EP0403965B1 - MS-MS-Flugzeit-Massenspektrometer - Google Patents
MS-MS-Flugzeit-Massenspektrometer Download PDFInfo
- Publication number
- EP0403965B1 EP0403965B1 EP90111293A EP90111293A EP0403965B1 EP 0403965 B1 EP0403965 B1 EP 0403965B1 EP 90111293 A EP90111293 A EP 90111293A EP 90111293 A EP90111293 A EP 90111293A EP 0403965 B1 EP0403965 B1 EP 0403965B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- ions
- ion
- diaphragm
- time
- mass spectrometer
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 150000002500 ions Chemical class 0.000 claims description 254
- 238000010884 ion-beam technique Methods 0.000 claims description 43
- 238000001819 mass spectrum Methods 0.000 claims description 40
- 239000002245 particle Substances 0.000 claims description 27
- 230000005284 excitation Effects 0.000 claims description 23
- 238000013467 fragmentation Methods 0.000 claims description 19
- 238000006062 fragmentation reaction Methods 0.000 claims description 19
- 238000000034 method Methods 0.000 claims description 17
- 230000005684 electric field Effects 0.000 claims description 11
- 238000010894 electron beam technology Methods 0.000 claims description 9
- 230000003287 optical effect Effects 0.000 claims description 7
- 230000008859 change Effects 0.000 claims description 5
- 238000006073 displacement reaction Methods 0.000 claims description 5
- 230000003247 decreasing effect Effects 0.000 claims description 4
- 230000001360 synchronised effect Effects 0.000 claims description 3
- 238000006243 chemical reaction Methods 0.000 claims description 2
- 230000036961 partial effect Effects 0.000 claims description 2
- 230000000704 physical effect Effects 0.000 claims description 2
- 230000000979 retarding effect Effects 0.000 claims 5
- 230000003993 interaction Effects 0.000 description 19
- 238000012937 correction Methods 0.000 description 18
- 239000012634 fragment Substances 0.000 description 15
- 238000004885 tandem mass spectrometry Methods 0.000 description 12
- 230000005540 biological transmission Effects 0.000 description 7
- UHOVQNZJYSORNB-UHFFFAOYSA-N Benzene Chemical compound C1=CC=CC=C1 UHOVQNZJYSORNB-UHFFFAOYSA-N 0.000 description 5
- 230000008901 benefit Effects 0.000 description 5
- 150000001793 charged compounds Chemical class 0.000 description 4
- 238000001514 detection method Methods 0.000 description 4
- 230000035945 sensitivity Effects 0.000 description 4
- 101100219264 Petunia hybrida C4H2 gene Proteins 0.000 description 3
- 238000010521 absorption reaction Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- 238000004458 analytical method Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 210000001520 comb Anatomy 0.000 description 2
- 230000000295 complement effect Effects 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000008030 elimination Effects 0.000 description 2
- 238000003379 elimination reaction Methods 0.000 description 2
- 238000001704 evaporation Methods 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 238000011835 investigation Methods 0.000 description 2
- 238000004949 mass spectrometry Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000006303 photolysis reaction Methods 0.000 description 2
- 239000005871 repellent Substances 0.000 description 2
- 230000000717 retained effect Effects 0.000 description 2
- 238000001228 spectrum Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 230000002123 temporal effect Effects 0.000 description 2
- 238000001269 time-of-flight mass spectrometry Methods 0.000 description 2
- 206010013710 Drug interaction Diseases 0.000 description 1
- 230000004913 activation Effects 0.000 description 1
- -1 benzene ions Chemical class 0.000 description 1
- 230000009172 bursting Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005274 electronic transitions Effects 0.000 description 1
- 230000005281 excited state Effects 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 238000000752 ionisation method Methods 0.000 description 1
- 150000002605 large molecules Chemical class 0.000 description 1
- 229920002521 macromolecule Polymers 0.000 description 1
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 231100000289 photo-effect Toxicity 0.000 description 1
- 238000005381 potential energy Methods 0.000 description 1
- 239000002243 precursor Substances 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000002829 reductive effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000001629 suppression Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J49/00—Particle spectrometers or separator tubes
- H01J49/004—Combinations of spectrometers, tandem spectrometers, e.g. MS/MS, MSn
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J49/00—Particle spectrometers or separator tubes
- H01J49/26—Mass spectrometers or separator tubes
- H01J49/34—Dynamic spectrometers
- H01J49/40—Time-of-flight spectrometers
Definitions
- the invention relates to a time-of-flight mass spectrometer with an ion source for generating a pulsed primary ion beam, which has at least 3 diaphragms with a common axis of symmetry, at which pulsed or time-constant electrical or U1, U b and U o potentials are present during operation of the spectrometer , having, wherein the ions between the first, ion-repellent and the second, ion-attracting aperture are generated at a distance a from the second aperture, which is smaller than the distance from the first from the second aperture, and with a device for pulsed, local sharply limited influence on the ions.
- MS-MS techniques in mass spectrometry allow secondary mass selection after a preferred mass from the variety of ions that is generated in the ion source has already been selected with a primary mass selector. These primarily selected ions experience an interaction of various kinds (eg excitation by collisions, light, etc.), which leads to fragmentation, the secondary fragments can be examined by a further mass analysis.
- MS-MS techniques can be used to study molecular decay kinetics, to elucidate molecular structures and to analyze unknown molecules; They represent one of the most complex, but also the most information-rich methods in these areas.
- MS-MS mass spectrometry So-called double-focusing devices, which consist of a combination of magnetic and electrostatic mass analyzers, are usually used for MS-MS mass spectrometry.
- MS-MS devices as well as their enhancement, MS-MS-MS devices, have reached a certain limit of their developability both in terms of their price / performance ratio and in terms of their technical possibilities.
- the so-called reflectron time-of-flight spectrometers overcome one of the greatest disadvantages of conventional time-of-flight mass spectrometers: the low mass resolution.
- a resolution (50% valley) of 5000 as standard (without readjustment) and of 10,000 without serious problems can be achieved (e.g. from: Boesl et al., Anal. Instrum. 16 (1987) 151).
- Even a resolution of 35,000 has already been achieved (T. Bergmann, T.P. Martin, H. Schaber Rev. Sci. Instrum. 60 (1989) 347).
- the excellent advantage of time-of-flight mass analyzers their extraordinarily high transmission and thus detection sensitivity, is almost unaffected.
- the resonant laser excitation serves for the ionization of molecules with the help of a multi-photon (mostly two-photon) absorption via a resonant intermediate state.
- a multi-photon mostly two-photon
- the inclusion of a molecule-specific, resonant optical transition already enables substance-selective ionization and thus a first one Step towards MS-MS methods.
- resonant laser excitation is also characterized by great flexibility: on the one hand, exceptionally gentle ionization is possible (see, for example, Grotemeyer et al., Org. Mass Spectrom.
- Fragmentation can be achieved, which can be varied from the generation of a few fragments with high involvement of metastable decays to extremely hard fragmentation (see, for example, Boesl et al., J. Chem. Phys. 72 (1980) 4327 and Chem. Phys. Lett. 87 ( 1982) 1).
- the present invention is therefore based on the object of providing a device composed of simple components with various options, in which, after ionization and before a final time-of-flight mass analysis, a further mass selection and / or a secondary fragmentation can take place, the mass resolution, the transmission and the sensitivity of detection is not inferior to that of known devices.
- the MS-MS time-of-flight mass spectrometer according to the present invention has the advantages over conventional MS-MS devices of very high transmission and thus high detection sensitivity and very high speed.
- Commercial reflectron time-of-flight spectrometers can be converted to an MS-MS device with minor modifications; the essential additional costs arise only through the selected, secondary access method and are far below the purchase price of the source device.
- high transmission and detection sensitivity are also intrinsic properties of the method, as is the speed: Secondary mass spectra can be carried out in the submillisecond range without losses in transmission or mass resolution.
- a combination with almost any access method, such as laser excitation, electron, ion, molecular and atomic beam or gas cells for shock activation is possible.
- the exact definition of the location focus ie the point of optimal energy correction of the primary ions leaving the ion source, is an essential prerequisite for the time-of-flight mass spectrometer according to the invention. While energy corrections of the first order have at most been implemented in the location focus, adherence to the above distance relationships between the diaphragms and the corresponding potential relationships presents an ion source which enables energy correction of the second order.
- the particles to be ionized can be provided either simply by introducing gas into the ion source, or by evaporating the particles in the ion source itself.
- the latter method is also suitable for the investigation of solid substances.
- the particles to be examined are introduced into the ion source by means of an atomic or molecular beam, so that the particles to be ionized located only in a narrowly defined area, which enables an exact definition of the ion site.
- the atomic or molecular beam can either cross the axis of symmetry of the diaphragms essentially at right angles between the first and the second diaphragm of the ion source at a distance a from the second diaphragm.
- the atomic or molecular beam enters the ion source collinearly to the axis of symmetry of the diaphragms through the first diaphragm, so that the structures for generating the atomic or molecular beam cannot be attached to the side of the mass spectrometer, but rather in an extension of its axis.
- Another advantage of this arrangement is that the particles which have not yet been ionized have a beam characteristic in the direction of the later ion beam.
- the particles to be examined can be ionized in the ion source either by photoeffect, by particle collisions or by field ionization.
- photoionization takes place, it is possible to keep the residual energy in the molecular ion to a minimum during the ionization process. It is a "gentle" method of ionization, in which even sensitive large molecules can be ionized without bursting.
- the cheapest is the use of a light beam from an incoherent source, in particular a UV source, for example a mercury vapor lamp for the continuous generation of high light output, or commercially available flash lamps.
- pulsed or continuous laser beams are used for the photoionization of the particles to be examined.
- the extraordinarily high frequency sharpness for laser light enables a high atom- or molecule-specific selectivity of photoionization. With that, quite selectively select only certain particles from a particle mixture offered in the ion source.
- pulsed lasers are used, the temporal characteristics of which are impressed on the pulsed ion beam.
- Another advantage of using lasers is the high power density that can be achieved, the possibility of a very sharp spatial bundling of laser beams and thus a very precise definition of the ion source, as well as the utilization of the frequency sharpness of the laser light with regard to the optical excitation of the particles to be examined.
- the particles to be examined are ionized by collisions using a beam of charged particles.
- This particle beam can either be an electron beam which is inexpensive and simple, e.g. high beam intensities and a good spatial beam definition can be achieved by means of a hot cathode and simple electron optics.
- the impact ionization takes place with the aid of an ion beam, which enables the mass spectrometric investigation of ion impact processes in the ion source.
- the ion formation site is particularly well defined at the point of intersection of the two rays.
- the pulse characteristic of the ion beam is generated by pulsed voltages on the diaphragms of the ion source, so that a continuous supply of the to investigating particles and continuous ionization is possible.
- the potentials are statically applied to the diaphragms, which enables considerably simpler electronics for the voltage supply to the diaphragms, but requires a pulsed ionizing beam.
- the potentials applied to the diaphragms of the ion source can be set separately in embodiments of the invention.
- a control device which automatically adjusts the potential U b at the second aperture at given distances a, b, c and given potential U 1 at the first aperture.
- an ion detector with a flat impact surface is provided at a distance c in the direction of flight of the ions behind the third aperture of the ion source on the trajectory of the ions, with which the position of the location focus can be determined precisely.
- the ion detector is arranged such that it can be moved out of the trajectory of the ions by means of a mechanical displacement device, so that the properties of the location focus can either be exploited by recording a mass spectrum in the location focus, or, after the adjustment of the location focus has been completed, the ion detector is moved out of the ion beam , and a secondary interaction can take place at the location focus.
- the secondary access to the ion beam at the location focus is modulo of a defined time delay compared to the time of generation of the ion pulses in the ion source.
- the ions at the location focus are influenced in a strictly localized manner. The location focus is thus the starting point for a secondary mass spectrum.
- the pulse triggering the interaction is synchronized with the primary ion pulse from the ion source.
- the ions are influenced by building up a pulsed electrical field which is transverse to the ion beam direction and which causes a selective deflection of ions in a specific propagation time window from the primary ion beam direction.
- a pulsed electrical field which is transverse to the ion beam direction and which causes a selective deflection of ions in a specific propagation time window from the primary ion beam direction.
- the transverse electrical field is generated by means of a mesh network. If the mesh network is fine enough, access to the ion beam is limited in space, and there is the possibility of time modulation of the secondary access via the changes in the electrical potential applied to the mesh network.
- the mesh consists of two comb-like structures, the teeth of which consist of very fine wires, the teeth of the comb-like structures lying opposite one another in the center grip without touching and all teeth belonging to a comb-like structure are connected to each other in an electrically conductive manner.
- the electrical fields generated by the two comb-like structures cancel out at a very short distance in front of and behind the mesh, so that there is no unwanted interference of the ion beam by fields that extend far into space, as are typical for conventional grids, uncontrollable interference cause.
- voltage pulses are applied to the two comb-like structures which are complementary to the potential U Potential applied to the third aperture of the ion source, that is to say they have the same amplitudes, the same pulse durations but opposite polarities. This can either cause the elimination of certain undesirable ion masses or a short time window for the passage of special ions, e.g. for targeted further secondary fragmentation.
- the secondary interaction in the location focus can take place by optical excitation, in particular with a laser beam. This can cause photodissociation and subsequent fragmentation of the primary ions.
- Optical excitation offers the advantage of being able to be tuned very precisely to a specific electronic transition and thus extremely high mass selectivity, and on the other hand is particularly gentle as a "soft" excitation method, so that even metastable states of larger molecules can be excited without first destroying them . On the other hand, it is variable from very soft to very hard Fragmentation and thus a variation of secondary mass spectra possible.
- the secondary interaction takes place in the location focus in the form of an ion shock excitation.
- the colliding particles come either from an electron beam or another ion beam that crosses the spatial focus perpendicular to the beam axis of the primary ions.
- the generation of an electron beam is particularly simple and inexpensive and does not require any complex optics.
- a second ion beam on the other hand, physical scattering experiments can be carried out in the location focus.
- the primary ions can either be brought into an excited state or can be broken up into smaller molecular fragments with sufficient energy.
- the ions are influenced with the aid of pulses which, owing to their short duration, ensure a sharp temporal, energetic and thus mass-specific selection of the primary ions to be influenced.
- the pulse duration can be virtually infinitely long, but then the selection of the primary ions to be excited is controlled by a sharply defined energy of the exciting particles or photons, in that very specific energy levels of the electron shell of these ions are excited.
- the physical state of the ions is additionally influenced in the region of the location focus, either by optical excitation of the ions by means of a laser beam or by shock excitation an electron beam, an additional ion beam or an atomic or molecular beam.
- This enables the acquisition of secondary mass spectra of very special ion masses that were previously selected in the location focus by a first access.
- the interaction of the primary ion beam can also be provided in a collision gas cell before access in the location focus. A secondary mass spectrum of the ions leaving the collision cell can then be recorded by successively displacing the time window selected in the location focus relative to the time of origin of a primary ion pulse in the ion source.
- the post-acceleration of the ions is provided after the location focus.
- the drastic decrease in the kinetic energy of the ion fragments after fragmentation which would negatively influence the mass resolution of the spectrometer, can be partially compensated for.
- a fourth diaphragm after the location focus is provided in the ion beam, which is electrically connected to the third diaphragm in the ion source via a tubular shield which encloses a field-free space.
- the post-acceleration is then brought about by a fifth aperture, which, viewed in the direction of flight of the ions, sits on the ion beam axis after the fourth aperture and lies at the ground potential of the time-of-flight spectrometer.
- an ion reflector is provided after the secondary interaction zone, which has one reflector end plate and several braking fields arranged at a distance in front on a common axis of symmetry contains defining brake electrodes, the reflector end plate being arranged displaceably along the axis of symmetry of the ion reflector.
- the electrical potential applied to it is tracked in such a way that the electrical field strength between the reflector end plate and the brake electrode initially located is not changed.
- Such an ion reflector initially serves to compensate for the time-of-flight differences of ions of the same mass but different initial energies, and thus to improve the mass resolution.
- the displaceable end plate makes it possible to mask out the ions of the primary beam: these have a higher kinetic energy than all fragment ions that are secondary to the primary ions, so that these primary ions have the greatest depth of penetration into the ion reflector. If you move the reflector end plate towards the incoming ion beam to such an extent that the primary ions hit the plate and are thus removed from the ion beam, only the low-energy secondary ions formed due to the secondary access leave the ion reflector. These can now be detected undisturbed by the relatively high intensity of the primary beam with high resolution. By pushing the reflector end plate further towards the last brake electrode, ions with lower kinetic energy are also hidden. In this operating mode, the ion reflector can therefore be used as an energy selector for recording secondary mass spectra.
- the easiest way to track the electrical potential of the reflector end plate when it is displaced is by means of a sliding contact.
- electronic voltage tracking is provided.
- the potentials of the other brake electrodes and of the reflector end plate are adjusted in such a way that the original relationships of the potentials to one another are retained before the change.
- the optimal setting of the ion reflector once found is automatically maintained even when the position of the reflector end plate is changed.
- the aperture openings of the brake electrodes are each provided with a network or a grid, which serves as a potential shield and for generating parallel equipotential surfaces.
- a front panel with a larger opening diameter than that of the brake electrodes is provided. The front panel is then at the ground potential of the time-of-flight mass spectrometer and enables a controlled extraction of the electric fields from the brake electrodes into the space in front of the ion reflector, and thus controlled steering of the ions arriving in and out of the ion reflector.
- the ions are normally deflected by the ion reflector from their original flight direction by an angle of more than 90 ° but less than 180 °.
- the axis of symmetry of the ion reflector is collinear with the direction of flight of the incoming ions, ie the ion beam is reflected back in itself.
- the ion detector sits on the ion beam axis between the ion reflector and the ion source and has an opening concentric to the ion beam axis for the passage of the incoming ions. This arrangement enables a very compact construction of the time-of-flight mass spectrometer.
- optimal time focusing for ions with less than the average kinetic energy of the ions is achieved by reducing the potentials applied to the brake electrodes and the reflector end plate.
- a secondary mass spectrum, in particular for molecular ions fragmented on the flight path, can thus be generated by tuning the fields and observing them in a fixed time fixed.
- the MS-MS time-of-flight mass spectrometer shown schematically in FIG. 1 comprises an ion source A, a secondary interaction zone B, an ion reflector C, in which the incident ion beam is reflected by an angle of more than 90 °, and a field-free ion drift distance D with an ion detector 10 for detecting the ions. All components are located within an evacuable housing, not shown.
- the ion source A has at least two accelerating pulsed or unpulsed electric fields which are generated with at least three diaphragms: an ion-repellent first diaphragm 1, an ion-attracting second diaphragm 2 and a post-accelerating third diaphragm 3.
- the diaphragms 2 and 3 have an opening for the passage of the accelerated ions.
- Separately adjustable voltages can be applied to all three diaphragms, namely the potential U 1 at the first diaphragm 1, the potential U b + U 0 at the second diaphragm 2 and the potential U 0 at the third diaphragm 3.
- U0 is identical to the ground potential of the equipment.
- the particles to be ionized are provided by introducing gas into the ion source or by evaporating the particles within the ion source.
- the ionization of the particles to be examined in the ion source takes place in the embodiments shown in FIGS. 1 and 2e by means of a beam irradiated perpendicular to the axis of symmetry 20 of the diaphragm arrangement between the first diaphragm 1 and the second diaphragm 2 at a distance a from the second diaphragm 2 5.
- the beam 5 can be either a laser beam, an electron beam or an ion beam. Accordingly, the particles to be examined are then ionized either by absorption of photon energy in the electron shell or by particle collision.
- a beam of incoherent light in particular from a UV source, is used instead of the laser beam.
- the ionizing beam 5 perpendicularly crosses the beam 4 of the particles to be ionized on the axis of symmetry 20 and is focused on the crossing point.
- the pulse behavior of the primary ion beam 25 generated in the ion source is caused by a correspondingly pulsed ionizing beam 5.
- the ionizing beam 5 can also be irradiated continuously over time, the pulse behavior of the primary ion beam 25 then being impressed by pulsed electrical fields which are generated by applying corresponding potentials to the diaphragms 1, 2, 3.
- the Ionization of the particles to be examined caused by strong electric fields.
- the point of origin of the primary ions which in the exemplary embodiment shown is located on the axis of symmetry 20 between the first diaphragm 1 and the second diaphragm 2 at a distance a from the second diaphragm 2, can be changed by correspondingly shifting the beams 4 and 5.
- the distance b between aperture 2 and 3 is fixed in the exemplary embodiment shown, but can be kept variable in other embodiments, e.g. by means of a second orifice 2 which can be displaced in parallel, but then the distance a of the point of origin of the primary ions from the second orifice 2 also changes accordingly.
- a decisive feature of all embodiments of the present invention is the exploitation of the fact that ion sources with pulsed ion generation have a so-called location focus, which in the exemplary embodiment shown is located on the axis of symmetry 20 of the diaphragm arrangement at a distance c in the direction of the primary ion beam 25 according to FIG third aperture 3 is located.
- the location focus 30 is therefore a spatial point of optimal energy correction.
- the order and thus the quality of this correction depends on the type of ion source. With a one-stage ion source (only apertures 1 and 2) you can achieve a 1st order correction, with a two-stage ion source (like the one described above) a 2nd order correction. So far, even for multi-stage ions only the first order location focus is observed.
- the second order location focus is used for the first time, which is derived below:
- the latter term (x k ) contributes not only to an energy blur but also to a time blur ("turn-around-time"), which must be taken into account separately.
- both the 1st order and the 2nd order terms must disappear in the above equation. From this condition, the relationships result for the quantities a, b, and c (see FIG.
- the longest possible flight distance c e.g. 10 to 20 cm
- a mass resolution of 500 to 1000 can already be achieved in such a location focus 30.
- such a location focus of the 2nd order is generated by a suitable choice of the aperture distances in the ion source A and by applying suitable potentials U 1, U b and U o to the apertures 1, 2, 3.
- a suitable ion detector 11 with a flat impingement surface is used for the exact adjustment of the location focus 30 to a defined distance c, which can be achieved by varying the distance a of the origin of the ions from the second aperture 2 and the voltages at the apertures 1 and 2; this detector can be brought into the ion trajectory of the primary ion beam 25 by means of a mechanical displacement device and can be removed again for MS-MS measurements.
- An electronic control device (not shown) is provided for automatically tracking the potential U b according to equation (II.) At a given potential U 1 and given distances a, b, c.
- the ion reflector C shown in FIG. 1 consists of a two-stage arrangement, namely the braking electrodes 6 and 7 defining a braking field and the reflector end plate 8, which together with the second braking electrode 7 viewed in the direction of the incident ion beam defines a reflector field.
- the brake electrodes 6, 7 are designed as pinholes.
- the reflector end plate 8 is attached so that it can be pushed into or out of the reflector. The voltage on this end plate is adjusted so that the field strength between Brake electrode 7 and reflector end plate 8 is not changed.
- the brake electrodes 6 and 7 have an opening several centimeters in size, which is either provided with a network for generating parallel aquipotential surfaces; or they are operated without networks, but then with a front panel 9, which lies on the apparatus mass of the time-of-flight mass spectrometer.
- the voltages required for such reflectors correspond to the values known from the literature.
- the axis of symmetry 40 of the ion reflector C can both, as shown in FIG. 1, have an angle to the ion flight direction, and can also run collinearly with it. In the latter case, however, a special ion detector is required (see below).
- the field-free ion drift distance D is simply formed by a sufficiently long, empty vacuum tube between a secondary interaction zone B and the ion reflector C, in accordance with known arrangements.
- Only a suitable ion detector 10 e.g. multichannel plate detector
- the ion detector 10 is located at the end of the ion trajectory, as close as possible to the secondary interaction zone B.
- the ion detector 10 is located on the incident ion flight direction with a concentric opening in the middle for the Passage of the ions coming from the ion source A and the secondary interaction zone B.
- the secondary interaction zone B contains the location focus 30 and is the heart of the MS-MS time-of-flight mass spectrometer.
- the focus 12 of a second laser pulse with selected wavelength and intensity is placed exactly in the location focus 30.
- This laser pulse can optionally be replaced by other pulsed, locally sharp access methods (eg electron beam). Varies If the time delay between the primary generation of ions in the ion source A and the secondary access in the location focus 30, the individual ions of different weights are selectively excited in accordance with their different flight times t ges and can therefore also be selectively fragmented by photodissociation. If the pulse length is only short enough and the focus 12 is only small enough (for example 0.1 mm), the maximum mass resolution possible in the location focus 30 can be obtained. Secondary access is therefore responsible for both secondary mass selection and secondary fragmentation.
- the ion reflector C is optimally corrected for the kinetic energy of the primary ions in the ion beam 25 and the second laser is not switched on, a usual primary mass spectrum is obtained.
- the voltage at the ion reflector C must now be continuously reduced, the ratio of the voltages at the brake electrodes 6, 7 and the reflector end plate 8 (and possibly the front panel 9) being retained .
- the entire ion reflector C is thus optimally corrected for decreasing ion energies.
- the kinetic energy of a molecular ion in relation to the mass of the fragments is distributed among them; secondary fragments with smaller mass therefore also have smaller kinetic energies.
- the energy correction of the ion level is thus coordinated with the decreasing masses of the secondary fragment ions.
- the ion reflector C with a displaceable reflector end plate 8 and time window works as a tunable energy analyzer and thus, according to what has been said above about the fragment energies, as an analyzer for the masses of the secondary fragment ions.
- 3b-d show such secondary mass spectra, the ordinate being the intensity of the incident ions measured at the ion detector 10 and the abscissa the voltage of the reflector end plate 8 calibrated in ion masses m.
- 3a shows a primary laser time-of-flight spectrum of benzene, in which the intensity of the first laser was chosen such that, in addition to the ionization, a partial fragmentation of the benzene ions also took place.
- FIG. 3b only the molecular ions in the location focus were detected, excited and fragmented by a suitable delay of the second laser; the secondary mass spectrum can be seen here.
- Fig. 3c only the fragment ions C4H4 im were selectively fragmented in location focus 30, in Fig.
- the movable reflector end plate 8 is provided.
- the voltages at the ion reflector C can thus be set to optimal energy correction; then the reflector end plate 8 is pushed so far into the reflector field that the point of reversal of the primary ions lies exactly on it.
- the reflector end plate 8 In order to leave the reflector field and thus the energy correction unaffected, the reflector end plate 8 must always be at a voltage which corresponds exactly to the equipotential surface of its respective position; In embodiments, this can be done by means of a sliding contact (not shown) or electronic voltage tracking.
- the secondary intervention consists in a special mesh network 23, which in turn is located precisely in the location focus 30.
- This mesh network 23 consists of two comb-like structures 13 and 14, the "teeth" of which engage in the center without touching one another.
- the "teeth” consist of the finest possible wires; all "teeth” belonging to a comb are electrically connected to one another; their distances are 0.3 mm and smaller, or 0.15 mm or smaller from the "teeth" of the other comb.
- Complementary voltage pulses ⁇ U (same amplitude, same length, opposite sign) are best applied to the two combs, so that ions that fly between the teeth at the right time sense a transverse electric field and are deflected laterally, so that but on the other hand, at a very short distance from the mesh network 23, the pulsed fields already cancel each other out.
- FIG. 2e represents to some extent a combination of the embodiments from FIGS. 2a and 2b.
- a secondary mass spectrum can only be obtained sequentially and not with a single laser pulse.
- the fact is used that a two-stage ion reflector can still correct 20% energy blur, that a mass resolution of 5000 is easily achieved.
- the fragment ions are accelerated after the location focus 30.
- the kinetic energy of the ions at the location focus 30 may only be a fraction of the final kinetic ion energy.
- the ion source A with the diaphragms 1, 2 and 3, the mesh network 23 in the local focus 30 and an additional, final fourth diaphragm 15 are placed at an increased potential U0.
- the post-acceleration then takes place between the fourth orifice 15 and a fifth orifice 16 which is at ground potential.
- a tube 17 which is at the same potential as the diaphragms 3 and 15 and corresponds to the reference potential of the mesh network 23.
- the mesh network 23 is attached in the location focus 30; selected primary ions are selected with high mass resolution.
- the focus 18 of a second laser or another pulsed access for example an electron beam or ion beam, is adjusted to the ion beam leaving the mesh on the axis of symmetry 20. If the voltage pulse on the mesh network 23 and the second laser pulse 18 or, in the case of embodiments, a different access pulse are precisely synchronized with the flight time of the primary ions of defined mass to be examined, a secondary mass spectrum of these ions is obtained.
- the mesh network 23 can also be replaced by the laser focus 18 (or other pulsed access methods); then, however, metastable ion decays, which take place in front of the location focus 30, can disrupt the secondary mass spectrum of the selected ion.
- the secondary access can also consist of a continuous interaction, such as a continuous electron beam, molecular or atomic beam or a collision gas cell. The latter must then be installed in front of the mesh and the post-acceleration as close as possible behind the mesh.
- the secondary mass spectrum can also be divided into two or more mass ranges, the energy correction of the reflector only having to be optimized in one of these ranges and thus only to 10%, 5% etc. energy deviation.
- the energy correction of the reflector only having to be optimized in one of these ranges and thus only to 10%, 5% etc. energy deviation.
- a “metastable mass spectrum” here means the mass spectrum of all productions from the metastable decay of a selected precursor ion that has arisen in the ion source. This metastable decay is usually induced by the additional excitation of the primary ions at the ionization site, for example by further absorption of a photon by laser 1 in the primary ion. A suggestion, e.g. by laser 2 is then not necessary. To record "metastable mass spectra" only laser 2 is switched off.
Landscapes
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Other Investigation Or Analysis Of Materials By Electrical Means (AREA)
- Electron Tubes For Measurement (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3920566 | 1989-06-23 | ||
DE3920566A DE3920566A1 (de) | 1989-06-23 | 1989-06-23 | Ms-ms-flugzeit-massenspektrometer |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0403965A2 EP0403965A2 (de) | 1990-12-27 |
EP0403965A3 EP0403965A3 (de) | 1991-07-31 |
EP0403965B1 true EP0403965B1 (de) | 1994-10-26 |
Family
ID=6383404
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP90111293A Expired - Lifetime EP0403965B1 (de) | 1989-06-23 | 1990-06-15 | MS-MS-Flugzeit-Massenspektrometer |
Country Status (3)
Country | Link |
---|---|
US (1) | US5032722A (enrdf_load_stackoverflow) |
EP (1) | EP0403965B1 (enrdf_load_stackoverflow) |
DE (2) | DE3920566A1 (enrdf_load_stackoverflow) |
Families Citing this family (54)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5180914A (en) * | 1990-05-11 | 1993-01-19 | Kratos Analytical Limited | Mass spectrometry systems |
GB2250632B (en) * | 1990-10-18 | 1994-11-23 | Unisearch Ltd | Tandem mass spectrometry systems based on time-of-flight analyser |
DE4106796A1 (de) * | 1991-03-04 | 1991-11-07 | Wollnik Hermann | Ein flugzeit-massenspektrometer als sekundaerstufe eines ms-ms systems |
DE4108462C2 (de) * | 1991-03-13 | 1994-10-13 | Bruker Franzen Analytik Gmbh | Verfahren und Vorrichtung zum Erzeugen von Ionen aus thermisch instabilen, nichtflüchtigen großen Molekülen |
US5300774A (en) * | 1991-04-25 | 1994-04-05 | Applied Biosystems, Inc. | Time-of-flight mass spectrometer with an aperture enabling tradeoff of transmission efficiency and resolution |
US6111645A (en) | 1991-04-29 | 2000-08-29 | Massachusetts Institute Of Technology | Grating based phase control optical delay line |
US6485413B1 (en) | 1991-04-29 | 2002-11-26 | The General Hospital Corporation | Methods and apparatus for forward-directed optical scanning instruments |
US5202563A (en) * | 1991-05-16 | 1993-04-13 | The Johns Hopkins University | Tandem time-of-flight mass spectrometer |
US5144127A (en) * | 1991-08-02 | 1992-09-01 | Williams Evan R | Surface induced dissociation with reflectron time-of-flight mass spectrometry |
US5160840A (en) * | 1991-10-25 | 1992-11-03 | Vestal Marvin L | Time-of-flight analyzer and method |
WO1995033279A1 (en) * | 1994-05-31 | 1995-12-07 | University Of Warwick | Tandem mass spectrometry apparatus |
GB2303962B (en) * | 1994-05-31 | 1998-07-08 | Univ Warwick | Tandem mass spectrometry apparatus |
US5614711A (en) * | 1995-05-04 | 1997-03-25 | Indiana University Foundation | Time-of-flight mass spectrometer |
US5625184A (en) * | 1995-05-19 | 1997-04-29 | Perseptive Biosystems, Inc. | Time-of-flight mass spectrometry analysis of biomolecules |
US6002127A (en) | 1995-05-19 | 1999-12-14 | Perseptive Biosystems, Inc. | Time-of-flight mass spectrometry analysis of biomolecules |
US5654545A (en) * | 1995-09-19 | 1997-08-05 | Bruker-Franzen Analytik Gmbh | Mass resolution in time-of-flight mass spectrometers with reflectors |
US5986258A (en) * | 1995-10-25 | 1999-11-16 | Bruker Daltonics, Inc. | Extended Bradbury-Nielson gate |
US5712480A (en) * | 1995-11-16 | 1998-01-27 | Leco Corporation | Time-of-flight data acquisition system |
DE19544808C2 (de) * | 1995-12-01 | 2000-05-11 | Bruker Daltonik Gmbh | Verfahren zur Untersuchung der Struktur von Ionen in einem Flugzeitmassenspektrometer |
US5742049A (en) * | 1995-12-21 | 1998-04-21 | Bruker-Franzen Analytik Gmbh | Method of improving mass resolution in time-of-flight mass spectrometry |
US5641959A (en) * | 1995-12-21 | 1997-06-24 | Bruker-Franzen Analytik Gmbh | Method for improved mass resolution with a TOF-LD source |
JPH11513176A (ja) * | 1996-07-03 | 1999-11-09 | アナリチカ オブ ブランフォード,インコーポレーテッド | 一次および二次の縦集束を有する飛行時間質量スペクトロメータ |
US5814813A (en) * | 1996-07-08 | 1998-09-29 | The Johns Hopkins University | End cap reflection for a time-of-flight mass spectrometer and method of using the same |
DE19631161A1 (de) * | 1996-08-01 | 1998-02-12 | Bergmann Thorald | Flugzeit-Flugzeit-Massenspektrometer mit differentiell gepumpter Kollisionszelle |
DE19631162A1 (de) * | 1996-08-01 | 1998-02-12 | Bergmann Thorald | Kollisionszelle mit integriertem Ionenselektor für Flugzeit-Flugzeit-Massenspektrometer |
JP2942815B2 (ja) * | 1996-11-05 | 1999-08-30 | 工業技術院長 | 粒子選択方法および飛行時間型選択式粒子分析装置 |
US6259101B1 (en) * | 1997-09-23 | 2001-07-10 | University Of Delaware | Method and instruments for the on-line detection, sizing or analysis of aerosol particles |
USRE39099E1 (en) * | 1998-01-23 | 2006-05-23 | University Of Manitoba | Spectrometer provided with pulsed ion source and transmission device to damp ion motion and method of use |
US6331702B1 (en) * | 1999-01-25 | 2001-12-18 | University Of Manitoba | Spectrometer provided with pulsed ion source and transmission device to damp ion motion and method of use |
US6348688B1 (en) | 1998-02-06 | 2002-02-19 | Perseptive Biosystems | Tandem time-of-flight mass spectrometer with delayed extraction and method for use |
US5969350A (en) * | 1998-03-17 | 1999-10-19 | Comstock, Inc. | Maldi/LDI time-of-flight mass spectrometer |
US6184523B1 (en) * | 1998-07-14 | 2001-02-06 | Board Of Regents Of The University Of Nebraska | High resolution charged particle-energy detecting, multiple sequential stage, compact, small diameter, retractable cylindrical mirror analyzer system, and method of use |
EP1116258B1 (en) * | 1998-09-23 | 2015-12-09 | Analytik Jena AG | Ion optical system for a mass spectrometer |
EP1124624B1 (en) * | 1998-09-25 | 2010-03-10 | The State Of Oregon Acting By And Through The Oregon Stateboard Of Higher Education On Behalf Of The University Of Oregon | Tandem time-of-flight mass spectrometer |
CA2255122C (en) * | 1998-12-04 | 2007-10-09 | Mds Inc. | Improvements in ms/ms methods for a quadrupole/time of flight tandem mass spectrometer |
US6507019B2 (en) | 1999-05-21 | 2003-01-14 | Mds Inc. | MS/MS scan methods for a quadrupole/time of flight tandem mass spectrometer |
US6445939B1 (en) | 1999-08-09 | 2002-09-03 | Lightlab Imaging, Llc | Ultra-small optical probes, imaging optics, and methods for using same |
US6570153B1 (en) | 2000-10-18 | 2003-05-27 | Agilent Technologies, Inc. | Tandem mass spectrometry using a single quadrupole mass analyzer |
DK1217643T3 (da) * | 2000-12-15 | 2009-01-19 | V & F Analyse & Messtechnik | Fremgangsmåde og indretning til vurdering af tilstanden i organismer og naturprodukter samt til analyse af en gasformig blanding med hoved- og bikomponenter |
WO2003103008A1 (en) * | 2002-05-30 | 2003-12-11 | The Johns Hopkins University | Time of flight mass specrometer combining fields non-linear in time and space |
US7372021B2 (en) * | 2002-05-30 | 2008-05-13 | The Johns Hopkins University | Time-of-flight mass spectrometer combining fields non-linear in time and space |
GB2390935A (en) | 2002-07-16 | 2004-01-21 | Anatoli Nicolai Verentchikov | Time-nested mass analysis using a TOF-TOF tandem mass spectrometer |
US7196324B2 (en) | 2002-07-16 | 2007-03-27 | Leco Corporation | Tandem time of flight mass spectrometer and method of use |
US7067803B2 (en) * | 2002-10-11 | 2006-06-27 | The Board Of Trustees Of The Leland Stanford Junior University | Gating device and driver for modulation of charged particle beams |
WO2004068531A1 (de) * | 2003-01-28 | 2004-08-12 | Comet Holding Ag | Time-of-flight massenspektrometer |
JP4928724B2 (ja) * | 2003-10-14 | 2012-05-09 | マイクロマス ユーケー リミテッド | 質量分析計 |
US7385186B2 (en) * | 2005-05-13 | 2008-06-10 | Applera Corporation | Methods of operating ion optics for mass spectrometry |
US7351959B2 (en) * | 2005-05-13 | 2008-04-01 | Applera Corporation | Mass analyzer systems and methods for their operation |
US7405396B2 (en) * | 2005-05-13 | 2008-07-29 | Applera Corporation | Sample handling mechanisms and methods for mass spectrometry |
US7501621B2 (en) * | 2006-07-12 | 2009-03-10 | Leco Corporation | Data acquisition system for a spectrometer using an adaptive threshold |
EP2831904B1 (en) | 2012-03-28 | 2020-01-01 | Ulvac-Phi, Inc. | Apparatus to provide parallel acquisition of mass spectrometry/mass spectrometry data |
US9490114B2 (en) * | 2012-10-10 | 2016-11-08 | Shimadzu Corporation | Time-of-flight mass spectrometer |
CN104392881A (zh) * | 2014-09-30 | 2015-03-04 | 青岛康和食品有限公司 | 一种离子源 |
CN116525402B (zh) * | 2023-05-19 | 2024-07-02 | 暨南大学 | 一种应用于飞行时间质量分析器的离子衰减装置及方法 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2938116A (en) * | 1956-04-02 | 1960-05-24 | Vard Products Inc | Molecular mass spectrometer |
GB1302193A (enrdf_load_stackoverflow) * | 1969-04-18 | 1973-01-04 | ||
US4072862A (en) * | 1975-07-22 | 1978-02-07 | Mamyrin Boris Alexandrovich | Time-of-flight mass spectrometer |
US4458149A (en) * | 1981-07-14 | 1984-07-03 | Patrick Luis Muga | Time-of-flight mass spectrometer |
DE3144604A1 (de) * | 1981-11-10 | 1983-05-19 | Leybold-Heraeus GmbH, 5000 Köln | Vorrichtung zur untersuchung einer probe |
FR2548448B1 (fr) * | 1983-06-28 | 1986-04-25 | Inst Nat Sciences Appliq | Miroir electrostatique de focalisation en temps de vol de particules chargees et son application a la spectrometrie de masse |
US4733073A (en) * | 1983-12-23 | 1988-03-22 | Sri International | Method and apparatus for surface diagnostics |
FR2560434B1 (fr) * | 1984-02-29 | 1987-09-11 | Centre Nat Rech Scient | Spectrometre de masse a temps de vol |
DE3524536A1 (de) * | 1985-07-10 | 1987-01-22 | Bruker Analytische Messtechnik | Flugzeit-massenspektrometer mit einem ionenreflektor |
US4818862A (en) * | 1987-10-21 | 1989-04-04 | Iowa State University Research Foundation, Inc. | Characterization of compounds by time-of-flight measurement utilizing random fast ions |
JPH03503815A (ja) * | 1987-12-24 | 1991-08-22 | ユニサーチ リミテッド | 質量分析計 |
-
1989
- 1989-06-23 DE DE3920566A patent/DE3920566A1/de active Granted
-
1990
- 1990-06-15 EP EP90111293A patent/EP0403965B1/de not_active Expired - Lifetime
- 1990-06-15 DE DE59007546T patent/DE59007546D1/de not_active Expired - Lifetime
- 1990-06-20 US US07/541,140 patent/US5032722A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE3920566C2 (enrdf_load_stackoverflow) | 1993-04-01 |
US5032722A (en) | 1991-07-16 |
EP0403965A3 (de) | 1991-07-31 |
EP0403965A2 (de) | 1990-12-27 |
DE3920566A1 (de) | 1991-01-10 |
DE59007546D1 (de) | 1994-12-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0403965B1 (de) | MS-MS-Flugzeit-Massenspektrometer | |
DE69230174T2 (de) | Flugzeitmassenspektrometer mit einer oeffnung zum ausgleich von uebertragungsvermoegen und aufloesung | |
DE69631556T2 (de) | Biomolekülenanalyse mittels Flugzeitmassenspektrometrie | |
DE10005698B4 (de) | Gitterloses Reflektor-Flugzeitmassenspektrometer für orthogonalen Ioneneinschuss | |
DE19638577C1 (de) | Simultane Fokussierung aller Massen in Flugzeitmassenspektrometern | |
DE112007002747B4 (de) | Verfahren zum Betreiben einer Mehrfachreflektionsionenfalle | |
DE60128419T2 (de) | Flugzeitmassenspektrometer mit auswählbarer Driftlänge | |
DE69419014T2 (de) | Ionenquelle und messenspektrometer mit einer solchen ionenquelle | |
DE10248814B4 (de) | Höchstauflösendes Flugzeitmassenspektrometer kleiner Bauart | |
DE10158924B4 (de) | Pulser für Flugzeitmassenspektrometer mit orthogonalem Ioneneinschuss | |
DE4442348C2 (de) | Verfahren und Vorrichtung zur verbesserten Massenauflösung eines Flugzeit-Massenspektrometers mit Ionenreflektor | |
DE19635643C2 (de) | Verfahren zur Spektrenaufnahme und lineares Flugzeitmassenspektrometer dafür | |
DE4134905A1 (de) | Tandem-massenspektrometer basierend auf flugzeitanalyse | |
DE102011013540A1 (de) | Tandem-Flugzeit-Massenspektrometer | |
DE102013015045A1 (de) | Flugzeit-Massenspektrometer und Verfahren zum Steuern desselben | |
DE10162267B4 (de) | Reflektor für Flugzeitmassenspektrometer mit orthogonalem Ioneneinschuss | |
DE2627085A1 (de) | Ionenstreuspektrometeranalysatoren, die vorzugsweise im tandem angeordnet sind | |
DE19635645C2 (de) | Verfahren für die hochauflösende Spektrenaufnahme von Analytionen in einem linearen Flugzeitmassenspektrometer | |
DE102013015046B4 (de) | Bildgebendes Massenspektrometer und Verfahren zum Steuern desselben | |
DE102007049640B3 (de) | Messung von Tochterionenspektren aus einer MALDI-Ionisierung | |
DE69127989T2 (de) | Massenspektrometer für neutrale gesputterte Atome, die mit Laser ionisiert sind | |
DE10109917B4 (de) | Hoher Durchsatz an Laserdesorptionsmassenspektren in Flugzeitmassenspektrometern | |
DE19636797C2 (de) | Geometrie eines höchstauflösenden linearen Flugzeitmassenspektrometers | |
EP2355129A1 (de) | Reflektor für ein Flugzeitmassenspektrometer | |
WO2006119966A2 (de) | Verfahren und vorrichtungen zum massenselektiven ionentransport |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): DE FR GB |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): DE FR GB |
|
17P | Request for examination filed |
Effective date: 19910719 |
|
17Q | First examination report despatched |
Effective date: 19930811 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE FR GB |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Effective date: 19941026 |
|
REF | Corresponds to: |
Ref document number: 59007546 Country of ref document: DE Date of ref document: 19941201 |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 19950131 |
|
EN | Fr: translation not filed | ||
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed | ||
REG | Reference to a national code |
Ref country code: GB Ref legal event code: IF02 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20090623 Year of fee payment: 20 Ref country code: DE Payment date: 20090626 Year of fee payment: 20 |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: PE20 Expiry date: 20100614 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20100614 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20100615 |