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Thermionic emission and Richardson equation

Short answer

Thermionic emission is electron ejection from a heated metal; work function Φ is the minimum energy from Fermi level to vacuum. The Richardson-Dushman current density is J = B0 T² exp(−Φ/kT) with B0 = 4πmek²/h³. The Schottky effect, due to an applied field ℰ, lowers the barrier by ΔΦ = √(e³ℰ/(4πε₀)), giving J = B0 T² exp[−(Φ−β_S√ℰ)/kT].

What is Thermionic emission and work function? Derive the Richardson's expression for the thermionic emission for Schottky effect.

Thermionic emission and work function

Work function Φ\Phi is the minimum energy needed to remove an electron from the Fermi level of a metal to the vacuum just outside it (Φ=Evac−EF\Phi = E_{vac} - E_F; e.g. W 4.5 eV, thoriated W 2.6 eV).

Thermionic emission is the emission of electrons from a heated metal. At high TT the Fermi-Dirac tail extends above EF+ΦE_F + \Phi, so some electrons have enough energy, in the direction normal to the surface, to escape. It is used in cathodes of vacuum tubes, CRTs and X-ray tubes.

 Energy
  ^  vacuum level -------------
  |                 ^
  |                 | Phi
  |  EF   ----------v----  <- top filled states
  |       /////////////////
  |  metal  (filled band)

Derivation of Richardson-Dushman equation

Take the surface normal to xx. Electrons escape if 12mvx2≥EF+Φ\tfrac{1}{2}m v_x^2 \ge E_F + \Phi. For these high-energy electrons E−EF≫kTE - E_F \gg kT, so f(E)≈exp⁡[−(E−EF)/kT]f(E) \approx \exp[-(E - E_F)/kT]. The number of electrons per unit volume with velocity in dvx dvy dvzdv_x\,dv_y\,dv_z (including spin) is

dn=2(mh)3exp⁡[−12m(vx2+vy2+vz2)−EFkT]dvx dvy dvzdn = 2\left(\frac{m}{h}\right)^3 \exp\left[-\frac{\tfrac12 m(v_x^2 + v_y^2 + v_z^2) - E_F}{kT}\right] dv_x\,dv_y\,dv_z

The current density is J=e∫vx dnJ = e\int v_x\, dn over all vy,vzv_y, v_z and over vx≥vx0v_x \ge v_{x0}, where 12mvx02=EF+Φ\tfrac12 m v_{x0}^2 = E_F + \Phi. Using ∫−∞∞e−mv2/2kTdv=2πkT/m\int_{-\infty}^{\infty} e^{-mv^2/2kT}dv = \sqrt{2\pi kT/m} for vyv_y and vzv_z:

J=2e(mh)3eEF/kT⋅2πkTm∫vx0∞vxe−mvx2/2kTdvxJ = 2e\left(\frac{m}{h}\right)^3 e^{E_F/kT} \cdot \frac{2\pi kT}{m} \int_{v_{x0}}^{\infty} v_x e^{-mv_x^2/2kT}dv_x

The last integral equals kTme−(EF+Φ)/kT\frac{kT}{m}e^{-(E_F+\Phi)/kT}. Therefore

J=4πmek2h3T2exp⁡(−ΦkT)=B0T2e−Φ/kTJ = \frac{4\pi m e k^2}{h^3} T^2 \exp\left(-\frac{\Phi}{kT}\right) = B_0 T^2 e^{-\Phi/kT}

with B0=4πmek2h3=1.20×106 A m−2K−2B_0 = \dfrac{4\pi m e k^2}{h^3} = 1.20 \times 10^{6}\ \text{A m}^{-2}\text{K}^{-2}. This is the Richardson-Dushman equation. Real metals have smaller B0B_0 (surface reflection).

Schottky effect (field-assisted emission)

With an accelerating field E\mathcal{E} at the cathode, the electron's potential energy outside the surface is (image force + applied field):

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

(measured from EFE_F). Setting d(PE)/dx=0d(PE)/dx = 0 gives the maximum at xm=e/(16πε0E)x_m = \sqrt{e/(16\pi\varepsilon_0\mathcal{E})}, and the barrier is lowered by

ΔΦ=e3E4πε0=βSE,βS=e34πε0\Delta\Phi = \sqrt{\frac{e^3\mathcal{E}}{4\pi\varepsilon_0}} = \beta_S\sqrt{\mathcal{E}}, \qquad \beta_S = \sqrt{\frac{e^3}{4\pi\varepsilon_0}}

So the effective work function is Φeff=Φ−βSE\Phi_{eff} = \Phi - \beta_S\sqrt{\mathcal{E}} and

J=B0T2exp⁡[−Φ−βSEkT]J = B_0 T^2 \exp\left[-\frac{\Phi - \beta_S\sqrt{\mathcal{E}}}{kT}\right]
 PE
  ^       ___ max (lowered)
  |  Phi /   \___
  |     /        \___  with field
  |    /             \___
  | EF|____________________> x
     surface   xm

Thus the emission current rises with field even at fixed temperature. Example: E=108\mathcal{E} = 10^8 V/m lowers Φ\Phi by about 0.38 eV.

✓ Answer checked by Claude Opus 5.5 (high effort)

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