Power Cycles. Ideal Cycles, Internal Combustion
|
|
- Ursula Alexander
- 5 years ago
- Views:
Transcription
1 Gas Power Cycles
2 Power Cycles Ideal Cycles, Internal Combustion Otto cycle, spark ignition Diesel cycle, compression ignition Sterling & Ericsson cycles Brayton cycles Jet-propulsion cycle Ideal Cycles, External Combustion Rankine cycle
3 Modeling
4 Ideal Cycles Idealizations & Simplifications Cycle does not involve any friction All expansion and compression processes are quasi-equilibrium processes Pipes connecting components have no heat loss Neglecting changes in kinetic and potential energy (except in nozzles & diffusers)
5 Carnot Cycle
6 Carnot Cycle
7 Gas Power Cycles Working fluid remains a gas for the entire cycle Examples: Spark-ignition engines Diesel engines Gas turbines
8 Air-Standard Assumptions Air is the working fluid, circulated in a closed loop, is an ideal gas All cycles, processes are internally reversible Combustion process replaced by heat-addition from external source Exhaust is replaced by heat rejection process which restores working fluid to initial state
9 Cold-Air-Standard Assumption Air has constant specific heats, values are for room temperature (25 C or 77 F)
10 Engine Terms Top dead center Bottom dead center Bore Stroke
11 Engine Terms Clearance volume Displacement volume Compression ratio
12 Mean effective pressure (MEP) Engine Terms
13 Otto Cycle Processes of Otto Cycle: Isentropic compression Constant-volume heat addition Isentropic expansion Constant-volume heat rejection
14 Otto Cycle
15 Otto Cycle Ideal Otto Cycle Four internally reversible processes 1-2 Isentropic compression 2-3 Constant-volume heat addition 3-4 Isentropic expansion 4-1 Constant-volume heat rejection
16 Otto Cycle Closed system, pe, ke 0 Energy balance (cold air std)
17 Otto Cycle Thermal efficiency of ideal Otto cycle: Since V 2 = V 3 and V 4 = V 1 Where r is compression ratio k is ratio of specific heats
18 Otto Cycle
19
20
21
22
23
24 Spark or Compression Ignition Spark (Otto), air-fuel mixture compressed (constant-volume heat addition) Compression (Diesel), air compressed, then fuel added (constant-pressure heat addition)
25 Diesel Cycle
26 Diesel Cycle Processes of Diesel cycle: Isentropic compression Constant-pressure heat addition Isentropic expansion Constant-volume heat rejection
27 Diesel Cycle For ideal diesel cycle With cold air assumptions
28 Diesel Cycle Cut off ratio r c Efficiency becomes
29
30
31
32
33
34 Brayton Cycle Gas turbine cycle Open vs closed system model
35 Brayton Cycle Four internally reversible processes 1-2 Isentropic Compression (compressor) 2-3 Constant-pressure heat addition 3-4 Isentropic expansion (turbine) 4-1 Constant-pressure heat rejection
36 Brayton Cycle Analyze as steady-flow process So With cold-air-standard assumptions
37 Brayton Cycle Since processes 1-2 and 3-4 are isentropic, P 2 = P 3 and P 4 = P 1 where
38 Brayton Cycle
39 Brayton Cycle Back work ratio Improvements in gas turbines Combustion temp Machinery component efficiencies Adding modifications to basic cycle
40
41
42
43
44 Actual Gas-Turbine Cycles For actual gas turbines, compressor and turbine are not isentropic
45
46
47
48
49 Regeneration
50 Regeneration Use heat exchanger called recuperator or regenerator Counter flow
51 Regeneration Effectiveness For cold-air assumptions
52
53
54 Brayton with Intercooling, Reheat, & Regeneration
55 Brayton with Intercooling, Reheat, & Regeneration For max performance
56
57
58
59
60
61
62 Ideal Jet-Propulsion Cycles
63
64 Ideal Jet-Propulsion Cycles Propulsive power Propulsive efficiency
65
66
67
68
69
70
71
72 Turbojet Engines Turbofan: for same power, large volume of slower-moving air produces more thrust than a small volume of fast-moving air (bypass ratio 5-6) Turboprop: by pass ratio of 100
73
74
75 Jets Afterburner: addition to turbojet Ramjet: use diffusers and nozzles Scramjet: supersonic ramjet Rocket: carries own oxidizer
76 Second Law Issues Ideal Otto, Diesel, and Brayton cycles are internally reversible 2 nd Law analysis identifies where losses are so improvements can be made Look at closed, steady-flow systems
77 Second Law Issues For exergy and exergy destruction for closed system: For steady-flow system:
78 Second Law Issues For a cycle that starts and end at the same state:
79
80
81
82
Idealizations Help Manage Analysis of Complex Processes
8 CHAPTER Gas Power Cycles 8-1 Idealizations Help Manage Analysis of Complex Processes The analysis of many complex processes can be reduced to a manageable level by utilizing some idealizations (fig.
More informationChapter 9 GAS POWER CYCLES
Thermodynamics: An Engineering Approach Seventh Edition in SI Units Yunus A. Cengel, Michael A. Boles McGraw-Hill, 2011 Chapter 9 GAS POWER CYCLES Mehmet Kanoglu University of Gaziantep Copyright The McGraw-Hill
More informationChapter 9 GAS POWER CYCLES
Thermodynamics: An Engineering Approach, 6 th Edition Yunus A. Cengel, Michael A. Boles McGraw-Hill, 2008 Chapter 9 GAS POWER CYCLES Copyright The McGraw-Hill Companies, Inc. Permission required for reproduction
More informationGas Power System. By Ertanto Vetra
Gas Power System 1 By Ertanto Vetra Outlines Introduction Internal Combustion Engines Otto Cycles Diesel Cycles Gas Turbine Cycles Gas Turbine Based Combined Cycles Gas Turbines for Aircrafts Turbojets
More informationIn this lecture... Gas power cycles
7 Lect-7 Gas power cycles In this lecture... he Carnot cycle and its significance Air-standard assumptions An oeriew of reciprocating engines Otto cycle: the ideal cycle for sparkignition engines Diesel
More informationL34: Internal Combustion Engine Cycles: Otto, Diesel, and Dual or Gas Power Cycles Introduction to Gas Cycles Definitions
Page L: Internal Combustion Engine Cycles: Otto, Diesel, and Dual or Gas Power Cycles Review of Carnot Power Cycle (gas version) Air-Standard Cycles Internal Combustion (IC) Engines - Otto and Diesel Cycles
More informationBASIC CONSIDERATIONS IN POWER CYCLE ANALYSIS THERMODYNAMICS CHAPTER 9
08.04.3. HERMODYNAMICS CHAPER 9 Gas power cycles Lecturer Axel GRONIEWSKY, PhD 5 th of February08 Most power-producing devices operate on cycles. Complexity of actual cycles are high idealizationsare required
More informationGAS POWER CYCLES. Dr Ali Jawarneh Department of Mechanical Engineering Hashemite University
Chapter 9 GAS POWER CYCLES Dr Ali Jawarneh Department of Mechanical Engineering i Hashemite University 2 Objectives Evaluate the performance of gas power cycles for which h the working fluid remains a
More informationProcess 1-2: Reversible adiabatic compression process. Process 2-3: Reversible isothermal heat addition
Vapor Power Cycles Process 1-2: Reversible adiabatic compression process from P1 to P2. Process 2-3: Reversible isothermal heat addition process at constant temperature TH. Process 3-4: Reversible adiabatic
More informationPrepared by: Dr. Assim Adaraje
Air-standard cycles Prepared by: Dr. Assim Adaraje CH. 2 ۱ Cold-air-standard assumptions: When the working fluid is considered to be air with constant specific heats at room temperature (25 C). Air-standard
More informationUNIT 1 GAS POWER CYCLES
THERMAL ENGINEERING UNIT 1 GAS POWER CYCLES Air Standard Cycles - Otto, Diesel, Dual, Brayton cycle with intercooling, reheating and regeneration- Calculation of airstandard efficiency and mean effective
More information(v) Cylinder volume It is the volume of a gas inside the cylinder when the piston is at Bottom Dead Centre (B.D.C) and is denoted by V.
UNIT II GAS POWER CYCLES AIR STANDARD CYCLES Air standard cycles are used for comparison of thermal efficiencies of I.C engines. Engines working with air standard cycles are known as air standard engines.
More informationContent : 4.1 Brayton cycle-p.v. diagram and thermal efficiency. 4Marks Classification of gas turbines.
Content : 4.1 Brayton cycle-p.v. diagram and thermal efficiency. 4Marks Classification of gas turbines. 4.2 Construction and working of gas turbines i) Open cycle ii) Closed cycle gas Turbines, P.V. and
More informationInternal Combustion Engines
Internal Combustion Engines Reading Problems 8-3 8-7 8-35, 8-45, 8-52 Definitions 1. spark ignition: a mixture of fuel and air is ignited by a spark plug applications requiring power to about 225 kw (300
More informationChapter 8 Production of Power from Heat
Chapter 8 Production of Power from Heat Different sources of power, such as solar energy (from sun), kinetic energy from atmospheric winds and potential energy from tides. The most important source of
More informationHeat engine. Heat engine
Heat engine Device that transforms heat into work. It requires two energy reservoirs at different temperatures An energy reservoir is a part of the environment so large wrt the system that its temperature
More informationThermodynamic Cycles. Alicia Ma. Esponda Cascajares
Thermodynamic Cycles Alicia Ma. Esponda Cascajares Power Cycles Cycles which convert a heat input into a mechanical work output. Power cycles can be divided according to the type of heat engine they seek
More informationWeek 10. Gas Power Cycles. ME 300 Thermodynamics II 1
Week 10 Gas Power Cycles ME 300 Thermodynamics II 1 Today s Outline Gas power cycles Internal combustion engines Four-stroke cycle Thermodynamic cycles Ideal cycle ME 300 Thermodynamics II 2 Gas Power
More informationIntroduction to Gas Turbine Engines
Introduction to Gas Turbine Engines Introduction Gas Turbine Engine - Configurations Gas Turbine Engine Gas Generator Compressor is driven by the turbine through an interconnecting shaft Turbine is driven
More informationGas Power Cycles. Tarawneh
Gas Power Cycles Dr.Mohammad Tarawneh ) Carnot cycle 2) Otto cycle ) Diesel cycle - Today 4) Dual Cycle 5) Stirling cycle 6) Ericsson cycles 7) Brayton cycle Carnot Cycle Reversible isothermal expansion
More informationMEB THERMAL ENGINEERING - I QUESTION BANK UNIT-I PART-A
MEB 420 - THERMAL ENGINEERING - I QUESTION BANK UNIT-I Each question carries 1 mark. PART-A 1. Define temperature. 2. Define intensive property 3. Explain the term absolute zero of temperature 4. State
More informationThermodynamics cycles can be classified into different categories depending on fluid used or the different processes:
Classification of thermodynamics cycles Thermodynamics cycles can be classified into different categories depending on fluid used or the different processes: Gas and vapor cycles - Gas cycle: the working
More informationSIDDHARTH INSTITUTE OF ENGINEERING & TECHNOLOGY :: PUTTUR (AUTONOMOUS) QUESTION BANK UNIT I I.C ENGINES
SIDDHARTH INSTITUTE OF ENGINEERING & TECHNOLOGY :: PUTTUR UNIT I I.C ENGINES 1 (a) Explain any six types of classification of Internal Combustion engines. (6M) (b) With a neat sketch explain any three
More informationAE Aircraft Performance and Flight Mechanics
AE 429 - Aircraft Performance and Flight Mechanics Propulsion Characteristics Types of Aircraft Propulsion Mechanics Reciprocating engine/propeller Turbojet Turbofan Turboprop Important Characteristics:
More informationIntroduction to Aerospace Propulsion
Introduction to Aerospace Propulsion Introduction Newton s 3 rd Law of Motion as the cornerstone of propulsion Different types of aerospace propulsion systems Development of jet engines Newton s Third
More informationCombustion engines. Combustion
Combustion engines Chemical energy in fuel converted to thermal energy by combustion or oxidation Heat engine converts chemical energy into mechanical energy Thermal energy raises temperature and pressure
More informationη th W = Q Gas Power Cycles: Working fluid remains in the gaseous state through the cycle.
Gas Power Cycles: Gas Power Cycles: Working fluid remains in the gaseous state through the cycle. Sometimes useful to study an idealised cycle in which internal irreversibilities and complexities are
More informationWelcome to Aerospace Engineering
Welcome to Aerospace Engineering DESIGN-CENTERED INTRODUCTION TO AEROSPACE ENGINEERING Notes 5 Topics 1. Course Organization 2. Today's Dreams in Various Speed Ranges 3. Designing a Flight Vehicle: Route
More informationIntroduction to I.C Engines CH. 1. Prepared by: Dr. Assim Adaraje
Introduction to I.C Engines CH. 1 Prepared by: Dr. Assim Adaraje 1 An internal combustion engine (ICE) is a heat engine where the combustion of a fuel occurs with an oxidizer (usually air) in a combustion
More informationCHAPTER I GAS POWER CYCLES
CHAPTER I GAS POWER CYCLES 1.1 AIR STANDARD CYCLES Air standard cycles are used for comparison of thermal efficiencies of I.C engines. Engines working with air standard cycles are known as air standard
More informationChapter 9. Two important areas of application for thermodynamics GAS POWER CYCLES. Objectives
Chapter 9 GAS POWER CYCLES Two important areas of application for thermodynamics are power generation and refrigeration. Both are usually accomplished by systems that operate on a thermodynamic cycle.
More informationME3264: LAB 9 Gas Turbine Power System
OBJECTIVE ME3264: LAB 9 Gas Turbine Power System Professor Chih-Jen Sung Spring 2013 A fully integrated jet propulsion system will be used for the study of thermodynamic and operating principles of gas
More informationScheme - G. Sample Test Paper-I. Course Name : Diploma in Mechanical Engineering Course Code : ME Semester : Fifth Subject Title : Power Engineering
Sample Test Paper-I Marks : 25 Time:1 hour Q1. Attempt any Three 3X3=9 a) Define i) Mean Effective Pressure ii) Piston Speed iii) Swept Volume b) Draw Carnot cycle on P-V and T-S Diagram c) State the need
More informationIntroduction to Aerospace Engineering
Introduction to Aerospace Engineering Lecture slides Challenge the future 1 18-9-2011 Introduction to Aerospace Engineering AE1101ab - Propulsion Delft University of Technology Prof.dr.ir. Challenge JaccotheHoekstra
More information1. Aero-Science B.Sc. Aero Science-I Total Mark: 100 Appendix A (Outlines of Tests) Aero-Engines : 100 Marks
1. Aero-Science B.Sc. Aero Science-I Total Mark: 100 Appendix A (Outlines of Tests) Aero-Engines : 100 Marks Note:- The questions will be set in each paper. Candidates are to attempt any five except in
More informationDEPARTMENT OF MECHANICAL ENGINEERING ME ENGINEERING THERMODYNAMICS TWO MARKS QUESTION AND ANSWER
DEPARTMENT OF MECHANICAL ENGINEERING ME 6301- ENGINEERING THERMODYNAMICS TWO MARKS QUESTION AND ANSWER 1. Define the term thermal engineering. Ans: Thermal engineering is the science that deals with the
More informationJET AIRCRAFT PROPULSION
1 JET AIRCRAFT PROPULSION a NPTEL-II Video Course for Aerospace Engineering Students Bhaskar Roy and A M Pradeep Aerospace Engineering Department I.I.T., Bombay 2 Brief outline of the syllabus Introduction
More informationEnd of Book Questions Chapter 7 Aircraft Power Plants
End of Book Questions Chapter 7 Aircraft Power Plants 7-1. What engine does NOT draw air from the outside to fuel the combustion process? A. Gas turbine B. Rocket C. Turboprop D. Turboshaft 7-2. How many
More informationKINGS COLLEGE OF ENGINEERING DEPARTMENT OF MECHANICAL ENGINEERING. Question Bank. UNIT-I THERMODYNAMIC CYCLES Part-A (2 Marks)
KINGS COLLEGE OF ENGINEERING DEPARTMENT OF MECHANICAL ENGINEERING Question Bank Sub. Code/Name: ME1351 - THERMAL ENGINEERING Year/Sem: III/VI 1. What is a thermodynamic cycle? UNIT-I THERMODYNAMIC CYCLES
More informationImportant Instructions to examiners: 1) The answers should be examined by key words and not as word-to-word as given in the model answer scheme. 2) The model answer and the answer written by candidate
More informationIn this lecture... Components of ramjets and pulsejets Ramjet combustors Types of pulsejets: valved and valveless, Pulse detonation engines
In this lecture... Components of ramjets and pulsejets Ramjet combustors Types of pulsejets: valved and valveless, ulse detonation engines Ramjet engines Ramjet engines consist of intakes, combustors and
More informationHours / 100 Marks Seat No.
17529 14115 3 Hours / 100 Seat No. Instructions (1) All Questions are Compulsory. (2) Answer each next main Question on a new page. (3) Illustrate your answers with neat sketches wherever necessary. (4)
More informationPage 2. (a) (i) Show that during the change AB the gas undergoes an isothermal change.
Q1.The Carnot cycle is the most efficient theoretical cycle of changes for a fixed mass of gas in a heat engine. The graph below shows the pressure volume (p V) diagram for a gas undergoing a Carnot cycle
More informationME2301 THERMAL ENGINEERING L T P C OBJECTIVE:
ME2301 THERMAL ENGINEERING L T P C 3 1 0 4 OBJECTIVE: To integrate the concepts, laws and methodologies from the first course in thermo dynamics into analysis of cyclic processes To apply the thermodynamic
More informationVETRI VINAYAHA COLLEGE OF ENGINEERING AND TECHNOLOGY DEPARTMENT OF MECHANICAL ENGINEERING ME6404 THERMAL ENGINEERING
VETRI VINAYAHA COLLEGE OF ENGINEERING AND TECHNOLOGY DEPARTMENT OF MECHANICAL ENGINEERING ME6404 THERMAL ENGINEERING UNIT I - GAS POWER CYCLES 1. What is a thermodynamic cycle? Thermodynamic cycle is defined
More informationClass Notes on Thermal Energy Conversion System
Class Notes on Thermal Energy Conversion System For the students of Civil & Rural 3 rd semester Ramesh Khanal Assistant Professorr Nepal Engineering College Bhaktapur, Nepal 2015 Course Structure MEC 209.3:
More informationGYANMANJARI INSTITUTE OF TECHNOLOGY (GMIT) SUBJECT: ELEMENTS OF MECHANICAL ENGINEERING Assignment Ch 1
1. 3. GYANMANJARI INSTITUTE OF TECHNOLOGY (GMIT) Assignment Ch 1 A steel ball having mass of 10 kg and a specific heat of 460 J/kg K is heated from 50 o C to 200 o C. Determine the heat required. In a
More informationSET - 1 II B. Tech II Semester Regular/Supplementary Examinations, April/May-2017 THERMAL ENGINEERING-I (Mechanical Engineering) Time: 3 hours Max. Marks: 70 Note: 1. Question Paper consists of two parts
More information(a) then mean effective pressure and the indicated power for each end ; (b) the total indicated power : [16]
Code No: R05220304 Set No. 1 II B.Tech II Semester Regular Examinations, Apr/May 2007 THERMAL ENGINEERING-I ( Common to Mechanical Engineering and Automobile Engineering) Time: 3 hours Max Marks: 80 Answer
More informationUNIVERSITY POLYTECHNIC B.I.T., MESRA, RANCHI
COURSE STRUCTURE SEMESTER V (Total Unit 7.0) Course Code Theory Unit Course Code Sessional Unit DMM 5001 Automobile Engineering 1.0 DMM 5002 Automobile Engineering 0.5 Lab. DMM 5003 CAD/CAM 1.0 DMM5004
More informationAssignment-1 Air Standard Cycles
Assignment-1 Air Standard Cycles 1. What do u mean by air standard cycle? List assumptions for air standard cycle & give reasons why air standard cycle differs from actual cycle. 2. Derive an equation
More informationFoundations of Thermodynamics and Chemistry. 1 Introduction Preface Model-Building Simulation... 5 References...
Contents Part I Foundations of Thermodynamics and Chemistry 1 Introduction... 3 1.1 Preface.... 3 1.2 Model-Building... 3 1.3 Simulation... 5 References..... 8 2 Reciprocating Engines... 9 2.1 Energy Conversion...
More informationCombustion Systems What we might have learned
Combustion Systems What we might have learned IMechE ADSC, 6 December 2012 Chris Whelan Contents Engines Big & Small Carnot, Otto & Diesel Thermodynamic Cycles Combustion Process & Systems Diesel & Otto
More informationInternal Combustion Engine. Prepared by- Md Ferdous Alam Lecturer, MEE, SUST
Internal Combustion Engine Prepared by- Md Ferdous Alam Lecturer, MEE, SUST What is an Engine? -a machine designed to convert one form of energy into mechanical energy Two types of engines : 1. Internal
More informationDEPARTMENT OF MECHANICAL ENGINEERING Question Bank ME THERMAL ENGINEERING. Part-A (2 Marks)
DEPARTMENT OF MECHANICAL ENGINEERING Question Bank ME1351 - THERMAL ENGINEERING UNIT I GAS POWER CYCLES Part-A (2 Marks) 1. What is a thermodynamic cycle? 2. What is meant by air standard cycle? 3.. Name
More informationEngine Cycles. T Alrayyes
Engine Cycles T Alrayyes Introduction The cycle experienced in the cylinder of an internal combustion engine is very complex. The cycle in SI and diesel engine were discussed in detail in the previous
More informationME Thermal Engineering Question Bank
ME2301 - Thermal Engineering Question Bank UNIT I GAS POWER CYCLES Otto, Diesel, Dual, Brayton cycles, Calculation of mean effective pressure, and air standard efficiency -Actual and theoretical PV diagram
More informationThe Internal combustion engine (Otto Cycle)
The Internal combustion engine (Otto Cycle) The Otto cycle is a set of processes used by spark ignition internal combustion engines (2-stroke or 4-stroke cycles). These engines a) ingest a mixture of fuel
More informationNoble Group of Institutions, Junagadh. Faculty of Engineering Department of Mechanical Engineering
Semester:1 st Subject: Elements of Mechanical Engineering (2110006) Faculty: Mr. Ishan Bhatt Year: 2017-18 Class: Comp. & IT Ele TUTORIAL 1 INTRODUCTION Q.1 Define: Force, Work, Pressure, Energy, Heat
More informationGas Turbine Power Plant
Gas Turbine Power Plant Dr. M. Zahurul Haq Professor Department of Mechanical Engineering Bangladesh University of Engineering & Technology (BUET) Dhaka-1000, Bangladesh zahurul@me.buet.ac.bd http://teacher.buet.ac.bd/zahurul/
More informationUnit WorkBook 4 Level 4 ENG U13 Fundamentals of Thermodynamics and Heat Engines UniCourse Ltd. All Rights Reserved. Sample
Pearson BTEC Levels 4 Higher Nationals in Engineering (RQF) Unit 13: Fundamentals of Thermodynamics and Heat Engines Unit Workbook 4 in a series of 4 for this unit Learning Outcome 4 Internal Combustion
More informationInternal Combustion Engines
Internal Combustion Engines The internal combustion engine is an engine in which the burning of a fuel occurs in a confined space called a combustion chamber. This exothermic reaction of a fuel with an
More informationUSO4CICV01/US04CICH02:
Natubhai V. Patel College of Pure & Applied Sciences S. Y. B.Sc. Semester-4 Industrial chemistry/ IC (Vocational) USO4CICV0/US04CICH02: Chemical Plant Utilities UNIT 5 Internal combustion engine In an
More informationUltra-High-Efficiency Engines: Integration, Optimization, Realization
Ultra-High-Efficiency Engines: Integration, Optimization, Realization Chris F. Edwards Greg Roberts, BJ Johnson, Rebecca Pass, Adelaide Calbry-Muzyka, Julie Blumreiter, Mark Donohue, Carol Regalbuto, John
More informationAssignment-1 Introduction
Assignment-1 Introduction 1. Compare S.I. engines with C.I engines. 2. Explain with the help of neat sketch, the working of a 2-stroke petrol engine. 3. Derive an equation of efficiency, work output and
More informationEngine Performance Analysis
Engine Performance Analysis Introduction The basics of engine performance analysis The parameters and tools used in engine performance analysis Introduction Parametric cycle analysis: Independently selected
More information2.61 Internal Combustion Engine Final Examination. Open book. Note that Problems 1 &2 carry 20 points each; Problems 3 &4 carry 10 points each.
2.61 Internal Combustion Engine Final Examination Open book. Note that Problems 1 &2 carry 20 points each; Problems 3 &4 carry 10 points each. Problem 1 (20 points) Ethanol has been introduced as the bio-fuel
More informationEnergimaskiner. Workshop efterår 2010
Energimaskiner Workshop efterår 2010 1 Program 08:15-09:30 Forelæsning 09:30-14:00 Miniprojekt i grupper 14:00-15:00 Fremlæggelse i plenum 2 Forlæsning Carnot Sterling (m. demo) Miniprojekter Varmepumpe
More informationVALVE TIMING DIAGRAM FOR SI ENGINE VALVE TIMING DIAGRAM FOR CI ENGINE
VALVE TIMING DIAGRAM FOR SI ENGINE VALVE TIMING DIAGRAM FOR CI ENGINE Page 1 of 13 EFFECT OF VALVE TIMING DIAGRAM ON VOLUMETRIC EFFICIENCY: Qu. 1:Why Inlet valve is closed after the Bottom Dead Centre
More informationThermodynamics II MIDTERM MECH 351/2 Fall 06 CONCORDIA UNIVERSITY FACULTY OF ENGINEERING AND COMPUTER SCIENCE DEPARTMENT OF MECHANICAL ENGINEERING
Thermodynamics II MIDTERM MEH 35/ Fall 06 ONORDIA UNIVERSITY FAULTY OF ENGINEERING AND OMPUTER SIENE DEPARTMENT OF MEHANIAL ENGINEERING Student s Name: I.D.: I. [50 points] A steam power plant operates
More informationDevelopment and Implementation of Interactive/Visual Software for Simple Aircraft Gas Turbine Design
Development and Implementation of Interactive/Visual Software for Simple Aircraft Gas Turbine Design Afshin J. Ghajar, Ronald D. Delahoussaye, Vandan V. Nayak School of Mechanical and Aerospace Engineering,
More informationApproved by AICTE, Government of India & affiliated to Dr. A.P.J. Abdul Kalam Technical University, Lucknow Department of Mechanical Engineering
Experiment No. - 1 Object: Study and working of four stroke petrol engine. Apparatus Required: S. No. Name of Apparatus Specifications Model of Four stroke petrol engine NA Figure 1: Working of four stroke
More informationSustainable Energy Mod.1: Fuel Cells & Distributed Generation Systems
Sustainable Energy Mod.1: Fuel Cells & Distributed Generation Systems Dr. Ing. Mario L. Ferrari Thermochemical Power Group (TPG) - DiMSET University of Genoa, Italy : fuel cell systems (hybrid systems)
More informationInvestigators: C. F. Edwards, Associate Professor, Mechanical Engineering Department; M.N. Svreck, K.-Y. Teh, Graduate Researchers
Development of Low-Irreversibility Engines Investigators: C. F. Edwards, Associate Professor, Mechanical Engineering Department; M.N. Svreck, K.-Y. Teh, Graduate Researchers This project aims to implement
More informationHeat Transfer in Engines. Internal Combustion Engines
Heat Transfer in Engines Internal Combustion Engines Energy Distribution Removing heat is critical in keeping an engine and lubricant from thermal failure Amount of energy available for use: Brake thermal
More informationFundamentals of Small Gas Engines
Fundamentals of Small Gas Engines Objectives: Describe the four-stroke cycle engine operation and explain the purpose of each stroke Explain the concept of valve timing Describe two-stroke engine operation
More informationJet Aircraft Propulsion Prof Bhaskar Roy Prof. A. M. Pradeep Department of Aerospace Engineering Indian Institute of Technology, Bombay
Jet Aircraft Propulsion Prof Bhaskar Roy Prof. A. M. Pradeep Department of Aerospace Engineering Indian Institute of Technology, Bombay Lecture No. # 01 Intro and Development of Jet Aircraft Propulsion
More informationScheme G Sample Question Paper Course Name : Diploma in Automobile Engineering Course Code : AE
Sample Question Paper Semester : Fourth Marks : 100 Time: 03 Hours Q1.A. Attempt any SIX a. State different types of ideal gas processes 12 Marks b. Define dryness fraction and degree of superheat. c.
More informationDEPARTMENT OF MECHANICAL ENGINEERING. 6 th Semester
jk"vªh; izks ksfxdh lalfkku] fetksje NATIONAL INSTITUTE OF TECHNOLOGY, MIZORAM (An Institute of National Importance under Ministry of HRD, Govt. of India) CHALTLANG, AIZAWL, MIZORAM 796012 Phone/Fax: 0389-2341699
More informationCONTENTS Duct Jet Propulsion / Rocket Propulsion / Applications of Rocket Propulsion / 15 References / 25
CONTENTS PREFACE xi 1 Classification 1.1. Duct Jet Propulsion / 2 1.2. Rocket Propulsion / 4 1.3. Applications of Rocket Propulsion / 15 References / 25 2 Definitions and Fundamentals 2.1. Definition /
More informationAutomobiles. Introductory Question. 6 Questions about Automobiles. Observations about Automobiles. Question 1. Heat Engines
Automobiles 1 Automobiles 2 Introductory Question Automobiles A car burns gasoline to obtain energy but allows some heat to escape into the air. Could a mechanically perfect car avoid releasing heat altogether?
More informationFUNDAMENTALS OF POWER PLANTS. Asko Vuorinen
FUNDAMENTALS OF POWER PLANTS Asko Vuorinen 1 Engine cycles Carnot Cycle Otto Cycle Diesel Cycle Brayton Cycle Rankine Cycle Combined Cycles 2 Carnot Engine 3 Carnot Cycle 4 Carnot Cycle, continued Ideal
More informationProf. João Melo de Sousa Instituto Superior Técnico Aerospace & Applied Mechanics. Part B Acoustic Emissions 4 Airplane Noise Sources
Prof. João Melo de Sousa Instituto Superior Técnico Aerospace & Applied Mechanics Part B Acoustic Emissions 4 Airplane Noise Sources The primary source of noise from an airplane is its propulsion system.
More informationTHERMAL ENGINEERING. SHIBIN MOHAMED Asst. Professor Dept. of Mechanical Engineering Al Ameen Engineering College.
THERMAL ENGINEERING SHIBIN MOHAMED Asst. Professor Dept. of Mechanical Engineering Al Ameen Engineering College Al- Ameen Engg. College 1 Steam Engine: Definition A steam engine is a heat engine that converts
More informationAerospace Propulsion Systems
Brochure More information from http://www.researchandmarkets.com/reports/1288672/ Aerospace Propulsion Systems Description: Aerospace Propulsion Systems is a unique book focusing on each type of propulsion
More informationThermodynamics Third Law Heat Engines
Thermodynamics Third Law Heat Engines Lana Sheridan De Anza College May 11, 2018 Last time heat engines heat pumps Carnot engines Overview efficiency of Carnot engines the Third Law real engines Heat Engine
More informationIf you like us, please share us on social media. The latest UCD Hyperlibrary newsletter is now complete, check it out.
Sign In Forgot Password Register ashwenchan username password Sign In If you like us, please share us on social media. The latest UCD Hyperlibrary newsletter is now complete, check it out. ChemWiki BioWiki
More informationdensity ratio of 1.5.
Problem 1: An 8cyl 426 ci Hemi motor makes 426 HP at 5500 rpm on a compression ratio of 10.5:1. It is over square by 10% meaning that it s stroke is 10% less than it s bore. It s volumetric efficiency
More informationGovernment of Karnataka Department of Technical Education Board of Technical Examinations, Bangalore
CIE- 25 Marks Government of Karnataka Department of Technical Education Board of Technical Examinations, Bangalore Prerequisites: Knowledge of basic mathematics and Applied Science Course Objectives: 1.
More informationAERONAUTICAL ENGINEERING
AERONAUTICAL ENGINEERING SHIBIN MOHAMED Asst. Professor Dept. of Mechanical Engineering Al Ameen Engineering College Al- Ameen Engg. College 1 Aerodynamics-Basics These fundamental basics first must be
More informationMetrovick F2/4 Beryl. Turbo-Union RB199
Turbo-Union RB199 Metrovick F2/4 Beryl Development of the F2, the first British axial flow turbo-jet, began in f 940. After initial flight trials in the tail of an Avro Lancaster, two F2s were installed
More informationDesigning Efficient Engines: Strategies Based on Thermodynamics
Designing Efficient Engines: Strategies Based on Thermodynamics Jerald A. Caton Texas A&M University College Station, TX for CRC Advanced Fuel & Engine Workshop Hyatt Regency Baltimore Inner Harbor Baltimore,
More informationUnit C: Agricultural Power Systems. Lesson 1: Understanding Principles of Operation of Internal Combustion Engines
Unit C: Agricultural Power Systems Lesson 1: Understanding Principles of Operation of Internal Combustion Engines 1 Terms Compression Compression stroke Connecting rod Crankshaft Cycle Cylinder Diesel
More informationIC ENGINES. Differences between SI and CI engines: Petrol is fuel, which has a high self ignition temperature
IC ENGINES SI Engines work at constant volume. They have a compression ratio of around 6-10. But CI engines work at constant pressure and has a compression ratio of 16-20. In four stroke engines, one power
More informationJet Propulsion. Lecture-13. Ujjwal K Saha, Ph. D. Department of Mechanical Engineering Indian Institute of Technology Guwahati
Lecture-13 Prepared under QIP-CD Cell Project Jet Propulsion Ujjwal K Saha, Ph. D. Department of Mechanical Engineering Indian Institute of Technology Guwahati 1 GE J79 Turbojet 2 Features Highly used
More informationDevelopment of Low-Exergy-Loss, High-Efficiency Chemical Engines
Development of Low-Exergy-Loss, High-Efficiency Chemical Engines Investigators C. F., Associate Professor, Mechanical Engineering; Kwee-Yan Teh, Shannon L. Miller, Graduate Researchers Introduction The
More informationD5.1 : System modelling and findings adopted in system design
D5.1 : System modelling and findings adopted in system design 1 sco2 turbine Work programme WP5, task 5.1 2 Why the sco2 cycle Because it is small 10 to 100 times smaller than Rankine Because it is efficient
More informationUNIVERSITY POLYTECHNIC B.I.T., MESRA, RANCHI COURSE STRUCTURE. (W.E.F Batch Students) (Total Unit 7.5) Sessional Unit Code
COURSE STRUCTURE (W.E.F. 2011 Batch Students) (Total Unit 7.5) Course Theory Unit Course Sessional Unit Code Code DAE 4001 Thermal Engineering 1.0 DAE 4002 Thermal Engineering Lab. 0.5 DAE 4003 Fluid Mechanics
More informationAircraft Propulsion Technology
Unit 90: Aircraft Propulsion Technology Unit code: L/601/7249 QCF level: 4 Credit value: 15 Aim This unit aims to develop learners understanding of the principles and laws of aircraft propulsion and their
More informationGas Turbine Power Plant Mr.B.Ramesh, M.E.,(Ph.D)
Gas Turbine Power Plant By Mr.B.Ramesh, M.E.,(Ph.D) Research Scholar, CEG, Anna University, Chennai. Associate Professor of Mechanical Engineering, St. Joseph s College of Engineering, Jeppiaar Trust,
More information