SlideShare une entreprise Scribd logo
1  sur  25
“Dual Combustion Engine”
Presented To:
Sir Qazi Shehzad
Presented by:
 Jawaria Bint Faheem (12063122-008)
Areeba Malik (12063122-050)
Areeba Asif (12063122-070)
Hina Usman (12063122-077)
Beenish Hafeez (12063122-085)
Engine???
• A Machine Designed To
Convert Energy Into
Useful Mechanical
Motion.
• Thermal Energy Raises
Temperature And
Pressure Of Gases Within
Engine, And Gas Expands
Against Mechanical
Mechanisms Of Engine.
History
• Oil Engine 1888.
• Ackroyd Staurt
(Automatic
Ignition).
• Rudolf Diesel Used
This Principle And
Developed Basis
Of Dual
Combustion
Engine.
Dual Combustion Engine
• It is an internal combustion four
stroke engine.
• “Dual” Because Combustion Takes
Place In Two Parts First At Constant
Pressure And Second At Constant
Volume.
• This makes it better than diesel
engine’s cycle.
Dual Combustion Cycle
• Also Known As The Limited Pressure Or Mixed
Cycle, Seiliger Cycle Or Sabathe Cycle.
• Thermal Cycle That Is A Combination Of The
Otto Cycle And The Diesel Cycle.
Characteristics
• It is a four stroke
engine.
• Improved and modern
form of old Diesel
engine’s cycles.
• Its one stroke is divided
into two parts allowing
it to carry out more
work..
• Have increased
efficiency.
Parts Of Engine
Stroke
• Each Cycle Of Piston Consists Of Two
Opposite Motions:
There Is A Motion In One Direction, And
Then A Motion Back In The Opposite
Direction. Each Of These Is Called A Stroke
• Stroke Is The Action Of A Piston Travelling
The Full Length Of Its Locomotive Cylinder Or
Engine Cylinder In One Direction.
Indicator Diagram
Sequence of Operations
The dual cycle consists of following
operations:
• Adiabatic compression
• Addition of heat at constant volume.
• Addition of heat at constant pressure.
• Adiabatic expansion.
• Rejection of heat at constant volume.
Explanation
1)Adiabatic Compression:
Adiabatically compressed air, it turned
hot. Fuel injection starts before the point
of maximum compression.(ignition phase)
2) Constant Volume Phase:
After a short delay the fuel warms up to
the air temperature causing a sudden rise
in pressure.
Continued …
3) Constant Pressure Phase:
Further Injection Keeps The Fuel Burning As
Volume Increases
4) Adiabatic Expansion:
After Cut Off, Hot Air Expands Isentropically.
5)Constant Volume (End Stroke):
Exhaust Valve Opens Producing A Sudden
Drop In Pressure Getting Heat Out.
Efficiency
• Engine efficiency of
thermal engines is the
relationship between the
total energy contained in
the fuel, and the amount
of energy used to
perform useful work.
Expression For Efficiency
• From first law of thermodynamics
Q = ∆U + W
And..
• ∆W = Q1 – Q2
• The efficiency of engine is defined as
ƞ = Output / input
Continued..
• The efficiency of engine is defined as useful
work done to the heat provided.
Where,
• Q1 is the heat absorbed
• Q1 – Q2 is work done.
Efficiency of dual combustion engine
The analysis of cycle is as follows:
The heat is supplied In two stages. hence
Qin = mcp(T4 – T3) + mcv(T3 – T2)
 The heat rejected is
Qout = mcv(T5 – T1)
Simplification
The thermal efficiency may b found as
follows:
ƞ = 1 – Qout/ Qin
= 1 – mcv(T5 – T1)/ mcv(T3 -T2)+mcp(T4 –
T3)
=1 – (T5 – T1)/ (T3 – T2) +ϒ(T4 – T3)
Simplification Of Formulae
• The formula can be further developed to
show that:
η = 1-(kβγ -1)/[(k-1) +γk(β-1)]rv
γ-1
• rv is the VOLUME COMPRESSION RATIO.
• rv = V1/V2
• β is the CUT OFF RATIO.
• β = V4/V3
• k is the ratio p3/p2.
• If k=1 then it becomes Otto cycle’s
efficiency.
“Applications”
Dual combustion engines are most commonly used
for mobile propulsion in vehicles and portable
machinery.
In mobile equipment, dual combustion is
advantageous since it can provide high power-to-
weight ratios.
“Automobiles”
• Generally using fossil fuel(mainly petroleum),
these engines have appeared in transport in
almost all vehicles
(automobiles, trucks, motorcycles, boats, and in
a wide variety of aircraft and locomotives).
Generators/Aircrafts
• Very high power-to-weight ratios are
required, dual combustion engines appear in
the form of gas turbines. These applications
include jet aircraft, helicopters, large ships
and electric generators.
“Future Energy Use”
There is a role for Dual Combustion engines for
future energy use, because
– Dual combustion engine has high power to
weigh ratio.
– Relatively low cost.
– Flexible fuel use.
– Established manufacturing investment.
References
Text books:
By Mcconkey And Rajput.
Web sources:
• www.marineinfo.com
• www.freestudy.co.uk
• http://www.brighthubengineering.com/
• en.wikipedia.org
• www.wartsila.com
Research Pappers:
• Gas Power Cycles Prof. U.S.P. Shet ,and Prof. J.M
. Mallikarjuna
• Performance Analysis of a Dual Cycle Engine by
Ebrahimi
Dual combustion cycle

Contenu connexe

Tendances

Reversed carnot cycle
Reversed carnot cycle   Reversed carnot cycle
Reversed carnot cycle Ihsan Wassan
 
Reciprocating Compressor
Reciprocating CompressorReciprocating Compressor
Reciprocating CompressorAditya Sharma
 
INTERNAL COMBUSTION ENGINES PPT
INTERNAL COMBUSTION ENGINES PPT INTERNAL COMBUSTION ENGINES PPT
INTERNAL COMBUSTION ENGINES PPT AKASH1001
 
Air compressor
Air compressorAir compressor
Air compressorsureshkcet
 
Four Stroke SI and CI engines
Four Stroke SI and CI enginesFour Stroke SI and CI engines
Four Stroke SI and CI enginesS.Vijaya Bhaskar
 
COMBUSTION IN S I & C I ENGINES
COMBUSTION IN S I & C I ENGINESCOMBUSTION IN S I & C I ENGINES
COMBUSTION IN S I & C I ENGINESJim Alex
 
Basic of Combustion in CI Engines
Basic of Combustion in CI EnginesBasic of Combustion in CI Engines
Basic of Combustion in CI EnginesSACHINNikam39
 
I.C.Engine performance parameters
I.C.Engine performance parametersI.C.Engine performance parameters
I.C.Engine performance parametersLokendra Kumar
 
CI Engine Knocking
CI Engine KnockingCI Engine Knocking
CI Engine KnockingRajat Seth
 
Thermodynamic Chapter 5 Air Standard Cycle
Thermodynamic Chapter 5 Air Standard CycleThermodynamic Chapter 5 Air Standard Cycle
Thermodynamic Chapter 5 Air Standard CycleMuhammad Surahman
 
Gas Turbine and Jet propulsion
Gas Turbine and Jet propulsionGas Turbine and Jet propulsion
Gas Turbine and Jet propulsionSLA1987
 
Basic Scheme Open Cycle Gas Turbine Plant
Basic Scheme Open Cycle Gas Turbine Plant Basic Scheme Open Cycle Gas Turbine Plant
Basic Scheme Open Cycle Gas Turbine Plant Aman Gupta
 
basics of Internal combution engine
basics of Internal combution enginebasics of Internal combution engine
basics of Internal combution enginenaphis ahamad
 
Principles of carburetion
Principles of carburetionPrinciples of carburetion
Principles of carburetiongurprits2
 
Basics of IC engine
Basics of IC engineBasics of IC engine
Basics of IC engineSLA1987
 
CLASSIFICATION OF COMPRESSORS
CLASSIFICATION OF COMPRESSORS CLASSIFICATION OF COMPRESSORS
CLASSIFICATION OF COMPRESSORS Srinivas Mylapalli
 

Tendances (20)

Reversed carnot cycle
Reversed carnot cycle   Reversed carnot cycle
Reversed carnot cycle
 
otto cycle
otto cycleotto cycle
otto cycle
 
Rotary compressors ppt
Rotary compressors pptRotary compressors ppt
Rotary compressors ppt
 
Reciprocating Compressor
Reciprocating CompressorReciprocating Compressor
Reciprocating Compressor
 
INTERNAL COMBUSTION ENGINES PPT
INTERNAL COMBUSTION ENGINES PPT INTERNAL COMBUSTION ENGINES PPT
INTERNAL COMBUSTION ENGINES PPT
 
Air compressor
Air compressorAir compressor
Air compressor
 
Four Stroke SI and CI engines
Four Stroke SI and CI enginesFour Stroke SI and CI engines
Four Stroke SI and CI engines
 
Compressor and Types
Compressor and TypesCompressor and Types
Compressor and Types
 
COMBUSTION IN S I & C I ENGINES
COMBUSTION IN S I & C I ENGINESCOMBUSTION IN S I & C I ENGINES
COMBUSTION IN S I & C I ENGINES
 
Basic of Combustion in CI Engines
Basic of Combustion in CI EnginesBasic of Combustion in CI Engines
Basic of Combustion in CI Engines
 
I.C.Engine performance parameters
I.C.Engine performance parametersI.C.Engine performance parameters
I.C.Engine performance parameters
 
CI Engine Knocking
CI Engine KnockingCI Engine Knocking
CI Engine Knocking
 
Thermodynamic Chapter 5 Air Standard Cycle
Thermodynamic Chapter 5 Air Standard CycleThermodynamic Chapter 5 Air Standard Cycle
Thermodynamic Chapter 5 Air Standard Cycle
 
Gas Turbine and Jet propulsion
Gas Turbine and Jet propulsionGas Turbine and Jet propulsion
Gas Turbine and Jet propulsion
 
Basic Scheme Open Cycle Gas Turbine Plant
Basic Scheme Open Cycle Gas Turbine Plant Basic Scheme Open Cycle Gas Turbine Plant
Basic Scheme Open Cycle Gas Turbine Plant
 
basics of Internal combution engine
basics of Internal combution enginebasics of Internal combution engine
basics of Internal combution engine
 
Principles of carburetion
Principles of carburetionPrinciples of carburetion
Principles of carburetion
 
Basics of IC engine
Basics of IC engineBasics of IC engine
Basics of IC engine
 
Brayton cycle
Brayton cycleBrayton cycle
Brayton cycle
 
CLASSIFICATION OF COMPRESSORS
CLASSIFICATION OF COMPRESSORS CLASSIFICATION OF COMPRESSORS
CLASSIFICATION OF COMPRESSORS
 

En vedette

Thermodynamic Chapter 4 Second Law Of Thermodynamics
Thermodynamic Chapter 4 Second Law Of ThermodynamicsThermodynamic Chapter 4 Second Law Of Thermodynamics
Thermodynamic Chapter 4 Second Law Of ThermodynamicsMuhammad Surahman
 
Hardware implementation of cots avionics system on unmanned
Hardware implementation of cots avionics system on unmannedHardware implementation of cots avionics system on unmanned
Hardware implementation of cots avionics system on unmannedUniversity of Gujrat, Pakistan
 
Kevin beyond theschlockofthenew_feb2015
Kevin beyond theschlockofthenew_feb2015Kevin beyond theschlockofthenew_feb2015
Kevin beyond theschlockofthenew_feb2015Plan
 
Stirling cycle & its applications
Stirling cycle & its applicationsStirling cycle & its applications
Stirling cycle & its applicationsLokesh Raju
 
Atkinson Cycle, Ericsson Cycle And Stirling Cycle
Atkinson Cycle, Ericsson Cycle And Stirling CycleAtkinson Cycle, Ericsson Cycle And Stirling Cycle
Atkinson Cycle, Ericsson Cycle And Stirling CycleDhaval Shukla
 
MET 401 Chapter 6 -_gas_turbine_power_plant_brayton_cycle_-_copy
MET 401 Chapter 6 -_gas_turbine_power_plant_brayton_cycle_-_copyMET 401 Chapter 6 -_gas_turbine_power_plant_brayton_cycle_-_copy
MET 401 Chapter 6 -_gas_turbine_power_plant_brayton_cycle_-_copyIbrahim AboKhalil
 
Multiplication & division instructions microprocessor 8086
Multiplication & division instructions microprocessor 8086Multiplication & division instructions microprocessor 8086
Multiplication & division instructions microprocessor 8086University of Gujrat, Pakistan
 
Christian Titze, "Hello From the Other Side: Adapting the Agile Agency to Cli...
Christian Titze, "Hello From the Other Side: Adapting the Agile Agency to Cli...Christian Titze, "Hello From the Other Side: Adapting the Agile Agency to Cli...
Christian Titze, "Hello From the Other Side: Adapting the Agile Agency to Cli...WebVisions
 

En vedette (20)

Dual cycle
Dual cycleDual cycle
Dual cycle
 
Diesel cycle
Diesel cycleDiesel cycle
Diesel cycle
 
Diesel cycle
Diesel cycleDiesel cycle
Diesel cycle
 
Natural disasters of pakistan
Natural disasters of pakistanNatural disasters of pakistan
Natural disasters of pakistan
 
Thermodynamic Chapter 4 Second Law Of Thermodynamics
Thermodynamic Chapter 4 Second Law Of ThermodynamicsThermodynamic Chapter 4 Second Law Of Thermodynamics
Thermodynamic Chapter 4 Second Law Of Thermodynamics
 
Helicopter Automation Using Low Cost Sensors
Helicopter Automation Using Low Cost SensorsHelicopter Automation Using Low Cost Sensors
Helicopter Automation Using Low Cost Sensors
 
Wireless sensors network in Avionic control system
Wireless sensors network in Avionic control systemWireless sensors network in Avionic control system
Wireless sensors network in Avionic control system
 
Hardware implementation of cots avionics system on unmanned
Hardware implementation of cots avionics system on unmannedHardware implementation of cots avionics system on unmanned
Hardware implementation of cots avionics system on unmanned
 
An autonomous uav with an optical flow sensor
An autonomous uav with an optical flow sensorAn autonomous uav with an optical flow sensor
An autonomous uav with an optical flow sensor
 
Internal microprocessor architecture
Internal microprocessor architectureInternal microprocessor architecture
Internal microprocessor architecture
 
Kevin beyond theschlockofthenew_feb2015
Kevin beyond theschlockofthenew_feb2015Kevin beyond theschlockofthenew_feb2015
Kevin beyond theschlockofthenew_feb2015
 
Stirling cycle & its applications
Stirling cycle & its applicationsStirling cycle & its applications
Stirling cycle & its applications
 
Probability And Random Variable Lecture 1
Probability And Random Variable Lecture 1Probability And Random Variable Lecture 1
Probability And Random Variable Lecture 1
 
Brayton cycle
Brayton cycleBrayton cycle
Brayton cycle
 
Atkinson Cycle, Ericsson Cycle And Stirling Cycle
Atkinson Cycle, Ericsson Cycle And Stirling CycleAtkinson Cycle, Ericsson Cycle And Stirling Cycle
Atkinson Cycle, Ericsson Cycle And Stirling Cycle
 
Brayton cycle
Brayton cycleBrayton cycle
Brayton cycle
 
MET 401 Chapter 6 -_gas_turbine_power_plant_brayton_cycle_-_copy
MET 401 Chapter 6 -_gas_turbine_power_plant_brayton_cycle_-_copyMET 401 Chapter 6 -_gas_turbine_power_plant_brayton_cycle_-_copy
MET 401 Chapter 6 -_gas_turbine_power_plant_brayton_cycle_-_copy
 
Bus interface 8086
Bus interface 8086Bus interface 8086
Bus interface 8086
 
Multiplication & division instructions microprocessor 8086
Multiplication & division instructions microprocessor 8086Multiplication & division instructions microprocessor 8086
Multiplication & division instructions microprocessor 8086
 
Christian Titze, "Hello From the Other Side: Adapting the Agile Agency to Cli...
Christian Titze, "Hello From the Other Side: Adapting the Agile Agency to Cli...Christian Titze, "Hello From the Other Side: Adapting the Agile Agency to Cli...
Christian Titze, "Hello From the Other Side: Adapting the Agile Agency to Cli...
 

Similaire à Dual combustion cycle

Chap 8: Internal Combustion Engine Power Plant
Chap 8: Internal Combustion Engine Power PlantChap 8: Internal Combustion Engine Power Plant
Chap 8: Internal Combustion Engine Power PlantMulugeta Wotango
 
Gas Turbine Engine For Automotive Application
Gas Turbine Engine For Automotive ApplicationGas Turbine Engine For Automotive Application
Gas Turbine Engine For Automotive ApplicationHASSAN ALESSA
 
2nd law of thermodynamics
 2nd law of thermodynamics 2nd law of thermodynamics
2nd law of thermodynamicsGM Red
 
Chapter 5 internal_combustion_engine
Chapter 5 internal_combustion_engineChapter 5 internal_combustion_engine
Chapter 5 internal_combustion_engineHashem Yahya Almahdi
 
Air standard cycles_PPT KM1.pptx .
Air standard cycles_PPT KM1.pptx          .Air standard cycles_PPT KM1.pptx          .
Air standard cycles_PPT KM1.pptx .happycocoman
 
Module 5 _TE_ Introduction.pptx
Module 5 _TE_ Introduction.pptxModule 5 _TE_ Introduction.pptx
Module 5 _TE_ Introduction.pptxPrabhatHambire
 
selfstudy-1.ppt
selfstudy-1.pptselfstudy-1.ppt
selfstudy-1.pptEanest
 
presention-150806044916-lva1-app6891.pdf
presention-150806044916-lva1-app6891.pdfpresention-150806044916-lva1-app6891.pdf
presention-150806044916-lva1-app6891.pdfssuser96912f1
 
Thermodynamic cycles4.ppt
Thermodynamic cycles4.pptThermodynamic cycles4.ppt
Thermodynamic cycles4.pptMehtab Rai
 
Energy Coservation In Gas turbine
Energy Coservation In Gas turbineEnergy Coservation In Gas turbine
Energy Coservation In Gas turbineparas garg
 
Basic Diesel Engine SANY_KOEL.PDF
Basic Diesel Engine SANY_KOEL.PDFBasic Diesel Engine SANY_KOEL.PDF
Basic Diesel Engine SANY_KOEL.PDFAvinashSilimkar2
 

Similaire à Dual combustion cycle (20)

Heat Engine
 Heat Engine Heat Engine
Heat Engine
 
Chap 8: Internal Combustion Engine Power Plant
Chap 8: Internal Combustion Engine Power PlantChap 8: Internal Combustion Engine Power Plant
Chap 8: Internal Combustion Engine Power Plant
 
Gas Turbine Engine For Automotive Application
Gas Turbine Engine For Automotive ApplicationGas Turbine Engine For Automotive Application
Gas Turbine Engine For Automotive Application
 
Otto engines
Otto enginesOtto engines
Otto engines
 
Petrol engine
Petrol enginePetrol engine
Petrol engine
 
Air standard cycles carnot, stirling, ericsson
Air standard cycles  carnot, stirling, ericssonAir standard cycles  carnot, stirling, ericsson
Air standard cycles carnot, stirling, ericsson
 
2nd law of thermodynamics
 2nd law of thermodynamics 2nd law of thermodynamics
2nd law of thermodynamics
 
Chapter 5 internal_combustion_engine
Chapter 5 internal_combustion_engineChapter 5 internal_combustion_engine
Chapter 5 internal_combustion_engine
 
Air standard cycles_PPT KM1.pptx .
Air standard cycles_PPT KM1.pptx          .Air standard cycles_PPT KM1.pptx          .
Air standard cycles_PPT KM1.pptx .
 
Air standard cycles carnot, stirling, ericsson
Air standard cycles  carnot, stirling, ericssonAir standard cycles  carnot, stirling, ericsson
Air standard cycles carnot, stirling, ericsson
 
Module 5 _TE_ Introduction.pptx
Module 5 _TE_ Introduction.pptxModule 5 _TE_ Introduction.pptx
Module 5 _TE_ Introduction.pptx
 
selfstudy-1.ppt
selfstudy-1.pptselfstudy-1.ppt
selfstudy-1.ppt
 
presention-150806044916-lva1-app6891.pdf
presention-150806044916-lva1-app6891.pdfpresention-150806044916-lva1-app6891.pdf
presention-150806044916-lva1-app6891.pdf
 
Combustion cycle
Combustion cycleCombustion cycle
Combustion cycle
 
Unit-1_PPT.pptx
Unit-1_PPT.pptxUnit-1_PPT.pptx
Unit-1_PPT.pptx
 
Basic of engine
Basic of engineBasic of engine
Basic of engine
 
Thermodynamic cycles4.ppt
Thermodynamic cycles4.pptThermodynamic cycles4.ppt
Thermodynamic cycles4.ppt
 
Carnot cycle
Carnot cycleCarnot cycle
Carnot cycle
 
Energy Coservation In Gas turbine
Energy Coservation In Gas turbineEnergy Coservation In Gas turbine
Energy Coservation In Gas turbine
 
Basic Diesel Engine SANY_KOEL.PDF
Basic Diesel Engine SANY_KOEL.PDFBasic Diesel Engine SANY_KOEL.PDF
Basic Diesel Engine SANY_KOEL.PDF
 

Plus de University of Gujrat, Pakistan

Constitutional development of pakistan since 1947 to thereayf
Constitutional development of pakistan since 1947 to thereayfConstitutional development of pakistan since 1947 to thereayf
Constitutional development of pakistan since 1947 to thereayfUniversity of Gujrat, Pakistan
 
Passive Thermal management for avionics in high temperature environment
Passive Thermal management for avionics in high temperature environmentPassive Thermal management for avionics in high temperature environment
Passive Thermal management for avionics in high temperature environmentUniversity of Gujrat, Pakistan
 
Future Integrated Systems Concept for Preventing Aircraft Loss-of-Control (L...
Future Integrated Systems Concept for Preventing Aircraft Loss-of-Control (L...Future Integrated Systems Concept for Preventing Aircraft Loss-of-Control (L...
Future Integrated Systems Concept for Preventing Aircraft Loss-of-Control (L...University of Gujrat, Pakistan
 
A wireless sensors network in Aircraft Control Systems
A wireless sensors network in Aircraft Control SystemsA wireless sensors network in Aircraft Control Systems
A wireless sensors network in Aircraft Control SystemsUniversity of Gujrat, Pakistan
 
Towards Automating Interface Control Documents Elaboration and Management
Towards Automating Interface Control Documents Elaboration and ManagementTowards Automating Interface Control Documents Elaboration and Management
Towards Automating Interface Control Documents Elaboration and ManagementUniversity of Gujrat, Pakistan
 
APPLICATION OF WIRELESS SENSOR NETWORKS TO AIRCRAFT CONTROL AND HEALTH MANAGE...
APPLICATION OF WIRELESS SENSOR NETWORKS TO AIRCRAFT CONTROL AND HEALTH MANAGE...APPLICATION OF WIRELESS SENSOR NETWORKS TO AIRCRAFT CONTROL AND HEALTH MANAGE...
APPLICATION OF WIRELESS SENSOR NETWORKS TO AIRCRAFT CONTROL AND HEALTH MANAGE...University of Gujrat, Pakistan
 
Rapid Start-Up / Restart Avionics Provide Robust Fault Tolerance with SCp (S...
Rapid Start-Up / Restart Avionics Provide Robust Fault  Tolerance with SCp (S...Rapid Start-Up / Restart Avionics Provide Robust Fault  Tolerance with SCp (S...
Rapid Start-Up / Restart Avionics Provide Robust Fault Tolerance with SCp (S...University of Gujrat, Pakistan
 
Improving Avionics using aircraft Information Sharing Network(Research Paper)
Improving Avionics using aircraft Information Sharing Network(Research Paper)Improving Avionics using aircraft Information Sharing Network(Research Paper)
Improving Avionics using aircraft Information Sharing Network(Research Paper)University of Gujrat, Pakistan
 

Plus de University of Gujrat, Pakistan (20)

Carnot cycle
Carnot cycleCarnot cycle
Carnot cycle
 
Constitutional development of pakistan since 1947 to thereayf
Constitutional development of pakistan since 1947 to thereayfConstitutional development of pakistan since 1947 to thereayf
Constitutional development of pakistan since 1947 to thereayf
 
Essay writing
Essay writingEssay writing
Essay writing
 
Letter writing (Communication Skills)
Letter writing (Communication Skills)Letter writing (Communication Skills)
Letter writing (Communication Skills)
 
Architecture of high end processors
Architecture of high end processorsArchitecture of high end processors
Architecture of high end processors
 
Architecture of pentium family
Architecture of pentium familyArchitecture of pentium family
Architecture of pentium family
 
Protected mode memory addressing 8086
Protected mode memory addressing 8086Protected mode memory addressing 8086
Protected mode memory addressing 8086
 
Passive Thermal management for avionics in high temperature environment
Passive Thermal management for avionics in high temperature environmentPassive Thermal management for avionics in high temperature environment
Passive Thermal management for avionics in high temperature environment
 
Future Integrated Systems Concept for Preventing Aircraft Loss-of-Control (L...
Future Integrated Systems Concept for Preventing Aircraft Loss-of-Control (L...Future Integrated Systems Concept for Preventing Aircraft Loss-of-Control (L...
Future Integrated Systems Concept for Preventing Aircraft Loss-of-Control (L...
 
A wireless sensors network in Aircraft Control Systems
A wireless sensors network in Aircraft Control SystemsA wireless sensors network in Aircraft Control Systems
A wireless sensors network in Aircraft Control Systems
 
Towards Automating Interface Control Documents Elaboration and Management
Towards Automating Interface Control Documents Elaboration and ManagementTowards Automating Interface Control Documents Elaboration and Management
Towards Automating Interface Control Documents Elaboration and Management
 
APPLICATION OF WIRELESS SENSOR NETWORKS TO AIRCRAFT CONTROL AND HEALTH MANAGE...
APPLICATION OF WIRELESS SENSOR NETWORKS TO AIRCRAFT CONTROL AND HEALTH MANAGE...APPLICATION OF WIRELESS SENSOR NETWORKS TO AIRCRAFT CONTROL AND HEALTH MANAGE...
APPLICATION OF WIRELESS SENSOR NETWORKS TO AIRCRAFT CONTROL AND HEALTH MANAGE...
 
AVIONIC CONTROL SYSTEMS FOR EDUCATION & DEVELOPMENT
AVIONIC CONTROL SYSTEMS FOR EDUCATION & DEVELOPMENTAVIONIC CONTROL SYSTEMS FOR EDUCATION & DEVELOPMENT
AVIONIC CONTROL SYSTEMS FOR EDUCATION & DEVELOPMENT
 
Flight control and system 100
Flight control and system 100Flight control and system 100
Flight control and system 100
 
Helicopter automation using low cost sensors
Helicopter automation using low cost sensorsHelicopter automation using low cost sensors
Helicopter automation using low cost sensors
 
Rapid Start-Up / Restart Avionics Provide Robust Fault Tolerance with SCp (S...
Rapid Start-Up / Restart Avionics Provide Robust Fault  Tolerance with SCp (S...Rapid Start-Up / Restart Avionics Provide Robust Fault  Tolerance with SCp (S...
Rapid Start-Up / Restart Avionics Provide Robust Fault Tolerance with SCp (S...
 
Improving Avionics using aircraft Information Sharing Network(Research Paper)
Improving Avionics using aircraft Information Sharing Network(Research Paper)Improving Avionics using aircraft Information Sharing Network(Research Paper)
Improving Avionics using aircraft Information Sharing Network(Research Paper)
 
Probability And Random Variable Lecture (Lec10)
Probability And Random Variable Lecture (Lec10)Probability And Random Variable Lecture (Lec10)
Probability And Random Variable Lecture (Lec10)
 
Probability And Random Variable Lecture(Lec9)
Probability And Random Variable Lecture(Lec9)Probability And Random Variable Lecture(Lec9)
Probability And Random Variable Lecture(Lec9)
 
Probability And Random Variable Lecture(Lec8)
Probability And Random Variable Lecture(Lec8)Probability And Random Variable Lecture(Lec8)
Probability And Random Variable Lecture(Lec8)
 

Dual combustion cycle

  • 1.
  • 2. “Dual Combustion Engine” Presented To: Sir Qazi Shehzad Presented by:  Jawaria Bint Faheem (12063122-008) Areeba Malik (12063122-050) Areeba Asif (12063122-070) Hina Usman (12063122-077) Beenish Hafeez (12063122-085)
  • 3. Engine??? • A Machine Designed To Convert Energy Into Useful Mechanical Motion. • Thermal Energy Raises Temperature And Pressure Of Gases Within Engine, And Gas Expands Against Mechanical Mechanisms Of Engine.
  • 4. History • Oil Engine 1888. • Ackroyd Staurt (Automatic Ignition). • Rudolf Diesel Used This Principle And Developed Basis Of Dual Combustion Engine.
  • 5. Dual Combustion Engine • It is an internal combustion four stroke engine. • “Dual” Because Combustion Takes Place In Two Parts First At Constant Pressure And Second At Constant Volume. • This makes it better than diesel engine’s cycle.
  • 6. Dual Combustion Cycle • Also Known As The Limited Pressure Or Mixed Cycle, Seiliger Cycle Or Sabathe Cycle. • Thermal Cycle That Is A Combination Of The Otto Cycle And The Diesel Cycle.
  • 7. Characteristics • It is a four stroke engine. • Improved and modern form of old Diesel engine’s cycles. • Its one stroke is divided into two parts allowing it to carry out more work.. • Have increased efficiency.
  • 9. Stroke • Each Cycle Of Piston Consists Of Two Opposite Motions: There Is A Motion In One Direction, And Then A Motion Back In The Opposite Direction. Each Of These Is Called A Stroke • Stroke Is The Action Of A Piston Travelling The Full Length Of Its Locomotive Cylinder Or Engine Cylinder In One Direction.
  • 11. Sequence of Operations The dual cycle consists of following operations: • Adiabatic compression • Addition of heat at constant volume. • Addition of heat at constant pressure. • Adiabatic expansion. • Rejection of heat at constant volume.
  • 12. Explanation 1)Adiabatic Compression: Adiabatically compressed air, it turned hot. Fuel injection starts before the point of maximum compression.(ignition phase) 2) Constant Volume Phase: After a short delay the fuel warms up to the air temperature causing a sudden rise in pressure.
  • 13. Continued … 3) Constant Pressure Phase: Further Injection Keeps The Fuel Burning As Volume Increases 4) Adiabatic Expansion: After Cut Off, Hot Air Expands Isentropically. 5)Constant Volume (End Stroke): Exhaust Valve Opens Producing A Sudden Drop In Pressure Getting Heat Out.
  • 14. Efficiency • Engine efficiency of thermal engines is the relationship between the total energy contained in the fuel, and the amount of energy used to perform useful work.
  • 15. Expression For Efficiency • From first law of thermodynamics Q = ∆U + W And.. • ∆W = Q1 – Q2 • The efficiency of engine is defined as ƞ = Output / input
  • 16. Continued.. • The efficiency of engine is defined as useful work done to the heat provided. Where, • Q1 is the heat absorbed • Q1 – Q2 is work done.
  • 17. Efficiency of dual combustion engine The analysis of cycle is as follows: The heat is supplied In two stages. hence Qin = mcp(T4 – T3) + mcv(T3 – T2)  The heat rejected is Qout = mcv(T5 – T1)
  • 18. Simplification The thermal efficiency may b found as follows: ƞ = 1 – Qout/ Qin = 1 – mcv(T5 – T1)/ mcv(T3 -T2)+mcp(T4 – T3) =1 – (T5 – T1)/ (T3 – T2) +ϒ(T4 – T3)
  • 19. Simplification Of Formulae • The formula can be further developed to show that: η = 1-(kβγ -1)/[(k-1) +γk(β-1)]rv γ-1 • rv is the VOLUME COMPRESSION RATIO. • rv = V1/V2 • β is the CUT OFF RATIO. • β = V4/V3 • k is the ratio p3/p2. • If k=1 then it becomes Otto cycle’s efficiency.
  • 20. “Applications” Dual combustion engines are most commonly used for mobile propulsion in vehicles and portable machinery. In mobile equipment, dual combustion is advantageous since it can provide high power-to- weight ratios.
  • 21. “Automobiles” • Generally using fossil fuel(mainly petroleum), these engines have appeared in transport in almost all vehicles (automobiles, trucks, motorcycles, boats, and in a wide variety of aircraft and locomotives).
  • 22. Generators/Aircrafts • Very high power-to-weight ratios are required, dual combustion engines appear in the form of gas turbines. These applications include jet aircraft, helicopters, large ships and electric generators.
  • 23. “Future Energy Use” There is a role for Dual Combustion engines for future energy use, because – Dual combustion engine has high power to weigh ratio. – Relatively low cost. – Flexible fuel use. – Established manufacturing investment.
  • 24. References Text books: By Mcconkey And Rajput. Web sources: • www.marineinfo.com • www.freestudy.co.uk • http://www.brighthubengineering.com/ • en.wikipedia.org • www.wartsila.com Research Pappers: • Gas Power Cycles Prof. U.S.P. Shet ,and Prof. J.M . Mallikarjuna • Performance Analysis of a Dual Cycle Engine by Ebrahimi

Notes de l'éditeur

  1. Chemical Energy Is Converted To Thermal Energy By Combustion (Oxidation)
  2. Diesel's first engine used coal dust blasted into the combustion chamber with compressed air. This developed into blasting in oil with compressed air. The air standard cycle for these old fashioned engines was deemed to be as described above but with no constant volume process. This cycle is called the DIESEL CYCLE. http://www.engrailhistory.info/e089.html
  3. Four-stroke: four piston movements over two engine revolutions for each engine cycle Two-stroke: two piston movements over one revolution for each engine cycle 7/