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Pierce Electron Gun
Introduction
An electron gun must be able to draw a sufficient current and accelerate the electrons to the desired speed. First the electrons are drawn from an electron source, such as a metal cathode or plasma. Then the electrons are accelerated using electric and magnetic forces.
The first part of an electron gun geometry, where electrons are first extracted, presents unique design challenges because the emitted electron speeds are usually lowest there, and therefore the space charge density usually reaches a maximum in this region. The high space charge density can cause an electron beam to spread out.
The Pierce electron gun design uses electrodes with a particular shape to counteract the Coulomb repulsion between electrons in the beam. As a result, the electrons in the beam propagate in straight lines. The emitted electrons at the cathode are assumed to be space charge limited; the initial thermal distribution of electron velocities is neglected.
Model Definition
The Pierce electron gun design uses electrodes of a specific shape, so that the outward component of the electric field at the edge of the beam is zero. This requires the electrodes to perfectly counterbalance the Coulomb repulsion between the beam electrons.
Inside the beam, both the cathode and anode are flat edges. Here the anode is understood to be a metal grid so that the electrons may pass through. At higher current it may be necessary to shoot the electron beam through a gap in the anode.
Outside the beam, the bottom electrode makes an angle of 67.5 degrees with the beam propagation direction. The anode is shaped so that
where r (SI unit: m) is the distance from the point where the flat part of the cathode meets the incline, d (SI unit: m) is the gap thickness between the cathode and anode at the beam center, and θ (SI unit: rad) is the angle that a line from this point makes with the beam propagation direction.
The determination of these electrode shapes is sometimes called the Pierce method of gun design. The full derivation is given in Appendix: Derivation of the Cathode Shape.
The gun geometry is shown in Figure 1. The interior edge separating the two domains is only kept for meshing purposes, since the space charge density distribution within the beam can be calculated more accurately using a finer mesh as shown in Figure 2.
Figure 1: Geometry of the Pierce electron gun.
Figure 2: A fine mapped mesh is used in the beam path. The mesh coarsens as the distance from the beam is increased.
Note that the lower end of the rectangular domain and the inclined electrode do not meet at a common vertex; the rectangle is a bit higher. This is because the electrons are released using the Space Charge Limited Emission feature. This feature emits model particles from a virtual cathode a short distance away from the real cathode. This is to avoid the infinite space charge density that occurs at the real cathode when the thermal distribution of released electron velocities is not taken into account.
Results and Discussion
The electric potential and some electric field streamlines are shown in Figure 3. Ideally the electric field streamlines within the beam path and the electron trajectories should be perfectly vertical.
Figure 3: Surface plot of the electric potential. Electric field streamlines are shown in black.
The electron trajectories are shown in Figure 4. The beam does become about 3% thinner by the time it reaches the anode, but a small deviation can be expected because this finite-size geometry is actually a truncated version of the ideal Pierce design. For more details, see Appendix: Derivation of the Cathode Shape. To better visualize the shape of the electric potential distribution in the beam, a contour plot with electric field streamlines is shown in Figure 5. A Filter node was used to hide part of the geometry.
Figure 4: Particle trajectories are shown as lines. The color expression is the particle speed.
Figure 5: Contour plot of the electric potential, Electric field streamlines are shown in black.
Reference
1. S. Humphries, Charged Particle Beams, Dover Publications, New York, 2013.
2. J. R. Pierce, “Rectilinear electron flow in beams”, Journal of Applied Physics, vol. 11, no. 8, pp. 548-554, 1940.
Application Library path: Particle_Tracing_Module/Charged_Particle_Tracing/pierce_electron_gun
Modeling Instructions
From the File menu, choose New.
New
In the New window, click  Model Wizard.
Model Wizard
1
In the Model Wizard window, click  2D.
2
In the Select Physics tree, select AC/DC>Particle Tracing>Particle Field Interaction, Non-Relativistic.
3
Click Add.
4
Click  Study.
5
In the Select Study tree, select Preset Studies for Selected Physics Interfaces>Charged Particle Tracing>Bidirectionally Coupled Particle Tracing.
6
Global Definitions
Parameters 1
1
In the Model Builder window, under Global Definitions click Parameters 1.
2
In the Settings window for Parameters, locate the Parameters section.
3
Geometry 1
Rectangle 1 (r1)
1
In the Geometry toolbar, click  Rectangle.
2
In the Settings window for Rectangle, locate the Size and Shape section.
3
In the Width text field, type w1.
4
In the Height text field, type d-db.
5
Locate the Position section. In the y text field, type db.
The bottom edge of the rectangle is the flat virtual cathode. The top edge is a flat anode grid that the released electrons can pass through. At high current it may be necessary to replace the grid with a gap in the anode so that the beam does not melt the grid.
Next add the curved part of the anode.
Parametric Curve 1 (pc1)
1
In the Geometry toolbar, click  More Primitives and choose Parametric Curve.
2
In the Settings window for Parametric Curve, locate the Parameter section.
3
In the Name text field, type theta.
4
In the Maximum text field, type 62*pi/180.
This maximum parameter value is somewhat arbitrary but must be less than 67.5 degrees.
5
Locate the Expressions section. In the x text field, type w1+d*sec(4*theta/3)^0.75*sin(theta).
6
In the y text field, type d*sec(4*theta/3)^0.75*cos(theta).
Add a Polygon to define the focusing electrode. An ideal Pierce gun extends infinitely, but here the polygon is cut off at a sufficient distance from the beam.
Polygon 1 (pol1)
1
In the Geometry toolbar, click  Polygon.
2
In the Settings window for Polygon, locate the Object Type section.
3
From the Type list, choose Open curve.
4
Locate the Coordinates section. In the table, enter the following settings:
Convert to Solid 1 (csol1)
1
In the Geometry toolbar, click  Conversions and choose Convert to Solid.
2
Select the objects pc1 and pol1 only.
3
In the Settings window for Convert to Solid, click  Build All Objects.
4
Click the  Zoom Extents button in the Graphics toolbar. The plot should look like Figure 1.
Definitions
Integration 1 (intop1)
1
In the Definitions toolbar, click  Nonlocal Couplings and choose Integration.
2
In the Settings window for Integration, locate the Source Selection section.
3
From the Geometric entity level list, choose Point.
4
This Integration coupling will be used to evaluate the electric potential at the end of the virtual cathode, in order to avoid discontinuities in the potential.
Materials
Material 1 (mat1)
1
In the Model Builder window, under Component 1 (comp1) right-click Materials and choose Blank Material.
2
In the Settings window for Material, locate the Material Contents section.
3
Charged Particle Tracing (cpt)
Particle Properties 1
1
In the Model Builder window, under Component 1 (comp1)>Charged Particle Tracing (cpt) click Particle Properties 1.
2
In the Settings window for Particle Properties, locate the Particle Species section.
3
From the Particle species list, choose Electron.
Electric Force 1
1
In the Model Builder window, click Electric Force 1.
2
In the Settings window for Electric Force, locate the Electric Force section.
3
From the E list, choose Electric field (es/ccn1).
Multiphysics
Space Charge Limited Emission 1 (scle1)
1
In the Physics toolbar, click  Multiphysics Couplings and choose Boundary>Space Charge Limited Emission.
2
3
In the Settings window for Space Charge Limited Emission, locate the Space Charge Limited Emission section.
4
In the os text field, type db.
The Space Charge Limited Emission node has two purposes: to release electrons and to determine the electric potential at the virtual cathode.
Electric Particle Field Interaction 1 (epfi1)
1
In the Model Builder window, click Electric Particle Field Interaction 1 (epfi1).
2
In the Settings window for Electric Particle Field Interaction, locate the Continuation Settings section.
3
Select the Use cumulative space charge density check box.
4
In the β text field, type 10.
When Use cumulative space charge density is selected, the space charge density of the electrons is gradually increased over the first few iterations of the study. This prevents the space charge density from being overestimated, which could possibly cause the initial particle velocity to point in the wrong direction.
Set up the boundary conditions for the Electrostatics interface. Specify the potentials on the anode and the focusing electrode. The left boundary is a symmetry plane so the default Zero Charge condition may be used.
Electrostatics (es)
In the Model Builder window, under Component 1 (comp1) click Electrostatics (es).
Anode
1
In the Physics toolbar, click  Boundaries and choose Electric Potential.
2
In the Settings window for Electric Potential, type Anode in the Label text field.
3
4
Locate the Electric Potential section. In the V0 text field, type V0.
Focusing Electrode
1
In the Physics toolbar, click  Boundaries and choose Electric Potential.
2
In the Settings window for Electric Potential, type Focusing Electrode in the Label text field.
3
Adjacent to Virtual Cathode
1
In the Physics toolbar, click  Boundaries and choose Electric Potential.
2
In the Settings window for Electric Potential, type Adjacent to Virtual Cathode in the Label text field.
3
4
Locate the Electric Potential section. In the V0 text field, type intop1(scle1.V0)*(y/db)^(4/3).
This expression uses the Integration coupling defined earlier. It ensures continuity between the zero potential at the focusing electrode and the nonzero potential on the edge of the virtual cathode.
Mesh 1
Define a very fine mapped mesh where the electron beam will propagate, to accurately accumulate the space charge density. The mesh is allowed to become coarser in the charge-free region away from the beam.
Mapped 1
1
In the Mesh toolbar, click  Mapped.
2
In the Settings window for Mapped, locate the Domain Selection section.
3
From the Geometric entity level list, choose Domain.
4
Distribution 1
1
Right-click Mapped 1 and choose Distribution.
2
3
In the Settings window for Distribution, locate the Distribution section.
4
In the Number of elements text field, type 20.
Distribution 2
1
In the Model Builder window, right-click Mapped 1 and choose Distribution.
2
3
In the Settings window for Distribution, locate the Distribution section.
4
In the Number of elements text field, type 100.
Free Triangular 1
1
In the Mesh toolbar, click  Free Triangular.
2
In the Settings window for Free Triangular, click  Build All. The plot should look like Figure 2.
Study 1
The Bidirectionally Coupled Particle Tracing study step alternates between stationary calculations of the electric potential and transient calculations of the particle trajectories, allowing the particles and the electric potential to influence each other.
Step 1: Bidirectionally Coupled Particle Tracing
1
In the Model Builder window, under Study 1 click Step 1: Bidirectionally Coupled Particle Tracing.
2
In the Settings window for Bidirectionally Coupled Particle Tracing, locate the Study Settings section.
3
From the Time unit list, choose ns.
4
In the Output times text field, type range(0,1,10).
5
Locate the Iterations section. In the Number of iterations text field, type 20.
6
In the Home toolbar, click  Compute.
Results
Streamline 1
The default plot shows the electric potential in the domain. First add some electric field lines. In order to show that the focusing electrode offsets the space charge of the beam, the electric field lines in the beam should be vertical.
1
Right-click Electric Potential (es) and choose Streamline.
2
3
In the Settings window for Streamline, locate the Streamline Positioning section.
4
In the Number text field, type 60.
5
In the Electric Potential (es) toolbar, click  Plot. The plot should look like Figure 3.
Particle Trajectories 1
1
In the Model Builder window, expand the Particle Trajectories (cpt) node, then click Particle Trajectories 1.
2
In the Settings window for Particle Trajectories, locate the Coloring and Style section.
3
Find the Line style subsection. From the Type list, choose Line.
4
In the Particle Trajectories (cpt) toolbar, click  Plot. The plot should look like Figure 4.
To better visualize the electric potential, add a Mirror dataset to fill in the left half of the geometry.
Mirror 2D 1
In the Results toolbar, click  More Datasets and choose Mirror 2D.
Using this new Mirror dataset, create a contour plot of the electric potential.
Contours with Field Lines
1
In the Results toolbar, click  2D Plot Group.
2
In the Settings window for 2D Plot Group, type Contours with Field Lines in the Label text field.
3
Locate the Data section. From the Dataset list, choose Mirror 2D 1.
4
Locate the Plot Settings section. Clear the Plot dataset edges check box.
Contour 1
1
Right-click Contours with Field Lines and choose Contour.
2
In the Settings window for Contour, locate the Coloring and Style section.
3
From the Contour type list, choose Filled.
4
From the Color table list, choose Traffic.
5
Select the Reverse color table check box.
Filter 1
1
Right-click Contour 1 and choose Filter.
2
In the Settings window for Filter, locate the Element Selection section.
3
In the Logical expression for inclusion text field, type x<5[cm].
Streamline 1
1
In the Model Builder window, right-click Contours with Field Lines and choose Streamline.
2
In the Settings window for Streamline, locate the Streamline Positioning section.
3
From the Entry method list, choose Coordinates.
4
In the x text field, type range(-0.05,0.002,0.05).
5
In the y text field, type 0.045.
Filter 1
1
Right-click Streamline 1 and choose Filter.
2
In the Settings window for Filter, locate the Element Selection section.
3
In the Logical expression for inclusion text field, type x<5[cm].
4
In the Contours with Field Lines toolbar, click  Plot.
5
Click the  Zoom Extents button in the Graphics toolbar. The plot should look like Figure 5.
 
Appendix: Derivation of the Cathode Shape
In a charge-free region of space, the electric potential V (SI unit: V) potential must satisfy Poisson’s equation,
The Pierce method for determining the shape of the electrodes takes advantage of the observation that any function of the complex variable y + ix will satisfy Poisson’s equation.
Define u = y + ix and consider an arbitrary function f(y + ix). It can be shown by repeated applications of the chain rule,
The function f must be defined so that it matches the space charge limited potential in the beam,
So the electric potential is
Then the cathode is the equipotential surface where V = 0, and the anode is the equipotential surface where V = Va. It is somewhat easier to determine the shape of these equipotential surfaces by expressing u in cylindrical polar coordinates,
Thus
Since r is real,
Invoking Euler’s theorem yields
The solution for V = 0 is a straight line with
(1)
That is, θ = 3π/8 or 67.5 degrees. Recalling that the beam propagation direction is the real axis, this means the equipotential surface is a straight line that makes a 67.5 degree angle with the beam propagation direction.
The solution for V = Va is
which can be rearranged and solved for r,
(2)
In fact, the line given by Equation 1 is the asymptote of Equation 2 as the radial coordinate r becomes very large. The ideal Pierce electron gun therefore has a thin sliver-like gap between the electrodes that is infinitely long, but the electrodes will never touch. In this example, the electrodes are simply truncated at a sufficient distance from the beam. The line cutting off this gap is drawn perpendicular to the lower boundary because this is approximately the direction in which the electric field will point there, so the disruption from imposing the default Zero Charge boundary condition along such an edge will be minimized.