Biomedical Engineering Reference
In-Depth Information
flow through the disc into
both pans. Under steady-state conditions (when no reactions and no transitions occur),
the differential signal
When the furnace is heated, the same amount of heat should
Δ
T
-
normally an electric potential difference
-
provides a baseline
for heat
flow due to differences in heat capacity between the sample and the reference.
When a transition occurs, the steady-state equilibrium is disturbed and a differential
signal is generated which is proportional to the difference in heat
flow rates to the sample
and to the reference.
Measured heat
ow rates
ϕ m are proportional to temperature differences:
furnace!sample - furnace!reference ≈ -D
T
ð
2
:
14
Þ
m
K m D
T
ð
2
:
15a
Þ
true ¼
K m:
ð
2
:
15b
Þ
Measured
flow rates are obtained by the manufacturer by careful
calibration with reference materials (to determine the parameters K m and K ϕ ). The heat
ϕ m and true
ϕ true heat
flux is expressed in μW or mW (power units).
The enthalpy difference
Δ
H in a phase transition, being the change in a state variable,
is a well-de
ned parameter. This enthalpy is always a function of pressure p, temperature
T and composition
, which is, in turn, related to structural changes.
The heat capacity C p, χ (T) at constant pressure and constant
χ
'
structural
'
composition of
the sample is
p ; χ :
Þ¼
H
C p ; χ ð
T
ð
2
:
16
Þ
T
The enthalpy change
H of the sample at constant temperature and pressure, due to a
phase transition, a chemical reaction or a mixing effect associated with changes of
composition
Δ
χ
, is given by
T ; p :
H
∂χ
D
¼
ð
2
:
17
Þ
H
DSC experiments measure the rate of change of the heat (or heat
flux) through the sample
during a temperature ramp, dQ m /dt:
dQ m
dt
m ¼
:
ð
2
:
18
Þ
At constant pressure and in the absence of any external energy perturbation, the total heat
flux is related to the enthalpy changes arising from the two contributions shown in ( 2.17 )
and ( 2.18 ). Differentiating these equations with respect to time,
dt ;
dT
dt þ
H
∂χ
d
m ð
T
;
p
; χÞ¼
C p ; χ ð
T
Þ
ð
2
:
19
Þ
p ; T
where dT/dt is the rate of change of the temperature (in general taken as constant). The
heat capacity C p, χ (T) is proportional to the sample mass m, while c p, χ (T) =C p, χ (T)/m is
the heat capacity per unit mass.
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