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Speed response without governor and isochronous governor

Short answer

Without governor, the speed response transfer function is ΔΩ(s)/ΔPL(s) = -1/(2Hs+D), leading to a steady-state speed drop -ΔPL/D. An isochronous governor uses an integrator (K/s) in the forward path, forcing the steady-state speed error to zero by adjusting gate position until Pm equals PL.

Derive the transfer function for speed response for load change in turbine-generator set in the absence of governor. Also, explain how isochronous governor can be incorporated together with turbine-generator with block diagram.

Transfer function without governor

Without a governor, the turbine gate is fixed, so ΔPm=0\Delta P_m = 0 and the speed is decided only by rotor inertia and load damping.

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}

With ΔPm=0\Delta P_m = 0:

ΔΩ(s)ΔPL(s)=−12Hs+D\frac{\Delta\Omega(s)}{\Delta P_L(s)} = \frac{-1}{2Hs + D}
 dPm=0  +    +--------------+
 ------>(+)->|      1       |----+--> d(omega)
         ^ - |   2Hs + D    |    |
         |   +--------------+    |
       dPL

For a step load ΔPL\Delta P_L:

Δω(t)=−ΔPLD(1−e−tD/2H)\Delta\omega(t) = -\frac{\Delta P_L}{D}\left(1 - e^{-tD/2H}\right)

The speed falls exponentially with time constant 2H/D2H/D and settles at −ΔPL/D-\Delta P_L/D, which is a large error because DD is small.

Incorporating an isochronous governor

An isochronous (constant speed) governor uses integral control. It measures speed, compares with the reference, and integrates the error to move the gate:

ΔY(s)=−Ks ΔΩ(s)\Delta Y(s) = -\frac{K}{s}\,\Delta\Omega(s)

The gate keeps moving as long as there is any speed error, so speed returns exactly to the set value.

                          dPL
                           | -
 +-------+  dPm            v      +-----------+
 |turbine|--------------->(+)---->| 1/(2Hs+D) |--+--> dw
 | Gt(s) |                 +      +-----------+  |
 +-------+                                       |
     ^ dY                                        |
 +-------+    -                                  |
 |  K/s  |<---(+)<-------------------------------+
 +-------+     ^ +
               | dw_ref = 0

Here Gt(s)G_t(s) is the turbine transfer function (for hydro, 1−Tws1+0.5Tws\frac{1 - T_w s}{1 + 0.5T_w s}).

Working: a load rise makes speed fall; the integrator output grows, gates open, PmP_m rises above PeP_e, the rotor accelerates and speed comes back to the reference. In steady state Δω=0\Delta\omega = 0 and ΔPm=ΔPL\Delta P_m = \Delta P_L.

The isochronous governor works well for a single unit supplying an isolated load. It cannot be used on several units in parallel, because each would try to fix the frequency at its own set point and they would fight for the load; for that, speed droop is added.

✓ Answer checked by Claude Opus 5.5 (high effort)

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