starting the output of the high-voltage pulse, so as to recharge the control terminal of the plus-side switching element or the minus-side switching element which is in the ON state.
2. The time-of-flight mass spectrometer according to claim 1, wherein: the time-of-flight mass spectrometer is a device configured to repeatedly perform, with a predetermined measurement period, a measurement in which ions are ejected from the ion ejector and detected after being made to fly in a flight space, and in which the measurement period is variable.
3. The time-of-flight mass spectrometer according to claim 2, wherein: a resistance value of the resistor in the adjustment circuit is determined so as to substantially satisfy critical damping conditions.
4. The time-of-flight mass spectrometer according to claim 2, wherein: the controller is configured to generate the second pulse signal for recharging and thereby recharge the control terminal of the minus-side switching element a specific length of time earlier than the point in time of the generation of the pulse signal for starting the output of the high-voltage pulse, when starting the output of the high-voltage pulse of the plus-side voltage, as well as generate the first pulse signal for recharging and thereby recharge the control terminal of the plus-side switching element a specific length of time earlier than the point in time of the generation of the pulse signal for starting the output of the high-voltage pulse, when starting the output of the high-voltage pulse of the minus-side voltage.
5. The time-of-flight mass spectrometer according to claim 2, wherein: a plurality of measurement periods are set to be substantially equal to integer multiples of a shortest ion ejection period, and a resistance value of the resistor in the adjustment circuit is determined according to the shortest ion ejection period and a control-terminal-recharging period with which the controller repeatedly sends the pulse signal for recharging.
6. The time-of-flight mass spectrometer according to claim 5, wherein: the control-terminal-recharging period is shorter than the shortest ion ejection period, and the resistance value of the resistor in the adjustment circuit is determined so that a state of overdamping occurs.
7. The time-of-flight mass spectrometer according to claim 5, wherein: the control-terminal-recharging period is longer than the shortest ion ejection period, and the resistance value of the resistor in the adjustment circuit is determined so that a state of insufficient damping occurs.
Description
BRIEF DESCRIPTION OF DRAWINGS
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DESCRIPTION OF EMBODIMENTS
(21) An OA-TOFMS as one embodiment of the present invention is hereinafter described with reference to the attached drawings.
(22)
(23) In the OA-TOFMS according to the present embodiment, the acceleration voltage generator 7 includes a primary-side driver section 71, pulse transformer 72, secondary-side driver section 73, switch circuit 74, high-voltage power source 75, and primary-side power source 76. The controller 6 control the switching operation in the switch circuit 74 to control the primary-side driver section 71.
(24) As shown in
(25) The pulse transformer 72 is a ring-core transformer. One ring core is provided for the gate terminal of the MOSFET 741 in each stage of the switch circuit 74. The secondary winding 72b wound on each ring core is connected to the transformer load resistor 730 and the MOSFETs 731 and 732 in the secondary-side driver section 73. A single turn of cable passed through the ring core is used as the primary winding 72a. For this cable, a high-voltage insulated wire is used, which electrically insulates the primary side from the secondary side. The number of turns of the secondary winding may be appropriately determined.
(26) The primary-side driver section 71 includes a plurality of MOSFETs 711, 712 and 715-718, as well as a plurality of transformers 713 and 714. Pulse signals a and b are sent from the controller 6 to a plus-side pulse signal input end 771 and minus-side pulse signal input end 772, respectively. The term “plus-side” in the “plus-side pulse signal input end 771” means that an input of a high-level signal to this input end turns on the plus-side MOSFET 741 (or maintains it in the ON state), as in a circuit operation which will be described later. Similarly, the term “minus-side” in the “minus-side pulse signal input end 772” means that an input of a high-level signal to this input end turns on the minus-side MOSFET 741 (or maintains it in the ON state), as in a circuit operation will be described later.
(27) As shown in
(28) Thus, a predetermined voltage is induced between the two ends of each secondary winding 72b of the pulse transformer 72. The voltage applied to the gate terminal of each MOSFET 741 via the transformer load resistor 730, MOSFETs 731 and 732, and gate discharge resistor 733 in the secondary-side driver section 73 as well as an adjustment circuit 742 in the switch circuit 74 (this voltage is hereinafter called the “gate voltage”) can be approximately expressed by the following equation:
[Gate Voltage]≈{[Primary-Side Voltage of Pulse Transformer 72]/[Number of MOSFETs 741 Serially Connected in Switch Circuit 74]}×[Number of Turns of Secondary Winding of Pulse Transformer 72] (1)
(29) For example, if the primary-side voltage (VDD) of the pulse transformer 72 is 175 V, number of MOSFETs 741 connected in series in the switch circuit 74 is 12, and number of turns of the secondary winding of the pulse transformer 72 is one, a voltage which is approximately 174/12=14 V is applied to the gate terminal of each MOSFET 741.
(30) When the voltage is applied in the forward direction between the gate terminal and source terminal of the six plus-side MOSFETs 741 in the switch circuit 74, those MOSFETs 741 simultaneously turn on. Meanwhile, the voltage is also applied in the reverse direction between the gate terminal and source terminal of the six minus-side MOSFETs 741 in the switch circuit 74, those MOSFETs 741 turns off. As a result, the voltage-supply end +V from the high-voltage power source 75 is almost directly connected to the voltage-output end 79, and a voltage of +V=+2500V is outputted to the voltage-output end 79.
(31) At time t1, the pulse signal a inputted to the plus-side pulse signal input end 771 is changed to the low level (voltage zero). Then, the voltage between the two ends of each primary winding 72a in the pulse transformer 72 becomes zero. However, the gate voltage of the MOSFET 741 is roughly maintained at the same level by the electric charges already accumulated in the input capacitance of the gate terminal of the MOSFET 741, i.e. by the charging voltage for the gate terminal. The output voltage from the voltage-output end 79 is maintained at +V=+2500V. At a later point in time t2, the pulse signal b inputted to the minus-side pulse signal input end 772 is changed to the high level. This time, the MOSFET 712 turns on, which turns on the MOSFETs 717 and 718. A voltage is thereby applied between the two ends of the primary winding 72a in the pulse transformer 72 in the direction opposite to the previous direction, thereby producing an electric current flowing in the opposite direction. Consequently, a voltage is induced between the two ends of each secondary winding 72b of the pulse transformer 72 in the direction opposite to the previous direction, so that the six plus-side MOSFETs 741 in the switch circuit 74 turn off, while the six minus-side MOSFETs 741 turn on. Consequently, the output voltage from the voltage-output end 79 becomes zero (i.e. the value of −V).
(32) When the pulse signal b inputted to the minus-side pulse signal input end 772 is changed to the low level (voltage zero), the voltage between the two ends of the primary winding 72a of the pulse transformer 72 becomes zero. However, the gate voltage of the MOSFETs 741 is roughly maintained at the same level by the electric charges already accumulated in the input capacitance of the gate terminal of each of the six minus-side MOSFETs 741, i.e. by the charging voltage for the gate terminal. Consequently, the output voltage from the voltage-output end 79 is maintained at 0V.
(33) By the previously described basic operation, the acceleration voltage generator 7 generates a high-voltage pulse with a pulse peak value of +2500V at the timing corresponding to the pulse signals a and b inputted to the plus-side pulse signal input end 771 and minus-side pulse signal input end 772. As is evident from
(34) In advance of a description concerning how the adjustment circuit 742 located between the secondary-side driver section 73 and the gate terminals of the MOSFETs 741 functions in the previously described operation, a specific description will be hereinafter given concerning a problem which occurs if the adjustment circuit 742 is not present, i.e. a problem with the conventional circuit.
(35)
(36) In the secondary-side circuit of the pulse transformer 72, a resonance occurs in the LC circuit including the leakage inductance L of the pulse transformer 72 and the input capacitance C of the control terminal of the MOSFET 741. Therefore, an overshoot as shown in
(37) As noted earlier, the timing of the start of the output of the high-voltage pulse is determined by the timing at which the MOSFETs 741 in the switch circuit 74 turn on/off, i.e. the timing of the rise/fall of the gate voltage of those MOSFETs 741. For example, in the case of the waveform shown in
(38) In principle, the rising/falling waveform of the gate voltage should be unaffected by the measurement period of the repetitive measurement. However, when the ion ejection period is changed in order to change the measurement period, the phenomenon of a slight change in the rising/falling waveform of the gate voltage is observed.
(39) In the present example, the gate terminal of the MOSFET 741 is charged from ˜19.0V to a predetermined positive voltage when the measurement period is 125 μs, whereas the gate terminal is charged from ˜18.3V to the predetermined positive voltage when the measurement period is 500 μs. That is to say, the voltage at the point in time where the gate voltage begins to rise varies depending on the measurement period. This is due to the effect of the overshoot mentioned earlier. The measurement period is one order of magnitude shorter than the settling time of the overshoot, which is a few to several milliseconds. Accordingly, it is necessary to generate the high-voltage pulse for the next measurement while the voltage is gradually decreasing (toward the target voltage) after the overshoot as shown in
(40) Such a variation in the voltage at the point in time where the gate voltage begins to rise causes a shift of the point in time where the gate voltage reaches the threshold voltage, as shown in
(41)
(42) In the OA-TOFMS according to the present embodiment, the adjustment circuit 742 including the gate resistor 742a has the function of eliminating the temporal discrepancy of the output voltage waveform depending on a change in measurement period which occurs due to the previously described cause.
(43) As shown in
(44) As shown in
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(46) In general, the elements used in each stage of the secondary-side drive section 73 or switch circuit 74 are the same. Therefore, the gate voltages respectively applied to the gate terminals of the MOSFETs 741 in those stages are almost equal to each other. Accordingly, in normal cases, the resistance values of the gate resistors 742a in those stages may also be the same. The appropriate resistance value of those gate resistors 742a can be experimentally determined by the manufacturers who offer the present device.
(47) As just described, the timing discrepancy of the generation of the high-voltage pulse due to a change in measurement period can be sufficiently decreased by providing the adjustment circuit 742 having a simple configuration on the wiring connected to the gate terminal of the MOSFET 741 in each stage. In the OA-TOFMS according to the present embodiment, the timing discrepancy of the generation of the high-voltage pulse due to the change in measurement period can be even more reduced by additionally performing a control which will be hereinafter described.
(48) As shown in
(49)
(50) The temporal interval of the high-voltage pulse shown in
(51) In order to perform the previously described control, it is necessary to generate either the dummy-pulse signal b′ at the timing which is the specific period of time tc earlier than the point in time of the generation of the high-voltage pulse, or to initially generate the dummy-pulse signal b′ in response to a command for the execution of the measurement and subsequently generate the high-voltage pulse after the passage of the specific period of time tc. Therefore, the previously described control cannot be performed in the case where the generation of the high-voltage pulse and that of the dummy-pulse signal b′ are not synchronized with each other in the controller 6. In such a case, it is preferable to perform the following control.
(52)
(53) In this case, the plurality of ion ejection periods (measurement periods) are set to be equal to integer multiples of the shortest ion ejection period tp. For example, if the shortest ion ejection period tp is 125 μs, the ion ejection periods are set at 125 μs, 250 μs and 500 μs. On the other hand, the gate-charging period tgc, which is the period of the generation of the dummy pulse signal b′, is set to be slightly shorter or longer than the shortest ion ejection period tp. For example, if the shortest ion ejection period tp is 125 μs, the gate-charging period tgc is set at 105 μs or 150 μs.
(54) [Case 1] Shortest Ion Ejection Period tp>Gate-Charging Period tgc (
(55) That is to say, in the present embodiment, the gate voltage is given a predetermined transient characteristic as shown in
(56) It should be noted that a gate capacitor may be added as needed to control the decrease in charging voltage due to the natural electric discharge so that the gate voltage immediately before the generation of the high-voltage pulse will be even more consistently maintained.
(57) [Case 2] Shortest Ion Ejection Period Tp<Gate-Charging Period Tgc (
(58) For example, this is the case where the shortest ion ejection period tp is 125 μs and the gate-charging period tgc is 150 μs. Since the shortest ion ejection period tp<the gate-charging period tgc, the longer the measurement period is, the shorter the period of time becomes from the point in time of the last charging of the gate terminal to the point in time of the generation of the high-voltage pulse, as shown in
(59) That is to say, in the present embodiment, the gate voltage is given a predetermined transient response as shown in
(60) As with the previously described case, a gate capacitor may be added as needed to control the decrease in charging voltage due to the natural electric discharge so that the gate voltage immediately before the generation of the high-voltage pulse will be even more consistently maintained.
(61)
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(63) The descriptions thus far have been concerned with the case where the measurement-target ion is a positive ion. In the case where the measurement-target ion is a negative ion, the ion is ejected by applying a high-voltage pulse having a pulse peak value −V (e.g. −2500V) to the push-out electrode 11. It is evident that such a high-voltage pulse can be generated in the acceleration voltage generator 7 by setting +V=0 and −V=−2500V as well as appropriately changing the timing of the pulse signals a and b.
(64) It should be noted that the previously described embodiment is a mere example of the present invention, and any change, addition or modification appropriately made within the spirit of the present invention will naturally fall within the scope of claims of the present application.
(65) For example, as opposed to the previously described embodiment in which the present invention is applied in an OA-TOFMS, the present invention may also be applied in other types of TOFMS, such as an ion trap time-of-flight mass spectrometer in which ions held within a three-dimensional quadrupole type or linear type of ion trap are accelerated and sent into a flight space, or a time-of-flight mass spectrometer in which ions generated from a sample by a MALDI ion source or similar device are accelerated and sent into a flight space.
REFERENCE SIGNS LIST
(66) 1 . . . Ion Ejector 11 . . . Push-Out Electrode 12 . . . Extraction Electrode 2 . . . Flight Space 3 . . . Reflector 31 . . . Reflection Electrode 32 . . . Back Plate 4 . . . Detector 5 . . . Data Processor 6 . . . Controller 7 . . . Acceleration Voltage Generator 71 . . . Primary-Side Driver Section 711, 712, 715-718, 731, 732, 741 . . . MOSFET 713, 72 . . . Transformer 72a . . . Primary Winding 72b . . . Secondary Winding 73 . . . Secondary-Side Driver Section 730 . . . Transformer Load Resistor 733 . . . Gate Discharge Resistor 74 . . . Switch Circuit 742 . . . Adjustment Circuit 742a . . . Gate Resistor 742b . . . Gate Capacitor 75 . . . High-Voltage Power Source 76 . . . Primary-Side Power Source 771 . . . Plus-Side Pulse Signal Input End 772 . . . Minus-Side Pulse Signal Input End 79 . . . Voltage-Output End 8 . . . Reflection Voltage Generator