Variable potential ion guide for mass spectrometry

Radiant energy – Ionic separation or analysis – Ion beam pulsing means with detector synchronizing means

Reexamination Certificate

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C250S282000, C250S3960ML

Reexamination Certificate

active

06657190

ABSTRACT:

STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT
Not Applicable.
FIELD OF THE INVENTION
This invention relates to the field of mass spectrometry and in particular to a variable potential ion guide which permits increased transmission and enhanced ion analysis in mass spectrometry.
BACKGROUND OF THE INVENTION
The field of mass spectrometry encompasses an area of analytical chemistry which analyzes substances by measuring the molecular mass of the constituent compounds. With the increasing importance of biomolecule analysis, time-of-flight mass spectrometry (TOF-MS) is becoming more and more popular in both industrial and academic labs. Time-of-flight mass spectrometers have shown sensitivity for samples in the range of a few hundred attomoles and have a mass range that is only limited by the ionization method. With the introduction of
252
Cf plasma desorption techniques and matrix assisted laser desorption ionization (MALDI), this mass range was extended into the useful range for biomolecule study. Because of the growing interest in biochemical pathways and identification of biomolecules that occur in only trace amounts, time-of-flight instruments are becoming the instrument of choice in analytical labs.
The principle of mass analysis is that ions of the same kinetic energy will have different velocities based on their mass. The fundamental equation used in time-of-flight mass spectrometry is as follows:
KE=
½
mv
2
The ability to accurately determine the mass of a specific sample ion depends on how well defined the kinetic energy is and the ability to determine the differences in the time-of-flight of the ions between two fixed points. Early instruments built for time-of-flight mass spectrometry improved the resolution of the instrument by increasing the length of the flight tube (FIG.
1
). By increasing the distance between the source and the detector, ions having small differences in velocity were allowed to become separated in space. Typical flight distances for commercial instruments were often two or three meters long to provide adequate resolution.
Many successful time-of-flight mass spectrometry instrument designs utilize an ion extraction surface that is perpendicular to the ion optical axis. This geometry prevents the loss of mass resolution due to spatial distribution effects related to sample position and the laser focal size. (Cotter, R.
Biomed. Environ. Mass Spectrom.,
1989, 18, 513-532). However, using this geometry, ions can acquire velocity components perpendicular to the ion optical axis, making it difficult to focus ions onto the detector. Although large acceleration potentials have been implemented to limit the effects of the initial kinetic energy distribution of extracted ions, velocity components perpendicular to the flight axis result in ion loss as the beam diverges away from a detectable axis.
A major advance in kinetic energy focusing was the introduction of the ion mirror or ion reflector first described by Mamyrin (Mamyrin, B. A.; Karataev, V. I.; Shmikk, D. V.; Zagulin, V. A.;
Sov. Phys
.-JETP, 1973, 37, 45-48.). With this approach, ions penetrate a retarding field at a depth proportional to their velocities. Ions with a high velocity travel a longer distance before exiting the field which creates tighter isomass ion packets. To simplify focusing characteristics and minimize ion loss, initial designs minimized the angle of incidence relative to the ion reflector. Although such ion mirrors result in greatly improved mass resolution, field lines in the center of the ion mirror tend to expand and redirect ion trajectories away from the flight axis. To attempt to control inhomogeneous field lines, multiple electrodes are added in an attempt to refine the electric field in the center of the ion mirror.
Another technique used to improve resolution is the lengthening of the flight region, but again, the extra length makes it more difficult to transport ions to the detector. Therefore, a significant loss of sensitivity can be experienced when going to the longer drift region. This loss in sensitivity was addressed by Oakey and Macfarlane with the introduction of an electrostatic particle guide. (Oakey, N.; Macfarlane, R.;
Nucl. Instrum. Methods,
1967, 49, 220-228). The electrostatic particle guide (EPG) is an isolated wire electrode that spans the length of the drift region of the flight tube, creating a potential field in the center which effectively “guides” ions to the detector. Ions that are accelerated in a direction slightly perpendicular to the ion optical axis are captured in the potential field and transported to the detector resulting in a dramatic improvement in sensitivity (Geno, P.; Macfarlane, R.;
Int. J. Mass Spectrom. Ion Proc.
1986, 74, 43-57: Brown, R.; Gilrich, N.;
Rapid Commun. Mass Spectrom.
1992, 6, 697-701).
In addition to improved transmission efficiency of ions, Macfarlane later demonstrated the utility of the EPG for elimination of neutrals (Wolf, B.; Macfarlane, R.;
J.A.S.M.S.
1992, 3, 706-715) and ion elimination (Geno, P.; Macfarlane, R.;
Int. J. Mass Spectrom. Ion Proc.
1986, 74, 43-57). Recently, as described by Just and Hanson (Just, C. L.; Hanson, C. D.;
Rapid Comm. Mass Spectrom.
1993, 7, 502-506), selective ion elimination has been accomplished using a pulsed bipolar EPG. This approach was shown to effectively eliminate intense, low-mass background ions while increasing the transmission efficiency of higher mass ions. This technique was also found to increase the signal-to-noise ratio by reducing the saturation of the detector. Furthermore, an EPG does not introduce radially inhomogeneous field lines and therefore does not result in positionally dependent ion acceleration. A bipolar pulsed electrostatic particle guide can therefore perform ion isolation by utilizing a multi-pulse sequence. In such a sequence, the first pulse would be used to eliminate low mass ions while subsequent pulses could be used to eliminate unwanted ions after the ions to be studied have arrived at the detector. In an experiment using a bipolar pulsed EPG to isolate ions, ions were isolated on the basis of their radial flight times and then selected ions were analyzed using the axial flight times. By using this approach, ion isolation can be performed with high resolution while maintaining high ion transmittance.
In my U.S. Pat. No. 6,013,913, an improved coaxial time-of-flight mass spectrometer is described which utilizes switched reflectrons at opposing ends of the spectrometer to cause particles to be reflected repeatedly along the same axis before allowing the particles to reach the detector. Using fast electrostatic switches, it is possible to orient the source, detector and analyzers on the same axis of ion motion. This geometry permits ions to make multiple passes through the drift region as they are continuously reflected between the ion mirrors. This creates a continuous zero angle reflecting time-of-flight instrument that maintains high ion transmission while providing improved resolution. Because the reflection fields are not at a constant potential, the single potential created by an EPG is inconsistent with the field requirements. Therefore, ions must leave the EPG guided flight region when entering into the reflectron region. Because of this, ions tend to diverge in the reflectron region and are lost. This effect ultimately limits the number of passes that an ion can effectively make within a coaxial reflectron due to ion loss in the reflectron regions.
In a device developed after invention of the coaxial time-of-flight mass spectrometer of U.S. Pat. No. 6,013,913, the particles under examination are reflected by a static reflectron on one end of a coaxial flight region, with the opposing reflectron being switched to allow the particles under examination to be passed to the detector when selected reflections have been accomplished. However, unlike the device described in U.S. Pat. No. 6,013,913, the single switched coaxial reflectron device suffers from substantial degradation of the yie

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