[0001] This invention relates to thyratrons.
[0002] Generally, a thyratron comprises a cathode and an anode contained within a gas-filled
envelope and having one or more apertured control grids located between them.
[0003] Previously, it has often proved difficult to maintain interior components of thyratrons
at the temperatures desired for optimum performance. In particular, the temperatures
of thyratron grids tend to be unsatisfactorily high.
[0004] The present invention seeks to provide an improved thyratron.
[0005] According to a first aspect of this invention there is provided a thyratron comprising
a grid having at least one passage therein through which, in operation, cooling fluid
is arranged to flow and at least one aperture through which a discharge is established.
[0006] By arranging that cooling fluid is passed through the grid itself, heat may be dissipated.
The cooling fluid may be air, water, oil or some other suitable gas or liquid. The
passage or passages may be straight or curved, for example in a serpantine shape.
If a plurality of passages are included, they may be arranged in different planes
in a uniform distribution. It is preferred that the grid is of solid metal except
for the passage or passages and the aperture or apertures. This aids in conducting
heat from the grid to the cooling fluid. The grid could be of a laminated or sectional
construction to enable a passage of a desired configuration to be used.
[0007] In one advantageous embodiment of the invention, the or a passage is extensive across
an aperture. The passage may then be arranged to support a centre portion of the grid
where the aperture is annular, for example. It could also be arranged to support the
whole grid within the envelope.
[0008] Preferably, the or a passage is extensive in a direction substantially normal to
the longitudinal axis of the thyratron, the longitudinal axis being that about which
the thyratron anode and cathode are co-axial. Temperature control may then be achieved
at a particular region along the longitudianal axis without the need to consider what
effects will be exerted by the anode and cathode on the cooling fluid, and no redesign
of the anode or cathode is necessary to accommodate this form of cooling.
[0009] It is preferred that the path length through the or an aperture is greater than the
smallest transverse dimension of the aperture so that the grid is what may be termed
a "thick" grid. Normally said path length will be substantially greater than the smallest
transverse dimension of the aperture, that is to say at least five times greater.
Preferably, said path length is at least ten times greater than the transverse dimension.
[0010] In previous thyratrons, the dimensions of the aperture or apertures in a grid have
been chosen to give field penetration through the aperture, so that the preferred
route of the discharge is through the aperture. This has led to the porvision of grid
apertures which have relatively large transverse dimensions in comparison with their
lengths to ensure that the discharge path from cathode to anode is through the aperture
or apertures in the grid rather than by a route involving grid arcing, in which the
discharge path goes from the cathode to the grid surface and then from another part
of the grid surface to the anode. However this approach has limited the surface area
for recombination presented by an aperture.
[0011] The present inventors have discovered that, surprisingly, thyratrons in accordance
with the invention with "thick" grids can be operated without grid arcing. A thyratron
with a "thick" grid in accordance with the invention may have larger operating voltages
than a conventional "thin" grid thyratron. Also it may be operated at a higher pulse
repetition rate than a conventional thyratron, since the walls of the aperture present
a relatively large surface area over which recombination may occur, thus giving faster
recovery rates. The relatively large surface area of the aperture is also advantageous
in improving cooling.
[0012] In one configuration, the aperture is arranged in a direction parallel to the longitudinal
axis of the thyratron. Thus in this arrangement the aperture is a straight passage
through the grid from the anode to the cathode facing side. However, in some applications
it may be convenient to have an aperture which is curved or otherwise convoluted.
The aperture could be straight but inclined to the anode and cathode facing grid surfaces.
[0013] In one advantageous configuration, the aperture is arranged to lie along the longitudinal
axis of the thyratron. This enables the thickness of the grid to be maximised for
a given path length through the aperture, the grid then having a high thermal capacity,
permitting low temperature operation. Another convenient configuration may include
an annular aperture, the transverse dimension in this case being the distance between
the inner and outer parts of the grid which define the aperture, that is, the width
of the annulus, and not the diameter of the annulus. In a further advantageous arrangement
a plurality of apertures are included. These may be arcuate slots arranged coaxially
about the longitudial axis of the thyratron, each slot having similar dimensions to
the other or others.
[0014] The aperture may be such that there is no straight-through path through the aperture
parallel to the longitudinal axis of the thyratron. Thus where the aperture is an
annulus, say, there is no overlap in a direction parallel to the longitudinal axis
between the opening at one face of the grid and that at its other face. This configuration
gives an increase in breakdown voltage over that where there is a straight through
path parallel to the longitudinal axis of the thyratron, since the component of the
electric field in the direction of the aperture is less than the electric field normal
to the grid surfaces facing the anode and cathode. Again, as realised by the present
inventors, there need not be field penetration through the aperture to prevent grid
arcing.
[0015] Advantageously, the grid forms part of the envelope of the thyratron, enabling radiative
cooling to take place from the outer surfaces of the grid into the surroundings, and
preferably cooling fluid is arranged to flow adjacent to that part of the grid which
forms part of the envelope. Thus, internal cooling of the grid, by the flow of cooling
fluid through the passage, and external cooling may be employed, and if the grid is
a "thick" grid, there are additional cooling and operational benefits.
[0016] The invention is now further described by way of example with reference to the accompanying
drawings, in which:
Figures 1 and 2 are schematic tranverse and longitudinal sections respectively of
a thyratron in accordance with the invention;
Figure 3 is a schematic transverse section of part of another thyratron in accordance
with the invention;
Figure 4 is a schematic transverse section of part of another thyratron in accordance
with the invention;
Figures 5 and 6 are schematic longitudinal and transverse sections respectively of
another thyratron; and
Figures 7 and 8 are schematic longitudinal and transverse sections of yet another
thyratron in accordance with the invention.
[0017] With reference to Figures 1 and 2, a thyratron in accordance with the invention includes
an anode 1, a cathode 2 and a control grid 3 located between them. The control grid
3 includes an annular aperture 4 therethrough, such that the grid 3 comprises an inner
core 3A and an outer portion 3B. The path length
l through the aperture 4 is substantially greater than the transverse dimension
a, which in this case is the distance between facing surfaces defining the annulus.
A tube 5 is arranged to pass through a containing envelope 6 and to connect with a
passage 7 in the control grid 3. In operation, a cooling fluid, which in this embodiment
is water, is arranged to flow through the passage 7 to effect cooling of the grid
3. The passage 7 includes tubular parts 8 which are arranged to support the centre
portion 3A of the grid and has extensive portions 9 which hold the grid 3 in position.
[0018] With reference to Figure 3, in another thyratron a thick control grid 10 includes
three arcuate apertures 11 therethrough, and three curved passages 12 for cooling
fluid which are uniformly distributed through the thickness of the grid 10.
[0019] With reference to Figure 4, a control grid 13 in a thyratron includes an aperture
14 therethrough which is annular, the diameter of the annulus being larger at the
surface facing the cathode than at the anode-facing surface. In this configuration,
the path length
l through the aperture 14 is greater than the thickness
t of the grid 13, and the transverse dimension
a is smaller than the width
b of the aperture 14 at the grid surfaces. Again, the path length
l is substantially greater than the transverse dimension
a. In this embodiment there is no overlap between the opening of the aperture 14 in
the surface facing the anode and that in the surface facing the cathode. A serpantine
passage 15 for cooling fluid is also included.
[0020] With reference to Figures 5 and 6, another thyratron in accordance with the invention
is similar to that shown in Figures 1 and 2, but in this embodiment, the grid 16 extends
across the envelope 17 and forms part of its wall, enabling radiative cooling to occur
from the outer surface 18 of the grid 16 in addition to that provided by the flow
of cooling fluid through passage 19.
[0021] With reference to Figures 7 and 8 a thyratron includes an anode 20 and a cathode
21 located within a ceramic envelope 22 which also contains a gas. A control grid
23 is located between the anode 20 and cathode 21 and has an aperture 24 therethrough
which is arranged to lie on the longitudinal axis X-X of the thyratron. The dimension
of the apertures are such that the path length
l through the aperture 24 is about ten times longer than the transverse dimension
a normal to the path length.
[0022] Two passages 25 and 26 are included in the grid through which, in operation, cooling
fluid is passed. The grid 23 is extensive across the thyratron and forms part of the
envelope 22. A metal tube 27 is arranged adjacent the grid 23 and cooling fluid passed
through that also.
[0023] During operation, the thyratron is initially non-conducting. A voltage is applied
between the anode 20 and cathode 21 and an electrostatic field exists between the
anode 20 and the grid 23 of about 30kV, and between the grid 23 and cathode 21 of
about 1kV. Equipotentials in the region of the grid 23 are illustrated by lines 28,
where it can be seen that the field penetrates only a small distance into the aperture
24 and that the anode and cathode-facing surfaces of the grid 23 are equipotential
surfaces. When a trigger pulse is applied to the grid 23 a discharge is established
and conduction occurs. When conduction ceases, recombination of charge is facilitated
because of the relatively large surface presented by the aperture 24 and because of
its small transverse dimension. The thickness of the grid 23 also gives improved cooling
over conventional 'thin' grids, since it has a large thermal capacity.
[0024] Of course, a plurality of grids may be included in a thyratron, and more than one
of these may include a passage along which cooling fluid is passed.
1. A thyratron comprising a grid having at least one passage therein through which,
in operation, cooling fluid is arranged to flow and at least one aperture through
which a discharge is established.
2. A thyratron as claimed in claim 1 wherein the grid is of solid metal except for
the passage or passages and the aperture or apertures.
3. A thyratron as claimed in claim 1 or 2 and wherein the or a passage is extensive
across an aperture.
4. A thyratron as claimed in claim 1,2 or 3 and wherein the or a passage is extensive
in a direction substantially normal to the longitudinal axis of the thyratron.
5. A thyratron as claimed in claim 1,2,3 or 4 wherein the path length through the
or an aperture is greater than the smallest transverse dimension of the aperture.
6. A thyratron as claimed in claim 5 wherein the path length through the or an aperture
is substantially greater than the smallest transverse dimension.
7. A thyratron as claimed in claim 6 and wherein the path length is at least ten times
greater than the transverse dimension.
8. A thyratron as claimed in any preceding claim wherein the aperture is arranged
in a direction parallel to the longitudinal axis of the thyratron.
9. A thyratron as claimed in claim 8, wherein the aperture is arranged to lie along
the longitudinal axis of the thyratron.
10. A thyratron as claimed in any of claims 1 to 8 wherein the aperture is annular
and the passage is arranged to support a centre portion of the grid.
11. A thyratron as claimed in any preceding claim wherein a plurality of apertures,
which are arcuate slots, are arranged co-axially about the longitudinal axis of the
thyratron, each slot having similar dimensions to the other or others.
12. A thyratron as claimed in any preceding claim wherein part of the passage is extensive
of the grid and is arranged to support it.
13. A thyratron as claimed in any preceding claim wherein the grid forms part of the
envelope of the thyratron.
14. A thyratron as claimed in claim 13 wherein cooling fluid is arranged to flow adjacent
to that part of the grid which forms part of the envelope.