THERMAL ENGINEERING (ME 2301 )

Slides:



Advertisements
Similar presentations
Problem Ideal and Actual Gas-Turbine (Brayton) Cycles 9–73
Advertisements

This Week > POWER CYCLES
Thermodynamics II Chapter 4 Internal Combustion Engines
Department of Mechanical Engineering ME 322 – Mechanical Engineering Thermodynamics Lecture 28 Internal Combustion Engine Models The Otto Cycle The Diesel.
İsmail ALTIN, PhD Assistant Professor Karadeniz Technical University Faculty of Marine Sciences Department of Naval Architecture and Marine Engineering.
Internal Combustion Engine Theory
Gas Power Cycles Cengel & Boles, Chapter 8 ME 152.
GAS POWER CYCLES Chapter 9. Introduction Two important areas of application for thermodynamics are power generation and refrigeration. Two important areas.
THE CARNOT CYCLE AND ITS VALUE IN ENGINEERING The Carnot cycle is composed of four totally reversible processes: isothermal heat addition, isentropic.
EGR 334 Thermodynamics Chapter 9: Sections 1-2
Chapter 1 VAPOR AND COMBINED POWER CYCLES
Lecture 11. Real Heat Engines and refrigerators (Ch. 4) Stirling heat engine Internal combustion engine (Otto cycle) Diesel engine Steam engine (Rankine.
Shaft Power Generation Devices - 1
Diesel / Brayton Cycles
Ideal Cycles, Air-Standard Assumptions, and The Otto Cycle
Thermodynamic Analysis of Internal Combustion Engines P M V SUBBARAO Professor Mechanical Engineering Department IIT Delhi Work on A Blue Print Before.
For next time: Read: § 8-6 to 8-7 HW11 due Wednesday, November 12, 2003 Outline: Isentropic efficiency Air standard cycle Otto cycle Important points:
Gas Power Cycle - Internal Combustion Engine
Engines, Motors, Turbines and Power Plants: an Overview Presentation for EGN 1002 Engineering Orientation.
INTERNAL COMBUSTION ENGINES (reciprocating). Geometry.
Applied Thermodynamics
Thermodynamic Cycles Air-standard analysis is a simplification of the real cycle that includes the following assumptions: 1) Working fluid consists of.
ENGR 2213 Thermodynamics F. C. Lai School of Aerospace and Mechanical Engineering University of Oklahoma.
Department of Mechanical Engineering ME 322 – Mechanical Engineering Thermodynamics Lecture 27 Gas Power Generation The Brayton Cycle.
EGR 334 Thermodynamics Chapter 9: Sections 5-6
Thermodynamic Cycles for CI engines In early CI engines the fuel was injected when the piston reached TC and thus combustion lasted well into the expansion.
Chapter 9 GAS POWER CYCLES
8 CHAPTER Gas Power Cycles.
Gas Power Cycles.
Combustion and Power Generation
Chapter 9 Gas Power Systems.
HEAT ENGINE D.A.DEGREE ENGG. & TECHNOLOGY
CHAPTER 9 GAS POWER CYCLES
Thermodynamic Cycles for CI engines
GAS TURBINE POWER PLANT
ENGR 2213 Thermodynamics F. C. Lai School of Aerospace and Mechanical Engineering University of Oklahoma.
TEKNIK PERMESINAN KAPAL II (Minggu – 3) LS 1329 ( 3 SKS) Jurusan Teknik Sistem Perkapalan ITS Surabaya.
Gas Power Cycles Thermodynamics Professor Lee Carkner Lecture 17.
Chapter 9 GAS POWER CYCLES
Chapter 9 Gas Power Cycles Study Guide in PowerPoint to accompany Thermodynamics: An Engineering Approach, 8th edition by Yunus A. Çengel and Michael.
AR Thermodynamics I Fall 2004 Course # 59:009 Chapter 9, Section 2 Professor Ratner.
Chapter 9 POWER AND REFRIGERATION CYCLES
ChemE 260 The Brayton Power Cycle and Variations
Heat engines and the second law of thermodynamic A heat engine: is any device that changes thermal energy into mechanical energy, such as steam engines.
Diesel Cycle and the Brayton Cycle Chapter 9b. Rudolph Diesel  German inventor who is famous for the development of the diesel engine  The diesel engine.
Internal combustion engines
THERMAL ENGINEERING (ME 2301 ) M.R.SWAMINATHAN Assistant Professor Department of Mechanical Engineering Anna University Chennai Chennai-25.
APPLIED THERMODYNAMICS UNIT- 2 Gas power cycle 1 Department of Mechanical Engineering,A.I.E.T.,Mijar 3)Air Standard Diesel Cycle/ Constant Pressure cycle:
ET375 Applied Thermodynamics 09 Thermodynamic Cycles Introduction to Gas Cycles 12/1/131rm.
Chapter 8. Production of Power from Heat 고려대학교 화공생명 공학과.
CHAPTER 9 Gas Power Cycles.
8. GAS POWER CYCLES. Objectives Evaluate the performance of gas power cycles for which the working fluid remains a gas throughout the entire cycle. Develop.
Chapter 20 Lecture 35: Entropy and the Second Law of Thermodynamics HW13 (problems):19.3, 19.10, 19.44, 19.75, 20.5, 20.18, 20.28,
Unit 61: Engineering Thermodynamics Lesson 12: Combustion Engines.
Basic Mechanical Engineering, First Edition by Dr Pravin Kumar Copyright © 2013 Dorling Kindersley (India) Pvt. Ltd. Chapter 6 Internal Combustion Engines.
Prepared by, Brijrajsinh Sarvaiya(13ME548) Jaypalsinh Jadeja(13ME517) Pradipsinh Jadeja(13ME518) Virendrasinh Parmar(13ME539) Gas power cycle.
THERMODYNAMIC ANALYSIS OF IC ENGINE Prepared by- Sudeesh kumar patel.
Gas Power Cycles.
A. Diesel cycle : The ideal cycle for CI engines
Chapter 9 GAS POWER CYCLES
BRAYTON CYCLE AND EFFECT OF INTERCOOLING , REHEAT AND REGENRATION
Unit 61: Engineering Thermodynamics
Unit 61: Engineering Thermodynamics
Chapter: 08 POWER CYCLES.
Combustion and Power Generation Engineering Thermodynamics ( )
Gas Power Cycle - Internal Combustion Engine
Engineering Thermodynamics ME-103
SI Engine Cycle Actual Cycle Intake Stroke Compression Power Exhaust
Thermo-Economic Analysis of Otto Cycle
Thermodynamic Analysis of Internal Combustion Engines
Presentation transcript:

THERMAL ENGINEERING (ME 2301 ) M.R.SWAMINATHAN Assistant Professor Department of Mechanical Engineering Anna University Chennai Chennai-25

SYLLABUS Unit-I – Air Standard Cycles, Valve Timing Unit-II – IC Engines Unit-III - Steam Turbines & Nozzles Unit-IV - Air Compressors Unit-V - Refrigeration & Air-Conditioning

AIR STANDARD CYCLES The working fluid is air, which continuously circulates in a loop and always behaves as an ideal gas. All the processes that make up the cycle are internally reversible. The combustion process is replaced by a heat-addition process from an external source. The exhaust process is replaced by a heat rejection process that restores the working fluid to its initial state.

Another assumption utilised to simplify the analysis even more is that the air has constant specific heats whose values are determined at room temperature (25°C, or 77°F). Assumptions are called the cold-air-standard assumptions. A cycle for which the air-standard assumptions are applicable is frequently referred to as an air-standard cycle

COMPRESSION RATIO The ratio of the maximum volume formed in the cylinder to the minimum (clearance) volume is called the compression ratio of the engine.

The compression ratio is a volume ratio and should not be confused with the pressure ratio. Mean effective pressure (MEP) is a fictitious pressure that, if it acted on the piston during the entire power stroke, would produce the same amount of net work as that produced during the actual cycle.

CARNOT CYCLE The Carnot cycle is composed of totally four reversible processes: isothermal heat addition, isentropic expansion, isothermal heat rejection isentropic compression

CARNOT CYCLE The Carnot cycle can be executed in a closed system (a piston-cylinder device)and either a gas or vapor can be used as the working fluid.

Otto Cycle: The ideal Cycle for Spark-Ignition Engines Figures below show the actual and ideal cycles in spark-ignition (SI) engines and their P- diagrams.

Ideal Otto Cycle The thermodynamic analysis of the actual four-stroke or two-stroke cycles can be simplified significantly if the air-standard assumptions are utilized. The T-s diagram of the Otto cycle is given in the figure at left.

The ideal Otto cycle consists of four internally reversible processes: 12 Isentropic compression 23 Constant volume heat addition 34 Isentropic expansion 41 Constant volume heat rejection

Thermal Efficiency of an Otto Cycle The Otto cycle is executed in a closed system, and disregarding the changes in kinetic and potential energies, we have

Engine Knock and Thermal Efficiency The thermal efficiency of the ideal Otto cycle increases with both the compression ratio and the specific heat ratio.

When high compression ratios are used, the temperature of the air-fuel mixture rises above the auto-ignition temperature produces an audible noise, which is called engine knock. (antiknock, tetraethyl lead?  unleaded gas) For a given compression ratio, an ideal Otto cycle using a monatomic gas (such as argon or helium, γ = 1.667) as the working fluid will have the highest thermal efficiency.

DIESEL CYCLE The diesel cycle is the ideal cycle for CI (Compression-Ignition) reciprocating engines. The CI engine first proposed by Rudolph Diesel in the 1890s, is very similar to the SI engine, differing mainly in the method of initiating combustion.

In diesel engines, ONLY air is compressed during the compression stroke, eliminating the possibility of auto-ignition. Diesel engines can be designed to operate at much higher compression ratios, typically between 12 and 24.

The fuel injection process in diesel engines starts when the piston approaches TDC and continues during the first part of the power stroke. Therefore, the combustion process in these engines takes place over a longer interval.

Because of this longer duration, the combustion process in the ideal Diesel cycle is approximated as a constant-pressure heat-addition process. This is the ONLY process where the Otto and the Diesel cycles differ.

Ideal Cycle for CI Engines

Thermal efficiency of Ideal Diesel Cycle Under the cold-air-standard assumptions, the efficiency of a Diesel cycle differs from the efficiency of Otto cycle by the quantity in the brackets.

The quantity in the brackets is always greater than 1 The quantity in the brackets is always greater than 1. Therefore, hth,Otto > hth, Diesel when both cycles operate on the same compression ratio. Also the cuttoff ratio, rc decreases, the efficiency of the Diesel cycle increases.

BRAYTON CYCLE – GAS TURBINE The open gas-turbine cycle can be modeled as a closed cycle, as shown in the figure below, by utilizing the air-standard assumptions

BRAYTON CYCLE - PROCESSES 12 Isentropic compression (in a compressor) 23 Constant pressure heat addition 34 Isentropic expansion (in a turbine) 41 Constant pressure heat rejection

The highest temperature in the cycle occurs at the end of the combustion process, and it is limited by the maximum temperature that the turbine blades can withstand.