EGR 334 Thermodynamics Chapter 9: Sections 1-2

Slides:



Advertisements
Similar presentations
ME 200 L36 Ground Transportation (Continued) (Air Standard Otto Cycle) 9.1 and 9.2 Kim See’s Office ME Gatewood Wing Room 2172 Examination and Quiz grades.
Advertisements

EGR 334 Thermodynamics Chapter 9: Sections 3-4 Lecture 32: Gas Power Systems: The Diesel Cycle Quiz Today?
THERMAL ENGINEERING (ME 2301 )
Problem Ideal and Actual Gas-Turbine (Brayton) Cycles 9–73
This Week > POWER CYCLES
Department of Mechanical Engineering ME 322 – Mechanical Engineering Thermodynamics Lecture 28 Internal Combustion Engine Models The Otto Cycle The Diesel.
Internal Combustion Engine Theory
GAS POWER CYCLES Chapter 9. Introduction Two important areas of application for thermodynamics are power generation and refrigeration. Two important areas.
EGR 334 Thermodynamics Chapter 6: Sections 6-8
Ship Propulsion Systems STEAMDIESELOTHERConventionalNuclear Slow Speed Medium Speed Gas Turbine Combined Cycle DIESEL PROPULSION.
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
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
EGR 334 Thermodynamics Chapter 6: Sections 11-13
EGR 334 Thermodynamics Chapter 12: Sections 1-4
EGR 334 Thermodynamics Chapter 5: Sections 1-9
EGR 334 Thermodynamics Chapter 9: Sections 7-8
INTERNAL COMBUSTION ENGINES (reciprocating). Geometry.
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.
EGR 334 Thermodynamics Chapter 9: Sections 5-6
EGR 334 Thermodynamics Chapter 8: Sections 1-2
Introduction Diesel Engine.
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.
EGR 334 Thermmodynamcis Chapter 3: Section 15
8 CHAPTER Gas Power Cycles.
Gas Power Cycles.
Chapter 9 Gas Power Systems.
TUTORIAL 1.
Thermodynamic Cycles for CI engines
ME 200 L35 Ground Transportation (Air Standard Otto Cycle) 9.1 and 9.2 Material not picked up this week may be recycled! ME 200 L35 Ground Transportation.
TEKNIK PERMESINAN KAPAL II (Minggu – 3) LS 1329 ( 3 SKS) Jurusan Teknik Sistem Perkapalan ITS Surabaya.
INTERNAL COMBUSTION ENGINES LECTURER PROF.Dr. DEMIR BAYKA.
Supreme Power Engine Basics The four cycle engine.
Gas Power Cycles Thermodynamics Professor Lee Carkner Lecture 17.
Chapter 9 Gas Power Cycles Study Guide in PowerPoint to accompany Thermodynamics: An Engineering Approach, 8th edition by Yunus A. Çengel and Michael.
MT 313 IC ENGINES LECTURE NO: 04 (24 Feb, 2014) Khurram Yahoo Group Address: ICE14.
AR Thermodynamics I Fall 2004 Course # 59:009 Chapter 9, Section 2 Professor Ratner.
The piston descends from the top of the cylinder to the bottom of the cylinder, reducing the pressure inside the cylinder. A mixture of fuel and air,
Engine Cycle Analysis. Air Standard Otto Cycle.
Presentation on HEAT ENGINE PREPARED BY: CHAUHAN SATISH(EN. NO: ) GAUTAM ASHISH(EN. NO: ) KETUL PATEL(EN. NO: ) SUB:
Internal combustion engines
ET375 Applied Thermodynamics 09 Thermodynamic Cycles Introduction to Gas Cycles 12/1/131rm.
Dr. Owen Clarkin School of Mechanical & Manufacturing Engineering Summary of Energy Topics Chapter 1: Thermodynamics / Energy Introduction Chapter 2: Systems.
Heat Engines A gasoline engine is a form of a heat engine, e.g. a 4-stroke engine INTAKE stroke: the piston descends from the top to the bottom of the.
1 3E-03 Fire Syringe RAPID COMPRESSION IS ADIABATIC GIVING RAPID RISE OF AIR TEMPERATURE IN THE CHAMBER WHICH EXCEEDS THE IGNITION TEMPERATURE OF THE FLAMMABLE.
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.
Analysis of Diesel Cycle and Scope for Modification P M V Subbarao Professor Mechanical Engineering Department Creation of Rational Models for Engines…
LECTURE 1.
THERMODYNAMIC ANALYSIS OF IC ENGINE Prepared by- Sudeesh kumar patel.
Real Heat Engines Stirling heat engine
Thermodynamics, Lesson 4-4: The Air Standard Diesel Cycle
Gas Power Cycles.
A. Diesel cycle : The ideal cycle for CI engines
Unit 61: Engineering Thermodynamics
Combustion and Power Generation Engineering Thermodynamics ( )
ES 211:Thermodynamics Tutorial 10
Gas Power Cycle - Internal Combustion Engine
Engineering Thermodynamics ME-103
SI Engine Cycle Actual Cycle Intake Stroke Compression Power Exhaust
Copyright © John Wiley & Sons Ltd.
Thermo-Economic Analysis of Otto Cycle
Thermodynamic Analysis of Internal Combustion Engines
Presentation transcript:

EGR 334 Thermodynamics Chapter 9: Sections 1-2 Lecture 33: Gas Power Systems: The Otto Cycle Quiz Today?

Today’s main concepts: Understand common terminology of gas power cycles. Be able to explain the processes of the Otto Cycle Be able to perform a 1st Law analysis of the Otto Cycle and determine its thermal efficiency. Be able to discuss limitations of the Otto cycle compared to real spark ignition power systems. Be able to state the assumptions of standard air analysis. Reading Assignment: Read Chapter 9, Sections 3-4 Homework Assignment: Problems from Chap 9: 1, 4, 11, 14

Two types of internal combustion engine Sec 9.1 : Introducing Engine Terminology Two types of internal combustion engine Spark Ignition (lower power & lighter) Compression Ignition (spontaneous combustion) Terminology Stroke : The distance the piston moves in one direction Top Dead Center : The piston has minimum volume at the top of the stroke. Bottom Dead Center : The piston has maximum volume at the bottom of the stroke. Clearance Volume : Min vol Displacement Volume : Max vol. – Min vol. Compression Ratio: Max vol. / min vol.

Intake stroke : fill cylinder Sec 9.1 : Introducing Engine Terminology Four Stroke Cycle : Two revolutions : Combusts mix of hydrocarbons + O2 Intake stroke : fill cylinder Spark cycle : fill with fuel and air mixture Compression cycle : fill with air Compression stroke : p , T , V , Win Spark cycle : spark near end of stroke Compression cycle : inject fuel Power stroke  : gas expands Exhaust stroke  : spent gas is exhausted U--Tube video of 4 stroke: http://www.youtube.com/watch?v=2Yx32F1cncg

Two Stroke Cycle : Two revolutions Power/Exhaust: Sec 9.1 : Introducing Engine Terminology Two Stroke Cycle : Two revolutions Power/Exhaust: The piston is forced down @ exhaust port, spent gas leaves Piston continues down and compresses air/fuel in crank case Compressed charge enters cylinder Intake/Compression Piston moves up compressing charge Draws vacuum in crank case. http://www.drivegreen.com/Auto_Basics_Engines.htm Two Stroke Animation: http://library.thinkquest.org/C006011/english/sites/2_taktmotor.php3?v=2

Mean Effective Pressure (mep) Sec 9.1 : Introducing Engine Terminology Mean Effective Pressure (mep) Air –standard Analysis (A simplification used to allow for thermodynamic analysis) Assumptions: -- Fixed amount of air modeled as closed system -- Air is treated as Ideal Gas -- Constant cp (cold air-standard) -- Combustion is modeled as a heat transfer to system, Exhaust as heat flow out of system -- All processes internally reversible

Ideal Gas Model Review State Equation: Energy Relationships: Chap 3: Quality Polytropic Process Ideal Gas Model Relations: Ideal Gas Model Review State Equation: Energy Relationships: where or look up values for k, cv, and cp on Table A-20 Entropy Relationships: where so values are found on Table A-22 Special case: isentropic process where s1 = s2 then ( assuming constant specific heats) ( vr and pr for use with Table A-22)

Assumption: At top dead center, heat addition occurs instantaneously Sec 9.2 : Air-Standard Otto Cycle Assumption: At top dead center, heat addition occurs instantaneously Otto Cycle: comprised of 4 internally reversible processes Process 1 – 2 : Isentropic compression of air (compression stroke). Process 2 – 3 : Constant volume heat transfer to the air from an external source while piston is at top dead center (ignition) Process 3 – 4 : Isentropic expansion (power stroke) Process 4 – 1 : Completes cycle by a constant volume process in which heat is rejected from the air while piston is at bottom dead center ignition power ignition compression power compression exhaust exhaust

Otto Cycle analysis Processes 1–2: ∆s = 0 and Q = 0 Sec 9.2 : Air-Standard Otto Cycle Otto Cycle analysis Closed system energy balance : Processes 1–2: ∆s = 0 and Q = 0 Process 3–4: ∆s = 0 and Q = 0 Processes 2–3 : ∆V = 0 and W = 0 Processes 4-1 : ∆V = 0 and W = 0

Otto Cycle Thermal Efficiency: Sec 9.2 : Air-Standard Otto Cycle Otto Cycle Thermal Efficiency: Thermal Efficiency can also be related to the compression ratio: clearance displacement As the compression ration, r, , the efficiency, η, 

Example (9.11): An air-standard Otto cycle has a compression ratio of 7.5. At the beginning of compression, p1 = 85 kPa and T1 = 32°C. The mass of air is 2 g, and the maximum temperature in the cycle is 960 K. Determine The heat rejection, in kJ. The net work, in kJ. The thermal efficiency. The mean effective pressure, in kPa. State 1 2 3 4 T (K) 305 960 p (kPa) 85 u (kJ/kg) v T3= 960 K p1=85 kPa T1=305 K

State 1: Using Ideal Gas Law: and Table A-22: Example (9.11): State 1 2 3 4 T (K) 305 960 p (kPa) 85 u (kJ/kg) v The heat rejection, in kJ. The net work, in kJ. The thermal efficiency. The mean effective pressure, in kPa. State 1: Using Ideal Gas Law: and Table A-22: State 2: Using compression ratio, ideal gas law, and Table A-22: 

State 3: using v3 = v2, ideal gas law, and Table A22: Example (9.11): State 1 2 3 4 T (K) 305 960 p (kPa) 85 u (kJ/kg) 217.67 v 1.0298 0.1373 The heat rejection, in kJ. The net work, in kJ. The thermal efficiency. The mean effective pressure, in kPa. State 3: using v3 = v2, ideal gas law, and Table A22: State 4: Using v4=v1:

then for isentropic process 1-2 using k = 1.361 and Table A-22: Example (9.11): State 1 2 3 4 T (K) 305 960 p (kPa) 85 2006.7 u (kJ/kg) 217.67 725.02 v 1.0298 0.1373 The heat rejection, in kJ. The net work, in kJ. The thermal efficiency. The mean effective pressure , in kPa. also knowing for isentropic processes then for isentropic process 1-2 using k = 1.361 and Table A-22: and for isentropic process 3-4:

Heat added during process 2-3: Example (9.11): State 1 2 3 4 T (K) 305 631 960 464 p (kPa) 85 1319 2006.7 129.3 u (kJ/kg) 217.67 458.55 725.02 328.5 v 1.0298 0.1373 The heat rejection, in kJ. The net work, in kJ. The thermal efficiency. The mean effective pressure, in kPa. Heat added during process 2-3: Heat rejected during process 4-1:

Net Work over the cycle: Example (9.11): State 1 2 3 4 T (K) 305 631 960 464 p (kPa) 85 1319 2006.7 129.3 u (kJ/kg) 217.67 458.55 725.02 328.5 v 1.0298 0.1373 The heat rejection, in kJ. The net work, in kJ. The thermal efficiency. The mean effective pressure, in kPa. Net Work over the cycle: Cycle Efficiency: Compare to

Mean Effective Pressure: Example (9.11): State 1 2 3 4 T (K) 305 631 960 464 p (kPa) 85 1319 2006.7 129.3 u (kJ/kg) 217.67 458.55 725.02 328.5 v 1.0298 0.1373 The heat rejection, in kJ. The net work, in kJ. The thermal efficiency. The mean effective pressure, in kPa. Mean Effective Pressure: where

End of Slides for Lecture 33