Summary: Pierce type electron gun essentials and most basic geometry
12 May 2021 - tsp
Last update 12 May 2021
6 mins
Introduction
After I wrote some blog posts about thermionic emission cathodes
as well as a simple improvised uncollimated electron source from scrape stuff
I thought itās time to write a blog post about one of the more simple types
of electron guns - the Pierce electron gun design.
As one knows the main problem for an electron gun to provide a collimated non
diverging beam of electrons is the divergence of the beam. This usually occurs
because electrons are charged negative and are repelling each other. This leads
to natural beam divergence in charged particle beams. The idea behind a Pierce
type electron gun is to counter this effect by the electric field formed by
the cathode-anode pair by choosing a clever geometry.
To recall the current limits for electron guns - there are two modes in which
a thermionic source can operate (for more details see my blog post about thermionic emission cathodes):
First thereās thermally limited mode. In thermally limited mode the number of electrons increases
as the temperature of the cathode increases. In this mode the Richardson-Dushman
equation describes the current density limit - $A$ is a material constant, $\psi$
is the work function and $T$ the temperature of the cathode:
[
J_{th} = A * T^2 * e^{- \frac{\psi}{k_B * T}}
]
The constant $k_B$ is the Boltzmann constant, the work function should be specified
in Joule ($1 eV \approx 1.602 * 10^{-19} J$).
[
k_B = 1.380 * 10^{-23} \frac{J}{K}
]
On the other hand thereās space charge limited mode thatās reached at higher
temperatures. In this mode the repulsive force between electrons inside the
electron cloud is limiting the release of electrons from the cathode. The current
limit is described by Childās law:
[
J_{sc} = \underbrace{\frac{4 \epsilon_0}{9} * \sqrt{\frac{2 e}{m_e}}}_{c_1} * \frac{V_a^{\frac{3}{2}}}{d^2} \\
J_{sc} = c_1 * \frac{V_a^{\frac{3}{2}}}{d^2}
]
The quantities $\epsilon_0$, $e$ and $m_e$ are the vacuum permittivity, the charge
of an electron and the mass of an electron respectively - and thus constant:
[
\epsilon_0 = 8.854 * 10^{-12} \frac{As}{Vm} \\
e = 1.602*10^{-19} C \\
m_e = 9.109 * 10^{-31} kg \\
\frac{4 \epsilon_0}{9} * \sqrt{\frac{2 e}{m_e}} \approx 2.2338 * 10^{-6} m A V^{-\frac{3}{2}}
]
The quantity $V_a$ is the acceleration voltage between cathode and anode, $d$ is the
distance between these two electrodes in meters.
Pierce type approach
Usually for Pierce type electron guns only space charge mode is assumed - the thermally
emitted electrons are basically ignored. The idea is pretty simple - the beam
emitted from an cathode should be emitted in a cylindrical form - the area
around the beam should be free of charge carriers. Since one knows that
[
U = \int E ds \\
\to \nabla U = E \\
\nabla * E = \underbrace{\frac{\rho}{\epsilon_0}}_{0} \\
\to \nabla * E = 0 \\
\to \nabla \underbrace{\nabla U}_{E} = 0 \\
\Delta U = 0
]
As one can see the requirement for charge carrier free space is just that the potential
fulfills the Laplace equation. This can be achieved with a huge number of geometric
configurations - the most basic Pierce type gun usually uses a pretty simply
construction.
Simple solution
One can show that the Laplace equation is satisfied by any function that depends
on a complex number and thatās twice differentiable:
[
u = y + i * x \\
\implies \Delta f(u) = 0
]
This can easily be shown:
[
\frac{\partial^2 f}{\partial x^2} + \frac{\partial^2 f}{\partial y^2} \\
= \frac{\partial}{\partial x} \left(\frac{\partial u}{\partial x} \frac{\partial f}{\partial u} \right) + \frac{\partial}{\partial y} \left(\frac{\partial u}{\partial y} \frac{\partial f}{\partial u}\right) \\
= \frac{\partial}{\partial x} \left(i * \frac{\partial f}{\partial u}\right) + \frac{\partial}{\partial y} \left(\frac{\partial f}{\partial u}\right) \\
= \frac{\partial u}{\partial x} \frac{\partial}{\partial u} \left(i \frac{\partial f}{\partial u}\right) + \frac{\partial u}{\partial y} \frac{\partial}{\partial u} \left(\frac{\partial f}{\partial u}\right) \\
= i^2 \frac{\partial^2 f}{\partial u^2} + \frac{\partial^2 f}{\partial u^2} \\
= -\frac{\partial^2 f}{\partial u^2} + \frac{\partial^2 f}{\partial u^2} = 0
]
This leads to a simple method to construct such a function. Simply define $V = \mathfrak{Re}(f(u)) \forall x > 0$.
Note that Iāll be using cylindrical coordinates during the construction. The origin
will be placed at the cathode, the beam will be traveling into positive y
direction and the x axis will be parallel to the plain cathode surface / perpendicular
to the beam and symmetry axis. $x=0$ will be located at a sharp edge of the beam.
For $x < 0$ one will enter the zone that contains charge carriers, $x > 0$ will
be charge carrier free. This will allow easy modeling.

Note that the graphically shown emitter surface might either be an electron emitting
surface itself or the emitting surface from a Wehnelt cylinder assembly.
Since one can assume that the potential has to be continuous at $x = 0$ one
can assume that - assuming space charge limited mode - at $x = 0, y = 0$ Childās
law provides the boundary condition for the potential:
[
V = V_a * \mathfrak{Re}\left(\left(\frac{u}{d}\right)^{\frac{4}{3}})\right)
]
Now moving to polar coordinates makes life easier:
[
u = r * e^{i * \theta} \\
V = V_a * \mathfrak{Re} \left( \left(\frac{r}{d} e^\theta\right)^{\frac{4}{3}} \right) \forall x > 0 \\
= V_a * \left(\frac{r}{d}\right)^\frac{4}{3} * \mathfrak{Re}\left(e^{\frac{4}{3}\theta}\right) \\
\to V = V_a \left(\frac{r}{d}\right)^{\frac{4}{3}} * \cos \left(\frac{4}{3} \theta\right)
]
Geometry of the cathode
Now first letās calculate the geometry of the cathode. Iām going to assume
arbitrary that $V=0$ for the cathode as this is a commonly chosen configuration
in electron tubes - for particle accelerators and similar equipment the cathode
might be placed at negative potential which would only add an total offset
to the voltage and thus not change the geometry of the electron gun anyways.
[
V=0 \to 0 = V_a \left(\frac{r}{d}\right)^{\frac{4}{3}} * \cos \left(\frac{4}{3} \theta\right) \\
\to \cos \left(\frac{4}{3} \theta\right) = 0 \\
\to \frac{4}{3} \theta = \frac{\pi}{2} \\
\implies \theta = \frac{3 \pi}{8} \\
\theta = 67.5^{\circ}
]
As one can see the angle outside the cathode surface will be fixed - itās simply
a cone with fixed angle
Geometry of the anode
The anode will be a little bit more complex. Weāll be assuming that $V=V_a$:
[
V=V_a \to V_a = V_a \left(\frac{r}{d}\right)^{\frac{4}{3}} * \cos \left(\frac{4}{3} \theta\right) \\
1 = \left(\frac{r}{d}\right)^{\frac{4}{3}} * \cos \left(\frac{4}{3} \theta\right) \\
1 = \frac{r}{d} \cos^{\frac{4}{3}}\left(\frac{4}{3} \theta \right) \\
r = d * \left(\frac{1}{\cos(\frac{4}{3}\theta)}\right)^{\frac{3}{4}}
]
This article is tagged: Physics, Particle source