Typically, when designing a TEC
system, the first steps are to identify the heat load (usually power rating) of
the system and the desired ΔT between the hot side and cold side. Once these
specifications are determined, then the TEC can be selected. Once a TEC is
selected, it is important to identify the rated Imax and
Vmax. Note that Imax and Vmax are not the
maximum ratings before the TEC is damaged; rather, they are the maximum ratings
before the heat generated by the TEC starts to degrade the heating or cooling
performance.
To operate the H-bridge correctly
and control the current going through the TEC, one channel of the LMP7704-SP (U1A) is used as a bidirectional current-sense amplifier,
which measures the current through the TEC. There is also a DC reference
generated by another channel of the LMP7704-SP (U1B) to account for the negative current since it is
assumed that the amplifier is operated from a single positive supply. A control
amplifier (U1C) utilizes the output of the bidirectional current-sense amplifier
(U1A) as feedback in conjunction with a control input signal (DAC, PID, and so
forth) to determine the drive level of the H-bridge. The control input signal
sets the desired current level through the TEC. The control amplifier is also
responsible for driving the half-bridge on the right side. The gate driver (U1D)
is responsible for driving the half-bridge on the left side. There are two
things to note:
U1D is DC biased by a
TL1431-SP (U2) voltage reference which defaults
the output of U1D to a high voltage. As the output of U1C increases, the
output of U1D will decrease (larger inverting signal).
When the N-channel FET
(low-side) on one half-bridge is ON (Q2 or Q4), the P-channel FET
(high-side) of the opposite half-bridge will be ON as well (Q3 or Q1).
This allows for current to flow in both directions based on which
diagonal pair of FETs is turned ON.
The LMP7704-SP supply voltage of 10V was selected according to the
derating specifications provided by the National Aeronautics and Space
Administration (NASA) in document EEE-INST-002 (April 2008) and the European
Cooperation for Space Standardization (ECSS) in document ECSS-Q-ST-30-11C Rev.1 (4 October 2011). The
documents specify an 80% and 90% derating of the absolute maximum supply voltage
for linear ICs, respectively.
For proper operation, the power
supplies must be decoupled. For supply decoupling, TI recommends placing 10-nF
to 1-µF capacitors as close as possible to the operational-amplifier power
supply pins. For the single supply configuration shown, place a capacitor
between the V+ and V– supply pins. Bypass capacitors must have a low ESR of less
than 0.1Ω.