A shock absorber is a mechanical device to damp shock impulse and convert kinetic energy into thermal energy. The damping effect of shock absorber depends on damping force and damping force is affected by various process parameters. In this analysis three process parameters damping diameter(A), number of holes(B) and suspension velocity(C) were considered and their effect on damping force of shock absorber was studied and accordingly suitable orthogonal array was selected by taguchi method. Experiment conducted on servo hydraulic testing machine and after conducting experiments damping force was measured and with the help of S/N ratio, ANOVA, Regression analysis optimum parameter values can be obtained and confirmation experiments was carried out. Twin tube shock absorber was used to carry out experimentation.
This document summarizes an experimental study on the slip factor in radial tipped centrifugal fans. It discusses that while previous studies assumed the slip factor only depends on impeller geometry, historical evidence and some experiments show it also depends on specific speed and flow rate. The objective of this study is to experimentally measure the slip factor at different locations around the impeller circumference for varying numbers of blades, and compare with theoretical correlations. An experimental setup was designed using a specially developed three-hole probe to measure local velocities. The slip factor is defined as the ratio of actual to theoretical exit whirl velocities. Theoretical velocities are calculated analytically, while actual velocities are measured experimentally for comparison.
CASE STUDY: Health analysis of reciprocating engines, compressors and gas pip...Abdul Basit Bashir
This paper refers to a detailed study conducted in March 2017 by SUMICO Technologies to evaluate the mechanical performance and condition of critical reciprocating engines, compressors and associated pipelines using state-of-the-art technologies at a natural gas booster station in Mari Gas Field (Sindh, Pakistan).
Results of the study revealed various hidden areas requiring attention to increase efficiency, reduce operational costs and increase reliability of the plant. This paper describes the technologies used, performance parameters analyzed,some interesting findings and the benefits gained through the study.
Prepared by Abdul Basit Bashir (SUMICO Technologies)
https://www.linkedin.com/in/abdulbasitb/
Diesel engine air swirl mesurements using avl test rigiaemedu
The document describes an experiment conducted to measure air swirl in diesel engine cylinders using an AVL steady flow test rig. Three inlet port designs - tangential, directed, and semi-helical - from engines of the same power range were tested. The AVL test rig measured parameters like mass flow rate, paddle wheel speed, and valve lift. Calculated parameters including swirl ratio, velocities, and flow coefficients were compared for the three port designs at varying valve lifts. The results provide insight into the air motion and swirl characteristics generated by each port design.
1. The document discusses experiments performed on converging and converging-diverging nozzles.
2. Converging nozzles accelerate fluid flow to supersonic speeds at the nozzle exit, while converging-diverging nozzles can accelerate fluids to both subsonic and supersonic regimes depending on pressure ratios.
3. Calculations are shown for mass flow rates through a nozzle at different pressure ratios using theoretical equations.
Vibration analysis of centrifugal blower impeller for various materials using...eSAT Publishing House
This document presents a vibration analysis of a centrifugal blower impeller made of different materials using finite element analysis. A centrifugal blower impeller model was created in CATIA and analyzed in ANSYS for three materials: steel, aluminum, and glass/epoxy composite. The analysis found that glass/epoxy composite had the lowest mass and equivalent stress but highest total and directional deformation compared to steel and aluminum. Steel and aluminum showed similar natural frequencies while glass/epoxy frequencies were much lower. Glass/epoxy also showed the highest deformational amplitude versus frequency. The study aims to evaluate materials for centrifugal blower impellers.
This document discusses strain gauge load cells for weight measurement. It describes the construction of a strain gauge load cell, which uses four strain gauges attached to a steel cylinder in a Wheatstone bridge configuration. It explains the principle of operation, where applied weight causes resistance changes in the strain gauges, unbalancing the bridge and creating an electrical output proportional to the load. Finally, it lists common applications of strain gauge load cells such as retail scales, crane scales, and vehicle weighing.
This document summarizes a study that used computational fluid dynamics (CFD) to simulate the performance of a single-stage axial flow compressor with varying blade aspect ratios of 1, 2, and 3. The study found that compressor performance is affected by aspect ratio, with the best operating conditions occurring between ratios of 2 and 3. Streamline analyses were conducted to analyze pressure and velocity distributions within the compressor and determine how parameters like mach number varied across different aspect ratio configurations. Modal analyses were also performed to study frequency responses at different vibration modes.
Characteristics of a simply converging nozzle through which steam is passesSaif al-din ali
1. The document describes experiments conducted on converging and converging-diverging nozzles. It discusses the theory behind how these nozzles work and how properties like pressure and velocity change within the nozzles.
2. Calculations are shown for the mass flow rate through the nozzles under different pressure ratios. The critical pressure ratio where the nozzle becomes choked is also calculated.
3. Results show the mass flow rate and critical pressure ratio for two test cases of varying inlet pressures.
This document summarizes an experimental study on the slip factor in radial tipped centrifugal fans. It discusses that while previous studies assumed the slip factor only depends on impeller geometry, historical evidence and some experiments show it also depends on specific speed and flow rate. The objective of this study is to experimentally measure the slip factor at different locations around the impeller circumference for varying numbers of blades, and compare with theoretical correlations. An experimental setup was designed using a specially developed three-hole probe to measure local velocities. The slip factor is defined as the ratio of actual to theoretical exit whirl velocities. Theoretical velocities are calculated analytically, while actual velocities are measured experimentally for comparison.
CASE STUDY: Health analysis of reciprocating engines, compressors and gas pip...Abdul Basit Bashir
This paper refers to a detailed study conducted in March 2017 by SUMICO Technologies to evaluate the mechanical performance and condition of critical reciprocating engines, compressors and associated pipelines using state-of-the-art technologies at a natural gas booster station in Mari Gas Field (Sindh, Pakistan).
Results of the study revealed various hidden areas requiring attention to increase efficiency, reduce operational costs and increase reliability of the plant. This paper describes the technologies used, performance parameters analyzed,some interesting findings and the benefits gained through the study.
Prepared by Abdul Basit Bashir (SUMICO Technologies)
https://www.linkedin.com/in/abdulbasitb/
Diesel engine air swirl mesurements using avl test rigiaemedu
The document describes an experiment conducted to measure air swirl in diesel engine cylinders using an AVL steady flow test rig. Three inlet port designs - tangential, directed, and semi-helical - from engines of the same power range were tested. The AVL test rig measured parameters like mass flow rate, paddle wheel speed, and valve lift. Calculated parameters including swirl ratio, velocities, and flow coefficients were compared for the three port designs at varying valve lifts. The results provide insight into the air motion and swirl characteristics generated by each port design.
1. The document discusses experiments performed on converging and converging-diverging nozzles.
2. Converging nozzles accelerate fluid flow to supersonic speeds at the nozzle exit, while converging-diverging nozzles can accelerate fluids to both subsonic and supersonic regimes depending on pressure ratios.
3. Calculations are shown for mass flow rates through a nozzle at different pressure ratios using theoretical equations.
Vibration analysis of centrifugal blower impeller for various materials using...eSAT Publishing House
This document presents a vibration analysis of a centrifugal blower impeller made of different materials using finite element analysis. A centrifugal blower impeller model was created in CATIA and analyzed in ANSYS for three materials: steel, aluminum, and glass/epoxy composite. The analysis found that glass/epoxy composite had the lowest mass and equivalent stress but highest total and directional deformation compared to steel and aluminum. Steel and aluminum showed similar natural frequencies while glass/epoxy frequencies were much lower. Glass/epoxy also showed the highest deformational amplitude versus frequency. The study aims to evaluate materials for centrifugal blower impellers.
This document discusses strain gauge load cells for weight measurement. It describes the construction of a strain gauge load cell, which uses four strain gauges attached to a steel cylinder in a Wheatstone bridge configuration. It explains the principle of operation, where applied weight causes resistance changes in the strain gauges, unbalancing the bridge and creating an electrical output proportional to the load. Finally, it lists common applications of strain gauge load cells such as retail scales, crane scales, and vehicle weighing.
This document summarizes a study that used computational fluid dynamics (CFD) to simulate the performance of a single-stage axial flow compressor with varying blade aspect ratios of 1, 2, and 3. The study found that compressor performance is affected by aspect ratio, with the best operating conditions occurring between ratios of 2 and 3. Streamline analyses were conducted to analyze pressure and velocity distributions within the compressor and determine how parameters like mach number varied across different aspect ratio configurations. Modal analyses were also performed to study frequency responses at different vibration modes.
Characteristics of a simply converging nozzle through which steam is passesSaif al-din ali
1. The document describes experiments conducted on converging and converging-diverging nozzles. It discusses the theory behind how these nozzles work and how properties like pressure and velocity change within the nozzles.
2. Calculations are shown for the mass flow rate through the nozzles under different pressure ratios. The critical pressure ratio where the nozzle becomes choked is also calculated.
3. Results show the mass flow rate and critical pressure ratio for two test cases of varying inlet pressures.
Axial compressor theory - stage-by-stage approach - 28th January 2010CangTo Cheah
The document discusses the stage-by-stage sizing approach for axial compressors. This approach allows designers to calculate blade angles and estimate pressure rise, temperature rise, and frictional losses at each stage. It introduces concepts like the de Haller number to minimize losses. A case study on the RB211-24G engine axial compressors is presented, showing blade angles and performance across 7 low pressure and 6 high pressure stages.
Numerical Simulation of the Aerodynamic Performance of a H-type Wind Turbine ...Capvidia NV
Wind Turbine Self Starting CFD Simulation with FlowVision This is a nice example for moving bodies. Moment of inertia of turbine is defined and rotation is induced by aerodynamics forces. Simulation results of rotation speed variation during self-starting are in well agreement with the experimental results.
Pressure distribution around a circular cylinder bodies | Fluid Laboratory Saif al-din ali
SAIF ALDIN ALI MADIN
سيف الدين علي ماضي
S96aif@gmail.com
A cylinder in a closed circuit wind tunnel will be experimented upon
to gather the pressure distribution acting on it
Laminar flow is defined when a fluid flows in parallel layers, with no
disruption between the layers. In comparison to this Turbulent flow
has a much more disorganized pattern, it is characterized by
mixing of the fluid by eddies of varying size within the flow.
The Reynolds number (Re), gives the measure for laminar and
turbulent flows. Laminar flow takes place when Reynolds number
is lower than 104, and for Turbulent flow the Re must be greater
than 3Ã-105.
The pressure is measured using the manometer, and then
therefore the pressure at the tapping must be the same as the
pressure head.
The cylinder being experimented on is placed in the wind tunnel.
The pressure upstream of the cylinder is sensed by a taping on the
tunnel wall and is connected to one of the tubes.
This document summarizes research conducted by students at the University of Illinois to analyze jet engine thrust performance through computational fluid dynamics (CFD) simulation and physical testing. The students used CFD software to model the flow through nozzle designs for a JetCat P140-RX miniature turbine engine. Thrust values predicted by the CFD simulations closely matched manufacturer specifications. The students also designed and built a test stand to physically validate thrust measurements of the engine mounted on bearings between parallel rails. Further CFD simulations and nozzle designs were planned to more fully validate simulation results against physical performance data.
Aircraft propulsion axial flow compressors off design performanceAnurak Atthasit
The document discusses axial flow compressors and their off-design performance. It covers topics such as compressor maps, surge lines, efficiency islands, best efficiency points, operating lines, surge margins, effects of inlet pressure distortion, Reynolds number, Mach number, and tip clearance on compressor performance. The conclusion summarizes that changes in total temperature, total pressure, Mach number, and density can affect compressor operation and efficiency.
Pressure distribution along convergent- divergent NozzleSaif al-din ali
SAIF ALDIN ALI MADIN
سيف الدين علي ماضي
S96aif@gmail.com
This aim of this practical was to investigate compressible flow in a
convergent-divergent nozzle. Different flow patterns that influence
the results of the investigation are also explored. The different
pressure distributions that occur at varying lengths in the nozzle
were also recorded and analyzed
This document presents a research paper on redesigning the compressor diffuser of a JetCat P90 turbine engine to improve efficiency. The objectives are to minimize the incidence angle of flow to the first stator vanes and reduce blockage in the diffuser. Computational fluid dynamics analysis was performed on the original and redesigned diffusers. The redesigned diffuser reduced total pressure loss by 7.4% compared to the original design. While theoretical improvements were shown, the redesign does not meet all geometry constraints of the engine.
Numerical Investigation of Single Stage of an Axial Flow Compressor for Effec...IJERA Editor
In present work, a compressor configuration is taken from literature which will be studied for aspect ratio (ratio between length of blade to chord length) influence over performance. Performance in the sense is pressure ratio of compressor. The aspect ratio of the blade is an important parameter and has a strong influence on the performance of axial flow compressor. There are so many literatures available on influence of design parameters of axial flow compressor over its performance. Few literatures only are available for effects of aspect ratio of blade over performance of compressor. A study is proposed to be carried out to verify the effect of aspect ratio on the performance of single stage subsonic compressor through ANSYS-CFX software. The analysis will be carried out for the constant tip diameter of the compressor rotor blade having an aspect ratio 1, 2 and 3 and to obtain the pressure loss and flow parameters of the compressor stage. Further increase in aspect ratio will lead to structural problem of compressor. Therefore, there will be optimum aspect ratio between 2 and 3. Simulation will be conducted to aspect ratios of 2.1, 2.2, 2.3, 2.4, 2.5, 2.6, 2.7, 2.8 and 2.9 to find optimum ratio using ANSYS-CFX commercial CFD software.
Design & Analysis of Centrifugal Pump Impeller by FEAIRJET Journal
This document summarizes the static analysis of a centrifugal pump impeller made of mild steel (MS) and stainless steel (SS) using finite element analysis. The analysis found that an SS impeller experienced slightly less stress (11.974 MPa) and slightly more deformation (0.002961 mm) compared to an MS impeller (12.043 MPa stress, 0.0028391 mm deformation). However, the SS impeller was lighter weight at 28.83 kg compared to 29.202 kg for the MS impeller. The analysis provides a comparison of these materials for use in centrifugal pump impellers to optimize strength and reduce weight.
Dynamic behaviour of hydraulic pressure relief valveIAEME Publication
1) The document analyzes the dynamic behavior of a direct spring-operated pressure relief valve and the influence of the poppet's radial clearance on that behavior.
2) A mathematical model is developed and represented in MATLAB/Simulink. Simulation results show that smaller radial clearances lead to longer opening times and greater pressure overshoots, while larger clearances result in shorter opening times and smaller overshoots.
3) An optimal poppet radial clearance is estimated that provides a settling time of 0.02 seconds and minimizes pressure overshoot. The model can predict valve behavior and help select optimal settings.
Axial compressor theory - stage-wise isentropic efficiency - 18th March 2010CangTo Cheah
This document discusses the theory of stage-wise isentropic efficiency in axial compressors. It covers determining the pitch and chord between blades, calculating the number of blades based on pitch, and formulas for static pressure rise and forces acting on cascades, including lift and drag forces. Graphs are presented for mean deflection and stagnation pressure loss as functions of incidence angle. The document aims to calculate coefficients for drag, lift, and loss based on these graphs and the presented formulas.
Influence of number of impeller and diffuser blades on the pressure recovery ...eSAT Journals
This document summarizes a numerical analysis that investigated the influence of the number of impeller and diffuser blades on the pressure recovery of a centrifugal fan. The analysis found that higher numbers of impeller blades (up to 14 blades) resulted in better pressure recovery due to improved blade loading. Additionally, a smaller number of diffuser blades (12 blades) produced higher pressure recovery by avoiding flow separation and stall near the blades. In general, the analysis showed that configurations with more impeller blades and fewer diffuser blades achieved better static pressure recovery and lower total pressure losses across the fan.
Using the convergent steam nozzle type in the entranceSaif al-din ali
This document discusses using a convergent steam nozzle in the entrance region of a steam turbine. It provides background on steam turbines and how they work, describing how steam is expanded through nozzles to convert heat energy to kinetic energy. It then discusses different types of steam nozzles, focusing on convergent nozzles, and how nozzle shape affects steam velocity and pressure distribution. A numerical simulation will be performed to analyze pressure and velocity within a simple convergent nozzle design.
Factors effecting vertical lift performanceJALEEL AHMED
This document discusses factors that affect vertical lift performance (VLP) in oil and gas wells. It explains that VLP is determined by calculating pressure losses versus production rate. The main factors that influence VLP are choke size, gas-liquid ratio, and tubing diameter. Changing the choke opening affects wellhead pressure and shifts the VLP curve. Increasing the gas-liquid ratio can initially improve VLP up to a point, by reducing density. Larger tubing diameters also initially increase flow rates and VLP, but beyond a critical size, pressure losses from friction and acceleration dominate.
The document outlines various SolidWorks simulation examples for analyzing components used in oil and gas applications. It describes structural, vibration and buckling analyses of skid platforms and weldments. Additional examples include pressure vessel design ensuring ASME code compliance, earthquake simulation, umbilical strength analysis, and manhole nozzle flange design. Flow simulations are shown for propane through a valve, air through a manifold system, and around a drill bit. HVAC analyses include airflow optimization and modeling advanced radiation transfer.
An On-Chip Bus Tracer Analyzer With Amba AHB For Real Time Tracing With Lossl...IJERA Editor
The Advanced Microcontroller Bus Architecture (AMBA) widely used as the on-chip bus in System-on-a-chip (SoC) designs. The important aspect of a SoC is not only which components or blocks it houses, but also how they are interconnected. AMBA is a solution for the blocks to interface with each other. The biggest challenge in SoC design is in validating and testing the system. AHB Bus Tracer is a significant infrastructure that is needed to monitor the on chip-bus signals, which is vital for debugging and performance analysis and also optimizing the SOC. Basically on chip signals are difficult to observe since they are deeply embedded in a SoC and no sufficient I/O pins are required to access those signals. Therefore, we embed a bus tracer in SoC to capture the bus signals and store them. The AMBA AHB should be used to which are high bandwidth and require the high performance of a pipelined bus interface. Performance can be improved at high-frequency operation. Performance is independent of the mark-space ratio of the clock. No special considerations are required for automatic test insertion. Our aim in this project is to Design the AHB- protocol with bus tracer. For real-time tracing, we should reduce the trace size as much as possible without reducing the original data.SYS-HMRBT supports tracing after/before an event triggering, named post-triggering trace/pre-triggering trace, respectively. SYS-HMRBT runs at 500 MHz and costs 42 K gates in TSMC 0.13- m technology, indicating that it is capable of real time tracing and is very small in modern SoCs.The experimental results show that trace compression ratio reduced by 96.32%. Finally this approach was designed successfully along with MODEL SIM and synthesis using Xilinx ISE. The SoC can be verified in field-programmable gate array.
Mmc1 2 The Lancet - Supplementary appendix 10/15/2014John Redaelli
This appendix formed part of the original submission and has been peer reviewed.
We post it as supplied by the authors.
Supplement to: Schwartz SD, Regillo CD, Lam BL, et al. Human embryonic stem
cell-derived retinal pigment epithelium in patients with age-related macular degeneration
and Stargardt’s macular dystrophy: follow-up of two open-label phase 1/2 studies. Lancet
2014; published online Oct 15. http://dx.doi.org/10.1016/S0140-6736(14)61376-3.
Parallel Processing Technique for Time Efficient Matrix MultiplicationIJERA Editor
The document proposes a parallel-parallel input single output (PPI-SO) design for matrix multiplication that reduces hardware resources compared to existing designs. It uses fewer multipliers and registers than existing designs, trading off increased completion time. Simulation results show the PPI-SO design uses 30% less energy and involves 70% less area-delay product than other designs.
Empirical Determination of Locations of Unstable and Blank Gsm Signal Network...IJERA Editor
In a GSM network coverage area there exist locations where network signal reception is always either unsteady or blank. These problems are the cause of intermittent call receptions or no network reception at some locations in cell sites. This paper discusses a practical work carried out in a cell site located in a remote area in Eastern Nigeria to determine such locations. To do that, received signal field strength measurements were initially conducted at 3m interval starting from 100m away from the base Station to determine the suspected locations of unsteady and blank network receptions in the field. Further extensive measurements were then taken at each of the suspect locations. Analyses of the data obtained shows that a lot of such phenomenon may exist in cell sites.
Axial compressor theory - stage-by-stage approach - 28th January 2010CangTo Cheah
The document discusses the stage-by-stage sizing approach for axial compressors. This approach allows designers to calculate blade angles and estimate pressure rise, temperature rise, and frictional losses at each stage. It introduces concepts like the de Haller number to minimize losses. A case study on the RB211-24G engine axial compressors is presented, showing blade angles and performance across 7 low pressure and 6 high pressure stages.
Numerical Simulation of the Aerodynamic Performance of a H-type Wind Turbine ...Capvidia NV
Wind Turbine Self Starting CFD Simulation with FlowVision This is a nice example for moving bodies. Moment of inertia of turbine is defined and rotation is induced by aerodynamics forces. Simulation results of rotation speed variation during self-starting are in well agreement with the experimental results.
Pressure distribution around a circular cylinder bodies | Fluid Laboratory Saif al-din ali
SAIF ALDIN ALI MADIN
سيف الدين علي ماضي
S96aif@gmail.com
A cylinder in a closed circuit wind tunnel will be experimented upon
to gather the pressure distribution acting on it
Laminar flow is defined when a fluid flows in parallel layers, with no
disruption between the layers. In comparison to this Turbulent flow
has a much more disorganized pattern, it is characterized by
mixing of the fluid by eddies of varying size within the flow.
The Reynolds number (Re), gives the measure for laminar and
turbulent flows. Laminar flow takes place when Reynolds number
is lower than 104, and for Turbulent flow the Re must be greater
than 3Ã-105.
The pressure is measured using the manometer, and then
therefore the pressure at the tapping must be the same as the
pressure head.
The cylinder being experimented on is placed in the wind tunnel.
The pressure upstream of the cylinder is sensed by a taping on the
tunnel wall and is connected to one of the tubes.
This document summarizes research conducted by students at the University of Illinois to analyze jet engine thrust performance through computational fluid dynamics (CFD) simulation and physical testing. The students used CFD software to model the flow through nozzle designs for a JetCat P140-RX miniature turbine engine. Thrust values predicted by the CFD simulations closely matched manufacturer specifications. The students also designed and built a test stand to physically validate thrust measurements of the engine mounted on bearings between parallel rails. Further CFD simulations and nozzle designs were planned to more fully validate simulation results against physical performance data.
Aircraft propulsion axial flow compressors off design performanceAnurak Atthasit
The document discusses axial flow compressors and their off-design performance. It covers topics such as compressor maps, surge lines, efficiency islands, best efficiency points, operating lines, surge margins, effects of inlet pressure distortion, Reynolds number, Mach number, and tip clearance on compressor performance. The conclusion summarizes that changes in total temperature, total pressure, Mach number, and density can affect compressor operation and efficiency.
Pressure distribution along convergent- divergent NozzleSaif al-din ali
SAIF ALDIN ALI MADIN
سيف الدين علي ماضي
S96aif@gmail.com
This aim of this practical was to investigate compressible flow in a
convergent-divergent nozzle. Different flow patterns that influence
the results of the investigation are also explored. The different
pressure distributions that occur at varying lengths in the nozzle
were also recorded and analyzed
This document presents a research paper on redesigning the compressor diffuser of a JetCat P90 turbine engine to improve efficiency. The objectives are to minimize the incidence angle of flow to the first stator vanes and reduce blockage in the diffuser. Computational fluid dynamics analysis was performed on the original and redesigned diffusers. The redesigned diffuser reduced total pressure loss by 7.4% compared to the original design. While theoretical improvements were shown, the redesign does not meet all geometry constraints of the engine.
Numerical Investigation of Single Stage of an Axial Flow Compressor for Effec...IJERA Editor
In present work, a compressor configuration is taken from literature which will be studied for aspect ratio (ratio between length of blade to chord length) influence over performance. Performance in the sense is pressure ratio of compressor. The aspect ratio of the blade is an important parameter and has a strong influence on the performance of axial flow compressor. There are so many literatures available on influence of design parameters of axial flow compressor over its performance. Few literatures only are available for effects of aspect ratio of blade over performance of compressor. A study is proposed to be carried out to verify the effect of aspect ratio on the performance of single stage subsonic compressor through ANSYS-CFX software. The analysis will be carried out for the constant tip diameter of the compressor rotor blade having an aspect ratio 1, 2 and 3 and to obtain the pressure loss and flow parameters of the compressor stage. Further increase in aspect ratio will lead to structural problem of compressor. Therefore, there will be optimum aspect ratio between 2 and 3. Simulation will be conducted to aspect ratios of 2.1, 2.2, 2.3, 2.4, 2.5, 2.6, 2.7, 2.8 and 2.9 to find optimum ratio using ANSYS-CFX commercial CFD software.
Design & Analysis of Centrifugal Pump Impeller by FEAIRJET Journal
This document summarizes the static analysis of a centrifugal pump impeller made of mild steel (MS) and stainless steel (SS) using finite element analysis. The analysis found that an SS impeller experienced slightly less stress (11.974 MPa) and slightly more deformation (0.002961 mm) compared to an MS impeller (12.043 MPa stress, 0.0028391 mm deformation). However, the SS impeller was lighter weight at 28.83 kg compared to 29.202 kg for the MS impeller. The analysis provides a comparison of these materials for use in centrifugal pump impellers to optimize strength and reduce weight.
Dynamic behaviour of hydraulic pressure relief valveIAEME Publication
1) The document analyzes the dynamic behavior of a direct spring-operated pressure relief valve and the influence of the poppet's radial clearance on that behavior.
2) A mathematical model is developed and represented in MATLAB/Simulink. Simulation results show that smaller radial clearances lead to longer opening times and greater pressure overshoots, while larger clearances result in shorter opening times and smaller overshoots.
3) An optimal poppet radial clearance is estimated that provides a settling time of 0.02 seconds and minimizes pressure overshoot. The model can predict valve behavior and help select optimal settings.
Axial compressor theory - stage-wise isentropic efficiency - 18th March 2010CangTo Cheah
This document discusses the theory of stage-wise isentropic efficiency in axial compressors. It covers determining the pitch and chord between blades, calculating the number of blades based on pitch, and formulas for static pressure rise and forces acting on cascades, including lift and drag forces. Graphs are presented for mean deflection and stagnation pressure loss as functions of incidence angle. The document aims to calculate coefficients for drag, lift, and loss based on these graphs and the presented formulas.
Influence of number of impeller and diffuser blades on the pressure recovery ...eSAT Journals
This document summarizes a numerical analysis that investigated the influence of the number of impeller and diffuser blades on the pressure recovery of a centrifugal fan. The analysis found that higher numbers of impeller blades (up to 14 blades) resulted in better pressure recovery due to improved blade loading. Additionally, a smaller number of diffuser blades (12 blades) produced higher pressure recovery by avoiding flow separation and stall near the blades. In general, the analysis showed that configurations with more impeller blades and fewer diffuser blades achieved better static pressure recovery and lower total pressure losses across the fan.
Using the convergent steam nozzle type in the entranceSaif al-din ali
This document discusses using a convergent steam nozzle in the entrance region of a steam turbine. It provides background on steam turbines and how they work, describing how steam is expanded through nozzles to convert heat energy to kinetic energy. It then discusses different types of steam nozzles, focusing on convergent nozzles, and how nozzle shape affects steam velocity and pressure distribution. A numerical simulation will be performed to analyze pressure and velocity within a simple convergent nozzle design.
Factors effecting vertical lift performanceJALEEL AHMED
This document discusses factors that affect vertical lift performance (VLP) in oil and gas wells. It explains that VLP is determined by calculating pressure losses versus production rate. The main factors that influence VLP are choke size, gas-liquid ratio, and tubing diameter. Changing the choke opening affects wellhead pressure and shifts the VLP curve. Increasing the gas-liquid ratio can initially improve VLP up to a point, by reducing density. Larger tubing diameters also initially increase flow rates and VLP, but beyond a critical size, pressure losses from friction and acceleration dominate.
The document outlines various SolidWorks simulation examples for analyzing components used in oil and gas applications. It describes structural, vibration and buckling analyses of skid platforms and weldments. Additional examples include pressure vessel design ensuring ASME code compliance, earthquake simulation, umbilical strength analysis, and manhole nozzle flange design. Flow simulations are shown for propane through a valve, air through a manifold system, and around a drill bit. HVAC analyses include airflow optimization and modeling advanced radiation transfer.
An On-Chip Bus Tracer Analyzer With Amba AHB For Real Time Tracing With Lossl...IJERA Editor
The Advanced Microcontroller Bus Architecture (AMBA) widely used as the on-chip bus in System-on-a-chip (SoC) designs. The important aspect of a SoC is not only which components or blocks it houses, but also how they are interconnected. AMBA is a solution for the blocks to interface with each other. The biggest challenge in SoC design is in validating and testing the system. AHB Bus Tracer is a significant infrastructure that is needed to monitor the on chip-bus signals, which is vital for debugging and performance analysis and also optimizing the SOC. Basically on chip signals are difficult to observe since they are deeply embedded in a SoC and no sufficient I/O pins are required to access those signals. Therefore, we embed a bus tracer in SoC to capture the bus signals and store them. The AMBA AHB should be used to which are high bandwidth and require the high performance of a pipelined bus interface. Performance can be improved at high-frequency operation. Performance is independent of the mark-space ratio of the clock. No special considerations are required for automatic test insertion. Our aim in this project is to Design the AHB- protocol with bus tracer. For real-time tracing, we should reduce the trace size as much as possible without reducing the original data.SYS-HMRBT supports tracing after/before an event triggering, named post-triggering trace/pre-triggering trace, respectively. SYS-HMRBT runs at 500 MHz and costs 42 K gates in TSMC 0.13- m technology, indicating that it is capable of real time tracing and is very small in modern SoCs.The experimental results show that trace compression ratio reduced by 96.32%. Finally this approach was designed successfully along with MODEL SIM and synthesis using Xilinx ISE. The SoC can be verified in field-programmable gate array.
Mmc1 2 The Lancet - Supplementary appendix 10/15/2014John Redaelli
This appendix formed part of the original submission and has been peer reviewed.
We post it as supplied by the authors.
Supplement to: Schwartz SD, Regillo CD, Lam BL, et al. Human embryonic stem
cell-derived retinal pigment epithelium in patients with age-related macular degeneration
and Stargardt’s macular dystrophy: follow-up of two open-label phase 1/2 studies. Lancet
2014; published online Oct 15. http://dx.doi.org/10.1016/S0140-6736(14)61376-3.
Parallel Processing Technique for Time Efficient Matrix MultiplicationIJERA Editor
The document proposes a parallel-parallel input single output (PPI-SO) design for matrix multiplication that reduces hardware resources compared to existing designs. It uses fewer multipliers and registers than existing designs, trading off increased completion time. Simulation results show the PPI-SO design uses 30% less energy and involves 70% less area-delay product than other designs.
Empirical Determination of Locations of Unstable and Blank Gsm Signal Network...IJERA Editor
In a GSM network coverage area there exist locations where network signal reception is always either unsteady or blank. These problems are the cause of intermittent call receptions or no network reception at some locations in cell sites. This paper discusses a practical work carried out in a cell site located in a remote area in Eastern Nigeria to determine such locations. To do that, received signal field strength measurements were initially conducted at 3m interval starting from 100m away from the base Station to determine the suspected locations of unsteady and blank network receptions in the field. Further extensive measurements were then taken at each of the suspect locations. Analyses of the data obtained shows that a lot of such phenomenon may exist in cell sites.
El documento analiza la ética del conocimiento de sí mismo en Pedro Abelardo. Abelardo creía que conocerse a uno mismo era fundamental para la ética y defendió propuestas éticas innovadoras que lo llevaron a conflictos con la Iglesia. Abelardo también distinguió entre vicios, pecados y acciones malas, y argumentó que factores naturales influyen en el comportamiento pero no determinan si una persona es pecadora.
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Experimental investigation of damping force of twin tube shock absorber
1. Sandip K. Kadu Int. Journal of Engineering Research and Applications www.ijera.com
ISSN : 2248-9622, Vol. 4, Issue 9( Version 5), September 2014, pp.59-64
www.ijera.com 59 | P a g e
Experimental investigation of damping force of twin tube shock absorber Sandip K. Kadu1, Milind S. Mhaske2 1(Department of Mechanical engineering, PUNE University, India) 2 (Department of Mechanical engineering, PUNE University, India) ABSTRACT A shock absorber is a mechanical device to damp shock impulse and convert kinetic energy into thermal energy. The damping effect of shock absorber depends on damping force and damping force is affected by various process parameters. In this analysis three process parameters damping diameter(A), number of holes(B) and suspension velocity(C) were considered and their effect on damping force of shock absorber was studied and accordingly suitable orthogonal array was selected by taguchi method. Experiment conducted on servo hydraulic testing machine and after conducting experiments damping force was measured and with the help of S/N ratio, ANOVA, Regression analysis optimum parameter values can be obtained and confirmation experiments was carried out. Twin tube shock absorber was used to carry out experimentation.
Keywords – Twin tube shock absorber, Taguchi method, damping force, process parameters
I. INTRODUCTION
Shock absorber is used to absorbs or dissipate energy. In vehicle it reduces the effect of travelling over rough road. Leading to improved ride quality and increase in comfort due to reduced amplitude and disturbances. Twin tube type shock absorber also known as a "two-tube" shock absorber, this device consists of two nested cylindrical tubes, an inner tube that is called the "working tube" or the "pressure tube", and an outer tube called the "reserve tube". At the bottom of the device on the inside is a compression valve or base valve. When the piston is forced up or down by bumps in the road, hydraulic fluid moves between different chambers via small holes or "orifices" in the piston and via the valve, converting the "shock". Twin tube type shock absorber consists of two tube like inner tube and outer tube. Also, consists components like spring, piston, piston rod, retracting spring, piston plate, shims etc. Out of these components piston plate has holes called damping holes of different diameter which plays more important role in damping effect along with the suspension velocity. For achieving maximum damping force, optimisation is done by varying process parameters such as, A) Damping diameter B) Number of damping holes C) Suspension velocity by using L9 orthogonal array of Taguchi method. The objective of optimization of damping force is to provide ride comfort and driving safety for passenger. In this paper test parameters was optimized for maximum damping force by taguchi method. It is
proved that signal to noise ratio is used to optimize various process parameters.[1][2][3]
II. THEORY
1. Elements of Twin tube rear shock absorber: Basically the shock absorber consists of a piston which moves up and down in a fluid-filled cylinder. The cylinder is fastened to the axle or, wheel suspension, and the piston is connected via the piston rod to the frame of' the vehicle. As the piston is forced to move with respect to the cylinder, a pressure differential is developed across the piston, causing the fluid to flow through orifices and valves in the piston. The portion of the cylinder above the piston is known as the rebound chamber, and the portion of the cylinder below the piston is known as the compression chamber. And the volume which surrounds the cylinder is known as the reservoir chamber. The reservoir chamber is partially filled with fluid and partially filled with a gas phase, normally air. The fluid flow between the compression and reservoir chambers passes through the body valve assembly at the bottom of the compression chamber shown in fig1.[4]
RESEARCH ARTICLE OPEN ACCESS
2. Sandip K. Kadu Int. Journal of Engineering Research and Applications www.ijera.com
ISSN : 2248-9622, Vol. 4, Issue 9( Version 5), September 2014, pp.59-64
www.ijera.com 60 | P a g e
Fig 1. Elements of Twin tube rear shock absorber
1. Top Spring Cover.
2. Outer Cylinder-Reservoir tube.
3. Spring Adjuster.
4. Axle Eye.
5. Inner helical Spring-Helper Spring.
6. Outer Helical Spring-Main Spring.
7. Spring Supporter.
8. Spring Seat.
9. Inner Tube-Reservoir.
10. Piston-Assembly.
11. Chassis Eye.
12. Base Valve.
2. Experimental set up: An experiment was carried out on servo hydraulic testing machine. The test system contains servo control system, signal acquisition system, function generator, security monitoring system, digital A/D interface system, servo valve driver and the twin-tube hydraulic shock absorber and so on.
Fig.2. Servo hydraulic testing machine The specific scheme of the testing is designed, as follows: Clamping the shock absorber: The lower end of a shock absorber is vertically fixed to the hydraulic servo-platform the upper end is fastened to the rigid beam equipped with force sensor. The shock absorber is adjusted along the vertical direction to ensure that piston does not produce eccentric wear during loading process. Then the initial position of servo-console should be adjusted to ensure the piston locate in the middle of effective stroke. Loading the shock absorber: The excitation frequency, amplitude and sampling frequency are all typed into computer. The driving signal of sinusoidal displacement is produced through a function generator. The signal is amplified by the digital A/D interface to make servo platform excite the shock absorber according to pre input frequency and amplitude. Collecting the data: Because the excitation method is displacement driving, the displacement signal of the shock absorber piston can be directly obtained by pre-input signal and the damping force can be recorded through force sensor on rigid beam. [5] . Experimental Details:
1) Design of experiments: Well organised experimental procedure is needed to identify system performance and to evaluate effect of input parameters on objective parameter. Traditional methods will increase number of experimentations. Taguchi method is used to identify optimal suspension parameter for maximum damping force. Taguchi method is an efficient tool for acquiring optimal process parameters. In this method, the
3. Sandip K. Kadu Int. Journal of Engineering Research and Applications www.ijera.com
ISSN : 2248-9622, Vol. 4, Issue 9( Version 5), September 2014, pp.59-64
www.ijera.com 61 | P a g e
number of experiments is reduced. In this method, two important tools are used: (1) orthogonal array and (2) signal-to noise ratio. In this study we have consider 3 factors which affect majorly on quality characteristic such as (A) Damping Diameter, (B) Number of damping holes (C) Suspension velocity. The design of experiment was carried out by Taguchi methodology In this technique the main objective is to optimize damping force of rear suspension that is influenced by various process parameters. 2) Selection of control factors: As damping force has adverse effect on riding comfort, driving safety and vehicle stability. So the damping force was considered as a response parameter for experimentation. 3) Selection of orthogonal array: An orthogonal array for process design is applied on the knowledge of control factors and levels. The number of experiments can be reduced using orthogonal array In this study, L9 orthogonal array have been selected This orthogonal array has three columns and nine experiment Since 3 controllable factors and three levels of each factor were considered L9 (3**3) Orthogonal Array was selected for this study. 4) Process parameters: Twin tube shock absorber of two wheeler selected for experimentation. The experiments were carried out on Servo Hydraulic test system for damping force testing. There are three input controlling factors selected as different damping diameter, different number of holes and different suspension velocity having three levels. Details of parameters and their levels used shown in the table1 Table 1. Process parameters and levels
A
Damping Dia.(mm)
1.8
1.9
2.0
B
No. of damping holes
4
6
8
C
S-Velocity(m/s)
0.3
0.5
1
Table 2. Layout for experimental design
Expt. No.
A
B
C
Result (Damping Force) N
1
1.8
4
0.3
400
2
1.8
5
0.5
500
3
1.8
6
1
600
4
1.9
4
0.5
500
5
1.9
5
1
650
6
1.9
6
0.3
350
7
2
4
1
600
8
2
5
0.3
300
9
2
6
0.5
450
III. RESULT AND DISCUSSIONS
1. S/N Ratio Analysis:
Signal-to-noise (S/N) ratio is then derived from the loss function. There are three types of S/N ratios depending upon type of characteristics Lower is better (LB), nominal is best (NB), higher is better (HB). In vehicle suspension system higher damping force be as a sign of better ride quality. Therefore “HB” is chosen for the damping force and it is calculated as the logarithmic transformation of the loss function as shown below. With the S/N and ANOVA analyses, the optimal combination of the process parameters can be predicted. In this study, in order to minimize the defects, higher is better S/N ratio is chosen. Higher is better S/N ratios are computed, and the values are recorded.
……………(1)
Where, n = number of repetitions or observations yi = the observed data. Table 3. S/N Ratio analysis of Damping Force
Exp. no.
A
B
C
Result (Damping Force)
S/N Ratio
1
1.8
4
0.3
400
52.0412
2
1.8
5
0.5
500
53.9794
3
1.8
6
1
600
55.563
4
1.9
4
0.5
500
53.9794
5
1.9
5
1
650
56.2583
6
1.9
6
0.3
350
50.8814
7
2
4
1
600
55.563
8
2
5
0.3
300
49.5424
9
2
6
0.5
450
53.0643
Higher value of S/N ratio corresponds to optimal level of input parameter. From table 3 it is cleared that optimal input parameter are damping diameter at level(2), number of holes at level(2), suspension velocity at level(3). i.e. Damping diameter (1.9 mm), No. of Holes (5), and suspension velocity (1 m/s).
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Table 4. Estimated model coefficient for S/N Ratio
Term
Coeff.
SE Coeff.
T
P
Constant
53.4303
0.2204
242.422
0
Dia 1.8
0.4309
0.3117
1.383
0.301
Dia 1.9
0.2761
0.3117
0.886
0.469
no. of h 4
0.4309
0.3117
1.383
0.301
no. of h 5
-0.2607
0.3117
-0.836
0.491
s.veloci 0.3
-2.6086
0.3117
-8.369
0.014
s.veloci 0.5
0.2441
0.3117
0.783
0.516
Summary of Model- S = 0.6612 R-Sq = 97.9% R-Sq(adj) = 91.5% Table 5. Response table for signal to noise ratio larger the better
Level
Diameter (mm)
No. of hole
Suspension velocity
1
53.86
53.86
50.82
2
53.71
53.17
53.67
3
52.72
53.26
55.79
Delta
1.14
0.69
4.97
Rank
2
3
1
2.Analysis of Variance (ANOVA): ANOVA is objective decision making for determining the average performance of group of parameter tested and it is helpful in determining the significance of all parameters. The analysis of variance was used to identify the important input parameters which effects Damping force. Once the experiment has been conducted, the ANOVA is carried out using the results of the experiments by making use of minitab14 software. The significant factors in the shock absorber defects were determined. The analysis of the experimental data is carried out using the software MINITAB 14 specially used for design of experiment applications. In order to find out statistical Significance of various factors like damping diameter (A), number of holes (B), and suspension velocity (C), and their interactions on damping force, analysis of variance (ANOVA) is performed on experimental data.
Table 6. Analysis of variance for S/N Ratios
Source
DF
Seq SS
Adj SS
Adj MS
F
P
A
2
2.2855
2.2855
1.1427
2.61
0.277
B
2
0.848
0.848
0.424
0.97
0.508
C
2
37.366
37.366
18.683
42.7
0.023
Error
2
0.8744
0.8744
0.4372
Total
8
41.374
The results of ANOVA are shown in table 6 it is clear that the parameters A, C, and D significantly affect the damping force. Larger F- value indicates that the variation of process parameters makes a big change on the performance. The last column of the table shows that p-value for the individual control factors. Smaller the p-value, greater the significance of the parameter. The ANOVA table for S/N ratio (Table 6) indicate that, the damping diameter (p=0.277), Number of hole (p= 0.508) and suspension velocity (p=0.023) in this order, are significant control factors affecting damping force. It means, the suspension velocity is the most significant factor followed by damping diameter and number of holes. Percent contribution(P) to the total sum of square can be used to evaluate the importance of a change in the process parameter on these quality characteristics. (P)=(SS’A/SST)*100…………………….(2) Table 7. Optimum condition and Percentage contribution
Sr.
Factors
Level Description
Level
Contribution
No.
(%)
1
A: Damping Dia.
1.9
2
5.52
2
B: No. of Hole
5
3
2.04
3
C: Suspension Velocity
1
1
90.31
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3. Regression analysis: The regression equation generated by minitab14 software is, Y=826-250*A-16.7*B+359*C ………(3) Where, Y is the response in terms of damping force and A, B, C is input parameters. S = 42.5923 R-Sq = 92.1% R-Sq (adj) = 87.4% If we put optimum parameters which are drawn by ANOVA in equation 1 it will give optimum value of quality characteristic which will maximum Damping force. Y = 826 - 250*A - 16.7*B + 359*C Y = 826 - 250*1.9 - 16.7*5 + 359*1 Y = 626.5 N predicted by regression equation. 4. Confirmation of Result: Confirmation experiments were carried out on optimal parameters that are A2B2C3 by setting up three trials. The results shown by experimented evaluation and predicted by regression equation with error of 1.08% which less than 5%. Hence this mathematical model is feasible and effective.
IV. CONCLUSION
It is found that taguchi method of parameter design can be performed with minimum number of experimentations and it provides simple, efficient, systematic methodology for optimizing the process parameters. The Taguchi method was applied to find an optimum setting of the damping force parameters process. The result from the Taguchi method chooses an optimum solution from combinations of factors
The results are summarized as follows:
Parameters like damping diameter, number of holes and suspension velocity are selected for maximization of damping force.
The largest impact on the characteristics of the damping force is from parameters like suspension velocity followed by damping diameter, number of holes.
From results we come to conclusion that damping diameter at level 2, the number of holes at level 2, suspension velocity at level 3 is recommended for maximization of damping force.
The results of confirmation experiment well satisfied with optimal setting.
The result of present investigation is valid within specified range of process parameters.
Also the prediction made by Regression Analysis is in good agreement with Confirmation results.
The optimal levels of Damping force process parameters for optimum damping force are:
Parameters
Optimum value
Damping Diameter (mm)
1.9
Number of Hole
5
Suspension Velocity (m/s)
1
REFERENCES
Journal Papers: [1] Arokiasamy Mariajayaprakash, Thiyagarajan Senthilvelan and Krishnapillai Ponnambal Vivekananthan,” Optimisation of shock absorber process parameters using failure mode and effect analysis and genetic algorithm”, International Journal of Industrial Engineering 2013 [2] Hashmi Ayas Jameel Ahmed, Rathi M.G., “Analysis of damping force of two wheeler front suspension”, International Journal of Engineering Research & Technology (IJERT) ISSN: 2278-0181 Vol. 2 Issue 6 (2013) 428- 434. [3] J .C.Dixon, Shock Absorber Handbook, john wiley and sons. [4] Choon-Tae Leea, Byung-Young Moon, “Simulation and experimental validation of vehicle dynamic characteristics for displacement-sensitive shock absorber using fluid-flow modeling” Mechanical Systems and Signal Processing 20 (2006) 373– 388.(elements of shock absorber)
error 2%
B: 2%
A: 6%
C:90.31%
Pie Chart
1
2
3
4
Obs.
Trial
Avg. damping force (N)
S/N Ratio
1
2
3
Expe.
Predi.
% Error
1
630
650
620
633.3
626.5
1.078
52.99
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[5] Yongijie Lu, Shaohua Li, Na Chen, “ Research on damping Charecteristics of shock absorber for heavy vehicle”, Reaserch journal of applied sciences, engineering and technology 5(3): 842-847, 2013.(Test rig) [6] Rama Rao. S, Padmanabhan Application of Taguchi methods and ANOVA in optimization of process parameters for metal removal rate in electrochemical machining of Al/5%SiC composites”, International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 Vol. 2, Issue 3, May-Jun 2012, pp. 192-197 [7] P.Senthil kumar, R.Kalidas, K.Sivakumar, E.Hariharan, B.Gautham,“Application of Taguchi method for optimizingpassenger- friendly vehicle suspension system”, International Journal of Latest Trends in Engineering and Technology (IJLTET), Vol. 2 [8] Douglas C.Montgomery , Design and Analysis of Experiments pp 393 [9] Taguchi G, Konishi S. Taguchi methods, orthogonal arrays and linear graphs, tools for quality American supplier institute. American Supplier Institute; (1987) 8–35. [10] M.A.Jadhav, S.B.Belkar, R.R.kharde, “Analysis of Displacement Sensitive Twin Tube Shock Absorber” International Journal of Engineering Research and Development, Volume 5, Issue 5 (2012) 31-41. [11] Keith Wordena, DarylHickey, et.al, “Nonlinear system identification of automotive dampers: A time and frequency- domain analysis”, Mechanical Systems and Signal Processing 23 (2009) 104–126