WO1997018579A1 - Low-vacuum mass spectrometer - Google Patents

Low-vacuum mass spectrometer Download PDF

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Publication number
WO1997018579A1
WO1997018579A1 PCT/IL1996/000149 IL9600149W WO9718579A1 WO 1997018579 A1 WO1997018579 A1 WO 1997018579A1 IL 9600149 W IL9600149 W IL 9600149W WO 9718579 A1 WO9718579 A1 WO 9718579A1
Authority
WO
WIPO (PCT)
Prior art keywords
mass spectrometer
beads
drift tube
vacuum
detector
Prior art date
Application number
PCT/IL1996/000149
Other languages
French (fr)
Inventor
Ron Naaman
Zeev Vager
Original Assignee
Yeda Research And Development Co. Ltd.
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Yeda Research And Development Co. Ltd. filed Critical Yeda Research And Development Co. Ltd.
Priority to US09/068,152 priority Critical patent/US5939613A/en
Priority to JP9518722A priority patent/JP2000500275A/en
Priority to EP96935321A priority patent/EP0888633B1/en
Priority to DE69609203T priority patent/DE69609203D1/en
Publication of WO1997018579A1 publication Critical patent/WO1997018579A1/en

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Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J49/00Particle spectrometers or separator tubes
    • H01J49/02Details
    • H01J49/025Detectors specially adapted to particle spectrometers
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J43/00Secondary-emission tubes; Electron-multiplier tubes
    • H01J43/04Electron multipliers
    • H01J43/06Electrode arrangements
    • H01J43/18Electrode arrangements using essentially more than one dynode
    • H01J43/22Dynodes consisting of electron-permeable material, e.g. foil, grid, tube, venetian blind
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J2237/00Discharge tubes exposing object to beam, e.g. for analysis treatment, etching, imaging
    • H01J2237/244Detection characterized by the detecting means
    • H01J2237/2444Electron Multiplier

Definitions

  • the present invention relates to a low-vacuum mass spectrometer, for use as a gas analyzer.
  • MS mass spectrometer
  • MS -6 an electric field in a vacuum of about 10 Torr, mass-selected and than detected by a charge detector (e.g., Faraday cap, electron multiplier or microchannel plate).
  • a charge detector e.g., Faraday cap, electron multiplier or microchannel plate.
  • the high vacuum is essential for the operation of MSs of any type.
  • MSs were modified to include atmospheric pressure ionization capability. In these devices, a pressure transducer is used to reduce the pressure as the ions accelerate towards the detector.
  • IMS Ion Mobility Spectrometer
  • a sample is ionized and is drifted inside a tube kept at a pressure of about 1 atm.
  • the interaction of the ions with the gas in the tube determines its time of arrival at the charge detector.
  • the charge detector is bound to be a Faraday cap, since no other charge detector can operate at atmospheric pressure.
  • the MS is typically a large system operating with expensive and large vacuum pumps.
  • the data obtained is based on the mass of the ions arriving at the detector.
  • the MS is sometimes coupled to gas chromatography (GC).
  • GC gas chromatography
  • the affinity between the analyzed gases and the material in the columns of the GC serves for achieving better analytical capability.
  • the IMS is compact in size and easy to operate. Its operation at atmospheric pressure makes it inexpensive.
  • a second severe drawback is the limited dynamic range. Since the ions are produced at low velocity, space charge limits the number of ions that can be created within the ionizing volume. This is the upper limit on signals that can be obtained. The low sensitivity of the Faraday cap used as the detector puts a lower limit on the number of ions that must be produced for a signal to become measurable. It has been established that, as a result from these two limits, the dynamic range typical for IMS is about 50, much too low for many analytical applications.
  • a low-vacuum mass spectrometer for use as gas analyzer, comprising a drift tube having a gas inlet and an ionization region at one end thereof, a power source for supplying the required high tension, a vacuum pump connectable to said drift tube to maintain a level of vacuum of up to 1 Torr, and a detector located at the other end of said drift tube, wherein said detector is a multisphere plate comprised of a multilayer arrangement of beads bonded together in a substantially close-packing order.
  • the gas to be analyzed is introduced into the ionizing area. It is ionized in a small volume by an ionizer means, such as an electron beam, a radioactive source or a laser.
  • a voltage is applied to a drift tube, through which the ions are moving towards the detector.
  • the drift tube is filled with gas up to a pressure of about 0.1 Torr. While drifting through the tube, the ions can either collide with the gas, whereby their velocity will be reduced, or they can actually react with the gas to form new ions. Passing along the drift tube, the ions impinge on a microsphere plate (MSP) detector which is capable of operating at these low vacuum conditions.
  • MSP microsphere plate
  • the MSP multiplies the signal by several orders of magnitude.
  • the time of flight between the instance of ionization and the instance of arrival at the detector can be measured with high precision, typically better than within 10 nanoseconds. It is the time-of-flight pattern that serves as a fingerprint of the analyzed molecules.
  • Fig. 1 is a schematic representation of the low-vacuum mass spectrometer (LVMS) according to the invention
  • Fig. 3 is a graph, showing the amplification ofthe MSP as a function of pressure.
  • Fig. 1 a schematic representation of the LVMS according to the invention, comprising a drift tube 2 having a gas inlet 4, an ionization region 6, a power source 8 supplying the required high voltage, a connector 10 to a small vacuum pump, several acceleration electrodes 12 (which are optional), and a detector 14 to be described further belou .
  • the sample to be analyzed is introduced into ionization region 6 via inlet 4 in the form of gaseous-phase molecules.
  • region 6 the sampled molecules are ionized by a short pulse of particles or photons.
  • Power source 8 provides a field which accelerates the ions formed in ionization region 6 through dri t tube 2. towards detector 14.
  • a voltage of a few keV is applied, with ionization region 6 biased positively relative to the surface of detector 14.
  • Drift tube 2 can have different lengths, depending on the specific application. Typically, its length is between 10 to 100 cm. It can be filled by different gases that serve either as colliders with the sampled ions or as reactants.
  • the pressure in drift tube 2 might be different than that prevailing near the detector and is kept at the desired value by a small pump.
  • Detector 14 a section of which is illustrated in Fig. 2, is in the form of a microsphere plate (MSP) 16, comprising a multilayer arrangement of spherical beads
  • MSP 16 which serves in fact as an electron multiplier, is configured so that the mean free path of the electrons at the operational pressure prevailing will be larger than the distance the electrons have to before colliding with a surface inside MSP 16. The average space d required
  • the microsphere plate 16 for a typical LVMS is of a thickness of about 0.7 mm and consists of glass beads of a diameter of about 70mm.
  • the outermost layers 20 are provided with metal coats for application of high voltage from a power source 22.
  • a detector of the above- described type is capable of working at pressures of up to about 1 Torr.
  • Fig. 3 is a graph illustrating the dependence of the amplification of the MSP on pressure. It is seen that amplification rises steeply at pressures lower than

Abstract

A low-vacuum mass spectrometer includes a drift tube (2) having a gas inlet (4) and an ionization region (6) at one end thereof; a power source (22) for supplying the required high tension; a vacuum pump port (10) connected to the drift tube (2) to maintain a level of vacuum of up to 1 Torr; and a detector (14) located at the other end of the drift tube (2). The detector (14) is a multisphere plate (16) comprised of a multilayer arrangement of beads (18) bonded together in a substantially close-packing order.

Description

LOW-VACUUM MASS SPECTROMETER Field of the Invention
The present invention relates to a low-vacuum mass spectrometer, for use as a gas analyzer. Background of the Invention
There exist two types of gas analyzers. The first and most commonly used is a mass spectrometer (MS). In the MS, a sample of material is ionized, accelerated by
-6 an electric field in a vacuum of about 10 Torr, mass-selected and than detected by a charge detector (e.g., Faraday cap, electron multiplier or microchannel plate). The high vacuum is essential for the operation of MSs of any type. Recently, MSs were modified to include atmospheric pressure ionization capability. In these devices, a pressure transducer is used to reduce the pressure as the ions accelerate towards the detector.
A second type of gas analyzer is the Ion Mobility Spectrometer (IMS). In the IMS, a sample is ionized and is drifted inside a tube kept at a pressure of about 1 atm. The interaction of the ions with the gas in the tube determines its time of arrival at the charge detector. In this device, the charge detector is bound to be a Faraday cap, since no other charge detector can operate at atmospheric pressure.
Due to the high vacuum requirements, the MS is typically a large system operating with expensive and large vacuum pumps. The data obtained is based on the mass of the ions arriving at the detector. In order to achieve better analytical capability, the MS is sometimes coupled to gas chromatography (GC). In this case, the affinity between the analyzed gases and the material in the columns of the GC serves for achieving better analytical capability.
Unlike the MS, the IMS is compact in size and easy to operate. Its operation at atmospheric pressure makes it inexpensive. Two main problems, however, exist in attempting to use it as a widely used analytical tool. Since it works at atmospheric pressure, the results are difficult to reproduce from place to place and from time to time. This is due to the different pressure depending on height above sea level and weather conditions. A second severe drawback is the limited dynamic range. Since the ions are produced at low velocity, space charge limits the number of ions that can be created within the ionizing volume. This is the upper limit on signals that can be obtained. The low sensitivity of the Faraday cap used as the detector puts a lower limit on the number of ions that must be produced for a signal to become measurable. It has been established that, as a result from these two limits, the dynamic range typical for IMS is about 50, much too low for many analytical applications.
It is thus one of the objects of the present invention to overcome the limits and drawbacks of existing gas analyzers by combining the dynamic range and sensitivity typical of the MS, and the ease of operation and low cost characteristic of the IMS. Summary of he Invention
According to the invention, this is achieved by providing a low-vacuum mass spectrometer for use as gas analyzer, comprising a drift tube having a gas inlet and an ionization region at one end thereof, a power source for supplying the required high tension, a vacuum pump connectable to said drift tube to maintain a level of vacuum of up to 1 Torr, and a detector located at the other end of said drift tube, wherein said detector is a multisphere plate comprised of a multilayer arrangement of beads bonded together in a substantially close-packing order.
In the present device, the gas to be analyzed is introduced into the ionizing area. It is ionized in a small volume by an ionizer means, such as an electron beam, a radioactive source or a laser. A voltage is applied to a drift tube, through which the ions are moving towards the detector. The drift tube is filled with gas up to a pressure of about 0.1 Torr. While drifting through the tube, the ions can either collide with the gas, whereby their velocity will be reduced, or they can actually react with the gas to form new ions. Passing along the drift tube, the ions impinge on a microsphere plate (MSP) detector which is capable of operating at these low vacuum conditions. The MSP multiplies the signal by several orders of magnitude. The time of flight between the instance of ionization and the instance of arrival at the detector can be measured with high precision, typically better than within 10 nanoseconds. It is the time-of-flight pattern that serves as a fingerprint of the analyzed molecules.
The invention will now be described in connection with certain preferred embodiments with reference to the following illustrative figures so that it may be more fully understood.
With specific reference now to the figures in detail, it is stressed that the particulars shown are by way of example and for purposes of illustrative discussion of the preferred embodiments of the present invention only and are presented in the cause of providing what is believed to be the most useful and readily understood description of the principles and conceptual aspects of the invention. In this regard, no attempt is made to show structural details of the invention in more detail than is necessary for a fundamental understanding of the invention, the description taken with the drawings making apparent to those skilled in the art how the several forms ofthe invention may be embodied in practice. Brief Description of the Drawings In the drawings: Fig. 1 is a schematic representation of the low-vacuum mass spectrometer (LVMS) according to the invention; Fig. 2 shows, to a highly enlarged scale, a section of the microsphere plate (MSP) that serves as the detector in the LVMS, and Fig. 3 is a graph, showing the amplification ofthe MSP as a function of pressure. Detailed Description of Preferred Embodiments
Referring now to the drawings, there is seen in Fig. 1 a schematic representation of the LVMS according to the invention, comprising a drift tube 2 having a gas inlet 4, an ionization region 6, a power source 8 supplying the required high voltage, a connector 10 to a small vacuum pump, several acceleration electrodes 12 (which are optional), and a detector 14 to be described further belou .
The sample to be analyzed is introduced into ionization region 6 via inlet 4 in the form of gaseous-phase molecules. Another type of samples is also possible, similarly to what is used in M.S. In region 6, the sampled molecules are ionized by a short pulse of particles or photons. Power source 8 provides a field which accelerates the ions formed in ionization region 6 through dri t tube 2. towards detector 14. Typically, a voltage of a few keV is applied, with ionization region 6 biased positively relative to the surface of detector 14. Drift tube 2 can have different lengths, depending on the specific application. Typically, its length is between 10 to 100 cm. It can be filled by different gases that serve either as colliders with the sampled ions or as reactants. The pressure in drift tube 2 might be different than that prevailing near the detector and is kept at the desired value by a small pump.
Detector 14. a section of which is illustrated in Fig. 2, is in the form of a microsphere plate (MSP) 16, comprising a multilayer arrangement of spherical beads
1 8, advantageously made of glass, which provide secondary emissions 19 when impinged upon by elecrons or other charged particles. When beads 18 are sintered together, a tortuous path is formed between them. MSP 16. which serves in fact as an electron multiplier, is configured so that the mean free path of the electrons at the operational pressure prevailing will be larger than the distance the electrons have to before colliding with a surface inside MSP 16. The average space d required
10 2 between beads 18 depends on the working pressure P, the relation being d < ,
with P in mbar and d in centimeters. Hence, for close packing of spherical beads 18, the latter have to have diameters of the order of d. The microsphere plate 16 for a typical LVMS is of a thickness of about 0.7 mm and consists of glass beads of a diameter of about 70mm. The outermost layers 20 are provided with metal coats for application of high voltage from a power source 22. A detector of the above- described type is capable of working at pressures of up to about 1 Torr.
The above-mentioned tortuous path prevents ion feed-back inside detector 14, while close packing of spherical beads 18 reduces the distance the electron has to travel within detector 14 before encountering a bead surface. It is these two characteristics of MSP 16 acting as detector 14, that enable the arrangement to operate at a low vacuum.
Fig. 3 is a graph illustrating the dependence of the amplification of the MSP on pressure. It is seen that amplification rises steeply at pressures lower than
. - 1
1 Torr, to level off, starting from about 10 Torr. being about 10 for a pressure of 10" Torr.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrated embodiments and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein.

Claims

1. A low-vacuum mass spectrometer for use as gas analyzer, comprising: a drift tube having a gas inlet and an ionization region at one end thereof; a power source for supplying the required high tension; a vacuum pump connectable to said drift tube to maintain a level of vacuum of up to 1 Torr, and a detector located at the other end of said drift tube, wherein said detector is a multisphere plate comprised of a multilayer arrangement of beads bonded together in a substantially close-packing order.
2. The mass spectrometer as claimed in claim 1 , further comprising acceleration electrodes spaced along the inside of said drift tube.
3. In a low-vacuum mass spectrometer, an improvement in the form of a detector consisting of a multilayer plate comprised of a multilayer arrangement of beads banded together in a close- packing order, the bead diameter D of said beads depending on the pressure P prevailing in said drift tube, with D ~ d, according to
10" the relationship d < . where d [cm] is the average space between said beads and
P [mbar] is the pressure.
4. The mass spectrometer as claimed in claim 3, wherein said beads are spherical.
5. The mass spectrometer as claimed in claim 3, wherein said beads are mutually bonded by sintering.
6. The mass spectrometer as claimed in claim 3, wherein at least some of the beads of the outer layers of said microsphere plate are provided with an electrically conductive coat over at least part of their surface, to facilitate application of high tension.
7. The mass spectrometer as claimed in claim 3, wherein the pressure prevailing in said drift tube is up to 1 Torr.
PCT/IL1996/000149 1995-11-14 1996-11-13 Low-vacuum mass spectrometer WO1997018579A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US09/068,152 US5939613A (en) 1995-11-14 1996-11-13 Low-vacuum mass spectrometer
JP9518722A JP2000500275A (en) 1995-11-14 1996-11-13 Low vacuum mass spectrometer
EP96935321A EP0888633B1 (en) 1995-11-14 1996-11-13 Detector in a low-vacuum mass spectrometer
DE69609203T DE69609203D1 (en) 1995-11-14 1996-11-13 DETECTOR IN A LOW VACUUM MASS SPECTROMETER

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IL115984 1995-11-14
IL11598495A IL115984A (en) 1995-11-14 1995-11-14 Low-vacuum mass spectrometer

Publications (1)

Publication Number Publication Date
WO1997018579A1 true WO1997018579A1 (en) 1997-05-22

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ID=11068181

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IL1996/000149 WO1997018579A1 (en) 1995-11-14 1996-11-13 Low-vacuum mass spectrometer

Country Status (6)

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US (1) US5939613A (en)
EP (1) EP0888633B1 (en)
JP (1) JP2000500275A (en)
DE (1) DE69609203D1 (en)
IL (1) IL115984A (en)
WO (1) WO1997018579A1 (en)

Cited By (1)

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WO2000057172A1 (en) * 1999-03-23 2000-09-28 Chao Yan Multiuse pressure electric chromatographic device

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JPH11233060A (en) * 1998-02-17 1999-08-27 Fujitsu Ltd Secondary-electron detector and electron beam device using the same
JPWO2003005408A1 (en) * 2001-07-05 2004-10-28 浜松ホトニクス株式会社 Electron tube and method of manufacturing the same
US6828714B2 (en) 2002-05-03 2004-12-07 Nova Scientific, Inc. Electron multipliers and radiation detectors
US6822225B2 (en) * 2002-09-25 2004-11-23 Ut-Battelle Llc Pulsed discharge ionization source for miniature ion mobility spectrometers
US7183701B2 (en) 2003-05-29 2007-02-27 Nova Scientific, Inc. Electron multipliers and radiation detectors
US7233007B2 (en) * 2004-03-01 2007-06-19 Nova Scientific, Inc. Radiation detectors and methods of detecting radiation
GB201104220D0 (en) 2011-03-14 2011-04-27 Micromass Ltd Ion guide with orthogonal sampling
CN111243938B (en) * 2012-12-31 2023-06-23 九零八图案公司 Mass spectrometer and method for measuring information about a sample using a mass spectrometer
JP2019091700A (en) * 2019-01-04 2019-06-13 908 デバイセズ インク.908 Devices Inc. Compact mass spectrometer

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US5189301A (en) * 1991-08-20 1993-02-23 Cpad Holdings, Ltd. Simple compact ion mobility spectrometer having a focusing electrode which defines a non-uniform field for the drift region
US5591969A (en) * 1995-04-12 1997-01-07 The United States Of America As Represented By The Secretary Of The Navy Inductive detector for time-of-flight mass spectrometers

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GB1434053A (en) * 1973-04-06 1976-04-28 Mullard Ltd Electron multipliers
IL87341A (en) * 1988-08-04 1992-11-15 Yeda Res & Dev Amorphous electron multiplier
US5770859A (en) * 1994-07-25 1998-06-23 The Perkin-Elmer Corporation Time of flight mass spectrometer having microchannel plate and modified dynode for improved sensitivity

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5189301A (en) * 1991-08-20 1993-02-23 Cpad Holdings, Ltd. Simple compact ion mobility spectrometer having a focusing electrode which defines a non-uniform field for the drift region
US5591969A (en) * 1995-04-12 1997-01-07 The United States Of America As Represented By The Secretary Of The Navy Inductive detector for time-of-flight mass spectrometers

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP0888633A4 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000057172A1 (en) * 1999-03-23 2000-09-28 Chao Yan Multiuse pressure electric chromatographic device
US6569325B1 (en) 1999-03-23 2003-05-27 Chao Yan Multiuse pressure electric chromatographic device

Also Published As

Publication number Publication date
IL115984A (en) 1998-08-16
DE69609203D1 (en) 2000-08-10
US5939613A (en) 1999-08-17
EP0888633A1 (en) 1999-01-07
IL115984A0 (en) 1996-01-31
EP0888633A4 (en) 1999-01-27
EP0888633B1 (en) 2000-07-05
JP2000500275A (en) 2000-01-11

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