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Image charge derivation for Schottky effect

Short answer

In thermionic emission, heated electrons with energy normal to the surface exceeding the work function Phi escape. Using the image charge method, an electron outside the metal sees an image potential -e^2/(16 pi epsilon0 x); an applied field E adds -eEx, lowering the barrier by Delta Phi = sqrt(e^3 E/(4 pi epsilon0)). The emission current density is J = B0 T^2 exp[-(Phi - beta_s sqrt(E))/kT] with beta_s = sqrt(e^3/(4 pi epsilon0)).

Explain the thermionic emission in metal. Using image charge method, derive an expression of emission current density for Schottky effect.

Thermionic emission in metals

In a metal, conduction electrons fill states up to EFE_F at 0 K. To leave the metal, an electron needs extra energy equal to the work function Φ\Phi. When the metal is heated, the Fermi-Dirac tail spreads above EFE_F, and the few electrons whose kinetic energy normal to the surface exceeds EF+ΦE_F + \Phi escape. This is thermionic emission. The emitted current density is given by the Richardson-Dushman equation

J=B0T2exp⁡(−ΦkT),B0=4πmek2h3≈1.2×106 A m−2K−2J = B_0 T^2 \exp\left(-\frac{\Phi}{kT}\right), \qquad B_0 = \frac{4\pi m e k^2}{h^3} \approx 1.2 \times 10^{6}\ \text{A m}^{-2}\text{K}^{-2}

JJ rises very fast with TT and is larger for a small Φ\Phi (hence oxide- or thorium-coated cathodes).

Image charge method

When an electron is at distance xx outside a flat conducting surface, the charges it induces on the metal act like a positive image charge +e+e at distance xx inside the surface, i.e. 2x2x away from the electron.

   metal  |  vacuum
          |
   (+e) - | - (-e)
    <--x-->|<--x-->
   image  |  electron

Attractive image force:

Fim=−e24πε0(2x)2=−e216πε0x2F_{im} = -\frac{e^2}{4\pi\varepsilon_0 (2x)^2} = -\frac{e^2}{16\pi\varepsilon_0 x^2}

Taking the potential energy as zero at infinity, the PE at xx is minus the work needed to pull the electron from xx out to infinity against this force:

PEim(x)=−e216πε0xPE_{im}(x) = -\frac{e^2}{16\pi\varepsilon_0 x}

Measured from EFE_F, the electron's PE without a field is Φ−e216πε0x\Phi - \dfrac{e^2}{16\pi\varepsilon_0 x}, which rises smoothly to Φ\Phi far from the surface.

Effect of an applied field

An applied field E\mathcal{E} that pulls electrons away adds −eEx-e\mathcal{E}x:

PE(x)=Φ−e216πε0x−eExPE(x) = \Phi - \frac{e^2}{16\pi\varepsilon_0 x} - e\mathcal{E}x

Maximum of the barrier:

d(PE)dx=e216πε0x2−eE=0⇒xm=e16πε0E\frac{d(PE)}{dx} = \frac{e^2}{16\pi\varepsilon_0 x^2} - e\mathcal{E} = 0 \quad\Rightarrow\quad x_m = \sqrt{\frac{e}{16\pi\varepsilon_0\mathcal{E}}}

Substituting xmx_m:

PEmax=Φ−e216πε016πε0Ee−eEe16πε0E=Φ−2e3E16πε0=Φ−e3E4πε0\begin{aligned} PE_{max} &= \Phi - \frac{e^2}{16\pi\varepsilon_0}\sqrt{\frac{16\pi\varepsilon_0\mathcal{E}}{e}} - e\mathcal{E}\sqrt{\frac{e}{16\pi\varepsilon_0\mathcal{E}}} \\ &= \Phi - 2\sqrt{\frac{e^3\mathcal{E}}{16\pi\varepsilon_0}} = \Phi - \sqrt{\frac{e^3\mathcal{E}}{4\pi\varepsilon_0}} \end{aligned}

So the effective work function is Φeff=Φ−βSE\Phi_{eff} = \Phi - \beta_S\sqrt{\mathcal{E}}, where βS=e3/(4πε0)\beta_S = \sqrt{e^3/(4\pi\varepsilon_0)}.

Emission current density (Schottky effect)

Replacing Φ\Phi by Φeff\Phi_{eff} in the Richardson-Dushman equation:

J=B0T2exp⁡[−Φ−βSEkT]=J0exp⁡(βSEkT)J = B_0 T^2 \exp\left[-\frac{\Phi - \beta_S\sqrt{\mathcal{E}}}{kT}\right] = J_0 \exp\left(\frac{\beta_S\sqrt{\mathcal{E}}}{kT}\right)

where J0J_0 is the zero-field current density. Thus ln⁡J\ln J increases linearly with E\sqrt{\mathcal{E}}. Example: at E=108\mathcal{E} = 10^8 V/m, ΔΦ≈0.38\Delta\Phi \approx 0.38 eV and xm≈1.9x_m \approx 1.9 nm.

✓ Answer checked by Claude Opus 5.5 (high effort)

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