Abstract:
A mass spectrometer 1 includes a vacuum container 5 divided into a first chamber 51 containing an ion trap 3 and a second chamber 52 containing a time-of-flight mass spectrometer 4. The ion trap 3 is held within an ion-trap-holding space 610 surrounded by a wall 61. In this wall 61, a cooling-gas discharge port 64 is formed in addition to an introduction-side ion passage port 62 and an ejection-side ion passage port 63. A cooling gas supplied into an ion-capturing space 315 of the ion trap 3 is discharged from the ion-trap-holding space 610 through the three ports. The provision of the cooling-gas discharge port 64 reduces the amount of cooling gas flowing into the ejection-side ion passage port 63 and interfering with the ejection of ions from the ion trap 3 into the time-of-flight mass spectrometer 4. Consequently, the detection intensity of the ions is improved.
Abstract:
A method of introducing and ejecting ions from an ion entry/exit device (4) is disclosed. The ion entry/exit device (4) has at least two arrays of electrodes (20,22). The device is operated in a first mode wherein DC potentials are successively applied to successive electrodes of at least one of the electrode arrays ((20,22) in a first direction such that a potential barrier moves along the at least one array in the first direction and drives ions into and/or out of the device in the first direction. The device is also operated in a second mode, wherein DC potentials are successively applied to successive electrodes of at least one of the electrode arrays (20,22) in a second, different direction such that a potential barrier moves along the array in the second direction and drives ions into and/or out of the device in the second direction. The device provides a single, relatively simple device for manipulating ions in multiple directions. For example, the device may be used to load ions into or eject ions from an ion mobility separator in a first direction, and may then be used to cause ions to move through the ion mobility separator in the second direction so as to cause the ions to separate.
Abstract:
An electrostatic ion trap for mass analysis includes a first array of electrodes and a second array of electrodes, spaced from the first array of electrode. The first and second arrays of electrodes may be planar arrays formed by parallel strip electrodes or by concentric, circular or part-circular electrically conductive rings. The electrodes of the arrays are supplied with substantially the same pattern of voltage whereby the distribution of electrical potential in the space between the arrays is such as to reflect ions isochronously in a flight direction causing them to undergo periodic, oscillatory motion in the space, focused substantially mid-way between the arrays. Amplifier circuitry is used to detect image current having frequency components related to the mass-to-charge ratio of ions undergoing the periodic, oscillatory motion.
Abstract:
A system for expressing an ion path in a time-of-flight (TOF) mass spectrometer. The present invention uses two successive curved sectors, with the second one reversed, to form S-shaped configuration such that an output ion beam is parallel to an input ion beam, such that the ions makes two identical but opposed turns, and such that the geometry of the entire system folds into a very compact volume. Geometry of a TOF mass spectrometer system in accordance with embodiments of the present invention further includes straight drift regions positioned before and after the S-shaped configuration and, optionally, a short straight region positioned between the two curved sectors with total length equal to about the length of the central arc of both curved sectors.
Abstract:
A Time of Flight mass analyzer is disclosed comprising an annular ion guide having a longitudinal axis and comprising a first annular ion guide section and a second annular ion guide section. Ions are introduced into the first annular ion guide section so that the ions form substantially stable circular orbits within the first annular ion guide section about the longitudinal axis. The ions are then orthogonally accelerated ions from the first annular ion guide section into the second annular ion guide section. An ion detector is disposed within the annular ion guide and has an ion detecting surface arranged in a plane which is substantially perpendicular to the longitudinal axis.
Abstract:
A multi-turn time-of-flight mass spectrometer creates, an accurate mass spectrum of a wide mass range, with the smallest number of measurements. Deflecting electrodes are provided on an ejection path through which ions deviating from a loop orbit fly to a detector having a two-dimensional array elements. A varying voltage applied to the deflecting electrodes creates an electric field. When two ions having different mass-to-charge ratios simultaneously arrive at the detector, these ions are affected with differing strengths since they pass through the deflecting electric field at different times. This results in arrival for the ions on a detection surface. The time an ion passing through the deflecting electric field can be calculated from the displacement of the arrival position of that ion. Then the flight speed of the ion is obtained and its number of turns is roughly deduced to arrive at its mass-to-charge ratio.
Abstract:
A mass spectrometer and method of mass spectrometry wherein charged particles in a beam undergo multiple changes of direction. A detection arrangement detects a first portion of the charged particle beam, and provides a first output based upon the intensity of the detected first portion of the charged particle beam. The detection arrangement detects a second portion of the charged particle beam that has travelled a greater path length through the mass spectrometer than the first portion of the charged particle beam, and provides a second output based upon the detected second portion of the charged particle beam. A controller adjusts the parameters of the charged particle beam and/or the detection arrangement, based upon the first output of the detection arrangement, so as to adjust the second output of the detection arrangement.
Abstract:
A variety of ions generated in an ion source are made to fly while bypassing a loop orbit and mass analyzed to create a mass spectrum. Among the peaks appearing on the mass spectrum, peaks complying with predetermined conditions are extracted to determine a plurality of mass ranges to be measured (S1 through S3). Next, the ion selection conditions for the timing when ions should be injected into the loop orbit and on the loop orbit are determined for each mass range. In addition, deviation conditions under which selected ions will not be mixed are determined (S4 and S5). When the second measurement is performed for the same sample, ions are put into the loop orbit and unnecessary ions are removed from the loop orbit in accordance with the ion selection conditions (S6 and S7). Thus, only the ions to be measured are left on the loop orbit with a high mass resolving power. Then, these ions are sequentially deviated from the loop orbit in accordance with the ion deviation conditions, dissociated, and then mass analyzed (S8). In this manner, MS/MS analyses are performed for each of the plurality of ions to be measured to create an MS/MS spectrum (S10).
Abstract:
A measurement is performed in a no-passing mode, in which ions having different masses are prevented from making a complete turn through a loop orbit, to obtain a time-of-flight spectrum without the passing of ions having different masses (S1 and S2). From the time of flight and other information of the peaks appearing on the time-of-flight spectrum (S3), the number of turns and the time of flight in the loop-turn mode are predicted. Based on this prediction, a set of segments are defined on a time-of-flight spectrum in the loop-turn mode. The time widths of those segments are determined taking into account the spreads of the time widths of the aforementioned peaks. Since the number of turns is unique within each segment, the numbers of turns and the masses of the peaks can be uniquely determined as long as none of the segments overlap each other. Accordingly, it is determined whether there is any overlapped portion in the segments defined on the time-of-flight spectrum in the loop-turn mode under provisionally predetermined conditions. When a condition under which no overlapping occurs has been found, the segment setting is fixed (S4-S6). As a result, the timing for switching an ejection switch, which is used for ejecting ions from the loop orbit, is also determined. Based on this timing, a measurement in the loop-turn mode is performed (S7).
Abstract:
A novel instrument and method for TOF/TOF mass spectrometry is offered. A spiral trajectory time-of-flight mass spectrometer satisfies the spatial focusing conditions for the direction of flight and a direction orthogonal to the direction of flight whenever ions make a turn in the spiral trajectory. An ion gate for selecting precursor ions is placed in the spiral trajectory of the spiral trajectory time-of-flight mass spectrometer. Electric sectors are placed downstream of the ion gate.