Field of the invention
[0001] The invention relates to an electron accelerator having a resonant cavity wherein
the electrons are accelerated a plurality of times and according to successive passages
through the cavity, increasing the energy of the electrons after each passage. A typical
example of such an accelerator is a Rhodotron® , which is an electron accelerator
having a single coaxial cavity wherein the electrons are first injected and then accelerated
transversally a plurality of times according to a trajectory having the overall shape
of a flower ("Rhodos" means flower in Greek).
[0002] The invention also relates to a material detection system comprising such an electron
accelerator and to a material irradiation system comprising such an electron accelerator.
Description of prior art
[0003] Such accelerators are known for example from US patent publication number
US-5107221, describing a Rhodotron® which typically includes the following subsystems:
- a resonant cavity presenting two coaxial cylindrical conductors which are shorted
at their ends and which present a plurality of circumferential holes at the level
of their median transversal plane so as to let electrons pass through,
- an electron source which is adapted generate and to inject a beam of electrons into
the cavity following a radial direction in the median transversal plane of the cavity,
- an RF source coupled to the cavity and adapted to generate a transverse electric field
into the cavity for accelerating the electrons of the electron beam a plurality of
times into the median transversal plane and according to successive trajectories following
angularly shifted diameters of the cavity,
- deflection magnets configured for receiving the electron beam after it emerges out
of the cavity and for redirecting the electron beam in the median transversal plane
towards the centre of the cavity, and
- an electron beam output port.
[0004] Such accelerator may for example operate under a continuous wave (CW) mode, which
means that, when in operation, RF power from the RF source is continuously applied
to the cavity and the electron source injects electrons into the cavity by bunches
at the same frequency as the RF frequency, which is typically about 100 MHz to 200
MHz for current commercial Rhodotrons®. Hence, a "continuous wave" of accelerated
electrons is delivered at the electron beam output port of the accelerator.
[0005] Rhodotrons®, such as those which have been commercialized by the applicant for instance,
typically deliver beam energies up to 10 MeV, with maximum beam power ranging from
25 KW to 700 KW.
[0006] Combined with peripheral equipment, such as beam guiding systems, beam focussing
systems, beam scanning systems, and detectors for instance, these kind of accelerators
are currently used for detection and security purposes for instance, such as for the
detection of forbidden or hazardous substances and goods (such as weapons, explosives,
drugs , etc.) which are hidden in containers.
[0007] For these and other applications in particular, it is desired to provide electron
beams at two or more different energies, because this enables to better discriminate
content materials having different atomic numbers.
[0008] International patent publication number
WO03043388 discloses for example a Rhodotron® which is adapted to deliver multiple electron
beams at respectively different energies, such as 7 MeV and 10 MeV for example.
[0009] However, since this accelerator has only a single electron source, it is not capable
of delivering these two beams simultaneously but rather one after the other. Concretely,
with this known accelerator, the 10 MeV beam is output at a first output port for
as long as all deflection magnets are energized, so that the electrons are accelerated
a maximum number of times through the cavity, whereas the 7 MeV beam is output at
a second output port after turning off downstream deflection magnets and for as long
as these downstream deflection magnets are kept off, so that the electrons are accelerated
less than the maximum number of times through the cavity.
[0010] Given the current and future needs of applications using such accelerators , such
as the requirements on detection speed and quality for security applications for instance,
the switching time between the two energies is however too slow with this conventional
technology. This switching time is also too slow for other applications such as for
the irradiation of materials or substances with the electron beams.
Summary of the invention
[0011] It is an object of the invention to provide a an electron accelerator of the recirculating
type which is capable of delivering at least two electron beams at respectively at
least two different energies and in a faster time-interlaced fashion than what known
accelerators of this type are capable to do.
[0012] The invention is defined by the independent claims. The dependent claims define advantageous
embodiments.
[0013] According to the invention, there is provided an electron accelerator comprising
:
- a resonant cavity having an outer conductor and an inner conductor,
- an electron source adapted to generate and to inject a beam of electrons transversally
into the cavity,
- an RF source coupled to the cavity and adapted to generate a resonant transverse electric
field into the cavity between the outer conductor and the inner conductor, so as to
accelerate the electrons of the electron beam a plurality of times into the cavity
and according to successive and different transversal trajectories until it reaches
a main accelerator output,
- beam deflectors arranged outside the cavity, each configured to receive the electron
beam from an exit port of the cavity and to redirect the electron beam according to
a nominal path to an entry port of the cavity,
wherein at least one of the beam deflectors comprises a plurality of beam deflection
magnets arranged in sequence, and wherein said plurality of deflection magnets comprises
a kicker magnet configured to deviate the electron beam away from said nominal path
towards an intermediate accelerator output.
[0014] Thanks to the kicker magnet - which can be made much smaller and much faster than
the other beam deflection magnets of the beam deflector - it becomes indeed possible
and at a faster pace to :
- deviate, for a first period of time, the electron beam from its nominal path before
it has made further or all acceleration passes through the cavity, thereby delivering,
to the intermediate accelerator output, a first electron beam at a first energy during
the first period of time,
and to
- not deviate, for a second period of time, the electron beam from its nominal path
before it has made further or all passes through the cavity, thereby delivering, to
a further intermediate accelerator output or to the main accelerator output, a second
electron beam at a second energy during the second period of time, different from
said first period of time, said second energy being higher than the first energy.
[0015] An electron accelerator according to the invention is therefore capable of delivering
at least two electron beams at respectively at least two different energies in a fast
time-interlaced fashion.
[0016] Preferably, the electron accelerator further comprises a control unit configured
to repeatedly switch the kicker magnet ON and OFF. More preferably, the control unit
is configured to repeatedly switch the kicker magnet ON and OFF with a minimum time
between two successive ON states which is less than 1/10 sec, preferably less than
1/100 sec, more preferably less than 2/1000 sec.
[0017] Preferably, the kicker magnet is configured to provide - when energized - a beam
bending angle smaller than 90°, preferably a beam bending angle comprised between
1 °and 20°, more preferably a beam bending angle comprised between 3° and 15°. With
such a small bending angle, the kicker magnet can be made small and can have fast
switching capabilities.
[0018] Preferably:
- the outer conductor and the inner conductor are coaxial cylindrical conductors of
axis A, both cylindrical conductors being shorted at their distal ends with respectively
a top conductive closure and a bottom conductive closure (14),
- the electron source is adapted to inject the beam of electrons into the cavity following
a radial direction in a median transversal plane of the cavity,
- the RF source is adapted to generate the transverse electric field into said cavity
so as to accelerate the electrons of the electron beam a plurality of times into the
median transversal plane and according to successive trajectories following angularly
shifted diameters of the outer cylindrical conductor, and
- the nominal path is in the median transversal plane.
[0019] Such kind of accelerator, sometimes called a Rhodotron®, is particularly well suited
to achieve the aforementioned object of the invention.
[0020] More preferably, the kicker magnet is configured to deviate the electron beam away
from said nominal path and towards the intermediate accelerator output while said
kicker magnet is switched ON by the control unit.
[0021] Such a configuration requires indeed the least modifications to the design of a conventional
accelerator. One can for instance place the kicker magnet upstream or downstream of
a conventional beam deflector without too many changes to the conventional beam deflector.
[0022] Even more preferably, the kicker magnet is the first deflection magnet in the sequence
of deflection magnets. With such a configuration, the required beam deflection angle
of the kicker magnet can be made smaller than with other configurations.
Short description of the drawings
[0023] These and further aspects of the invention will be explained in greater detail by
way of example and with reference to the accompanying drawings in which:
- Fig.1
- schematically shows an axial cross section of an electron accelerator according to
the invention;
- Fig.2
- schematically shows a transversal cross section of the electron accelerator of Fig.1,
according to a first embodiment;
- Fig.2a
- schematically shows a transversal cross section of the electron accelerator of Fig.1,
according to a preferred first embodiment;
- Fig.3
- schematically shows a transversal cross section of the electron accelerator of Fig.1,
according to a second embodiment;
- Fig.4
- schematically shows a transversal cross section of the electron accelerator of Fig.1,
according to a third embodiment;
- Fig.5a
- shows exemplary time diagrams for various beam and magnet currents in case of the
accelerators of Figs. 2, 2a, 3 and 4 when these accelerators operate in continuous
wave mode.
- Fig.5b
- shows exemplary time diagrams for various beam and magnet currents in case of the
accelerators of Figs. 2, 2a, 3 and 4 when these accelerators operate in pulsed mode.
- Fig.6
- schematically shows a transversal cross section of the electron accelerator of Fig.1,
according to a fourth embodiment;
- Fig.7
- schematically shows a transversal cross section of the electron accelerator of Fig.1,
according to a fifth embodiment;
- Fig.8a
- shows exemplary time diagrams for various beam and magnet currents in case of the
accelerators of Figs. 6 and 7 when these accelerators operate in continuous wave mode.
- Fig.8b
- shows exemplary time diagrams for various beam and magnet currents in case of the
accelerators of Figs. 6 and 7 when these accelerators operate in pulsed mode.
- Fig.9
- schematically shows a part of a material detection system according to the invention.
- Fig.10
- schematically shows a part of a material irradiation system according to the invention.
[0024] The figures are not drawn to scale. Generally, similar or identical components are
denoted by the same reference numerals in the figures.
Detailed description of preferred embodiments of the invention
[0025] Fig.1 schematically shows an axial cross section of an electron accelerator (1) according
to the invention and comprising :
- a resonant cavity (10) having a cylindrical outer conductor (11) and a coaxial cylindrical
inner conductor (12) of axis A, both cylindrical conductors being shorted at their
distal ends with respectively a top conductive closure (13) and a bottom conductive
closure (14),
- an electron source (20) adapted to generate and to inject a beam of electrons (40)
into the resonant cavity (10) following a radial direction in a median transversal
plane (MP) of the resonant cavity (10),
- an RF source (50) coupled to the resonant cavity (10) and adapted to generate a transverse
electric field (E) into the resonant cavity (10) between the outer conductor (11)
and the inner conductor (12), so as to accelerate the electrons of the electron beam
(40) a plurality of times into the median transversal plane (MP), into the cavity
(10) and according to successive trajectories following angularly shifted diameters
of the outer cylindrical conductor (11), until they reach an accelerator output (41
a, 42a),
- beam deflectors (30) arranged outside the resonant cavity (10), each configured to
receive the electron beam from an exit port (15) of the cavity (10) and to redirect
the electron beam according to a nominal path to an entry port (16) of the resonant
cavity (10), said nominal path being in the median transversal plane (MP).
[0026] Such an electron accelerator (1) is sometimes called a "Rhodotron®" and is basically
well known in the art. Other types of accelerators, such as recirculating Linacs for
example, may also be used.
[0027] Attention will now be drawn more specifically to the beam deflectors (30) and to
their control unit (90).
[0028] In an accelerator according to the invention, at least one of the beam deflectors
(30) comprises a plurality of beam deflection magnets arranged in sequence. Said plurality
of beam deflection magnets comprises a kicker magnet (80) configured to deviate the
electron beam (40) away from said nominal path towards an intermediate accelerator
output (41 a) for use by an application such as those described hereafter for example
(material detection or material irradiation).
[0029] The electron accelerator (1) preferably further comprises a control unit (90) configured
to repeatedly switch said kicker magnet (80) ON and OFF. Preferably, the control unit
(90) is configured to repeatedly switch said kicker magnet (80) ON and OFF with a
minimum time between two successive ON states which is less than 1/10 sec, preferably
less than 1/100 sec, more preferably less than 2/1000 sec.
[0030] Such control unit (90) may for example comprise a pulse generator and a current amplifier,
the current amplifier being steered by the pulse generator and delivering a pulsed
excitation current to the kicker magnet (current I
k, as can be seen on Figs. 5a, 5b, 8a, and 8b). The control unit (90) may alternatively
be a programmable current source. An exemplary programmable current source is the
GMW-231 HC bipolar current amplifier commercialized by GMW Associates, which allows
for USB or direct analogue programming of the current output.
[0031] Fig.2 schematically shows a transversal cross section of the electron accelerator
(1) of Fig.1, and according to a first embodiment.
[0032] In this exemplary first embodiment, the outer cylindrical conductor (11) of the cavity
(10) comprises four beam entry ports and four beam exit ports, as well as thee beam
deflectors (30) arranged outside the cavity (10), each beam deflector (30) being configured
to receive the electron beam from an exit port (15) of the cavity (10) and to redirect
the electron beam according to a nominal path towards an entry port (16) of the cavity
(10), as shown on Fig.2. The nominal path of the electron beam (40) is indicated by
a dashed line starting from the electron source (20) and ending at the main accelerator
output (42a). Obviously, the accelerator may comprise more than three beam deflectors
(30) or less than three beam deflectors (30), and, accordingly, more or less than
four entry and exit ports in the outer conductor (11).
[0033] As shown on Fig.2 and encircled by a long-dashed line, one of the beam deflectors
(30) comprises two beam deflection magnets arranged in sequence: a kicker magnet (80),
followed by a main magnet (81). The kicker magnet (80) and the main magnet (81) are
preferably electromagnets. The kicker electromagnet (80) may use either a standard
iron-laminated yoke or a ferrite-based yoke, the latter being known to be more suitable
at higher switching frequencies because it generates less Eddy currents.
[0034] The kicker magnet (80) is preferably placed in the straight path of the electron
beam (40) after leaving the exit port (15) of the cavity (10) and is arranged and
designed in such a way that, when it is switched OFF by the control unit (90), the
electron beam (40) will simply pass through it without deviation and will continue
its straight trajectory towards the main magnet (81) which will then redirect the
electron beam (40) towards the corresponding entry port (16) of the cavity (10) for
further acceleration into the cavity. Hence, for as long as the kicker magnet (80)
remains switched OFF, the electron beam (40) will continue its trajectory towards
the main accelerator output (42a) and therefore make a total of four acceleration
passes through the cavity (10) in the present example. For as long as the kicker magnet
(80) remains switched OFF, the main accelerator output (42a) will therefore deliver
a second electron beam (42) at an energy corresponding to these four successive acceleration
passes.
[0035] The kicker magnet (80) is furthermore arranged and designed in such a way that, when
it is switched ON by the control unit (90), it will generate a magnetic field which
will deviate the electron beam away from said nominal trajectory towards an intermediate
accelerator output (41 a), as shown by a dashed-dotted line on Fig.2. Hence, for as
long as the kicker magnet (80) remains switched ON, the electron beam will make a
total of only two acceleration passes through the cavity (10) in the present example.
For as long as the kicker magnet (80) remains switched ON, the intermediate accelerator
output (41 a) will therefore deliver a first electron beam (41) at an energy corresponding
to these two successive acceleration passes.
[0036] This accelerator is therefore capable of delivering two electron beams at respectively
two accelerator outputs (intermediate output and main output) and at respectively
two different energies, in a fast time-interlaced fashion.
[0037] In the example of Fig.1 and Fig.2, the main magnet (81), when energized, provides
a total beam bending angle of 225°, whereas the kicker magnet (80), when energized,
provides a beam bending angle much smaller than 225°. In all embodiments of the present
invention, the kicker magnet (80) is preferably configured to provide, when energized,
a beam bending angle smaller than 90°, preferably a beam bending angle comprised between
1 °and 20°, more preferably a beam bending angle comprised between 3°and 15°.
[0038] It is to be noted that the main magnet (81) may be in one part, as shown on Fig.2,
or in several successive parts, as will be described in relation to Fig.4 for example.
[0039] Fig.2a schematically shows a transversal cross section of the electron accelerator
of Fig.1, according to a preferred first embodiment. It is similar to the embodiment
shown on Fig.2, except that, in this preferred first embodiment, the kicker magnet
(80) and the main magnet (81) are arranged and configured in such a way that the first
electron beam (41), i.e. the electron beam leaving the kicker magnet (80) when the
kicker magnet (80) is ON, falls under the influence of the magnetic field generated
by the main magnet (81). In other words, the kicker magnet (80) and the main magnet
(81) are arranged and configured in such a way that the first electron beam (41),
passes between the poles of the main magnet (81) for at least a part of its trajectory
for as long as the kicker magnet (80) is ON. To achieve this, and as illustrated on
Fig.2a, one may for example make the poles of the main magnet wider than they are
in the case of Fig.2, and/or by placing the main magnet (81) closer to the kicker
magnet (80).
[0040] Hence, the first electron beam (41) will be bent by said magnetic field of the main
magnet after said first electron beam (41) has left the excited kicker magnet. Such
a preferred configuration allows to redirect the first electron beam (41) to a direction
which is different than the direction it had when leaving the kicker magnet (80),
yet without requiring extra beam bending magnets. The main magnet therefore has a
double function in this preferred first embodiment: it bends the electron beam back
to the entry port (16) of the cavity for further acceleration into the cavity while
the kicker magnet is OFF, and it deviates the electron beam to a different direction
than the direction it had when leaving the kicker magnet while the kicker magnet is
ON.
[0041] Fig.3 schematically shows a transversal cross section of the electron accelerator
(1) of Fig.1, according to a second embodiment. This second embodiment is similar
to the first embodiment, except that the kicker magnet (80) is in this case placed
after (downstream of) the main magnet (81) instead of before (upstream of) the main
magnet.
[0042] Fig.4 schematically shows a transversal cross section of the electron accelerator
(1) of Fig.1, according to a third embodiment. This third embodiment is similar to
the first embodiment, except that the main magnet is divided into two parts (81 a,
81 b) and except that the kicker magnet (80) is in this case placed in the beam path
between these two parts of the main magnet. In this example, the two parts (81 a,
81 b) of the main magnet are arranged symmetrically and each part provides a total
beam bending angle of 112,5 °, but many other configurations in two or more parts
of the main magnet may of course be used.
[0043] In the case of this third embodiment, and by analogy with the configuration illustrated
in Fig.2a, the kicker magnet (80) and the second part (81 b) of the main magnet (81)
are preferably arranged and configured in such a way that the first electron beam
(41), i.e. the electron beam leaving the kicker magnet (80) when the kicker magnet
(80) is ON, falls under the influence of the magnetic field generated by the said
second part (81 b) of the main magnet (81). In other words, the kicker magnet (80)
and the second part (81 b) of the main magnet (81) are arranged and configured in
such a way that the first electron beam (41), passes between the poles of the second
part (81 b) of the main magnet (81) for at least a part of its trajectory for as long
as the kicker magnet (80) is ON.
[0044] To achieve this, one may for example make the poles of the second part (81 b) of
the main magnet (81) wider than they are in the case of Fig.4, and/or by placing the
main magnet (81) closer to the second part (81 b) of the main magnet (81). Hence,
the first electron beam (41) will be bent by said magnetic field of the second part
(81 b) of the main magnet (81) after said first electron beam (41) has left the excited
kicker magnet.
[0045] Such a preferred configuration allows to redirect the first electron beam (41) to
a direction which is different than the direction it had when leaving the kicker magnet
(80), yet without requiring extra beam bending magnets. The second part (81 b) of
the main magnet (81) therefore has a double function in this preferred third embodiment:
it bends the electron beam back to the entry port (16) of the cavity for further acceleration
into the cavity while the kicker magnet is OFF, and it deviates the electron beam
to a different direction than the direction it had when leaving the kicker magnet
while the kicker magnet is ON.
[0046] Fig.5a shows exemplary time diagrams for various beam and magnet currents in case
of the accelerators of Figs. 2, 2a, 3 and 4, when these accelerators operate in continuous
wave (CW) mode.
[0047] The first time diagram shows the excitation current (I
k) of the kicker magnet (80) over time. This excitation current is provided by the
control unit (90). In the present example, the excitation current is periodic and
has a frequency f
k, but it may as well be aperiodic.
[0048] The second time diagram shows the electron beam current (I
0) at an output of the electron source (20). For clarity reasons, this diagram does
not show a possible microstructure in this beam current. With actual commercial Rhodotrons®,
the electron source (20) injects indeed electrons into the cavity (10) by bunches
at the same frequency as the RF frequency, which is typically about 100 MHz to 200
MHz.
[0049] The third time diagram shows the electron beam current (I
1) at the intermediate accelerator output (41 a).
[0050] The fourth time diagram shows the electron beam current (I
2) at the main accelerator output (42a).
[0051] Since the excitation current (I
k) of the kicker magnet (80) is periodic in the present example, the electron beam
current at the intermediate accelerator output (I
1) and at the main accelerator output (I
2) will also be periodic and at the same frequency f
k.
[0052] Obviously, the duty cycle of the excitation current (I
k) of the kicker magnet (80) will determine the pulse duration at the intermediate
accelerator output (TP1) and at the main accelerator output (TP2).
[0053] Fig.5b shows exemplary time diagrams for various beam and magnet currents in case
of the accelerators of Figs. 2, 2a, 3 and 4, when these accelerators operate in pulsed-mode.
A pulsed-mode accelerator has for example been described in patent publication number
WO2014184306A1, which is incorporated herein by reference.
[0054] The first time diagram shows the excitation current (I
k) of the kicker magnet (80) over time. This excitation current is provided by the
control unit (90). In the present example, the excitation current is periodic and
has a frequency f
k, but it may as well be aperiodic.
[0055] The second time diagram shows the electron beam current (I
0) at an output of the electron source (20). Again for clarity reasons, this diagram
does not show a possible microstructure in this beam current. In the present example,
the electron beam current is periodic and has a frequency f
0 with a pulse duration TP
0, but it may as well be aperiodic.
[0056] The third time diagram shows the electron beam current (I
1) at the intermediate accelerator output (41 a).
[0057] The fourth time diagram shows the electron beam current (I
2) at the main accelerator output (42a).
[0058] Since the excitation current (I
k) of the kicker magnet (80) is periodic in the present example, the electron beam
current at the intermediate accelerator output (I
1) and at the main accelerator output (I
2) will also be periodic and at the same frequency f
k.
[0059] Obviously, the pulse duration (TP
0) of the electron beam current (I
0) will determine the pulse duration at the intermediate accelerator output (41 a)
and at the main accelerator output (42a).
[0060] Obviously, the duty cycle of the excitation current (I
k) of the kicker magnet (80) will determine the interlacing patterns of the electron
beam current (I
1) at the intermediate accelerator output (41 a) and the electron beam current (I
2) at the main accelerator output (42a).
[0061] Fig.6 schematically shows a transversal cross section of the electron accelerator
(1) of Fig.1, according to a fourth embodiment.
[0062] This fourth embodiment is similar to the first embodiment, except that the kicker
magnet (80) is arranged and controlled differently.
[0063] The kicker magnet (80) is placed in the trajectory of the electron beam (40) leaving
the exit port (15) of the cavity (10) and it is in this case arranged and designed
in such a way that, when it is switched ON by the control unit (90), the electron
beam will be deviated towards the main magnet (81) which will then redirect the beam
towards the corresponding entry port (16) of the cavity (10) for further acceleration
into the cavity. Hence, for as long as the kicker magnet (80) remains switched ON,
the electron beam will continue its trajectory towards the main accelerator output
(42a) and therefore make a total of four acceleration passes through the cavity (10)
in the present example. The main accelerator output (42a) will therefore deliver a
second electron beam (42) at an energy corresponding to these four successive acceleration
passes, for as long as the kicker magnet (80) remains switched ON.
[0064] The kicker magnet (80) is furthermore arranged and designed in such a way that, when
it is switched OFF by the control unit (90), the electron beam will simply pass through
it without deviation and continue a straight trajectory towards the intermediate accelerator
output (41 a), as shown by a dashed-dotted line on Fig.6. Hence, for as long as the
kicker magnet (80) remains switched OFF, the electron beam makes a total of only two
acceleration passes through the cavity (10) in the present example. The intermediate
accelerator output (41 a) will therefore deliver a first electron beam (41) at an
energy corresponding to these two successive acceleration passes, for as long as the
kicker magnet (80) remains switched OFF.
[0065] This electron accelerator is therefore also capable of delivering two electron beams
at respectively two accelerator outputs (main output and intermediate output) and
at respectively two different energies, in a fast time-interlaced fashion.
[0066] In the case of this fourth embodiment, and again by analogy with the configuration
illustrated in Fig.2a, the kicker magnet (80) and the main magnet (81) are preferably
arranged and configured in such a way that the first electron beam (41), i.e. the
electron beam leaving the kicker magnet (80) when the kicker magnet (80) is OFF, falls
under the influence of the magnetic field generated by the main magnet (81), so that
the first electron beam (41) will be bent by said magnetic field after said first
electron beam (41) has left the unexcited kicker magnet. In other words, the kicker
magnet (80) and the main magnet (81) are arranged and configured in such a way that
the first electron beam (41), passes between the poles of the main magnet (81) for
at least a part of its trajectory for as long as the kicker magnet (80) is OFF. To
achieve this, one may for example make the poles of the main magnet wider than they
are in the case of Fig.6, and/or by placing the main magnet (81) closer to the kicker
magnet (80). Hence, the first electron beam (41) will be bent by said magnetic field
of the main magnet after said first electron beam (41) has left the unexcited kicker
magnet.
[0067] Fig.7 schematically shows a transversal cross section of the electron accelerator
(1) of Fig.1, according to a fifth embodiment.
[0068] This fifth embodiment is similar to the fourth embodiment shown in Fig.6, except
that the kicker magnet (80) is placed after (downstream of) the main magnet (81) in
this case.
[0069] Fig.8a shows exemplary time diagrams for various beam and magnet currents in case
of the accelerators of Figs. 6 and 7, when these accelerators operate in continuous
wave mode. The order of the time diagrams and the symbols used are the same as in
Fig. 5a.
[0070] Fig.8b shows exemplary time diagrams for various beam and magnet currents in case
of the accelerators of Figs. 6 and 7, when these accelerators operate in pulsed mode.
The order of the time diagrams and the symbols used are the same as in Fig. 5b.
[0071] In any embodiment of the accelerator according to the invention, the control unit
(90) is preferably configured to vary the time during which the kicker magnet (80)
is switched ON and/or to vary the time during which the kicker magnet (80) is switched
OFF. A pulse width modulator can be used for this purpose for instance. This allows
to change the duty cycle and hence the interlacing patterns at the accelerator outputs.
[0072] Furthermore, in case the control unit (90) is configured to repeatedly switch the
kicker magnet (80) ON and OFF in a periodic fashion at a switching frequency, the
control unit (90) is preferably adapted to vary said switching frequency.
[0073] Preferably, the RF source (50) is adapted to energize the cavity (10) at a nominal
RF frequency which is higher than 50MHz and lower than 500 MHz.
[0074] An electron accelerator (1) according to the invention may be used for various purposes.
It may for example be used for the detection of hidden and/or forbidden and/or hazardous
substances and/or goods - such as weapons, explosives, drugs , etc - from an image
formed either directly by the accelerated electrons or indirectly, for example by
X-rays produced by said electrons after hitting a metal target for instance. It may
also be used for the irradiation of substances by the electron beams, for example
for sterilization purposes, such as food sterilization.
[0075] Fig.9 schematically shows a part of a material detection system according to the
invention. It comprises an electron accelerator (1) according to the invention as
described herein and which is hence adapted to produce and output in a fast time-interlaced
fashion:
- a first electron beam (41) at a first energy, at an intermediate accelerator output
(41 a), and
- a second electron beam (42) at a second energy, at a main accelerator output (42a),
the first energy being smaller than the second energy.
[0076] The material detection system further comprises a first RX conversion target (102)
and a second RX conversion target (102) arranged respectively in the paths of the
first and second electron beams coming from respectively the main and the intermediate
accelerator outputs. An RX conversion target is for example a material plate which
converts impinging energetic electrons into X-Rays by the so-called "Bremsstrahlung"
effect.
[0077] The material detection system further comprises a first RX detector (110) and a second
RX detector (120) arranged respectively in the paths of the X-rays generated respectively
by the first and the second RX conversion targets (101, 102) when bombarded by respectively
the first and second electron beams. When the material detection system is in operation,
a container (500) - whose material content is to be inspected - may for example be
moved in translation between the conversion targets and the detectors, as indicated
by a plain arrow on Fig. 9. Analysis and/or imaging of the signals delivered by the
RX detectors (110, 120) allows to detect materials contained into the container (500).
Obviously, the material detection system may also comprise other known subsystems
such as electron beam benders, scanners and/or shapers, which are not illustrated
for the sake of clarity.
[0078] Fig.10 schematically shows a part of a material irradiation system according to the
invention. It comprises an electron accelerator (1) according to the invention as
described herein and which is hence adapted to produce and output in a fast time-interlaced
fashion:
- a first electron beam (41) at a first energy, at an intermediate accelerator output
(41 a), and
- a second electron beam (42) at a second energy, at a main accelerator output (42a),
the first energy being smaller than the second energy.
[0079] The first electron beam (41) is directed to a first material product to be irradiated
(601), whereas the second electron beam (42) is directed to a second material product
to be irradiated (602).
[0080] These material products (601, 602) may for example be food products, which will be
sterilized after having been irradiated by the electron beams (41, 42). Complete irradiation
of the material products may be achieved by moving these products across the electron
beams or by scanning or spreading the electron beams over the products or by any other
equivalent means.
[0081] Obviously, the material irradiation system may also comprise other known subsystems
such as electron beam benders, scanners and/or shapers, which are not illustrated
for the sake of clarity.
[0082] Many other system configurations making use of an electron accelerator (1) according
to the invention may of course be envisaged. One may for example conceive a hybrid
system wherein the first electron beam (41) (i.e. the low energy beam) is directed
to a material product to be irradiated, as partly shown in Fig.10 for example, and
wherein the second electron beam (42) (i.e. the high energy beam) is directed to an
RX conversion target for material detection purposes, as partly shown in Fig.9 for
example, or vice versa.
[0083] In the examples given hereinabove, only one of the beam deflectors (30) comprises
a kicker magnet (80) and the accelerator comprises consequently two electron beam
outputs - one intermediate output and one main output - providing two electron beams
at respectively two different energies.
[0084] The invention nevertheless also provides an accelerator wherein more than one beam
deflector (30) comprises a kicker magnet (80), thereby providing more than one intermediate
output in addition to the main output (42a), and therefore being adapted to deliver
more than two electron beams at respectively more than two different energies. In
such a case, the control unit (90) is configured to repeatedly and alternatively switch
these kicker magnets ON and OFF, with a minimum time between two successive ON states
of a given kicker magnet which is less than 1/10 sec, preferably less than 1/100 sec,
preferably less than 2/1000 sec. Preferably only one kicker magnet is switched ON
at a time by the control unit (90) in case of the embodiments of Figs. 2, 3 and 4,
whereas preferably only one kicker magnet is switched OFF at a time by the control
unit (90) in case of the embodiments of Figs. 6 and 7.
[0085] In any embodiment of the electron accelerator (1) according to the invention, the
main magnet(s) (81, 81 a, 81 b) of a beam deflector (30) is (are) preferably kept
permanently switched ON while the accelerator accelerates electrons towards any of
its outputs (41 a, 42a), i.e. while the kicker magnet (80) is switched ON and OFF.
The main magnet(s) are those beam deflection magnets of a beam deflector (30) which
are not kicker magnets (80). Switching the main magnet(s) ON and keeping them switched
ON while the kicker magnet (80) is switched ON and OFF, may be performed by the control
unit (90) which controls the kicker magnet(s) (80) or by any other control unit. An
advantage of this preferred feature is that the magnetic field(s) of the main magnet(s)
can be stabilized once, generally at the start-up of the accelerator, and remain stable
for the operation time of the accelerator, so that the switching rate between the
different accelerator outputs will depend mainly on the switching rate capacity of
the kicker magnet(s).
[0086] The present invention has been described in terms of specific embodiments, which
are illustrative of the invention and not to be construed as limiting. Reference numerals
in the claims do not limit their protective scope.
[0087] Use of the verbs "to comprise", "to include", "to be composed of", or any other variant,
as well as their respective conjugations, does not exclude the presence of elements
other than those stated.
[0088] Use of the article "a", "an" or "the" preceding an element does not exclude the presence
of a plurality of such elements.
[0089] Summarized, the invention may also be described as follows: an electron accelerator
having a resonant cavity (10), an electron source (20) for injecting a beam of electrons
(40) into the cavity, an RF source (50) adapted to generate an electric field (E)
into the cavity for accelerating the electrons (40) a plurality of times inside the
cavity according to angularly shifted trajectories up to a main accelerator output
(42a), and beam deflectors (30) arranged outside the cavity and configured to redirect
outgoing electrons back into the cavity for further acceleration into the cavity.
At least one of the beam deflectors (30) comprises a plurality of deflection magnets
arranged in sequence and including a kicker magnet (80) configured to deviate the
electron beam from a nominal trajectory and towards an intermediate accelerator output
(41 a). The electron accelerator preferably also comprises a control unit (90), which
is configured to repeatedly switch the kicker magnet ON and OFF with a minimum time
between two successive ON states which is less than 1/10 sec, preferably less than
1/100 sec, more preferably less than 2/1000 sec.
1. Electron accelerator comprising :
- a resonant cavity (10) having an outer conductor (11) and an inner conductor (12),
- an electron source (20) adapted to generate and to inject a beam of electrons (40)
transversally into the cavity (10),
- an RF source (50) coupled to the cavity (10) and adapted to generate a transverse
electric field (E) into the cavity between the outer conductor and the inner conductor
so as to accelerate the electrons of the electron beam a plurality of times into the
cavity and according to successive and different transversal trajectories until it
reaches a main accelerator output (42a),
- beam deflectors (30) arranged outside the cavity (10) and each configured to receive
the electron beam from an exit port (15) of the cavity and to redirect the electron
beam according to a nominal path to an entry port (16) of the cavity,
characterized in that at least one of the beam deflectors (30) comprises a plurality of beam deflection
magnets arranged in sequence, said plurality of deflection magnets comprising a kicker
magnet (80) configured to deviate the electron beam away from said nominal path towards
an intermediate accelerator output (41 a).
2. Electron accelerator according to claim 1, characterized in that it further comprises a control unit (90) configured to repeatedly switch the kicker
magnet (80) ON and OFF.
3. Electron accelerator according to claim 2, characterized in that the control unit (90) is configured to repeatedly switch the kicker magnet (80) ON
and OFF with a minimum time between two successive ON states which is less than 1/10
sec, preferably less than 1/100 sec, more preferably less than 2/1000 sec.
4. Electron accelerator according to any of claims 1 to 3, characterized in that the kicker magnet (80) is configured to provide a beam bending angle smaller than
90°, preferably a beam bending angle comprised between 1 °and 20°, more preferably
a beam bending angle comprised between 3°and 15°.
5. Electron accelerator according to any of claims 1 to 4,
characterized in that:
- the outer conductor (11) and the inner conductor (12) are coaxial cylindrical conductors
of axis A, both cylindrical conductors being shorted at their distal ends with respectively
a top conductive closure (13) and a bottom conductive closure (14),
- the electron source (20) is adapted to inject the beam of electrons (40) into the
cavity (10) following a radial direction in a median transversal plane (MP) of the
cavity (10),
- the RF source (50) is adapted to generate the transverse electric field (E) into
said cavity so as to accelerate the electrons of the electron beam (40) a plurality
of times into the median transversal plane (MP) and according to successive trajectories
following angularly shifted diameters of the outer cylindrical conductor (11),
- the nominal path is in the median transversal plane (MP);
6. Electron accelerator according to any of claims 1 to 5, characterized in that the kicker magnet (80) is configured to deviate the electron beam away from said
nominal path towards the intermediate accelerator output (41 a) while said kicker
magnet is switched ON.
7. Electron accelerator according to claim 6,
characterized in that said plurality of deflection magnets of the at least one of the beam deflectors (30)
comprises a main deflection magnet (81, 81 b) arranged downstream of the kicker magnet
(80) and
in that said main deflection magnet (81, 81 b) is configured:
- to receive the electron beam from the kicker magnet and to redirect the received
electron beam according to the nominal path to the entry port (16) of the cavity while
the kicker magnet is switched OFF, and
- to receive the electron beam from the kicker magnet and to redirect the received
electron beam to another direction while the kicker magnet is switched ON.
8. Electron accelerator according to any of claims 1 to 5, characterized in that the kicker magnet (80) is configured to deviate the electron beam away from said
nominal path towards the intermediate accelerator output (41 a) while said kicker
magnet switched OFF.
9. Electron accelerator according to claim 8,
characterized in that said plurality of deflection magnets of the at least one of the beam deflectors (30)
comprises a main deflection magnet (81, 81 b) arranged downstream of the kicker magnet
(80) and
in that said main deflection magnet (81, 81 b) is configured:
- to receive the electron beam from the kicker magnet and to redirect the received
electron beam according to the nominal path to the entry port (16) of the cavity while
the kicker magnet is switched ON, and
- to receive the electron beam from the kicker magnet and to redirect the received
electron beam to another direction while the kicker magnet is switched OFF.
10. Electron accelerator according to any of preceding claims, characterized in that the kicker magnet (80) is the first deflection magnet in said sequence of deflection
magnets.
11. Electron accelerator according to any of preceding claims, characterized in that the control unit (90) is configured to vary the time during which the kicker magnet
(80) is switched ON and/or to vary the time during which the kicker magnet (80) is
switched OFF.
12. Electron accelerator according to any of preceding claims, characterized in that the control unit (90) is configured to repeatedly switch the kicker magnet (80) ON
and OFF in a periodic fashion at a switching frequency.
13. Electron accelerator according to any of preceding claims, characterized in that the control unit (90) is configured to keep the beam deflection magnets of a beam
deflector, other than the kicker magnets, permanently switched ON while the kicker
magnet (80) is switched ON and OFF.
14. Material detection system comprising an electron accelerator (1) according to any
of preceding claims, a first RX conversion target (101) and a second RX conversion
target (102) arranged in the paths (41, 42) of the electron beams coming from respectively
the intermediate and the main accelerator outputs (41 a, 42a), a first RX detector
(110) and a second RX detector (120) arranged in the paths of the X-rays generated
respectively by the first and the second RX conversion targets (101, 102).
15. Material irradiation system comprising an electron accelerator (1) according to any
of preceding claims, said electron accelerator being configured for irradiating a
material product (600) with the electron beam coming from the main accelerator output
(42a) and/or from the intermediate accelerator output (41 a).