This document reports on an experimental study investigating the effect of burner shape on flashback in gas turbines. Specifically, it aims to modify a small commercial diesel burner to operate with LPG, determine the burner's operating window with LPG, and investigate how burner geometry affects the operating window. It presents results showing increased burner neck length moves the flame stagnation point outward and widens the operating window by providing higher stability at constant equivalence ratios. However, a longer neck also precipitates flashback. The study concludes neck length and shape impact flame structure, stability and emissions, warranting future work exploring confinement effects and different neck geometries.
Experimental Investigate the Effect of Burner Geometry on the Operation Windo...Jameel Tawfiq
The purpose of this paper is to conduct an experimental study of a swirl burner with different lengths for a fixed diameter. Three models of rim length (5 cm, 10 cm and 15 cm) were taken. The results show that any change in the ratio of length to diameter will affect the flame position and structure of the downstream. It turns out that the flame settles near the edge as the rim length increases. The result indicates that increasing the length of the burner neck will reduce the structure of the swirl and weaken it, thus increasing the incidence of flashback phenomenon. The operating window of three burner neck models was studied above. It was found that the 5 cm rim has an equivalent ratio of (0.38-0.82) and for the 10 cm rim that is equivalent ratio (0.39-0.84), as well as for the rim 15 cm in equivalent ratio (0.4-0.83) with air velocity stabilization. For the above three models. Through the equivalent ratio of the above models. It was found that the 10 cm rim gave a larger operating window and therefore higher stability than the other two models.
Burner rim geometry effect on flame stabilityJameel Tawfiq
We studied a swirl burner in atmospheric pressure combustion system with different burner lengths to
burner rim diameter ratios (L/D). Three ratios, of L/D 1, 2 and 3, were used to investigate the effect of the
burner’s geometry on the stability window. The results show that the position of the flame front stabilization
changes with L/D ratio. The flame front stabilizes closer to the burner rim as the length of the burner is
increased. The equivalence ratio of the mixture was taken as constant for the comparison’s sake. The flame
stabilizes closer to the rim with an increase of the rim length
Effect of rim geometry on burner stability Conference paper2019Jameel Tawfiq
A swirl burner with different length to rim diameter ratio L/D. A three ratios 1,2 and 3 were studied. The results show that a change in the L/D ratio will effect on the stabilization position of the flame in downstream. The equivalence ratio of the mixture was taken a constant for the comparison sake. The flame stabilizes closer to the rim with an increase of the rim length.
The blowoff limits and flashback limits for different diameter to length rati...Jameel Tawfiq
A 129 kWh swirl gas burner was used, where the effect of the burner geometry on the operation window was studied. Using LPG. The length of the burner edge was studied by taking three values of length (5 cm, 10 cm and 15 cm) which represent the ratio (1,2 and 3) to the diameter of the burner respectively. To enhance the combustion stability a swirl vane guide was used to obtain swirl flow and improve the flame structure. The result show that the increase in length of burner neck will decrease the swirl coherent structure and turn the flow to diffusion flow which increase the ability to have boundary layer flashback. However with the limit of burner used, increasing the length of burner neck gives a good result in blowoff side by bush it to leaner limits around ɸ=0.38 but in term of flashback it will bring it to leaner limits too, which is not preferable.. Although, this improvement is linked to the fuel type in first place but the flow structure has a significant impact on flame stability.
Experimental Investigate the Effect of Burner Geometry on the Operation Windo...Jameel Tawfiq
The purpose of this paper is to conduct an experimental study of a swirl burner with different lengths for a fixed diameter. Three models of rim length (5 cm, 10 cm and 15 cm) were taken. The results show that any change in the ratio of length to diameter will affect the flame position and structure of the downstream. It turns out that the flame settles near the edge as the rim length increases. The result indicates that increasing the length of the burner neck will reduce the structure of the swirl and weaken it, thus increasing the incidence of flashback phenomenon. The operating window of three burner neck models was studied above. It was found that the 5 cm rim has an equivalent ratio of (0.38-0.82) and for the 10 cm rim that is equivalent ratio (0.39-0.84), as well as for the rim 15 cm in equivalent ratio (0.4-0.83) with air velocity stabilization. For the above three models. Through the equivalent ratio of the above models. It was found that the 10 cm rim gave a larger operating window and therefore higher stability than the other two models.
Burner rim geometry effect on flame stabilityJameel Tawfiq
We studied a swirl burner in atmospheric pressure combustion system with different burner lengths to
burner rim diameter ratios (L/D). Three ratios, of L/D 1, 2 and 3, were used to investigate the effect of the
burner’s geometry on the stability window. The results show that the position of the flame front stabilization
changes with L/D ratio. The flame front stabilizes closer to the burner rim as the length of the burner is
increased. The equivalence ratio of the mixture was taken as constant for the comparison’s sake. The flame
stabilizes closer to the rim with an increase of the rim length
Effect of rim geometry on burner stability Conference paper2019Jameel Tawfiq
A swirl burner with different length to rim diameter ratio L/D. A three ratios 1,2 and 3 were studied. The results show that a change in the L/D ratio will effect on the stabilization position of the flame in downstream. The equivalence ratio of the mixture was taken a constant for the comparison sake. The flame stabilizes closer to the rim with an increase of the rim length.
The blowoff limits and flashback limits for different diameter to length rati...Jameel Tawfiq
A 129 kWh swirl gas burner was used, where the effect of the burner geometry on the operation window was studied. Using LPG. The length of the burner edge was studied by taking three values of length (5 cm, 10 cm and 15 cm) which represent the ratio (1,2 and 3) to the diameter of the burner respectively. To enhance the combustion stability a swirl vane guide was used to obtain swirl flow and improve the flame structure. The result show that the increase in length of burner neck will decrease the swirl coherent structure and turn the flow to diffusion flow which increase the ability to have boundary layer flashback. However with the limit of burner used, increasing the length of burner neck gives a good result in blowoff side by bush it to leaner limits around ɸ=0.38 but in term of flashback it will bring it to leaner limits too, which is not preferable.. Although, this improvement is linked to the fuel type in first place but the flow structure has a significant impact on flame stability.
Review on Recent Advances in Pulse Detonation EnginesBBIT Kolkata
Pulse detonation engines (PDEs) are new exciting propulsion technologies for future propulsion applications. The operating cycles
of PDE consist of fuel-air mixture, combustion, blowdown, and purging. The combustion process in pulse detonation engine is the
most important phenomenon as it produces reliable and repeatable detonation waves.The detonation wave initiation in detonation
tube in practical system is a combination of multistage combustion phenomena. Detonation combustion causes rapid burning of
fuel-air mixture, which is a thousand times faster than deflagration mode of combustion process. PDE utilizes repetitive detonation
wave to produce propulsion thrust. In the present paper, detailed review of various experimental studies and computational analysis
addressing the detonation mode of combustion in pulse detonation engines are discussed. The effect of different parameters on
the improvement of propulsion performance of pulse detonation engine has been presented in detail in this research paper. It is
observed that the design of detonation wave flow path in detonation tube, ejectors at exit section of detonation tube, and operating
parameters such as Mach numbers aremainly responsible for improving the propulsion performance of PDE. In the present review
work, further scope of research in this area has also been suggested.
Pendulum Dampers for Tall RC Chimney Subjected To WindIJERA Editor
Chimneys are a part of industrial growth in any country. Most current chimney design standards require analysis of dynamic analysis of chimney for earthquake and wind induced loads. Because of variation in dimensions of chimney along its height structural analysis such as wind oscillations have become more critical. If ductility is an important consideration in earthquake resistant design, control of deflection become critical in wind induced vibrations. Pendulum dampers are of the devices to control the deflection. In the present work pendulum dampers of different natural frequencies have been tried. The one which has the largest equivalent logarithmic decrement is found to reduce the response significantly. The response is compared with that of chimney with a tip mass. The paper discusses the dynamic analysis of 150m high RCC chimney subjected to wind. Analysis has been carried out for fixed base case.
Experimental investgation of the effect of burner geometrey on flame stabilityJameel Tawfiq
Combustion and its control are essential to our existence on this planet since we knew it. Nowadays, the largest share of the world's electricity and most of our transportation systems are powered by combustion. In addition, industrial processes also rely heavily upon combustion. In most industrial combustion systems, combustion occurs under turbulent now conditions that can produce combustion instabilities. These are problematical since they can result in oscillations in thrust, low- or high-cycle fatigue of system components, flame blowoff or flashback, and oscillations in combustion efficiency together with high emission levels or even damage to the combustion systems. Thus, flame stabilization is of fundamental importance in the design, the efficient performance and the reliable operation of the combustion systems.
The effect of the burner geometry on operation window of small commercial burner (12-14 Kwh) was studied. The burner in origin using diesel as a fuel and modified by the researcher to operate with LPG. The length of the burner rim was studied by taking three values of length (5 cm , 10cm and 15cm) which represent a ratio of (1,2 and 3) to burner diameter respectively . The modification shows that the ability to use dual fuel in such small combustion unit is possible with minimum additional cost for control. To enhance the combustion stability, a swirl vane guide was used to obtain swirl flow and improve the flame structure. The results show that the increase in length of burner neck will decrease the swirl coherent structure and turn the flow to diffusion flow which increase the ability to have boundary layer flashback. However with the limit of burner used, increasing the length of burner neck gives a good result in blowoff side by bushing it to leaner limits around ɸ=0.38 but in term of flashback it will bring it to leaner limits too, which is not preferable. In term of the burner power, the LPG fuel combined with swirl flow increase the burner power to around 130Kwh. Although, this improvement is linked to the fuel type in first place but the flow structure has a significant impact on flame stability.
International Journal of Engineering Research and Applications (IJERA) is an open access online peer reviewed international journal that publishes research and review articles in the fields of Computer Science, Neural Networks, Electrical Engineering, Software Engineering, Information Technology, Mechanical Engineering, Chemical Engineering, Plastic Engineering, Food Technology, Textile Engineering, Nano Technology & science, Power Electronics, Electronics & Communication Engineering, Computational mathematics, Image processing, Civil Engineering, Structural Engineering, Environmental Engineering, VLSI Testing & Low Power VLSI Design etc.
How to get the combustible stability of the flame.
As well as reducing polluting emissions to the environment.
Work on designing modern combustion burner techniques to avoid combustion problems.
Jet pump is a type of mechanical device where the extra energy is provide by jet in mixing chamber. This jet is the fluid again circulate from diffuser exit to mixing chamber for better performance. This is also known as motive fluid. So the effects of change in geometrical parameter (Diffuser angle) on its performance were investigated. The set of experiment were carried out to study the effect of diffuser angle on the performance of jet pump. The performance of the jet pump is described by three sets of curves, Discharge vs. Head, Input power vs. Head, and Efficiency vs. Head. Changing the diffuser angle will affect jet pump behavior. Venturi diffuser angle was found to be an important geometrical parameter to characterize the maximum suction lift of the jet pump.
Behaviour and Analysis of Large Diameter Laterally Loaded PilesHenry Pik Yap Sia
75% of UK offshore wind turbines are supported on monopile foundations (Doherty and Gavin, 2012). The piles are subjected to large lateral loading from wind and tide surges as well as seabed movement. British Standards (BS EN 61400-3:2009) suggested p-y curve to predict the behaviour of laterally loaded offshore piles. P-y curve has certain assumptions including negligible rotational resistance along the pile length.
This report presents our investigation on the effect of rotational resistance on a typical large diameter pile. It also describes how the finite difference (FD) program has been written from first principles, the Winkler’s Method and Euler-Bernoulli Beam theory. To calculate the rotational resistance, the slice method proposed by McVay and Niraula (2004) is implemented in our model. Our linear-elastic FD model calculates the displacement, bending moment, shear force and soil pressure for laterally loaded piles for two cases: (a) when rotational resistance is considered and (b) when rotational resistance is neglected. The later represents the values used in the industry.
Sensitivity study, through our model produced good results within its scope. The results suggested that the change in the soil and pile properties was found to be dependent on the length-to-depth (L/D) ratio of the pile and the stiffness of the soil next to the pile. In other words, when reached critical ratio, the rotational resistance becomes very significant, specifically for short, rigid piles. Therefore, we computed curves to recommend the range of L/D values where rotational resistance can be safely neglected.
Recommendations and suggestions are made to improve the model and research to fully encapsulate the behaviour of offshore monopiles, such as cyclic loading, elastic continuum, plasticity and non-linearity.
Lastly, we have sufficient confidence from this research to conclude that rotational resistance of a laterally loaded large diameter pile are important and that current design standards for offshore monopiles are conservative.
NO1 Uk best vashikaran specialist in delhi vashikaran baba near me online vas...Amil Baba Dawood bangali
Contact with Dawood Bhai Just call on +92322-6382012 and we'll help you. We'll solve all your problems within 12 to 24 hours and with 101% guarantee and with astrology systematic. If you want to take any personal or professional advice then also you can call us on +92322-6382012 , ONLINE LOVE PROBLEM & Other all types of Daily Life Problem's.Then CALL or WHATSAPP us on +92322-6382012 and Get all these problems solutions here by Amil Baba DAWOOD BANGALI
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Review on Recent Advances in Pulse Detonation EnginesBBIT Kolkata
Pulse detonation engines (PDEs) are new exciting propulsion technologies for future propulsion applications. The operating cycles
of PDE consist of fuel-air mixture, combustion, blowdown, and purging. The combustion process in pulse detonation engine is the
most important phenomenon as it produces reliable and repeatable detonation waves.The detonation wave initiation in detonation
tube in practical system is a combination of multistage combustion phenomena. Detonation combustion causes rapid burning of
fuel-air mixture, which is a thousand times faster than deflagration mode of combustion process. PDE utilizes repetitive detonation
wave to produce propulsion thrust. In the present paper, detailed review of various experimental studies and computational analysis
addressing the detonation mode of combustion in pulse detonation engines are discussed. The effect of different parameters on
the improvement of propulsion performance of pulse detonation engine has been presented in detail in this research paper. It is
observed that the design of detonation wave flow path in detonation tube, ejectors at exit section of detonation tube, and operating
parameters such as Mach numbers aremainly responsible for improving the propulsion performance of PDE. In the present review
work, further scope of research in this area has also been suggested.
Pendulum Dampers for Tall RC Chimney Subjected To WindIJERA Editor
Chimneys are a part of industrial growth in any country. Most current chimney design standards require analysis of dynamic analysis of chimney for earthquake and wind induced loads. Because of variation in dimensions of chimney along its height structural analysis such as wind oscillations have become more critical. If ductility is an important consideration in earthquake resistant design, control of deflection become critical in wind induced vibrations. Pendulum dampers are of the devices to control the deflection. In the present work pendulum dampers of different natural frequencies have been tried. The one which has the largest equivalent logarithmic decrement is found to reduce the response significantly. The response is compared with that of chimney with a tip mass. The paper discusses the dynamic analysis of 150m high RCC chimney subjected to wind. Analysis has been carried out for fixed base case.
Experimental investgation of the effect of burner geometrey on flame stabilityJameel Tawfiq
Combustion and its control are essential to our existence on this planet since we knew it. Nowadays, the largest share of the world's electricity and most of our transportation systems are powered by combustion. In addition, industrial processes also rely heavily upon combustion. In most industrial combustion systems, combustion occurs under turbulent now conditions that can produce combustion instabilities. These are problematical since they can result in oscillations in thrust, low- or high-cycle fatigue of system components, flame blowoff or flashback, and oscillations in combustion efficiency together with high emission levels or even damage to the combustion systems. Thus, flame stabilization is of fundamental importance in the design, the efficient performance and the reliable operation of the combustion systems.
The effect of the burner geometry on operation window of small commercial burner (12-14 Kwh) was studied. The burner in origin using diesel as a fuel and modified by the researcher to operate with LPG. The length of the burner rim was studied by taking three values of length (5 cm , 10cm and 15cm) which represent a ratio of (1,2 and 3) to burner diameter respectively . The modification shows that the ability to use dual fuel in such small combustion unit is possible with minimum additional cost for control. To enhance the combustion stability, a swirl vane guide was used to obtain swirl flow and improve the flame structure. The results show that the increase in length of burner neck will decrease the swirl coherent structure and turn the flow to diffusion flow which increase the ability to have boundary layer flashback. However with the limit of burner used, increasing the length of burner neck gives a good result in blowoff side by bushing it to leaner limits around ɸ=0.38 but in term of flashback it will bring it to leaner limits too, which is not preferable. In term of the burner power, the LPG fuel combined with swirl flow increase the burner power to around 130Kwh. Although, this improvement is linked to the fuel type in first place but the flow structure has a significant impact on flame stability.
International Journal of Engineering Research and Applications (IJERA) is an open access online peer reviewed international journal that publishes research and review articles in the fields of Computer Science, Neural Networks, Electrical Engineering, Software Engineering, Information Technology, Mechanical Engineering, Chemical Engineering, Plastic Engineering, Food Technology, Textile Engineering, Nano Technology & science, Power Electronics, Electronics & Communication Engineering, Computational mathematics, Image processing, Civil Engineering, Structural Engineering, Environmental Engineering, VLSI Testing & Low Power VLSI Design etc.
How to get the combustible stability of the flame.
As well as reducing polluting emissions to the environment.
Work on designing modern combustion burner techniques to avoid combustion problems.
Jet pump is a type of mechanical device where the extra energy is provide by jet in mixing chamber. This jet is the fluid again circulate from diffuser exit to mixing chamber for better performance. This is also known as motive fluid. So the effects of change in geometrical parameter (Diffuser angle) on its performance were investigated. The set of experiment were carried out to study the effect of diffuser angle on the performance of jet pump. The performance of the jet pump is described by three sets of curves, Discharge vs. Head, Input power vs. Head, and Efficiency vs. Head. Changing the diffuser angle will affect jet pump behavior. Venturi diffuser angle was found to be an important geometrical parameter to characterize the maximum suction lift of the jet pump.
Behaviour and Analysis of Large Diameter Laterally Loaded PilesHenry Pik Yap Sia
75% of UK offshore wind turbines are supported on monopile foundations (Doherty and Gavin, 2012). The piles are subjected to large lateral loading from wind and tide surges as well as seabed movement. British Standards (BS EN 61400-3:2009) suggested p-y curve to predict the behaviour of laterally loaded offshore piles. P-y curve has certain assumptions including negligible rotational resistance along the pile length.
This report presents our investigation on the effect of rotational resistance on a typical large diameter pile. It also describes how the finite difference (FD) program has been written from first principles, the Winkler’s Method and Euler-Bernoulli Beam theory. To calculate the rotational resistance, the slice method proposed by McVay and Niraula (2004) is implemented in our model. Our linear-elastic FD model calculates the displacement, bending moment, shear force and soil pressure for laterally loaded piles for two cases: (a) when rotational resistance is considered and (b) when rotational resistance is neglected. The later represents the values used in the industry.
Sensitivity study, through our model produced good results within its scope. The results suggested that the change in the soil and pile properties was found to be dependent on the length-to-depth (L/D) ratio of the pile and the stiffness of the soil next to the pile. In other words, when reached critical ratio, the rotational resistance becomes very significant, specifically for short, rigid piles. Therefore, we computed curves to recommend the range of L/D values where rotational resistance can be safely neglected.
Recommendations and suggestions are made to improve the model and research to fully encapsulate the behaviour of offshore monopiles, such as cyclic loading, elastic continuum, plasticity and non-linearity.
Lastly, we have sufficient confidence from this research to conclude that rotational resistance of a laterally loaded large diameter pile are important and that current design standards for offshore monopiles are conservative.
NO1 Uk best vashikaran specialist in delhi vashikaran baba near me online vas...Amil Baba Dawood bangali
Contact with Dawood Bhai Just call on +92322-6382012 and we'll help you. We'll solve all your problems within 12 to 24 hours and with 101% guarantee and with astrology systematic. If you want to take any personal or professional advice then also you can call us on +92322-6382012 , ONLINE LOVE PROBLEM & Other all types of Daily Life Problem's.Then CALL or WHATSAPP us on +92322-6382012 and Get all these problems solutions here by Amil Baba DAWOOD BANGALI
#vashikaranspecialist #astrologer #palmistry #amliyaat #taweez #manpasandshadi #horoscope #spiritual #lovelife #lovespell #marriagespell#aamilbabainpakistan #amilbabainkarachi #powerfullblackmagicspell #kalajadumantarspecialist #realamilbaba #AmilbabainPakistan #astrologerincanada #astrologerindubai #lovespellsmaster #kalajaduspecialist #lovespellsthatwork #aamilbabainlahore#blackmagicformarriage #aamilbaba #kalajadu #kalailam #taweez #wazifaexpert #jadumantar #vashikaranspecialist #astrologer #palmistry #amliyaat #taweez #manpasandshadi #horoscope #spiritual #lovelife #lovespell #marriagespell#aamilbabainpakistan #amilbabainkarachi #powerfullblackmagicspell #kalajadumantarspecialist #realamilbaba #AmilbabainPakistan #astrologerincanada #astrologerindubai #lovespellsmaster #kalajaduspecialist #lovespellsthatwork #aamilbabainlahore #blackmagicforlove #blackmagicformarriage #aamilbaba #kalajadu #kalailam #taweez #wazifaexpert #jadumantar #vashikaranspecialist #astrologer #palmistry #amliyaat #taweez #manpasandshadi #horoscope #spiritual #lovelife #lovespell #marriagespell#aamilbabainpakistan #amilbabainkarachi #powerfullblackmagicspell #kalajadumantarspecialist #realamilbaba #AmilbabainPakistan #astrologerincanada #astrologerindubai #lovespellsmaster #kalajaduspecialist #lovespellsthatwork #aamilbabainlahore #Amilbabainuk #amilbabainspain #amilbabaindubai #Amilbabainnorway #amilbabainkrachi #amilbabainlahore #amilbabaingujranwalan #amilbabainislamabad
Sachpazis:Terzaghi Bearing Capacity Estimation in simple terms with Calculati...Dr.Costas Sachpazis
Terzaghi's soil bearing capacity theory, developed by Karl Terzaghi, is a fundamental principle in geotechnical engineering used to determine the bearing capacity of shallow foundations. This theory provides a method to calculate the ultimate bearing capacity of soil, which is the maximum load per unit area that the soil can support without undergoing shear failure. The Calculation HTML Code included.
Saudi Arabia stands as a titan in the global energy landscape, renowned for its abundant oil and gas resources. It's the largest exporter of petroleum and holds some of the world's most significant reserves. Let's delve into the top 10 oil and gas projects shaping Saudi Arabia's energy future in 2024.
Industrial Training at Shahjalal Fertilizer Company Limited (SFCL)MdTanvirMahtab2
This presentation is about the working procedure of Shahjalal Fertilizer Company Limited (SFCL). A Govt. owned Company of Bangladesh Chemical Industries Corporation under Ministry of Industries.
Experimental study of the effect of the burner shape on the flashback in gas turbines
1. Experimental study of the effect of the
burner shape on the flashback in gas
turbines
supervisors
Asst .prof .Dr. Qahtan A. Abed
Lect .Dr. Mohammed AL- fahham
Jameel AL-Naffakh
4-Dec.-2019
8. Flashback
A. Combustion Induced
Vortex Breakdown (CIVB).
B. Boundary Layer Flashback
(BLF).
C. Turbulent Core Flashback.
D. Combustion instabilities
flashback
0
1
2
3
4
5
6
7
0.1 0.6 1.1
TangentialVelocitym/s
Equivaliance Ratio
Blow Off
Flashback
9. AIM OF STUDY
Modifying an exist small commercial diesel burner to
work with LPG without any additional cost.
Finding the operation widow (stability map) of the
burner after using LPG.
Investigating the effect of burner geometry on the
operation window of the burner. The blowoff limits and
flashback limits will be addressed for different diameter
to length ratio burner .
18. CONCLUSION
The possibility of modifying any external combustion system (Burner)
powered by diesel fuel to use liquefied gas fuel (LPG), and without any
distortion of the system while maintaining the basic parts of the system
and thus not affecting the overall design of the system.
From the aerodynamic point of view, it is concluded that the strength of
the vortex will decrease with increase length due the friction with burner
inner walls. As a consequence, the swirl flow will turn to jet or diffusion.
19. Through practical experiments, it was shown that the increased
length of the burner's neck leads to move the stagnation point
towards the edge of the burner where it was graphically
represented.
Increasing the length of the neck of the burner leads to higher
stability in term of the equivalent ratio. At constant equivalence
value, the burner showed higher stability than the other two
models and therefore requires
increase in the rate of air flow in the mixture area and thus get a
poor mixture so it works it is application in the few loads for
power plants.
Increasing the length of the burner neck has precipitated the
flashback phenomenon.
20. Recommendations (future work)
Studying the effect of the use of confinement in the
combustion area on the stability of the flame and the
operating window.
Studying the amount of emissions with a change in the
length and shape of the burner neck.
Studying the effect of changing the shape of the burner
neck from the cylindrical to other forms such as slot
(rectangular), square, triangular or oval on the amount
of the operating window.
21. Multi-Knowledge Electronic
Comprehensive Journal For
Education And Science Publications
( MECSJ ) ISSUE(24),sep(2019) ISSN:
2616-9185 (ISI)
Energy Research Journal
DOI: 10.3844/erjsp.2019. Scopus
3rd International Conference on
Engineering Sciences (ICES.ME52)
Scopus
Accepted and published papers
Paper Title Journal Name
1- Burner rim geometry effect
on flame stability
2- Experimental Investigate the
Effect of Burner Geometry on the
Operation Window of the Burner
3- The blowoff limits and
flashback limits for different
diameter to length ratio burner
لقد ازداد الطلب على إنتاج الطاقة بشكل كبير منذ بداية الثورة الاقتصادية لتلبية احتياجات الحياة البشرية بطريقة تجعل الطاقة هي المقياس الخاص للتطور في أي مجتمع.
ومع ذلك ، جلب الاستهلاك المفرط للطاقة قضية كبيرة من التلوث البيئي. وبالتالي يؤدي إلى تغير المناخ وبالتالي يسبب الكوارث والأوبئة.
طور المصنعون والمصممون تقنية حديثة للحد من ظاهرة التلوث الناتجة عن أنظمة الاحتراق الخارجي التي تعمل بالوقود السائل. كان من الضروري العثور على وقود بديل وفير متاح يقلل من التلوث الناتج عن الاحتراق ويزيد من الكفاءة الحرارية ، وبالتالي اخترنا الغاز المسال (LPG).
ومع ذلك ، فإن التحدي الرئيسي في استخدام الغاز المسال يتطلب تحكمًا عاليًا في ثبات شعلة محتوى الغاز المسال على عدد ذرات الهيدروجين المرتفعة (C3H8) وإيجاد خريطة لنافذة التشغيل للظواهر Flashback و blowoff .
على الجانب الاقتصادي ، أدى استخدام غاز البترول المسال (LPG) إلى زيادة الطاقة الحرارية الناتجة عن الموقد إلى 120 كيلو واط في الساعة. تم حساب الطاقة الحرارية المولدة بناءً على الحد الأقصى لمعدل التدفق للمنفاخ ونسبة معادلة تبلغ 0.9 كما هو موضح في الملحق (أ).
وأوضح الفرق الكبير في السعة الحرارية لنفس الهندسة عن طريق التذكير بحقيقة عدم وجود عملية احتراق مثالية. خاصة إذا كان الوقود في المرحلة السائلة كديزل في هذه الحالة التي تسقط كفاءة الموقد. إن استخدام غاز البترول المسال (LPG) وخلطه مسبقًا بعيدًا عن منطقة الاحتراق وتقديمه كوقود مسبق الخلط بالكامل ، سوف يحسن عملية الاحتراق. من ناحية أخرى ، فإن دوامة التدفق تكون بنية التدفق واللهب كنتيجة لذلك. سيضمن هذا التماسك عدم تمييع الخليط بالهواء النقي الخارجي وإعطاء عملية الاحتراق استهلاكًا أكبر من الخليط. سوف يكون التسخين المتولد من هذا الاحتراق بتحد أكبر بكثير من توليده عند استخدام الديزل كوقود.
بعد إجراء التجارب المعملية ورسم حدود نافذة التشغيل ، وجد أن طول الموقد كان له تأثير على بنية اللهب. يخرج الخليط (الهواء / الوقود) من حافة الموقد في شكل دوامة نتيجة للمرور عبر دليل الريشة ، مما يؤدي إلى الحصول على الخليط بنية قوية ومتماسكة تحافظ على الشكل الثابت للخليط عند قدومه خارج حافة الموقد ويقلل من عملية الخلط مع المنطقة الخارجية. ينعكس هذا التأثير بوضوح من خلال اللون الأزرق للهب ، والذي يظهر علامات على عملية احتراق شبه كاملة.
من منظور الديناميكا الهوائية ، تعتمد قوة هيكل الدوامة على ما يعرف برقم الدوامة (S) ، والذي يمثل شدة زخم الدوامة إلى شدة الزخم المحوري. ومع ذلك ، فإن طول عنق الموقد سوف يحفز ما يعرف باسم تدهور دوامة ، وكمية فقدان الزخم بسبب الاحتكاك بين الخليط والجدران الموقد.
ينعكس هذا التأثير في شكل انكماش في قطر اللهب كما هو موضح في الصور أدناه. في حالة العنق 5 سم ، كان قطر الشعلة حوالي 1.75 د (8.5 سم) ، في حين كان حوالي 7 سم أو 1.4 د للرقبة من 10 سم ، مع زيادة طول الرقبة بحيث تدفق من تدفق منتشر مثل اللهب يأخذ شكل V وقطر الشعلة حوالي 5 سم.
بالنسبة للتجارب التي أجريت ، تم الحفاظ على نوع الوقود ونسبة التكافؤ لدراسة تأثير الرقم الثابت على المسافة التي يجلس بها اللهب بعيدًا عن حافة الموقد أو ما يعرف بنقطة ركود اللهب.
أظهرت التجارب أن زيادة طول الرقبة يؤدي إلى قرب نقطة الركود من حافة الموقد وكما هو موضح في الصور أدناه.
العلاقة بين طول رقبة الموقد ومسافة ركود اللهب من حافة الموقد تم تمثيلها كما هو موضح
يتم قياس كفاءة أنظمة الاحتراق الخارجي من خلال الاستقرار الذي توفره الشعلة في ظروف التشغيل المختلفة ، على سبيل المثال في محطات الطاقة ، المعيار الرئيسي هو القدرة على الحفاظ على استقرار الاحتراق عندما ينخفض الطلب على الطاقة ، مما يؤدي إلى تشغيل الموقد في الحد الأقصى وبالتالي ، يجب السيطرة على الخليط إما الفقيرة أو الغنية. وفي المحطة. في كلتا الحالتين ، يكون النطاق بين الاثنين أفضل.
إن تأثير طول عنق الموقد على حدود التشغيل (نافذة التشغيل) ، مهم للغاية حيث أن طول عنق الموقد أقصر حيث أن اللهب يتحرك بعيدًا عن حافة الموقد وتحدث ظاهرة الانفجار وأطول تزداد رقبة الموقد مع اقتراب اللهب من مصدر الحافة وتحدث ظاهرة الفلاش باك.
عند تكرار العملية لأكثر من معدل تدفق الهواء والوقود ، نحصل على ما يعرف بخريطة الاستقرار كما هو موضح في الصور أدناه.
إمكانية تعديل أي نظام احتراق خارجي (Burner) مدعوم من وقود الديزل لاستخدام وقود الغاز المسال (LPG) ، ودون أي تشويه للنظام مع الحفاظ على الأجزاء الأساسية للنظام وبالتالي لا يؤثر على التصميم العام للنظام.
من وجهة النظر الديناميكية الهوائية ، استنتج أن قوة الدوامة ستنخفض مع زيادة طول بسبب الاحتكاك مع الجدران الداخلية الموقد. نتيجة لذلك ، سوف يتحول تدفق الدوامة إلى نفاث أو انتشار.
من خلال التجارب العملية ، تبين أن زيادة طول رقبة الموقد تؤدي إلى تحريك نقطة الركود نحو حافة الموقد حيث تم تمثيلها بيانياً.
تؤدي زيادة طول عنق الموقد إلى ثبات أعلى في مدة النسبة المكافئة. في قيمة التكافؤ الثابت ، أظهر الموقد ثباتًا أعلى من النموذجين الآخرين وبالتالي يتطلب ذلك
زيادة في معدل تدفق الهواء في منطقة الخليط وبالتالي الحصول على خليط فقير بحيث يعمل وهو تطبيق في الأحمال القليلة لمحطات الطاقة.
زيادة طول الرقبة الموقد عجلت ظاهرة الفلاش باك.