16 research outputs found

    A Critical Analysis of the Characterization of Scroll Compressors Energy Consumption

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    This paper presents the analysis of the energy consumption of scroll type compressors. The study has included the data of several AHRI reports: (especially AHRI-11 and AHRI-21) as well as data from other source. A total of 8 different scroll compressors, of different size, some of them tested with various refrigerants (R134a, R32, R410A, R404A…) have been considered in the study. The values of the compressor consumption, and of the corresponding compressor efficiency, and the shape of the corresponding response surfaces, for all the studied compressors and refrigerants, have been analyzed with the objective of understanding better the dependence of the energy compressor consumption on the operating conditions and the refrigerant. The analyzed data include tests following different superheat control, i.e. constant superheat or constant return temperature, so the effect of the inlet temperature on the energy consumption and efficiency are also discussed. The paper includes the analysis of the compressor consumption as dependent of the temperatures of the tested points, and alternatively as dependent of the corresponding pressures, and as a result it will be shown that the representation as a function of pressures is more universal than the one made with temperatures. Two simple correlation polynomials, based on suction and discharge pressures, are presented, which require less empirical information and have better interpolation-extrapolation characteristics than the AHRI standard correlation

    Compressor Calorimeter Test of R-404A Alternatives ARM-31a, D2Y-65, L-40, and R32 + R-134a Mixture using a Scroll Compressor

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    As a contribution to the AHRI Low-GWP Alternative Refrigerants Evaluation Program (AREP), this study compares the performance of four lower-GWP alternative refrigerants, ARM-31a, D2Y-65, L-40, and R-32 + R-134a mixture, to that of refrigerant R-404A (baseline) in a scroll compressor designed for medium temperature refrigeration applications. These comparisons were carried out via compressor calorimeter tests performed on a compressor designed for refrigerant R-404A and having a nominal rated capacity of 23,500 Btu/hr. Tests were conducted over a suction dew point temperature range of -10 F to 35 F in 5 F increments and a discharge dew point temperature range of 70 F to 140 F in 10 F increments. All the tests were performed with 20 F superheat, 40 F superheat, and 65 F suction temperature. A liquid subcooling level of 10 F to 15 F was maintained for all the test conditions. However, the cooling capacities reported in this study are normalized for 0 F subcooling. The tests showed that the compressor energy efficiency ratio (EER) and cooling capacity with all four alternative refrigerants tested are higher at higher saturation suction and saturation discharge temperature and lower at lower saturation suction and saturation discharge temperature, compared to that of R-404A. Discharge temperatures of all the alternative refrigerants were higher than that of R-404A at all test conditions

    Optimization of Ventilation Energy Demands and Indoor Air Quality in the ZEBRAlliance Homes

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    High Performance Window Retrofit

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    The US Department of Energy (DOE) Office of Energy Efficiency and Renewable Energy (EERE) and Traco partnered to develop high-performance windows for commercial building that are cost-effective. The main performance requirement for these windows was that they needed to have an R-value of at least 5 ft2 F h/Btu. This project seeks to quantify the potential energy savings from installing these windows in commercial buildings that are at least 20 years old. To this end, we are conducting evaluations at a two-story test facility that is representative of a commercial building from the 1980s, and are gathering measurements on the performance of its windows before and after double-pane, clear-glazed units are upgraded with R5 windows. Additionally, we will use these data to calibrate EnergyPlus models that we will allow us to extrapolate results to other climates. Findings from this project will provide empirical data on the benefits from high-performance windows, which will help promote their adoption in new and existing commercial buildings. This report describes the experimental setup, and includes some of the field and simulation results

    Compressor Calorimeter Test of R-410A Alternatives R-32, DR-5, and L-41a

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    As a contribution to the AHRI Low-GWP Alternative Refrigerants Evaluation Program (AREP), this study compares performance of alternative refrigerants R32, DR-5, and L-41A to that of refrigerant R-410A (baseline) in a scroll compressor designed for air-conditioning and heat pump applications. Compressor calorimeter tests were performed to evaluate the performance of the lower-GWP alternative refrigerants in place of the common refrigerant R-410A in a 36,000 Btu/hr compressor calorimeter using a compressor having a nominal rated capacity of 21,300 Btu/hr. Tests were conducted over a suction dew point temperature range of 10 F to 55 F in 5 F increments and a discharge dew point temperature range of 70 F to 140 F in 10 F increments. All the tests were performed with 20 F superheat, 40 F superheat and 65 F suction temperature. A liquid subcooling level of 15 F was maintained for all the test conditions. The tests showed that performance of these three lower-GWP alternative refrigerants is comparable to that of R-410A. For the 20 F superheat and 15 F subcooling test conditions, EERs of R32, DR-5, and L-41A were 90% to 99%, 96% to 99%, and 94% to 101%, respectively, compared to that of R-410A. Similarly, cooling capacities of R32, DR-5, and L-41A were 98% to 103%, 92% to 96%, and 84% to 92%, respectively, compared to that of R-410A

    Microwave and Millimeter Wave Nondestructive Testing of the Space Shuttle External Tank Insulating Foam

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    The space shuttle Columbia\u27s catastrophic failure has been attributed to a piece of external fuel tank insulating foam (spray on foam insulation) striking the leading edge of the left wing of the orbiter causing significant damage to some of the protecting heat tiles. The accident emphasizes the growing need to develop effective, robust and life cycle oriented methods of nondestructive testing (NDT) of complex conductor backed insulating foam and protective acreage heat tiles used in the space shuttle fleet and in future multilaunch space vehicles. The insulating spray on foam is constructed from closed cell foam. In the microwave regime, this foam is in the family of low permittivity and low loss dielectric materials. Near field microwave and millimeter wave NDT techniques were one of the techniques chosen for testing this material. (Microwaves are electromagnetic waves with frequencies between 0.3 and 300 GHz. Those in the frequency range above about 30 GHz are generally referred to as millimeter waves because their wavelengths in free space are conveniently measured in millimeters.) To this end, several flat and thick spray on foam insulation panels, two structurally complex panels similar to the external fuel tank and a blind panel were used in this investigation. Several discontinuities such as voids and disbonds were embedded in these panels at various locations. The location and properties of the embedded discontinuities in the blind panel were not disclosed to the investigating team prior to the investigation. Three frequency bands were used in this investigation, covering a frequency range of 8 to 75 GHz. Moreover, the influence of signal polarization was also investigated. Overall, the results of this investigation were very promising for detecting the presence of discontinuities in different panels covered with relatively thick insulating spray on foam. Different types of discontinuities were detected in foam up to 229 mm (9 in.) thick. Many of the discontinuities in the more complex panels were also detected. When investigating the blind panel, no false positives were detected. Discontinuities in between and underneath bolt heads were not easily detected. This paper presents the results of this investigation along with a discussion of the capabilities of the technique used
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