Environmental Engineering Reference
In-Depth Information
Fig. 4.29
The magnetic
eld pro
les and the corresponding
fl
uid
fl
ow periods for the AMR
thermodynamic cycles investigated in the experiment
The
˄
mag
= 0.75 s was taken in all the experimental analyses shown in this section.
The
s thermodynamic cycle
(information about this period is provided in the text below). In addition to
˄
f
was changed for a particular test of the AMR
'
˄
mag
and
˄
f
, the response time of the data acquisition and control elements was, in all the
cases, equal to
˄
0
= 0.2 s per cycle. The frequency of the operation was therefore
de
ned by the duration of the total period. In the case of the Brayton-like AMR
refrigeration cycles this equals to 1/(2
˄
0
). However, in the case of the
Ericsson-like AMR cycle, the frequency of operation was de
˄
mag
+2
˄
f
+
ned as 1/(2
˄
f
+
˄
0
),
since the
ow was performed during all the thermodynamic processes. In the
Hybrid AMR cycle the frequency was de
fl
uid
fl
˄
f
+
˄
mag/2
)+
˄
0
).
ned as 1/(2(
rst tests were performed for no cooling load conditions in order to measure
the maximum possible temperature span for a given AMR thermodynamic cycle.
For this purpose, the utilization factor and the working frequency were varied.
Figure
4.30
shows the ratio between the maximum no-load temperature spans
(obtained at U = optimum, which has been de
The
ned at the maximum temperature
span) and the adiabatic temperature change
ʔ
T
ad
for different frequencies (we
denote this as the regeneration factor). As can be seen from Fig.
4.30
, the largest
regeneration factor (6.6 at f = 0.3 Hz and
˄
f
= 0.85 s) was obtained with the Hybrid
Fig. 4.30
The experimentally obtained no-load maximum temperature span as a function of the
operating frequency for a parallel-plate gadolinium AMR
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