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Speed control by inertia and load damping

Short answer

Without a governor, gate position is fixed; inertia (H) determines the initial rate of speed fall, while load damping (D) reduces load as frequency drops, establishing a steady-state deviation of -Delta P_L/D. The transfer function is DeltaOmega(s)/DeltaP_L(s) = -1/(2Hs + D) with time constant T = 2H/D.

Below figure shows the block diagram of water turbine driving an electric generator without speed governor. Explain how the inertia and load damping constant can control the speed of the system against small change in load. Derive the transfer function showing the effect of inertia and load damping constant. [Figure: turbine coupled by a shaft to a generator, which supplies a composite load]

Without a governor, the gate (and so mechanical power PmP_m) stays fixed. When load changes, speed is held back only by two natural effects: the inertia of the rotating masses, which slows the rate of speed change, and the load damping, which reduces the load as frequency falls so that a new balance is reached.

Derivation of the transfer function

Inertia (rotating mass): for small changes, in per unit, the swing equation is

2Hd Δωdt=ΔPm−ΔPe2H\frac{d\,\Delta\omega}{dt} = \Delta P_m - \Delta P_e

where HH = inertia constant (s), Δω\Delta\omega = speed deviation (pu). Taking the Laplace transform,

ΔΩ(s)=12Hs[ΔPm(s)−ΔPe(s)]\Delta\Omega(s) = \frac{1}{2Hs}\big[\Delta P_m(s) - \Delta P_e(s)\big]

Load damping: a composite load has frequency-insensitive parts (lighting, heating) and frequency-sensitive parts (motors). So

ΔPe=ΔPL+D Δω\Delta P_e = \Delta P_L + D\,\Delta\omega

where ΔPL\Delta P_L = non-frequency-sensitive load change and DD = load damping constant (% change in load per % change in frequency, typically 1–2).

Substituting,

2Hs ΔΩ(s)=ΔPm(s)−ΔPL(s)−D ΔΩ(s)ΔΩ(s)=ΔPm(s)−ΔPL(s)2Hs+D\begin{aligned} 2Hs\,\Delta\Omega(s) &= \Delta P_m(s) - \Delta P_L(s) - D\,\Delta\Omega(s) \\ \Delta\Omega(s) &= \frac{\Delta P_m(s) - \Delta P_L(s)}{2Hs + D} \end{aligned}

Without a governor ΔPm=0\Delta P_m = 0, so

ΔΩ(s)ΔPL(s)=−12Hs+D=−1/D1+sT,T=2HD\frac{\Delta\Omega(s)}{\Delta P_L(s)} = \frac{-1}{2Hs + D} = \frac{-1/D}{1 + sT}, \qquad T = \frac{2H}{D}
 dPm=0  +    +--------------+
 ------>(+)->|      1       |----+--> d(omega)
         ^ - |   2Hs + D    |    |
         |   +--------------+    |
       dPL

Response to a small step change in load

For a step ΔPL(s)=ΔPL/s\Delta P_L(s) = \Delta P_L / s:

Δω(t)=−ΔPLD(1−e−t/T),T=2HD\Delta\omega(t) = -\frac{\Delta P_L}{D}\left(1 - e^{-t/T}\right), \qquad T = \frac{2H}{D}
 d(omega)
   0 |-----.
     |      \
     |       '-.
     |          '--.______  -dPL/D
     +------------------------> t
           T = 2H/D

Role of inertia and load damping

  • Inertia (H): At the first instant PmP_m is unchanged, so the extra load is supplied from the kinetic energy of the rotor. Speed starts to fall at a rate dΔω/dt=−ΔPL/2Hd\Delta\omega/dt = -\Delta P_L/2H. Larger HH gives a slower fall and a larger time constant T=2H/DT = 2H/D. Inertia does not change the final value; it only slows the change.
  • Load damping (D): As frequency falls, motor loads take less power (D ΔωD\,\Delta\omega). The fall stops when this reduction equals ΔPL\Delta P_L, giving steady-state deviation Δωss=−ΔPL/D\Delta\omega_{ss} = -\Delta P_L/D. Larger DD gives a smaller final speed error and a faster settling.
  • Since DD is small (1–2), the steady speed error is large: e.g. ΔPL=0.01\Delta P_L = 0.01 pu and D=1D = 1 gives a 1 % drop in frequency. So a governor is needed to restore speed; inertia and damping only make the system self-regulating for small changes.

✓ Answer checked by Claude Opus 5.5 (high effort)

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