Chapter 3 EXPERIMENTAL: EQUIPMENT, SET-UP, AND PROCEDURE

Similar documents
Lab 3 Introduction to Quantitative Analysis: Pumps and Measurements of Flow

MEMORIAL UNIVERSITY OF NEWFOUNDLAND Faculty of Engineering and Applied Science FLUID MECHANICS LABORATORY PIPE FRICTION

Operating Instructions

CHAPTER 2 EXPERIMENTAL SETUP AND PROCEDURE

S.A. Klein and G.F. Nellis Cambridge University Press, 2011

2. Determine how the mass transfer rate is affected by gas flow rate and liquid flow rate.

Experimental Analysis on Vortex Tube Refrigerator Using Different Conical Valve Angles

Another convenient term is gauge pressure, which is a pressure measured above barometric pressure.

CPE562 Chemical Process Control HOMEWORK #1 PROCESS & INSTRUMENTATION DIAGRAM

AIR EJECTOR WITH A DIFFUSER THAT INCLUDES BOUNDARY LAYER SUCTION

Third measurement MEASUREMENT OF PRESSURE

Effect of Hot End Obstruction and Nozzle on the Performance of Vortex Tube

FOAM TANK (1/2) DATA SHEET

Experiment 8: Minor Losses

Reclaim Basic Set Up

Operating Instructions

An Experimental Performance Study of Vortex Tube Refrigeration System

CHEM 355 EXPERIMENT 7. Viscosity of gases: Estimation of molecular diameter

Pressure Equipment Directive (PED) 97/23/EC Page 033 of 124

OIL SUPPLY SYSTEMS ABOVE 45kW OUTPUT 4.1 Oil Supply

Chlorinator MODEL MK-I

ASSIGNMENT 2 CHE 3473

Gas Absorption Draft Standard Operating Procedure

A. M. Dalavi, Mahesh Jadhav, Yasin Shaikh, Avinash Patil (Department of Mechanical Engineering, Symbiosis Institute of Technology, India)

The Compact, Portable, Efficient and Economical Solution to boost Shop Compressed Air Pressure by 2 or 3 times

BioAerosol Nebulizing Generator. Operation and Maintenance User Manual

FOAM TANK (1/2) DATA SHEET

DEVELOPMENT OF HIGH ALTITUDE TEST FACILITY FOR COLD JET SIMULATION

FABRICATION OF VERTICAL AXIS WIND TURBINE WITH WIND REDUCER AND EXPERIMENTAL INVESTIGATIONS

DEMONSTRATION 2.1 PROPERTIES OF CO 2. Chapter 2: Gases

ASSIGNMENT 2 CHE 3473

HYDRAULICS. H89.8D - Hydraulic Bench

THERMODYNAMICS, HEAT AND MASS TRANSFER TUTORIAL NO: 1 (SPECIFIC VOLUME, PRESSURE AND TEMPERATURE)

Old-Exam.Questions-Ch-14 T072 T071

Use equation for the cylindrical section and equation or for the ends.

Flow Material Length. Weight GPM LPM. Style 3095

Heat Pump Connections and Interior Piping

Applied Fluid Mechanics

Thermocirc Installation and Maintenance Instructions

Cash Valve TYPE KP PILOT OPERATED BACK PRESSURE VALVE. ISSUED - DECEMBER 2000 CAVMC-0518-US-0208 ISO 9001 Certified

Hours / 100 Marks Seat No.

Highest Quality. Gas Chlorination Systems

Adsorption Unit Operating Procedures: CO2 Adsorption on to Activated Carbon

Hours / 100 Marks Seat No.

Introduction to Pumps

Installation Operation Maintenance

This portion of the piping tutorial covers control valve sizing, control valves, and the use of nodes.

PHYS 101 Previous Exam Problems

Universities of Leeds, Sheffield and York

Background information. normal force on a surface area of the surface

GAS DEHYDRATION SYSTEM

Cover Page for Lab Report Group Portion. Compressible Flow in a Converging-Diverging Nozzle

Structure of Mechanically Agitated Gas-Liquid Contactors

GREIG FILTERS, INC. OPERATION MANUAL

Chapter 13 Gases, Vapors, Liquids, and Solids

The Discussion of this exercise covers the following points:

for Building facilities Industrial facilities etc.,multipurpose Pilot operated type(high capacity)

Investigation on Divergent Exit Curvature Effect on Nozzle Pressure Ratio of Supersonic Convergent Divergent Nozzle

LOW PRESSURE EFFUSION OF GASES adapted by Luke Hanley and Mike Trenary

Free Surface Flow Simulation with ACUSIM in the Water Industry

Micro Channel Recuperator for a Reverse Brayton Cycle Cryocooler

Irrigation &Hydraulics Department lb / ft to kg/lit.

VERTICAL BLADDER TANK

Increase in Evaporation Caused by Running Spa Jets swhim.com

Gas Measurement Fundamentals Certification. Curriculum

HORIZONTAL BLADDER TANK

MWEA MAINTENANCE SEMINAR SPECIALTY VALVES POWER GLOBES

Digester Processes. 1. Raw Sludge Pumping System

Advanced Test Equipment Rentals ATEC (2832)

ABSTRACT. flotek.g Innovative Solutions in Flow Measurement and Control - Oil, Water and Gas August 28-30, 2017, FCRI, Palakkad, Kerala, India

Foam Chamber Model-FC

BACK PRESSURE / SUSTAINING

Validation of Custody Transfer Metering Skid at Site After Laboratory Proving

DARSHAN INSTITUTE OF ENGINEERING AND TECHNOLOGY

PETROLEUM & GAS PROCESSING TECHNOLOGY (PTT 365) SEPARATION OF PRODUCED FLUID

Design Review Agenda

Ir HN Lam BSc(Eng), MSc(Eng), CEng, MIMechE, MCIBSE, MASHRAE, MASME, MHKIE. Test Report on Non-Return Valve for Water Closets

Development of High-speed Gas Dissolution Device

Diffusivity in Gases Experiment ver 5.10b

Experimental Investigation and Modification of Ranque Hilsch Vortex Tube

Lab # 03: Visualization of Shock Waves by using Schlieren Technique

Exercise 5-2. Bubblers EXERCISE OBJECTIVE DISCUSSION OUTLINE. Bubblers DISCUSSION. Learn to measure the level in a vessel using a bubbler.

PENBERTHY SERIES LM, ELL, FL, GL, GH, U, L AND 2NC FOR PUMPING GASES

AIR FOAM CHAMBER DATA SHEET

Diffusivity in Gases Experiment ver 05.10a

WATER MADE EASY MARINE ENERGY MUNICIPAL INDUSTRIAL

CHAPTER 31 IDEAL GAS LAWS

CFD Analysis and Experimental Study on Impeller of Centrifugal Pump Alpeshkumar R Patel 1 Neeraj Dubey 2

BACK PRESSURE / SUSTAINING

AF100. Subsonic Wind Tunnel AERODYNAMICS. Open-circuit subsonic wind tunnel for a wide range of investigations into aerodynamics

(Refer Slide Time: 2:16)

Permitted MSS Emissions Tracking, Recordkeeping, and Reporting. Presented by ACES April 24, 2008

FLUID POWER FLUID POWER EQUIPMENT TUTORIAL ACCUMULATORS. This work covers part of outcome 2 of the Edexcel standard module:

Operational Settings:

Generating Calibration Gas Standards

Installation, operating and maintenance Instructions for Seemag bypass level indicator

Development of Gasdynamic Probe for Total Temperature Measurement in gases

AIRFLOW GENERATION IN A TUNNEL USING A SACCARDO VENTILATION SYSTEM AGAINST THE BUOYANCY EFFECT PRODUCED BY A FIRE

Spirax Compact FREME Flash Recovery Energy Management Equipment

An Investigative and Synoptic Review on Helium Liquefaction Using a Commercial 4 K Gifford- McMahon Cryocooler

Transcription:

Chapter 3 EXPERIMENTAL: EQUIPMENT, SET-UP, AND PROCEDURE 72

3.0 Introduction The experimental work was carried out in three stages. First stage: a laboratory scale single nozzle horizontal jet ejector was employed (setup 1). Second stage: a multi nozzle vertical jet ejector was used to study (setup 2) the effect of number of nozzles on the mass transfer characteristics. Third stage: industrial scale multi nozzle jet ejector was investigated for mass transfer characteristics and scale-up (setup 3). The detail of jet ejectors used to carry out experiments for three setups are summarized in Table 3.1. 3.1 Setup 1 3.1.1 Experimental set up The experimental setup used in this work is shown schematically in Figure 3.2. The experimental set up is comprised of two systems: (i) liquid system and (ii) gas system. 1. Liquid system The liquid system comprises of (i) Tank (12) of 600 liters capacity with provisions of electrical heating. (ii) A circulating pump (5) (iii) Shell and tube heat exchanger (15) to control temperature. (iv) Pressure gauge (6) to measure the liquid phase pressure. (v) A separator (2) for gas liquid separation. The outlet steam from separator was either recycled or drained depending upon the requirement. 2. Gas system The system consist of (i) Chlorine / carbon dioxide gas cylinder (10). (ii) Soap film meter (9) to measure gas flow rate accurately. (iii) Soap film meter (8) to measure air flow rate. 73

Table 3.1 : Dimensions of ejectors Setup I Setup - II Setup - III Nozzle diameter ( ) D N 3.28 3.28 2.0 1.50 8.2 4.7 3.7 Number of Nozzle (orifice) n 1 1 3 5 1 3 5 Nozzle No. 1 2 3 4 5 6 7 pitch * -- ܦ 2 ܦ 2 Area ratio (appx) ** ܣ 9.3 9.3 9.3 Diameter of Throat/ mixing tube ( ) ܦ 10 10 25 Length of Throat/ mixing tube *** ( ) ܮ 60 60 150 Projection ratio # 2 4.5 4.5 Angle of convergent ߠ well rounded well rounded well rounded Angle of divergence of conical diffuser ## Length of the conical diffuser ( ) Diameter of the diffuser exit ( ) Diameter of extended contactor ( ) Length of extended contactor ( ) Diameter of the suction chamber ( ) Length of the suction chamber ( ) Distance between nozzle & commencement of throat ( ) Diameter of secondary gas inlet ( ) ௩ 7 7 7 ߠ 120 120 425 ܮ 25 25 77 ܦ ( ) 25 25 ܦ ( ) 1000 1000 ܮ D S 25 25 77 40 45 122 ܮ ܮ 20 45 112, 10 10 25 ܦ Volume of free jet ( 3) 0.75 10 1.689 10 26.32 10 Volume of throat ( 3) 4.71 10 4.710 10 73.6 10 Volume of divergence ( 3) 30.6 10 30.600 10 1156.78 10 Total ejector volume ( 3) / 36.061 10 37.000 10 1256.7 10 Reference : * Panchal (1991), ** Acharjee et al (1975), *** Biswas et al. (1975), # Yadav et a., (2008) ## Mukherjee et al. (1988) 74

Figure 3.1 : Detail of jet ejector used in experimental setup 1 Figure 3.2 : Schematic diagram of experimental setup 1 75

(iv) (v) (vi) (vii) (viii) Tee (11) to mix air and. ଶ ܥ/ chlorine The tee is connected by 2 meter long tube (for thorough mixing of air and chlorine ( ଶ ܥ/ to the secondary fluid inlet of the jet ejector. Manometer (7) to measure suction pressure of gas stream. Jet ejector (1) having detail as described in Table 3.1. The primary fluid inlet of the ejector is connected to outlet of pump (5) through control valve (4B). Bypass line is connected to reservoir (12) thorough valve (4A) and heat exchanger (13). Secondary fluid inlet is connected to a gas mixture line coming from Tee (11). Contactor (3) : Ejector outlet is connected to contactor. At the outlet of the contactor is a gas liquid separator (2). Separator is vented to atmosphere and hence outlet pressure measuring device is not installed. Sample points S1, S2, S3 are provided to withdraw the sample of reaction product. S1, S2 and S3 sample points are provided along the length of the ejector and sample S0 is drawn from the tank (12). 3.1.2 Experimental procedure 1. Preparation of caustic solution First circulation of water through bypass line was started. Then required quantity of caustic lye was added slowly in tank (12). The strength of caustic was estimated by titrating against solution ܥܪ using phenolphthalein as indicator. When the required strength was /10 attained the addition of caustic lye was stopped. The solution was cooled to required temperature by heat exchanger (13). The temperature was kept at 30 ܥ through out the experiment. 2. Adjusting flow rate of Air After the desired strength of caustic soda was achieved the flow of caustic soda solution through the ejector was started. The velocity of air was measured by using soap film meter (8). The flow rate of air was adjusted by setting the operating pressure. The liquid flow rate as well as air flow rate was kept constant for all experiments. 76

3. Adjusting / flow rate Chlorine/Carbon dioxide rate was adjusted by the pressure regulator attached with the chlorine/carbon dioxide cylinder (10). The circulation of caustic solution was stopped while chlorine flow rate was being set. The chlorine flow rate was kept very low compared to the air. The chlorine/ carbon dioxide flow rate were measured by using soap film meter (9). 4. Operation and sampling First all the flow rates were adjusted and then the pump (5) was started. The caustic solution and air-chlorine mixture were circulated through the ejector. Sufficient time was given to flush the system before taking the samples. The sample was withdrawn using syringe form sample point no. S1. The samples were drawn one by one from sample point no. S2 and S3 after closing sample point S1. The above samples were analyzed. The procedure was repeated for different set of liquid concentration and gas concentration. The results are tabulated in Table A1.1. 3.2 Setup 2 3.2.1 Experimental set up The experimental setup for Stage 2 is shown schematically in Figure 3.4. In this setup the ejector having detail as Figure 3.3 and Table 3.1 is installed vertically. (photograph A.5.1) The schematic flow diagram is self indicative and self explanatory. There are two rotameters, RT1 and RT2, to measure flow rates of operating liquid and air respectively. The ଶ ܥ/ ଶ ܥ flow rate is measured with the help of soap film meter (GM2). There are four sample points S0, S1, S2 and S3 to collect liquid samples to measure concentration of caustic at inlet of ejector, immediate after free jet, at the end of the throat and at the end of diffuser respectively. There are two liquid tanks (1) separation vessel (SV) (2) solution reservoir (ST).The system contains V-1, V-2, V-3,V-4 and V-5 control valves to control the flow of fluids. 3.2.2 Experimental procedure The procedure is described stepwise as follows: 1. The nozzle plate to be studied was fixed on the jet ejector. Then empty runs were conducted by using water and air to check the leakage. 77

Figure 3.3 : Details of jet ejector used in experimental setup 2 2. Required strength of sodium hydroxide solution was prepared by circulating liquid through by pass line by adjusting valve V-3, V-4 and V-5. 3. Air flow rate and gas concentration were adjusted by circulating liquid from the tank (SV). During this process solution tank was kept isolated by keeping valve V-3 and V-4 closed. 78

SV = Separation Vessel ST = Solution Reservoir RT1 = Rotameter for Measuring Liquid flow rate RT 2 = Rotameter for Measuring Air flow rate RT3 = Rotameter for Measuring Solute gas GM1 & GM2 = Gas Film Meter P1 = Pumps S1, S2 & S3 = Sample points V1, V2, V3, V4, CV1, CV2, CV3 = Control Valves Figure 3.4 : Schematic diagram of experimental setup 2 4. After adjusting gas flow rate and gas concentration, valve V-2 was closed and required flow rate of caustic solution was adjusted by operating valve V-3, V-4 and V-5. 5. Once liquid flow rate, gas flow rate and gas concentration were set, the required samples were drawn and analyzed. 79

6. The procedure is repeated for another set of nozzle plate, liquid concentration and gas concentration. 7. The results are tabulated in Table A1.2. 3.3 Setup 3 3.3.1 Experimental set up 1. The experimental Setup 3 is shown schematically in Figure 3.6. This experiments were conducted on industrial stage ejector. The details of ejector are shown in Figure 3.5 and Table 3.1. (photograph A.5.2 and A.5.3 in appendix) Figure 3.5 : Detail of the jet ejector used in experimental setup 3 80

2. The schematic flow diagram is self indicative. 3. The ejector is having 3 sample point S1, S2 and S3. Sample S0 is drawn from tank T1 directly. The air flow rate is measured by using electronic anemometer. There is a rotameter for measuring ଶ ܥ flow rate and a soap film meter to calibrate the rotameter. There are two tanks T1 and T2. Tank T1 is used to prepare sodium hydroxide solution and tank T2 is ejector outlet tank. V1, V2, V3 and V4 are control valves. The pump P1 is provided to circulate sodium hydroxide solution through the ejector. Pressure gauge P1 is provided to measure the primary fluid pressure (water). Figure 3.6 : Schamatic diagram of experimental setup 3 3.3.2 Experimental procedure 1. The experimental procedure is almost same as in setup 1and setup 2. Before starting the experiment the rotameter for chlorine was calibrated by soap film meter. 2. The required nozzle plate was fitted. 3. The required sodium hydroxide concentration was prepared by circulating the solution and operating valve V5, V4, V2 and V3. 81

4. The primary fluid (aqueous ܪ solutions) flow rate was adjusted to the required value by operating valve V5 and V4. The secondary air flow rate was measured by electronic anemometer. The flow rate is kept constant throughout the experiment. 5. The required chlorine rate was adjusted by operating valve V1. After the system reaches steady state the liquid sample S0, S1, S2 and S3 were drawn and analyzed. 6. The experiment was repeated for different concentrations of sodium hydroxide and chlorine and nozzle plates. 7. The results are tabulated in Table A1.3. 82