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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