Acoustic Determination of Thermophysical Properties and Critical Parameters for R404A and Critical Line of xCO2 + (1 - x)R404A
Esperanca, J. M. S. S.[Jose M. S. S.], Pires, P. F.[Pedro F.], Guedes, H. J. R.[Henrique J. R.], Ribeiro, N.[Nuno], Costa, T.[Tania], Aguiar-Ricardo, A.[Ana]
The thermophysical properties and critical parameters for the alternative refrigerant R404A (52 wt % of 1,1,1-trifluoroethane (R143a) + 44 wt % of pentafluoroethane (R125) + 4 wt % of 1,1,1,2-tetrafluoroethane (R134a)) were investigated using two different acoustic techniques. The critical behavior of the system xCO2 + (1 - x)R404A was also investigated. Experimental data of speed of sound in liquid R404A from 258 K to 338 K and pressures up to 65 MPa were measured using a pulse-echo method. Derived thermodynamic properties are calculated, combining our experimental data with density and isobaric heat capacity values published by other authors. Measurements of the critical temperature Tc and pressure pc on (R404A) and mixtures of xCO2 + (1 - x)R404A were performed using another simple ultrasonic time-delay technique. The binary critical line was determined over the whole composition range showing that this system deviates only slightly from ideality since the critical line is a continuous line. The Peng-Robinson equation of state with conventional mixing and combining rules was used to correlate the binary experimental data.
Compounds
#
Formula
Name
1
C2H3F3
1,1,1-trifluoroethane
2
C2HF5
pentafluoroethane
3
C2H2F4
1,1,1,2-tetrafluoroethane
Datasets
The table above is generated from the ThermoML associated json file (link above).
POMD and RXND refer to PureOrMixture and Reaction Datasets. The compound numbers are included in properties, variables, and phases, if specificied;
the numbers refer to the table of compounds on the left.
Type
Compound-#
Property
Variable
Constraint
Phase
Method
#Points
POMD
2
1
3
Speed of sound, m/s ; Liquid
Temperature, K; Liquid
Pressure, kPa; Liquid
Mass fraction - 1; Liquid
Mass fraction - 2; Liquid
Liquid
non intrusive technique with two piezoelectric transducers based on the time of flight