11 results on '"Kasthurirengan, Srinivasan"'
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2. Study on a twin‐bed adsorption refrigeration system using R134a‐activated carbon pair.
- Author
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Pinto, Samson Paul, Basavapatna Govindasetty, Raghavendra, Karanam, Praveen, Behera, Upendra, and Kasthurirengan, Srinivasan
- Subjects
HEAT pipes ,PLATE heat exchangers ,ACTIVATED carbon ,HEAT exchangers ,ADSORPTION (Chemistry) ,REFRIGERATION & refrigerating machinery - Abstract
A low capacity twin‐bed adsorption refrigeration system has been built with R134a as a refrigerant and activated carbon as the adsorbent. Simple tube‐in‐tube heat exchangers have been fabricated and have been used as the adsorber beds. Activated carbon (granular type) has been filled in the annular space of the inner tube and outer tube. A plate heat exchanger has been used as the condenser and the temperature of cooling water has been maintained between 25°C and 30°C, also the evaporator has been custom designed as per requirements. A mathematical model has also been developed and the results obtained have been found to be comparable. While operating the system in the single‐bed mode a cooling power of 250.4 W has been obtained with a coefficient of performance (COP) of 0.38 with an average evaporator temperature of 18.4°C against a predicted value of 263.7 W with a COP of 0.41. While operating in the twin‐bed mode a cooling power of 281.3 W with a COP of 0.47 with an average evaporator temperature of 17.6°C has been obtained against a predicted value of 294.5 W with a COP of 0.52. [ABSTRACT FROM AUTHOR]
- Published
- 2019
- Full Text
- View/download PDF
3. Development and studies of low capacity adsorption refrigeration systems based on silica gel-water and activated carbon-R134a pairs.
- Author
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Pinto, Samson Paul, Karanam, Praveen, Raghavendra, B. G., Boopathi, V., Mathad, Prafulkumar, Behera, Upendra, and Kasthurirengan, Srinivasan
- Subjects
REFRIGERATION & refrigerating machinery ,ADSORPTION capacity ,SILICA gel ,ACTIVATED carbon ,HEAT exchangers - Abstract
Adsorption Refrigeration Systems (ARS) are gaining considerable importance in view of their applications in several areas and in particular to transport industries. The refrigerants used in these systems are also quite acceptable from the points of view of Global warming and Ozone depletion. In our efforts to develop such refrigeration systems for transport vehicles, a sub-atmospheric Silicagel-Water ARS (SWARS) and a positive pressure Activated Carbon / R134a ARS (ACRARS) have been designed, fabricated and experimentally studied to evaluate their performances. A lumped parameter simulation model has been used to describe the dynamic behavior of these systems. The rate of adsorption / desorption of the refrigerants in both cases are assumed to be governed by the Linear Drive Force (LDF) model. The amount of refrigerants in adsorbent at equilibrium conditions are assumed to be described by the equations for modified Freundlich and Dubinin-Astakhov models for SWARS and ACRARS respectively. The simulation models are numerically solved by finite difference method with the simulation programs coded in MATLAB. The simulation results are found to be in good agreement with experimental results in both cases. A two-bed Silicagel-water adsorption refrigeration system has been built and it is well known that the refrigeration is produced at the evaporator. If the refrigeration power is not used to cool an external heat load (for example, by allowing the circulation of water through the heat exchanger coil embedded in the evaporator), the evaporator reaches the lowest temperature. This is the no-load condition at which the refrigeration power produced by the system is zero. When the evaporator temperature is higher than this lowest temperature, a finite refrigeration power is produced which increases with increasing evaporator temperature. The above Silicagel-water system reaches the lowest temperature of 5.3°C at no load conditions and produces a refrigeration power of ~ 284 ± 9 W at 18°C, which refers to the average temperature (T
avg ) of the flowing water through the heat exchanger coil within the evaporator. An experimental COP of 0.52 has been measured for this system. On the other hand, the simulation model predicts a refrigeration power of 325 W at 18 °C with a COP of 0.55. Using Activated Carbon - R134a pair, a four bed adsorption refrigeration system has been designed and developed. The refrigeration system is designed such that it can be operated in three different configurations and they are: (A) A single bed (i.e. all four beds arranged in parallel), (B) A twin bed, (i.e. the four beds get grouped in two pairs and undergo the opposite processes of the adsorption cycle and (C) Four independent beds each undergoing the different processes of the adsorption cycle. The measured lowest temperatures under no-load conditions are 14.5 °C, 13.3 °C and 11.9 °C for configurations A, B and C respectively as against the predictions of the simulations which are 13.3°C, 12.5 °C & 11.4°C. The experimentally measured refrigeration powers are 430 ± 13 W, 556 ± 17 W and 657 ± 20 W at the Tavg temperature of 28.5 °C for configurations A, B and C respectively. On the other hand, the refrigeration powers predicted by simulation are 450 W, 582 W and 690 W for the respective configurations. The measured COP values are 0.5, 0.65 and 0.70 for configurations A, B and C respectively as against those predicted by simulation which are 0.54, 0.67 and 0.73 respectively. It is observed that the experimental results are reasonably in good agreement with those predicted by the simulations. The highlight of the present work is that the Activated Carbon - R134a Adsorption Refrigeration System produces continuous refrigeration power which can be very useful for practical applications. Efforts are now underway to adopt this refrigeration system for cooling of truck cabins. [ABSTRACT FROM AUTHOR]- Published
- 2019
- Full Text
- View/download PDF
4. Generalized Linear Two-Point Hedging Rule for Water Supply Reservoir Operation.
- Author
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Kumar, Kranthi and Kasthurirengan, Srinivasan
- Abstract
A generalized linear two-point hedging rule is proposed for the operation of a water supply reservoir that integrates four possible linear two-point hedging types, which are identified based on two possibilities of starting water availability and two possibilities of ending water availability, arising from the respective bounds on release and carryover storage being active. The proposed rule is appropriately parameterized for implementation into a simulation-optimization (S-O) framework to investigate the trade-off between the shortage characteristics, total shortage ratio, and Vulnerability resulting from the long-term monthly operation of a water supply reservoir, and the efficacy of the same is illustrated using a case example, namely the Dharoi reservoir, located on the Sabarmati River in India. Significant improvement in the reservoir performance trade-off is achieved by the proposed generalized linear two-point hedging rule over the conventional standard operating policy (SOP)-based linear two-point hedging rule for the cases of constant as well as time-varying hedging parameters. [ABSTRACT FROM AUTHOR]
- Published
- 2018
- Full Text
- View/download PDF
5. Numerical analysis on thermoacoustic prime movers for development of pulse tube cryocoolers.
- Author
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Behera, Upendra, Kasthurirengan, Srinivasan, Skaria, Mathew, Shafi, K. A., Kamble, Bharatbhushan Vishnu, and Kuzhiveli, Biju
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NUMERICAL analysis ,THERMOACOUSTICS ,PULSE tube refrigerators ,PERFORMANCE evaluation ,LOW temperature engineering ,MATHEMATICAL models ,SOLAR energy ,MICROFABRICATION ,ENERGY development - Abstract
Thermo Acoustic Prime Movers (TAPMs) are being considered as the ideal choice for driving the Pulse Tube Cryocoolers replacing the conventional compressors. The advantages are the absence of moving components and they can be driven by low grade energy as such as fuel, gas, solar energy, waste heat etc. While the development of such TAPMs is in progress in our laboratory, their design and fabrication should be guided by numerical modeling and this may be done by several methods such as solving the energy equation [1], enthalpy flow model [2], CFD [3], etc. We have used CFD technique, since it provides a better insight into the velocity and temperature profiles. The analysis is carried out by varying parameters such as (a) temperature difference across the stack, (b) stack and resonator lengths and (c) different working fluids such as air, nitrogen, argon etc. The theoretical results are compared with the experimental data wherever possible and they are in reasonably good agreement with each other. The analysis indicate that (i) larger temperature difference across the stack leads to increased acoustic amplitude, (ii) longer resonator leads to decrease in frequency with lesser amplitude and (iii) there exists an optimal stack length for the best performance of TAPM. These results are presented here. [ABSTRACT FROM AUTHOR]
- Published
- 2012
- Full Text
- View/download PDF
6. Performances of single and two-stage pulse tube cryocoolers under different vacuum levels with and without thermal radiation shields.
- Author
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Kasthurirengan, Srinivasan, Behera, Upendra, Nadig, D. S., and Krishnamoorthy, V.
- Subjects
PULSE tube refrigerators ,LOW temperature engineering ,COOLING ,HEAT radiation & absorption ,VACUUM ,MICROFABRICATION ,STAINLESS steel - Abstract
Single and two-stage Pulse Tube Cryocoolers (PTC) have been designed, fabricated and experimentally studied. The single stage PTC reaches a no-load temperature of ~ 29 K at its cold end, the two-stage PTC reaches ~ 2.9 K in its second stage cold end and ~ 60 K in its first stage cold end. The two-stage Pulse Tube Cryocooler provides a cooling power of ~ 250 mW at 4.2 K. The single stage system uses stainless steel meshes along with Pb granules as its regenerator materials, while the two-stage PTC uses combinations of Pb along with Er3Ni / HoCu2 as the second stage regenerator materials. Normally, the above systems are insulated by thermal radiation shields and mounted inside a vacuum chamber which is maintained at high vacuum. To evaluate the performance of these systems in the possible conditions of loss of vacuum with and without radiation shields, experimental studies have been performed. The heat-in-leak under such severe conditions has been estimated from the heat load characteristics of the respective stages. The experimental results are analyzed to obtain surface emissivities and effective thermal conductivities as a function of interspace pressure. [ABSTRACT FROM AUTHOR]
- Published
- 2012
- Full Text
- View/download PDF
7. Comparison of 1D and 2D flow numerical analysis applied to two stage pulse tube cryocooler.
- Author
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Krishnappa, G. B., Madhu, D., and Kasthurirengan, Srinivasan
- Subjects
COMPARATIVE studies ,NUMERICAL analysis ,LOW temperature engineering ,PULSE tube refrigerators ,PUMPING machinery ,COMPUTATIONAL fluid dynamics - Abstract
In the recent years, for several applications such as cooling of sensors, super conducting magnets, cryo-pumping etc., there are worldwide efforts to replace cooling with liquid helium by cooling with closed cycle cryocoolers. The internal working processes in pulse tube cryocoolers are quite complex due to unsteady, oscillating compressible gas flow in the pulse tube. Although considerable theoretical studies have been carried out phenomena occurring in pulse tubes are still to be understood. Three different numerical models namely isothermal model, adiabatic model and energy equation model based on the assumption of one-dimensional flow are compared with a Computational Fluid Dynamics (CFD) model based on a two dimensional flow approach to analyze a two stage pulse tube cryocooler. The various experimental parameters have been incorporated in the models to carry out the analysis. The various losses of the pulse tube cryocooler are calculated separately and incorporated into the 1D models. CFD analysis is carried out without any assumptions except the helium is treated as ideal gas. The numerical results are compared with the experimental results obtained for a two stage pulse tube cryocooler for validation. [ABSTRACT FROM AUTHOR]
- Published
- 2012
- Full Text
- View/download PDF
8. Development of experimental setup for study of adsorption characteristics of porous materials down to 4.2 K.
- Author
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Behera, Upendra, Kasthurirengan, Srinivasan, Krishnamoorthy, V., Senthil Kumar, A., Kuzhiveli, Biju T., and Gangradey, Ranjana
- Subjects
ADSORPTION (Chemistry) ,POROUS materials ,TEMPERATURE effect ,ACTIVATED carbon ,SORPTION ,PUMPING machinery ,MICROFABRICATION ,REFRIGERATORS - Abstract
The knowledge of adsorption characteristics of activated carbon (porous material) in the temperature range from 5 to 20 K is essential when used in cryosorption pumps for nuclear fusion applications. However, such experimental data are very scarce in the literature, especially below 77 K. So, an experimental system is designed and fabricated to measure the adsorption characteristics of porous materials under variable cryogenic temperatures (from 5 K to 100 K). This is based on the commercially available micropore-analyser coupled to a closed helium cycle two-stage Gifford McMahon (GM) Cryocooler, which allows the sample to be cooled to 4.2 K. The sample port is coupled to the Cryocooler through a heat switch, which isolates this port from the cold head of the Cryocooler. By this, the sample temperature can now be varied without affecting the Cryocooler. The setup enables adsorption studies in the pressure range from atmospheric down to 10-4 Pa. The paper describes the details of the experimental setup and presents the results of adsorption studies at 77 K for activated carbon with nitrogen as adsorbate. The system integration is now completed to enable adsorption studies at 4.2 K. [ABSTRACT FROM AUTHOR]
- Published
- 2012
- Full Text
- View/download PDF
9. Experimental studies of thermoacoustic drive for the development of a pulse tube cryocooler.
- Author
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Kamble, Bharatbhushan Vishnu, Kuzhiveli, Biju T., Kasthurirengan, Srinivasan, Behera, Upendra, Krishnamoorthy, V., Hariharan, N. M., and Sivashanmugam, P.
- Subjects
PULSE tube refrigerators ,THERMOACOUSTICS ,LOW temperature engineering ,PERFORMANCE evaluation ,PRESSURE ,MICROFABRICATION ,ELECTRIC resonators ,WORKING fluids - Abstract
Thermoacoustically driven Pulse Tube Cryocooler (PTC) totally eliminates the moving components and is totally reliable towards cryogenic applications. In an objective to development of such a system, we need to design the Thermo Acoustic Prime Mover (TAPM) to drive the Pulse Tube cryocooler. We have made detailed design of the standing wave twin TAPM using the simplified linear thermoacoustic model of short stack and boundary layer approximations, based on the procedures outlined by Swift [1] and Tijani [2]. The theoretical design indicates the dependence of the system performance on stack geometry and its relative position with respect to other components for different working fluids. Based on the above design, the TAPM with different resonator lengths were fabricated and experimented. Studies have been conducted to evaluate their performance characteristics with respect to several parameters such as the resonator length, the working fluid and the operating pressure. The optimized TAPM has been used as the prime mover for a single stage Pulse Tube Cryocooler. A temperature difference of ~42 K has been measured between the hot and cold ends of the Pulse Tube. These results are presented here. [ABSTRACT FROM AUTHOR]
- Published
- 2012
- Full Text
- View/download PDF
10. Note: Development of a cryocooler based high efficiency cryosorption pump.
- Author
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Verma, Ravi, Chatterjee, Aritra, Kasthurirengan, Srinivasan, Shivaprakash, N. C., and Behera, Upendra
- Subjects
THERMAL conductivity ,NITROGEN ,ARGON ,HYDROGEN ,HELIUM - Abstract
In this communication, we report the development of a cryosorption pump, whose pumping speeds are higher at least by a factor of 1.5 compared to the commercial pumps in specific pressure ranges. This uses a material of high adsorbing capacity along with an adhesive of high thermal conductivity. The measured pumping speeds of these pumps for different gases such as nitrogen, argon, hydrogen, and helium are higher than the commercial cryopumps in the pressure range from 5 x 10
-6 mbar to 5 x 10-5 mbar. The developed pump will be quite useful for fusion applications. [ABSTRACT FROM AUTHOR]- Published
- 2017
- Full Text
- View/download PDF
11. Studies of Adsorption Characteristics of Activated Carbons in between 4.5 to 10 K for Cryopump Applications.
- Author
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Krishnamoorthy, V., Udgata, Satya Swarup, Tripathi, Vijai Shankar, Gangradey, Ranjana, Kasthurirengan, Srinivasan, and Behera, Upendra
- Published
- 2012
- Full Text
- View/download PDF
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