Diesel Cycle Analysis



Similar documents
FUNDAMENTALS OF ENGINEERING THERMODYNAMICS

APPLIED THERMODYNAMICS. TUTORIAL No.3 GAS TURBINE POWER CYCLES. Revise gas expansions in turbines. Study the Joule cycle with friction.

How To Calculate The Performance Of A Refrigerator And Heat Pump

APPLIED THERMODYNAMICS TUTORIAL 1 REVISION OF ISENTROPIC EFFICIENCY ADVANCED STEAM CYCLES

Engineering Problem Solving as Model Building

An analysis of a thermal power plant working on a Rankine cycle: A theoretical investigation

CO MPa (abs) 20 C

The First Law of Thermodynamics

Jet Propulsion. Lecture-2. Ujjwal K Saha, Ph.D. Department of Mechanical Engineering Indian Institute of Technology Guwahati 1

Chapters 7. Performance Comparison of CI and SI Engines. Performance Comparison of CI and SI Engines con t. SI vs CI Performance Comparison

Lesson. 11 Vapour Compression Refrigeration Systems: Performance Aspects And Cycle Modifications. Version 1 ME, IIT Kharagpur 1

OUTCOME 2 INTERNAL COMBUSTION ENGINE PERFORMANCE. TUTORIAL No. 5 PERFORMANCE CHARACTERISTICS

UNIT 2 REFRIGERATION CYCLE

Physics 5D - Nov 18, 2013

CHAPTER 7 THE SECOND LAW OF THERMODYNAMICS. Blank

Energy Analysis and Comparison of Advanced Vapour Compression Heat Pump Arrangements

Thermodynamics - Example Problems Problems and Solutions

ES-7A Thermodynamics HW 1: 2-30, 32, 52, 75, 121, 125; 3-18, 24, 29, 88 Spring 2003 Page 1 of 6

C H A P T E R T W O. Fundamentals of Steam Power

Pushing the limits. Turbine simulation for next-generation turbochargers

ME 201 Thermodynamics

STEAM TURBINE 1 CONTENT. Chapter Description Page. V. Steam Process in Steam Turbine 6. VI. Exhaust Steam Conditions, Extraction and Admission 7

EXPERIMENT NO. 3. Aim: To study the construction and working of 4- stroke petrol / diesel engine.

70 Mpa Hydrogen Refuelling Stations

FEASIBILITY OF A BRAYTON CYCLE AUTOMOTIVE AIR CONDITIONING SYSTEM

MECHANICAL ENGINEERING EXPERIMENTATION AND LABORATORY II EXPERIMENT ENGINE PERFORMANCE TEST

Supplementary Notes on Entropy and the Second Law of Thermodynamics

Sheet 5:Chapter 5 5 1C Name four physical quantities that are conserved and two quantities that are not conserved during a process.

The Second Law of Thermodynamics

Problem Set MIT Professor Gerbrand Ceder Fall 2003

PG Student (Heat Power Engg.), Mechanical Engineering Department Jabalpur Engineering College, India. Jabalpur Engineering College, India.

Development of a model for the simulation of Organic Rankine Cycles based on group contribution techniques

WEEKLY SCHEDULE. GROUPS (mark X) SPECIAL ROOM FOR SESSION (Computer class room, audio-visual class room)

A Performance Comparison of Vapour Compression Refrigeration System Using Eco Friendly Refrigerants of Low Global Warming Potential

PERFORMANCE ANALYSIS OF VAPOUR COMPRESSION REFRIGERATION SYSTEM WITH R404A, R407C AND R410A

The final numerical answer given is correct but the math shown does not give that answer.

1. A belt pulley is 3 ft. in diameter and rotates at 250 rpm. The belt which is 5 ins. wide makes an angle of contact of 190 over the pulley.

Exergy: the quality of energy N. Woudstra

AN INTRODUCTION TO THE CONCEPT OF EXERGY AND ENERGY QUALITY. Truls Gundersen

The Ogunmuyiwa Engine Cycle

Refrigeration and Airconditioning Prof. M. Ramgopal Department of Mechanical Engineering Indian Institute of Technology, Kharagpur

Answer, Key Homework 6 David McIntyre 1

Technical Thermodynamics

OPTIMIZATION OF DIAMETER RATIO FOR ALPHA-TYPE STIRLING ENGINES

DE-TOP User s Manual. Version 2.0 Beta

INTERNAL COMBUSTION (IC) ENGINES

ENERGY TRANSFER SYSTEMS AND THEIR DYNAMIC ANALYSIS

A knowledge-based system for Waste Heat Recovery. Richard Law

Comparison between Natural Gas and Diesel Fuel Oil Onboard Gas Turbine Powered Ships

OPTIMAL DESIGN AND OPERATION OF HELIUM REFRIGERATION SYSTEMS *

Condensers & Evaporator Chapter 5

Stirling heat engine Internal combustion engine (Otto cycle) Diesel engine Steam engine (Rankine cycle) Kitchen Refrigerator

C H A P T E R F I V E GAS TURBINES AND JET ENGINES

MECHANICAL LOSS REDUCTION OF A 100 W CLASS STIRLING ENGINE. Koichi HIRATA National Maritime Research Institute, Japan

Air Flow Optimization via a Venturi Type Air Restrictor

REAL AND IDEAL GAS THERMODYNAMIC ANALYSIS OF SINGLE RESERVOIR FILLING PROCESS OF NATURAL GAS VEHICLE CYLINDERS

Cylinder Pressure in a Spark-Ignition Engine: A Computational Model

Chapter 8 Maxwell relations and measurable properties

Energy savings in commercial refrigeration. Low pressure control

UNDERSTANDING REFRIGERANT TABLES

A.Pannirselvam*, M.Ramajayam, V.Gurumani, S.Arulselvan and G.Karthikeyan *(Department of Mechanical Engineering, Annamalai University)

Warm medium, T H T T H T L. s Cold medium, T L

THERMAL TO MECHANICAL ENERGY CONVERSION: ENGINES AND REQUIREMENTS

Chapter 3.4: HVAC & Refrigeration System

Dharam V. Punwani President, Avalon Consulting, Inc. Presented at Turbine Inlet Cooling Association Webinar April 9, 2014

Exhaust emissions of a single cylinder diesel. engine with addition of ethanol

A LAMINAR FLOW ELEMENT WITH A LINEAR PRESSURE DROP VERSUS VOLUMETRIC FLOW ASME Fluids Engineering Division Summer Meeting

Optimising Glass Melting Processes with Energy & Mass Balance Calculations

Chapter 17. For the most part, we have limited our consideration so COMPRESSIBLE FLOW. Objectives

9. ENERGY PERFORMANCE ASSESSMENT OF HVAC SYSTEMS

Percent per Degree Rule of Thumb for Refrigeration Cycle Improvement

a) Use the following equation from the lecture notes: = ( J K 1 mol 1) ( ) 10 L

Wind Turbine Power Calculations

The Second Law of Thermodynamics

Comparing Air Cooler Ratings Part 1: Not All Rating Methods are Created Equal

LECTURE 28 to 29 ACCUMULATORS FREQUENTLY ASKED QUESTIONS

C18 ACERT Fire Pump Tier bkw/ rpm

Dynamic Process Modeling. Process Dynamics and Control

Feasibility Study for Mobile Sorption Storage in Industrial Applications

Chapter 10 Temperature and Heat

COGENERATION. This section briefly describes the main features of the cogeneration system or a Combined Heat & Power (CHP) system. 36 Units.

Engine Efficiency and Power Density: Distinguishing Limits from Limitations

The Use of Control Valve Sizing Equations with Simulation Based Process Data

Evaluation of mobile storage systems for heat transport. G. Storch, A. Hauer, A. Krönauer ZAE Bayern, Walther-Meißner-Str. 6, Garching, Germany

CONTROL VALVE PRESSURE DROP AND SIZING

Copyright 1984 by ASME. NOx ABATEMENT VIA WATER INJECTION IN AIRCRAFT-DERIVATIVE TURBINE ENGINES. D. W. Bahr. and T. F. Lyon

NUMERICAL ANALYSIS OF THE EFFECTS OF WIND ON BUILDING STRUCTURES

PERFORMANCE EVALUATION OF NGCC AND COAL-FIRED STEAM POWER PLANTS WITH INTEGRATED CCS AND ORC SYSTEMS

AIR REVERSING R744 AIR CONDITIONING SYSTEM

(1) The size of a gas particle is negligible as compared to the volume of the container in which the gas is placed.

ME THERMODYNAMICS I

How to Calculate Compression Ratio in a Single Cylinder. Lesson 9

Introductory Study of Variable Valve Actuation for Pneumatic Hybridization

Metrics for Data Centre Efficiency

Transcription:

Engineering Software P.O. Box 1180, Germantown, MD 20875 Phone: (301) 540-3605 FAX: (301) 540-3605 E-Mail: info@engineering-4e.com Web Site: http://www.engineering-4e.com Diesel Cycle Analysis Diesel Cycle Analysis by Engineering Software Course Category: Engineers Course Level: Intermediate Credit: 1 Hour -- i --

Course Description The ideal cycle for a simple diesel engine is the Diesel Cycle. In this one hour course, the open, simple Diesel Cycle used for stationary power generation is considered. The Diesel Cycle thermal efficiency is presented only for the air as the working fluid. The thermal efficiency derivation is presented with a simple mathematical approach. The Diesel Cycle is presented in the p - V and T - s diagrams and its major performance trends (thermal efficiency and power output) are plotted in a few figures as a function of compression and cut off ratio values and combustion temperature for fixed cylinder geometry. It should be noted that this online course does not deal with costs (capital, operational or maintenance). In this course, the student gets familiar with the Diesel Cycle, its components, p - V and T - s diagrams, operation and major performance trends. This course includes a multiple choice quiz at the end. -- ii --

Performance Objectives At the conclusion of this course, the student will: Understand basic energy conversion engineering assumptions and equations Know basic components of the Diesel Cycle and its p - V and T - s diagrams Be familiar with the Diesel Cycle operation Understand general Diesel Cycle performance trends -- iii --

Introduction Over the years, diesel engine has become the premier transportation system for intermediate and high loads. Diesel engines are compact, lightweight, easy to operate and come in sizes ranging from several kilowatts to a few megawatts. Diesel engines require relatively low capital investment, have high operating flexibility, high thermal efficiency and can be used for various transportation and industrial applications. Diesel engines can help provide reliable power to meet the future demand using both high and low heat content fuels, with low emissions. -- iv --

Table of Contents Diesel Cycle... 2 Analysis... 2 Assumptions... 10 Governing Equations... 11 Input Data... 12 Results... 12 Conclusions... 14 -- 1 --

Diesel Cycle This section provides a Diesel Cycle analysis when the working fluid is air. Analysis In the presented Diesel Cycle analysis, only air is considered as the working fluid behaving as a perfect gas -- specific heat has a constant value. Ideal gas state equation is valid -- pv = RT. Air enters a cylinder at point 1 when compression starts and it ends at point 2. Isentropic compression is considered with no entropy change. Heat addition starts at point 2 and it ends at point 3. At a constant pressure, combustion takes place (fuel is added to the cylinder and the air temperature raises) and/or heat gets added to air. Expansion starts at point 3 and it ends at point 4. Isentropic expansion is considered with no entropy change. Air heat rejection starts at point 4 and it ends at point 1. At a constant volume, air gets cooled and the working fluid temperature decreases. It should be mentioned that air at point 1 enters the compression process again and the cycle is repeated. Figure 1 presents a Diesel Cycle pressure vs volume diagram. -- 2 --

Figure 1 - Diesel Cycle Pressure vs Volume Diagram Figure 2 presents a Diesel Cycle temperature vs entropy diagram. -- 3 --

Figure 2 - Diesel Cycle Temperature vs Entropy Diagram The thermal cycle efficiency can be given as a function of specific external work (specific net power output) and heat added to the working fluid as follows: η = w/qh = (we - wc)/qh = (qh - ql)/qh or η = 1 - ql/qh = 1 - (cv(t4 - T1))/(cp(T3 - T2)) = 1 - (T1(T4/T1-1))/(ϰT2(T3/T2-1)) where η - thermal efficiency [/] w - specific external work (specific net power output) [kj/kg] we - expansion specific power output [kj/kg] -- 4 --

wc - compression specific power input [kj/kg] W - external work (net power output) [kw] We - expansion power output [kw] Wc - compression power input [kw] qh - heat added to the working fluid [kj/kg] ql - heat rejected from the working fluid [kj/kg] cp - specific heat at constant pressure [kj/kg*k] cv - specific heat at constant volume [kj/kg*k] m - working fluid mass flow rate [kg/s] ε - compression ratio [/] φ - cut off ratio [/] For isentropic compression and expansion: T2/T1 = (p2/p1) (ϰ-1)/ϰ = (V1/V2) (ϰ-1) T4/T3 = (p4/p3) (ϰ-1)/ϰ = (V3/V4) (ϰ-1) where ϰ = cp/cv - for air ϰ = 1.4 [/] p1, p2, p3, p4 - pressure values at points 1, 2, 3 and 4 [atm] T1, T2, T3, T4 - temperature values at points 1, 2, 3 and 4 [K] Knowing that s3 - s2 = s4 - s1 and s3 - s2 = cpln(t3/t2) s4 - s1 = cvln(t4/t1) s1, s2, s3, s4 - specific entropy values at points 1, 2, 3 and 4 [kj/kg*k] It follows -- 5 --

(T3/T2) ϰ = T4/T1 It follows that T3/T4 = T2/T1 = (V1/V2) (ϰ-1) = ε (ϰ-1) When combustion takes place at a constant pressure: T3/T2 = V3/V2 where ε = V1/V2 φ = V3/V2 Therefore, after some mathematical operations the thermal efficiency is: η = 1 - (T1((T3/T2) ϰ - 1)))/(ϰT2(T3/T2-1)) If the temperature ratio is substituted in terms of the volume/compression ratio: η = 1 - (φ ϰ - 1)/(ϰε (ϰ-1) (φ - 1)) Figure 3 presents the Diesel Cycle efficiency as a function of the compression ratio and cut off ratio. It should be noted that the inlet conditions are standard ambient conditions: temperature of 298 [K] and absolute pressure of 1 [atm]. -- 6 --

Figure 3 - Diesel Cycle Efficiency Figure 4 presents the Diesel Cycle efficiency as a function of the compression ratio and combustion temperature. -- 7 --

Figure 4 - Diesel Cycle Efficiency Figure 5 presents the Diesel Cycle cut off ratio as a function of the combustion temperature and compression ratio. -- 8 --

Figure 5 - Diesel Cycle Cut Off Ratio Figure 6 presents the Diesel Cycle power output as a function the combustion temperature and compression ratio. It should be noted that the number of revolutions is 60 [1/s] for given geometry of the four cylinder and four stroke Diesel engine. -- 9 --

Figure 6 - Diesel Cycle Power Output One can notice that the Diesel Cycle efficiency increases with an increase in the compression ratio and a decrease of the cut off ratio values. One can notice that the Diesel Cycle power output increases with an increase in the compression ratio and combustion temperature values. Assumptions Working fluid is air. There is no friction. Compression and expansion are isentropic -- there is no entropy change. During heat addition and heat rejection, the air temperature does change. Ideal gas state equation is valid -- pv = RT. Air behaves as a perfect gas -- specific heat has a constant value. -- 10 --

Governing Equations T2/T1 = (V1/V2) (ϰ-1) V1/V2 = (T2/T1) 1/(ϰ-1) T3/T4 = (V4/V3) (ϰ-1) V4/V3 = (T3/T4) 1/(ϰ-1) ϰ = cp/cv cp - cv = R pv = RT w = qh - ql qh = cp(t3 - T2) ql = cv(t4 - T1) w = cp(t3 - T2) - cv(t4 - T1) W = (cp(t3 - T2) - cv(t4 - T1))m η = 1 - (φ ϰ - 1)/(ϰε (ϰ-1) (φ - 1)) ε = V1/V2 φ = V3/V2 -- 11 --

Input Data T1 = 298 [K] p1 = 1 [atm] T3 = 1,500, 1,800 and 2,100 [K] ε = 7.5, 10, 12.5, 15 and 17.5 [/] φ = 3 and 4 [/] R = 0.2867 [kj/kg*k] cp = 1.004 [kj/kg*k] ϰ = 1.4 [/] Results Diesel Cycle Efficiency [%] Cut Off Ratio [/] Diesel Cycle Efficiency Compression Ratio [/] 7.5 10 12.5 15 17.5 3 41.69 48.03 52.46 55.81 58.45 4 36.57 43.46 48.29 51.93 54.80 Diesel Cycle Efficiency [%] Compression Ratio [/] Diesel Cycle Efficiency Combustion Temperature [K] 1,500 1,800 2,100 10 53.39 51.12 49.20 15 61.94 60.12 58.49 Diesel Cycle Cut Off Ratio -- 12 --

Cut Off Ratio [/] Compression Ratio [/] Combustion Temperature [K] 1,500 1,800 2,100 10 2.00 2.40 2.80 15 1.70 2.05 2.39 Power Output [kw] Compression Ratio [/] Diesel Cycle Power Output Combustion Temperature [K] 1,500 1,800 2,100 10 311 417 514 15 297 433 557 -- 13 --

Conclusions The Diesel Cycle efficiency increases with an increase in the compression ratio and a decrease in the cut off ratio values. Also, the Diesel Cycle power output increases with an increase in the compression ratio and combustion temperature values. Please use the material you just read to answer the quiz questions at the end of this course. When you get a chance, please visit the following URL: http://www.engineering-4e.com The above URL provides lots of free online and downloadable e-material and e-solutions on energy conversion. -- 14 --