U.S. patent number 3,720,828 [Application Number 05/064,734] was granted by the patent office on 1973-03-13 for apparatus for and method of controlling relativistic charged particle beam distribution and transport.
This patent grant is currently assigned to Energy Sciences, Inc.. Invention is credited to Sam V. Nablo.
United States Patent |
3,720,828 |
Nablo |
March 13, 1973 |
APPARATUS FOR AND METHOD OF CONTROLLING RELATIVISTIC CHARGED
PARTICLE BEAM DISTRIBUTION AND TRANSPORT
Abstract
The present disclosure involves methods and apparatus for
actively controlling the charged particle density in a controlled
pressure region or in the ambient atmosphere, from an accelerator
capable of producing high intensity relativistic charged particle
streams in a pulsed manner. The techniques are applicable to both
high repetition rate applications, typical of industrial
processors, electron tubes or accelerator/fusion reactor injectors,
and to single pulse or low repetition rate systems. These methods
utilize the self-magnetic forces of relativistic beams to
accomplish controlled distribution, and avoid the complexities of
electromagnetic scanners or lenses heretofore used for this
purpose. Methods are also disclosed which utilize force control in
partially charged neutralized beams as well as plasma conductivity
control in freely drifting beam systems.
Inventors: |
Nablo; Sam V. (Lexington,
MA) |
Assignee: |
Energy Sciences, Inc.
(Burlington, MA)
|
Family
ID: |
22057948 |
Appl.
No.: |
05/064,734 |
Filed: |
August 18, 1970 |
Current U.S.
Class: |
250/311;
219/121.34; 315/111.01; 219/121.27; 219/121.35; 313/420;
976/DIG.428 |
Current CPC
Class: |
H01J
5/18 (20130101); G21K 1/02 (20130101); H01J
33/00 (20130101); H01J 35/186 (20190501) |
Current International
Class: |
G21K
1/02 (20060101); H01J 33/00 (20060101); H01J
35/14 (20060101); H01J 35/00 (20060101); H01J
5/18 (20060101); H01J 5/02 (20060101); H01j
035/00 () |
Field of
Search: |
;250/49.5R ;219/121EB
;313/83,74 ;328/228 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Lawrence; James W.
Assistant Examiner: Church; C. E.
Claims
What is claimed is:
1. Apparatus for controlling charged relativistic particle beam
flux over a predetermined area, having, in combination, high-vacuum
and low-pressure gas-containing chambers interconnected by
low-pressure beam-permeable window means and with the low-pressure
chamber provided with a further beam-permeable window means
communicating with the external atmosphere and over a predetermined
area of which a predetermined beam density is to be maintained,
means for propagating the said beam from the high-vacuum chamber
through said low-pressure window means and upon said predetermined
area of said further window means, means disposed proximal to said
further window means for monitoring the charge density at a region
of said predetermined area, and means controlled by the monitoring
means for varying the gas pressure within said low-pressure chamber
in accordance with the density monitored by said monitoring means
in order to maintain the said predetermined beam flux over said
predetermined area of said further window means.
2. Apparatus as claimed in claim 1 and in which means is provided
for pulsing said beam.
3. Apparatus as claimed in claim 2 and in which means is provided
for adjusting the beam current density to a value of sufficient
intensity to enable self-focusing of said current within said
low-pressure chamber, acting as a drift space.
4. Apparatus as claimed in claim 2 and in which the walls of said
low-pressure chamber are conducting and there is provided
intermediate and within the drift space thereof, a plurality of
spaced conducting vane members.
5. Apparatus as claimed in claim 4 and in which dielectric layer
means is provided at the vane members near the centerline of the
beam.
6. Apparatus as claimed in claim 4 and in which the said walls are
curved.
7. Apparatus as claimed in claim 2 and in which means is provided
in the low-pressure chamber for maintaining a predetermined glow
discharge.
8. Apparatus as claimed in claim 7 and in which means is provided,
responsive to the said monitoring means, for controlling the glow
discharge to effect control of the said beam density over the said
predetermined area of said further window means.
9. Apparatus for controlling charged relativistic particle beam
density over a predetermined area having, in combination, a
conducting low-pressure drift-space chamber, means including a
high-vacuum chamber for propagating a charged particle beam into
and along said drift-space chamber, and a plurality of spaced
electrically floating conducting vane members dispersed along said
drift-space chamber for producing beam image charge forces in the
central region of the beam.
10. Apparatus for controlling charged relativistic particle beam
density over a predetermined area having, in combination, a
low-pressure chamber having means including a high-vacuum chamber
for introducing a charged particle beam at one end and for
permitting exit of the same at its other end through beam-permeable
window means, means for maintaining a predetermined glow discharge
in said low-pressure chamber, means disposed proximal to the window
means for monitoring the charge density at a region thereof, and
means controlled by the monitoring means for varying the said glow
discharge in said low-pressure chamber in accordance with the
density monitored by said monitoring means.
11. Apparatus for controlling charged relativistic particle beam
density over a predetermined area having, in combination, a
gas-containing low-pressure chamber having means including a
high-vacuum chamber for introducing a charged particle beam at one
end and for permitting exit of the same at its other end through
beam-permeable window means, means disposed proximal to the window
means for monitoring the charge density at a region thereof, and
means controlled by the monitoring means for varying the
conductivity of the said gas in the said low-pressure chamber in
accordance with the density monitored by said monitoring means.
12. A method for controlling the charged relativistic particle beam
density over a predetermined area of a beam-permeable exit window
of a gas-containing low-pressure chamber, into which chamber high
intensity charge-particle beam impulses are introduced from a
high-vacuum chamber, said method comprising, propagating said
introduced beam through said low-pressure chamber as a drift space
to the exit window, subjecting the beam to image charge force
distribution along the low-pressure chamber to control
self-focusing of the beam, monitoring the beam density near said
exit window, and controlling at least one of the gas pressure and
gas conductivity within said low-pressure chamber in response to
said monitoring.
Description
The present invention relates to apparatus for and methods of
controlling a relativistic charged particle beam distribution and
transport, including automatically and continually controlling the
charge particle density distribution of high intensity electron and
other charged particles.
Various techniques have been employed over the years to try to
ensure a uniform or other predetermined high intensity electron or
other beam density at a target or window region over a
predetermined area. These prior proposals have included the
utilization of scanning or deflection mechanisms that cause the
beam repetitively to scan over a predetermined area in different
types of scanning paths, and thus try to accomplish the above
objective, as described, for example, by M. L. Rossi et al., "A
Wide Area Electron Beam Scanner," IEEE Transactions on Nuclear
Sciences, Volume NS- 12,Number 3, June 1965, page 279.
Unfortunately, such techniques have the disadvantage that they
require deflection and scanning equipment. In addition, they
inherently do not provide for the simultaneous presence of the
desired beam density at all points of the predetermined area and
because they scan the beam at the current densities provided by the
accelerator, high instantaneous dose rates are encountered in the
irradiated matter, often leading to decreased radiation induced
changes in, or degradation of, the target material.
Another approach has been to control the focusing of the beam, as
in electron beam welding and similar systems; but this again is not
suited to the problem of controlling the beam density over sizeable
areas, since the focusing adjustment is only most effective for
converging the beam onto a small point or area.
It is to the solution of this problem of effective and automatic
control of high intensity charged particle beam density over
predetermined target or window areas and the like, accordingly,
that the present invention is primarily directed, it being an
object of the invention to provide a new and improved method of and
apparatus for such control of relativistic charged particle beam
distribution and transport.
In applications where the electron beam or other charged particle
beam is to be pulsed, moreover, as in the case of nanosecond high
voltage pulses of the order of tens of thousands of amperes, with
energies of hundreds of kilovolts, such prior art scanning and
focusing techniques are not useful in view of the indexing and
location problem inherent in turning the beam on and off and
ensuring that the beam energy covers exactly the predetermined area
during each pulse. More than this, the use of very high energy beam
pulses requires the spreading out of the beam over a predetermined
area to avoid local damage in the target area.
A further objective of the invention, therefore, is to provide
novel apparatus for such control of high energy pulsed charged
particle beams.
Other and further objects will be explained hereinafter and are
more particularly delineated in the appended claims. In summary,
however, the invention contemplates, in one of its important
aspects, beam-permeable window-separated high vacuum
charged-beam-generating and low-pressure drift-space chambers. The
charge density at or near the exit window of the drift-space
chamber is monitored and used to control the gas pressure within
the low-pressure chambers to insure the desired predetermined beam
density and area coverage at the exit window. Preferred details are
hereinafter set forth.
The invention will now be described with reference to the
accompanying drawings,
FIG. 1 of which is a combined longitudinal section and schematic
circuit diagram of apparatus constructed in accordance with a
preferred embodiment that practices the method of the
invention;
FIG. 5 is a graph illustrating net beam current behavior as a
function of gas pressure in the low-pressure drift chamber of the
apparatus of FIG. 1;
FIGS. 2 and 4 are views similar to FIG. 1 of modifications; and
FIG. 3 is a longitudinal section taken along the line 3 -- 3 of
FIG. 2, looking in the direction of the arrows.
The practical application of intense charged particle beams,
particularly electrons, largely depends upon the ability to deliver
such beams in a controlled manner into the atmosphere, so that the
current density (i.e. flux of energy or dose rate) delivered at the
ultimate product plane, shown at 1 in FIG. 1, may be precisely
controlled. Suitable means for the generation of such intense
pulsed streams, typically of tens of thousands of amperes at
energies of hundreds of kilovolts or above for periods of tens of
nanoseconds, are described, for example, in U.S. Letters Pat. Nos.
3,397,337 and 3,344,398. In general, these beams are formed by the
application of negative high voltage impulses P, FIG. 1, to an
insulated collector plate 2, to which a cold cathode 3 is affixed,
such that electrons are released from the cathode 3 during the tens
of nanoseconds duration of each pulse. Electrons are accelerated
within the chamber or region 3' to ground plane 5 from the gas
plasma formed about the cold cathode surface 3 in the region of
field intensification. Typical applications of such beams, as
described, for example, in my prior U.S. Letters Pat. No. 3,489,944
with A. S. Denholm, have involved their transfer from the
relatively high vacuum acceleration chamber or region 3',
maintained at approximately 10.sup..sup.-5 torr by means of active
pumping through port 6, through an electron permeable window 7,
into a relatively low pressure chamber or drift region 8. The
chamber or drift region 8 is maintained at a pressure differing
from that of the accelerating region 3' by means of a differential
pumping port 9 in chamber 8, which can be fitted with, for example,
a variable conductance butterfly valve 11 to permit precise
pressure control of the volume enclosed by chamber 8, typically
filled with ambient air or nitrogen gas. Beam entrance to the
atmosphere is defined by a second electron permeable window 10 at
the far end of the chamber 8 and which is capable of supporting one
atmosphere across the opening. The electron windows may, for
example, be of 0.001 inch Titanium foil clamped in a vacuum fitting
flange as at 10', as described in my said prior patent and in my
article with S. E. Graybill entitled "The Generation and Diagnosis
of Pulsed Relativistic Electron Beams Above 10.sup.10 Watts," Proc.
IEEE Transactions on Nuclear Sciences, Volume NS-14, No. 3, page
782, 1967.
The behavior of a high current density beam of sufficient intensity
that self-magnetic focusing results, was predicted by W. H.
Bennett, Phys. Rev. 45, p. 890, 1934 and 98, p. 1584, 1955 and
others. Bennett showed that electrostatically neutralized beams
could be self-focusing for currents above
I.sup.2 = (8.pi. /.mu..sub.o) Nk (T.sub.e + T.sub.i),
where N is the number of charges per unit length of the beam, k is
the Boltzmann constant, .mu..sub.o is the permeability of vacuum
(4.pi. .times. 10.sup..sup.-7), and T.sub.e and T.sub.i are the
electron and ion temperatures, respectively. This prediction was
first confirmed experimentally by the said Graybill and me, Applied
Physics Letters, 8, p. 18, 1966, with apparatus in which current
density (energy flux) behavior was first measured experimentally
with relativistic electron beams of sufficient intensity to permit
controlled study of these phenomena.
Study of the current-field balance in the relatively low-pressure
chamber or drift region 8 has resulted in a good understanding of
those conditions providing optimum beam propagation and current
density where no external fields are applied. In the region of 1 mm
pressure for the conditions experienced with the apparatus of my
said prior patent, a condition of magnetic neutrality results.
Thus, in the system of FIG. 1, an azimuthal magnetic field,
schematically designated at 13, is generated by the primary beam
12, and it is neutralized or counteracted by an opposed field 13'
generated by the return current 12' flowing in the plasma generated
by the primary stream. Under conditions of electrostatic
neutralization (i.e. N.sub.i = N.sub.e), this condition will result
in laminar or parallel flow of the electron beam. Precise control
of the plasma conductivity (through pressure variation in chamber
8) will in turn define the current 12' and counterfield 13'. As a
result, the diameter and current density distribution at the exit
window 10 can be determined through control of the pumping
conductance valve 9. As illustrated in FIG. 5, for example,
increased pressure will lead to decreased current density at 10
(i.e. beam expansion, defocusing or increased magnetic
neutralization); while decreased pressure will lead to increased
magnetic focusing or current density at 10 (i.e. beam compression
or focusing). Active control of the butterfly or leak valve 11 in
port 9 of the chamber wall 8, is effected by a feed back system 23
from a charge monitor or sensor 15 of any conventional type, which
may be internal or external to 8, as shown, and preferably is
disposed adjacent the window 10 at the periphery of the beam.
Alternatively, a Rogowski loop sensor 14 may be inserted into the
drift chamber 8 near the window 10 such that the proper level of
magnetic neutrality in the drifting stream is continuously and
actively maintained. Further control of the system to provide
active control of the integrated charge or dose delivered
ultimately at the product plane 1 can be effected utilizing an
integrated charge monitor in the wall of 8 (not shown) which
detects back-scattered electrons from window 10. The magnetically
neutralized configuration proposed renders this monitoring
technique possible since unneutralized systems result in intense
azimuthal fields which present charge particle flow to the
periphery of the system.
The magnetic neutralization scheme is practically useful, however,
only for pulsed systems, since the induced return current 12' and
associated azimuthal field 13' arise or are induced in the plasma
during the passage of the front or rising edge of the primary
current pulse 12. Experiments with 40,000 ampere, 30 nanosecond,
1.5 million electron volt beams, as described in my before-cited
publications with Graybill, have shown that the return current
density holds up well beyond the time defined by the rising portion
or leading edge of the primary current pulse due to the dependence
of the induced or back electromotive force on the difference
between currents 12 and 12'. An example of the high degree of
magnetic neutralization in the 1-10 torr pressure region is
demonstrated by the graph of such a stream. In this case, the net
current (current 12 minus current 12') flowing in chamber 8 is
plotted along the ordinate, indicating the control region of
interest (0.5 - 10 torr), for automatic pressure variation
stabilization of the exit current density, plotted along the
abscissa in FIG. 5.
In the modification of FIG. 2, a conducting chamber 16 is used for
the low-pressure drift chamber, preferably with a plurality of
conducting vanes 16' to improve current density uniformity at the
ultimate window 18, as now to be explained.
The condition of force neutralization in a relativistic beam where
the radial electrostatic forces are just neutralized by the
focusing magnetic forces, is described by the condition.
.nu. .times. B = E.sub.r ,
where B is the azimuthal self magnetic field generated by the beam
12 in FIG. 2 and E.sub.r is the radial electric field generated by
the unneutralized charge in the beam. For a beam of small
divergence, uniform ionization and current density with constant
longitudinal velocity as experienced in drift chamber section 16,
J. D. Lawson has shown (Journal Electronics and Control, 5, p. 146,
1958) that the force neutralized condition is realized when f, the
ion-electron density ratio in the drift region occupied by the
beam, is equal to 1-.beta..sup.2, where .beta. is the ratio of the
particle drift velocity to that of light.
Now for typical operating conditions, as explained in my said
Applied Physics Letters article with Graybill, with medium energy
(0.5 - 10 MeV) relativistic electron beam accelerators,
.beta..sup.2 is large and approaches unity; e.g., for
force-neutralized conditions in a 2 million electron volt beam
where .beta. = 0.98, f = 1 -.beta..sup.2 = 0.04. Since such a
condition is appropriate for both efficient propagation and current
density variation in a large area beam, positive ion densities only
a few percent (4 percent at 2 MeV), of those of the primary beam
electron density are required. Numerically, a 2 MeV intense
electron beam at a current density of 100 amperes/cm.sup.2
possesses a charge density of only 2.1 .times. 10.sup.10 e/c.c. and
requires a resident ion density of only 8 .times. 10.sup.8 /c.c. to
accomplish force neutralization.
Under such conditions of beam drift with the primary beam 12
delivered to an external target at plane 1 beyond the conducting
vessel 16, shown as somewhat conical, and fitted with differential
pumping ports 6 and 17, shown dotted, the only return current
flowing in the walls of the vessel 16 results from the small amount
of charge stopped in the window assembly 18 and that resulting from
secondary charge generated by ionization and scattering of 12 in
the chamber 16. Under these conditions, the image current forces
due to the charge in the conducting walls of 16 are repulsive to
primary stream 12, since the attractive forces are less than
1-.beta..sup.2 of the repulsive forces arising from these walls
charges. As a consequence, the primary stream is affected by the
image charge distribution in the conducting wall 16.
The geometry of FIG. 2 has been employed to utilize this effect in
"scanning" or "redistributing" an initially cylindrically symmetric
beam generated by cathode 3 at window 7, into a "strip" or two
dimensional distribution as shown in the longitudinal section at
plane 18 of chamber 16 in FIG. 3. An improvement of this simple
self-distributing geometry under neutralized flow is represented by
the addition of spaced converging planar conducting vanes 16' in
chamber 16, substantially parallel to the opposite portions of the
walls of chamber 16 and of floating potential, such that stronger
image force distribution results in the central region of the beam,
with a resulting improvement in the current density uniformity at
window 18 and the ultimate product plane 1.
A further improvement in the simple image force-self-distributing
geometry of FIG. 2 would be represented by the use of dielectric
layers, such as quartz or titania, at opposing or inner regions 16"
of the planar vanes 16' near the beam centerline, so that the image
field effects will be enhanced by the such high permittivity
material. The combination of conducting vanes in the beam and such
high permittivity surfaces above the beam centerline in the chamber
16 provides for enhancement of the lateral spreading image forces
on the beam.
A further variation of the system to improve the uniformity of the
initially cylindrically symmetric beam 12 will be the use of a
chamber 16 cross-section of double hyperbdic or "dumbell" geometry,
instead of the single conically curved wall, or flattened frustum,
to improve the image force distribution in spreading the stream
into the uniform two dimensional profile desired at exit window 18
and product plane 1.
A further modification is shown in FIG. 4, wherein a gas discharge
in the chamber 8 of FIG. 1 is maintained by a power supply 19 which
applies a discharge voltage suitable for maintenance of glow
discharge conditions in the drift chamber 8, at reduced pressure,
by means of electrodes 20 and 21 positioned in said chamber 8, or
by other means of ionization, pulsed or dc. By this technique, a
preformed plasma of constant conductivity is generated so that the
elapsed time required to establish sufficient conductivity in the
drift region, to maintain the return current 12', is not required.
This is particularly important for very short pulses where
significant amounts of primary current 12 are lost until adequate
conductivity is established to support return neutralizing current
12'. This time is given by .tau..apprxeq.(1-.beta..sup.2) /
n.sigma..beta.C, where .beta. = the particle velocity .div.
velocity of light, n is the ambient gas number density and .sigma.
the ionization cross section. For example, for an electron energy
of 2 MeV (.beta. = 0.98) and .sigma. = 10.sup.-.sup.19 cm.sup.2
/gas atom for nitrogen, .tau. = 12 nanoseconds for 100 .mu.
pressure and varies as 1/.rho.. It is observed that this loss can
be significant for 20-30 nanosecond beams in the control pressure
region indicated in FIG. 5, especially for beams whose risetimes
are a significant fraction of the total pulse width. For very
narrow pulses in the 10 nanosecond range, such a "preformed" plasma
technique is mandatory for efficient transport and manipulation of
such relativistic streams.
The current density distribution of beam 12 at window 10 and at
product pulse 1 can be controlled by conductivity variation of
plasma 22 sustained in the drift chamber 8 by conducting electrodes
20 and 21. Detector 15 (or loop 14 of FIG. 1), used in conjunction
with integrating monitor 23, may be used to determine current
density distribution near the plane 10 of exit into the air, so
that feedback control via 19' of the supply 19 can be used to vary
the voltage of electrodes 20-21, thereby varying gas conductivity,
also to readjust the exit current density to the value preselected
by charge integrator 23. The described technique is particularly
important for the control of beam current density distribution and
propogation over great distances, in the conductivity-dominated
regime of relativistic flow, typically 500 .mu. - 10 mm of air for
electron beams of medium energy (0.5 - 10 MeV).
Further modifications will also occur to those skilled in this art
and are considered to fall within the spirit and scope of the
invention as defined in the appended claims.
* * * * *