| Literature DB >> 22778611 |
Eliseo Bustamante1, Enrique Guijarro, Fernando-Juan García-Diego, Sebastián Balasch, Antonio Hospitaler, Antonio G Torres.
Abstract
The rearing of poultry for meat production (broilers) is an agricultural food industry with high relevance to the economy and development of some countries. Periodic episodes of extreme climatic conditions during the summer season can cause high mortality among birds, resulting in economic losses. In this context, ventilation systems within poultry houses play a critical role to ensure appropriate indoor climatic conditions. The objective of this study was to develop a multisensor system to evaluate the design of the ventilation system in broiler houses. A measurement system equipped with three types of sensors: air velocity, temperature and differential pressure was designed and built. The system consisted in a laptop, a data acquisition card, a multiplexor module and a set of 24 air temperature, 24 air velocity and two differential pressure sensors. The system was able to acquire up to a maximum of 128 signals simultaneously at 5 second intervals. The multisensor system was calibrated under laboratory conditions and it was then tested in field tests. Field tests were conducted in a commercial broiler farm under four different pressure and ventilation scenarios in two sections within the building. The calibration curves obtained under laboratory conditions showed similar regression coefficients among temperature, air velocity and pressure sensors and a high goodness fit (R(2) = 0.99) with the reference. Under field test conditions, the multisensor system showed a high number of input signals from different locations with minimum internal delay in acquiring signals. The variation among air velocity sensors was not significant. The developed multisensor system was able to integrate calibrated sensors of temperature, air velocity and differential pressure and operated successfully under different conditions in a mechanically-ventilated broiler farm. This system can be used to obtain quasi-instantaneous fields of the air velocity and temperature, as well as differential pressure maps to assess the design and functioning of ventilation system and as a verification and validation (V&V) system of Computational Fluid Dynamics (CFD) simulations in poultry farms.Entities:
Keywords: air velocity; isotemporal measurements; multipoint measurements; poultry building; sensors; troubleshooting
Mesh:
Year: 2012 PMID: 22778611 PMCID: PMC3386710 DOI: 10.3390/s120505752
Source DB: PubMed Journal: Sensors (Basel) ISSN: 1424-8220 Impact factor: 3.576
Figure 1.Scheme of the measurement system.
Figure 2.Circuit of the temperature sensor.
Figure 3.Circuit of the air velocity sensor.
Figure 4.A scheme of the wind tunnel showing the position of the air velocity and temperature sensors.
Figure 5.Differential pressure electronic circuit.
Trial scenarios.
| Section A | 30 | 233,163 | Large | |
| 38 | 276,204 | Large + Small | ||
| 50 | 193,518 | Large | ||
| 50 | 250,472 | Large + Small | ||
| Section B | 30 | 233,163 | Large | |
| 38 | 276,204 | Large + Small | ||
| 50 | 193,518 | Large | ||
| 50 | 250,472 | Large + Small |
Ventilation rates were measured in each scenario as indicated by [43].
Figure 6.Tripod with a multiplexer at its centre and two air velocity and temperature sensors at the level of the birds (0.25 metres) and at 1.75 metres.
Figure 7.Location of the measurements in the two sections of the poultry farm.
Results of regressions of temperature calibrations.
|
| |||||
|---|---|---|---|---|---|
|
| |||||
| 14 | 644 | 2.00 | 0.152 | 0 | (20) |
| 4 | 184 | 2.00 | 0.148 | 0 | (21) |
| 4 | 184 | 1.98 | 0.154 | −0.000053 | (22) |
| 1 | 46 | 2.00 | 0.154 | 0 | (23) |
| 1 | 46 | 1.98 | 0.152 | 0 | (24) |
Figure 8.Regression curve of a velocity sensor calibration.
ANOVA of the air velocity scenarios.
| Section | 1 | 0.37 | 0.37 | 3.06 | 0.7935 |
| Boundary | 3 | 1.41 | 0.47 | 12.19 | 0.9051 |
| Height | 1 | >0.00 | >0.00 | 0.00 | 0.9909 |
| Sensor(Height) | 22 | 16.82 | 0.76 | 1.05 | 0.4428 |
| Section × Boundary | 3 | 0.10 | 0.03 | 0.11 | 0.9471 |
| Section × Height | 1 | 0.35 | 0.35 | 0.46 | 0.5076 |
| Boundary × Height | 3 | 0.82 | 0.27 | 0.72 | 0.5760 |
| Section*Boundary×Height | 3 | 0.79 | 0.26 | 2.46 | 0.0700 |
| Section × Sensor(Height) | 22 | 13.46 | 0.61 | 5.71 | <0.0001 |
| Boundary × Sensor(Height) | 66 | 14.69 | 0.22 | 2.08 | 0.0017 |
| Residual | 66 | 7.08 | 0.11 | - | - |
| Total (corrected) | 191 | 55.88 |
Air velocities in m/s (mean ± standard deviation) in the field experiment. The number of data is indicated in parenthesis.
| I | 0.25 m | 0.62 ± 0.86 (12) | 0.37 ± 0.30 (12) | 0.50 ± 0.65 (24) |
| 1.75 m | 0.37 ± 0.39 (12) | 0.66 ± 1.00 (12) | 0.52 ± 0.76 (24) | |
| All | 0.50 ± 0.67 (24) | 0.53 ± 0.74 (24) | 0.51 ± 0.70 (48) | |
| II | 0.25 m | 0.70 ± 0.35 (12) | 0.71 ± 0.29 (12) | 0.71 ± 0.33 (24) |
| 1.75 m | 0.47 ± 0.32 (12) | 0.68 ± 0.47 (12) | 0.58 ± 0.41 (24) | |
| All | 0.59 ± 0.35 (24) | 0.70 ± 0.38 (24) | 0.64 ± 0.37 (48) | |
| III | 0.25 m | 0.78 ± 0.41 (12) | 0.80 ± 0.31 (12) | 0.79 ± 0.35 (24) |
| 1.75 m | 0.63 ± 0.34 (12) | 0.77 ± 0.50 (12) | 0.70 ± 0.42 (24) | |
| All | 0.71 ± 0.37 (24) | 0.79 ± 0.41 (24) | 0.75 ± 0.39 (48) | |
| IV | 0.25 m | 0.42 ± 0.26 (12) | 0.65 ± 0.59 (12) | 0.54 ± 0.46 (24) |
| 1.75 m | 0.72 ± 0.69 (12) | 0.77 ± 0.87 (12) | 0.74 ± 0.75 (24) | |
| All | 0.57 ± 0.53 (24) | 0.71 ± 0.71 (24) | 0.64 ± 0.62 (48) | |
| All | 0.25 m | 0.63 ± 0.53 (48) | 0.63 ± 0.41 (48) | 0.63 ± 0.47 (96) |
| 1.75 m | 0.55 ± 0.47 (48) | 0.72 ± 0.71 (48) | 0.63 ± 0.61 (96) | |
| All | 0.59 ± 0.50 (96) | 0.68 ± 0.58 (96) | 0.63 ± 0.54 (192) |