ACADEMIC YEAR 2014-2015 COMBUSTION PROCESSES In order to achieve this outcome you will need to become familiar with the chemistry of combustion of hydrocarbon fuels. There is a requirement to understand and use some of the concepts in chemistry such as atomic and molecular mass. The mathematical level is that of simple arithmetic. This outcome will be presented to you in one section. The section includes 6. COMBUSTION CHEMISTRY 7. ENERGY OF COMBUSTION 8. PRODUCTS OF COMBUSTION Recommended textbooks are Bolton W Mechanical Science Blackwell Science Hannah and Hillier Mechanical Engineering Science Addison Wesley Longman Ltd Rayner Joel 1999 Basic Engineering Thermodynamics in SI units Longman 0 582 42423 2 [Type here] 1993 ACADEMIC YEAR 2014-2015 6. COMBUSTION CHEMISTRY 6.1 INTRODUCTION Chemistry is an essential part of our daily lives. The air that we breathe, the liquids that we drink and the food that we eat is converted by a series of chemical reactions to provide us with the energies and substances that we need to sustain life. During this outcome we will look at the basic nature of matter and explore how the elements and compounds that surround us have been utilised to provide us with so much useful energy. As engineers we can convert energy from one form to another, and in doing so do some useful work. 6.2 BASIC NATURE OF MATTER The most basic building block of any substance is the atom. A quantity of any substance comprises an enormous numbers of atoms. Frequently these atoms combine together to form larger units. When they combine with atoms of their own substance they are known as molecules. A molecule is the smallest amount of a substance that displays its properties. When they combine with atoms of another substance they are called compounds, although you can, of course have a molecule of a compound. As far as we are concerned there are only three principal components to an atom. The NEUTRON, which is a relatively large lump, and is found in the centre of the atom. The PROTON, which has the same mass as a NEUTRON, and is also found in the centre. Finally, the ELECTRON, which is about 0.0005 of the mass of the others, and orbits around the others. A bit like a solar system. Most of the mass of an atom is clearly in the centre. Most of the activity of an atom is focussed on the electrons. [Type here] ACADEMIC YEAR 2014-2015 The arrangement of the electrons determines many of the substances properties, both mechanical and physical. It contributes to its degree of reactivity, and to the type of compounds that it will form. The simplest atom is that of hydrogen. It consists of one PROTON and one orbiting ELECTRON. The PROTON has a single positive charge associated with it, and the ELECTRON a single negative charge. On an atomic scale therefore the hydrogen atom is neutral. The orbiting ELECTRON is kept in its orbit by these opposite charges that are analogous to the centripetal and centrifugal forces that we have met before. As atoms get bigger they have more PROTONS and ELECTRONS, but also NEUTRONS. Generally there are as many protons as electrons, and as many neutrons as protons. As the neutrons do not affect the charge balance of the atom it is possible to have elements that have a range of neutrons in their nucleus. When that occurs they are known as ISOTOPES. The best-known isotopes are those of uranium, which exist as uranium 237 and uranium 235. The numbers refer to the atomic mass that is the total number of neutrons and protons in the nucleus. In a simple manner we could conclude that an atom of uranium 235 is 235 times heavier than an atom of hydrogen. This does ignore the electron mass, but as we would need 1840 electrons to match the mass of a proton it is a reasonable assumption. To further complicate the issue we need to consider the orbits of the electrons. The electrons of any one atom do not all orbit at the same distance from the nucleus. Orbits get full. The number of electrons needed to fill a particular orbit is given by 2n2, where n is the number of the orbit. So, for example, an atom will have its first orbit filled by 2(1)2 electrons, or 2. Similarly the second orbit needs 8 electrons to fill it, and the third 18. [Type here] ACADEMIC YEAR 2014-2015 This arrangement is not quite as simple as I have made it, as the electrons in the larger orbits tend to exist at different energy levels. This means that the third orbit that would be filled by 18 electrons will have ‘sub orbits’ and the completion of a sub orbit can affect the behaviour of the element. I am not going into this any deeper as it is outside the scope of our course. Any ‘A’ level text book on Chemistry will provide the more curious of you with a full explanation of the s,p,d and f energy levels within the atom, and the implications for behaviour. At this juncture it might be helpful to look at the periodic table of the elements, which tells us their names, their number and their mass. We will also look at some of the behaviours. The table is overleaf. Let us consider the first two elements, hydrogen and helium. Hydrogen has one electron in its first orbit. For that orbit to be complete there needs to be two electrons. What this means is that hydrogen is likely to react with any elements that enable it to fill that orbit. This will make hydrogen a reasonably reactive substance, particularly if it can react with an element that is going to gain from the relationship. Helium, however, has two electrons in the first orbit and is therefore satisfied. Helium is an inert gas, reacting with little because it simply has no need to do so. Look at two other elements, sodium (Na,11) and chlorine (Cl,17). [Type here] ACADEMIC YEAR 2014-2015 Select an element from the periodic table. Group 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 Period 1 1 He 3 2 Li 3 Na 4 2 H 11 19 K 4 Be Rb 6 Cs 7 Fr 55 87 B 12 13 Mg Al 20 21 Ca Sc 38 39 37 5 5 Sr 56 Ba 88 Ra Y * * * 71 40 Zr 72 Lu Hf 103 104 Lr 57 *Lanthanoids * La **Actinoids * * Ac [Type here] 22 Ti 89 Rf 58 Ce 90 Th 23 V 41 Nb 73 Ta 105 Db 59 24 Cr 42 Mo 74 W 106 Sg 60 Pr Nd 91 92 Pa U 25 Mn 43 Tc 75 26 Fe 44 27 Co 45 Ru Rh 28 Ni 46 Pd Re Os 76 77 Ir Pt 107 108 109 110 Bh 61 Pm 93 Np Hs 62 Sm 94 Pu Mt 63 Eu 95 Am 78 Ds 64 Gd 96 Cm 29 Cu 47 Ag 79 Au 111 Rg 65 Tb 97 Bk 30 Zn 48 Cd 80 Hg 112 Uub 66 Dy 98 Cf 31 Ga 49 In 81 Tl 113 Uut 67 Ho 99 Es 6 7 8 C N O 14 15 16 Si 32 Ge 50 Sn 82 Pb 114 Uuq 68 Er 100 Fm P 33 As 51 Sb 83 Bi 115 Uup 69 Tm 101 Md S 34 9 F 17 Cl 35 Se Br 52 53 Te 84 Po 116 Uuh 70 Yb 102 No I 85 At 117 Uus 10 Ne 18 Ar 36 Kr 54 Xe 86 Rn 118 Uuo ACADEMIC YEAR 2014-2015 The eleven electrons of sodium will occupy the first orbit (2), the second orbit (8) and leave one electron in the third orbit. What sodium would really like to do is either lose this electron to leave a completely filled second orbit, or obtain some more so that the third orbit contains a stable number of electrons. Along comes chlorine. It has seventeen electrons. Two fill the first orbit, eight fill the second, and there are seven left in the third orbit. At this stage you may see that the seven electrons in chlorine’s third orbit could be added to the one in sodium’s third orbit to make a total of eight. This may then satisfy both of their needs in that there is a sub-orbit of the third orbit that has eight electrons in it, and consequently might be less reactive. That is what happens. Two highly reactive elements, sodium and chlorine, combine to form the relatively unreactive compound sodium chloride, which is common salt. Taken individually these elements will kill us. In combination they take a lot longer! SELF TEST 6.2a Examine the periodic table above. Try to identify five pairs of elements that might combine to form an unreactive compound. Do not use the same element twice. Name the compound. Briefly explain its use. (maximum imagination required here!) [Type here] ACADEMIC YEAR 2014-2015 6.3 VALENCY This is a term used to describe the way in which atoms can join together. It is connected with the number of electrons that are available to be shared between atoms. It is a complicated issue with the full and detailed explanation better left elsewhere. We can look at a simple example to try to get an understanding of the type of thing happening. Consider the element hydrogen (H). We already know that it has one electron in its outermost orbit. If it had two it would be fairly unreactive, so hydrogen meets this condition by going around in pairs. This hydrogen molecule is fairly stable because both atoms are sharing the two electrons. Because the hydrogen molecule consists of two atoms it is represented as H2. As there is only one electron available to be shared by an atom of hydrogen we say that hydrogen has a valency of one. Oxygen (O), on the other hand, has eight electrons. Two will be in the first orbit and six in the second. You will recall that the second orbit is satisfied when it has eight electrons in it. So oxygen has a need of two electrons, which it can get, amongst other ways, by sharing the two electrons from an hydrogen molecule. Oxygen has a valency of two, as it needs to share two electrons. The hydrogen molecule and oxygen atom obtain satisfaction from the mutual sharing of these two electrons, so the compound formed, H2O (water), is unreactive. Diagrammatically we can represent a water molecule as below. H ----- 0 ----- H Where the lines represent the bonds, or valency. [Type here] ACADEMIC YEAR 2014-2015 Our studies of combustion will focus on hydrocarbon fuels. Because carbon is such an important element we will spend a little time looking at the peculiarities of this element. Carbon is element number six, with six electrons and an atomic mass of 12. The atomic mass refers to the sum of the protons and the neutrons in the element. As the electrons are so small, they are an insignificant part of the atoms mass. Where carbon is unusual is that it can exhibit a valency of either one, two, three or four. This is because carbon has only four electrons in its second orbit and therefore requires sharing four more. It is happy to share with hydrogen, or another atom of itself or with some other elements. There are therefore numerous ways in which carbon can unite with hydrogen. The study of carbon and its various compounds is a science all of its own, and is known as organic chemistry. Let us look at the simplest compound of carbon and hydrogen, called methane. H H C H H Here one atom of carbon has bonded with four atoms of hydrogen to form one molecule of methane. Each hydrogen atom is sharing it’s electron with the outer orbit of carbon, giving it effectively eight, and at the same time each hydrogen atom is sharing one of the four electrons in carbon’s outer orbit giving it effectively two. [Type here] ACADEMIC YEAR 2014-2015 Methane is a gas that is most commonly associated with the decaying of vegetation or decomposition in swamps. It is the first member of a family called the paraffins. The next member of that family is called ethane and the structure uses two carbon atoms sharing one of each atoms electrons. The diagram below shows this substance. H H H C C H H H In shorthand notation methane is written as CH4, and ethane as C2H6. SELF TEST 6.3a Construct the diagrams similar to the ones above for methane and ethane that shows the next three members of the paraffin family. The periodic table shows us that carbon has an atomic weight of 12, and hydrogen an atomic weight of 1. When methane is formed the molecule consists of one carbon atom and four hydrogen atoms, which gives it a molecular weight of 16. Determine the molecular weights of the three paraffins that you have constructed. See if you can find their names and their boiling points. Draw a graph to see if there is a connection between the molecular weights and their boiling points for all of the first five paraffins. [Type here] ACADEMIC YEAR 2014-2015 As has been mentioned, carbon can have a valency from one to four. You will realise that the previous family uses a valency of one. If we look at the simplest arrangement where carbon exhibits a valency of two, then we will get the following diagram. H H C C H H Here we have the double bond arrangement that carbon can utilise. Another way to look at it is shown below. H H C C H H Where the blue dots represent the electrons belonging to hydrogen, the red dots show the electrons belonging to one carbon atom and [Type here] ACADEMIC YEAR 2014-2015 the green dots the electrons belonging to the other carbon atom. In this way stability occurs in this molecule. This substance is ethylene, and is the first member of the olefin family. SELF-TEST 6.3b Determine the structure, calculate the molecular weight and find the boiling point of the first four members of the olefin family. Add this data to the graph drawn for SELF-TEST 6.3.a 6.4 BASIC CHEMICAL REACTIONS We will now spend some time examining the basis for calculating the quantities involved in some basic chemical reactions. Using the information that oxygen has an atomic weight of 16, and hydrogen has an atomic weight of 1, we can easily determine that a molecule of water (H2O) will have a molecular weight of 16+1+1=18. To write this in its accepted format we acknowledge the fact that both hydrogen and oxygen exist as di-atomic molecules, that is they cannot exist as single atoms. We have 2H2 + O2 = 2H2O Using the molecular weights we get 2x2 + 32 = 2x18 If we consider the reaction between sodium (Na) and water (H2O) we will find the following. The products will be sodium hydroxide and hydrogen gas. Na + H2O = NaOH + H [Type here] ACADEMIC YEAR 2014-2015 However we need to ensure that H occurs as H2, so the equation above needs to be doubled up to allow this to happen. The equation becomes 2Na + 2H2O = 2NaOH + H2 If we now make use of the molecular masses we can calculate that 2 atoms of sodium (2x22units of weight) will react with 2 molecules of water (2x18 units of weight) to form 2 molecules of sodium hydroxide (2x39 units of weight) and 1 molecule of hydrogen (1x2 units of weight). A check will reveal that there are 80 units of weight before and after the reaction. Now that we have covered the fundamentals of reactions we will move on to the combustion reactions. 6.5 COMBUSTION CHEMISTRY We can carry out an investigation of the principles of combustion chemistry without needing to examine the behaviour of the long chained complex molecules that make up oil based fuels. As has been stated before, the hydrocarbon fuels consist of the two elements hydrogen and carbon. You have seen that carbon can exist with several valencies, as we have noted with the paraffins and the olefins. We will now examine the well-known hydrocarbon acetylene. This is widely used in welding as the combustion process generates a large amount of heat, sufficient to melt metals such as steel. This is perhaps the key point. The combustion of a hydrocarbon fuel is an exothermic process. That means that a great deal of heat is given out when a hydrocarbon fuel is burnt. The amount of heat [Type here] ACADEMIC YEAR 2014-2015 given out is called the calorific value of the fuel. A typical value for a hydcarbon fuel is 40 000kJ/kg. Let us actually consider the implications of this value. If we burn 1kg of a fuel with a calorific value of 40 000kJ/kg we will release 40 000kJ of heat energy. For a car travelling at a steady speed of 50 miles/hr (22m/s) the combined drag and friction would be about 400N. With no loss of efficiency the distance travelled would be 40 000kJ/400N = 100km. Rough conversion gives us 225miles/gallon fuel consumption. Clearly we cannot get 100% efficiency, but nevertheless the enormous potential of harnessing the energy of combustion is clear. SELF-TEST 6.5a A small engine burns a hydrocarbon fuel with a calorific value of 36MJ/kg. It is coupled to a small electrical generator and the transmission efficiency is 80%. If it burns the fuel at the rate of 2kg/hr, calculate the generator output in kW. Assume the generator efficiency is 100%. (You will need to use knowledge gained in previous outcomes here!) Acetylene has the formula C2H2. The two carbon atoms are joined by a triple bond that allows only one bond each for hydrogen. The diagram is shown below. [Type here] ACADEMIC YEAR 2014-2015 H C C H You may wish to represent this arrangement similarly to the lower diagram on page 110. When a hydrocarbon fuel is burnt completely in air, the products of complete combustion are carbon dioxide and water vapour. The only constituent of air that contributes to the combustion process is oxygen. Let us look exactly at burning acetylene. The combustion equations will show that C2H2 + 5O = 2CO2 + H2O As oxygen cannot exist as a single atom we need to double up as before. Correct is 2C2H2 + 5O2 = 4CO2 + 2H2O Using numbers we find that 2 molecules of acetylene (2x26) will combine with 5 molecules of oxygen (5x32) to give 4 molecules of carbon dioxide (4x44) and two molecules of water (2x18). 52 + 160 = 176 + 36 The key information here is that contained on the left hand side of the equation. It tells us that 52 units of acetylene need 160 units of oxygen for complete combustion. If we consider that air contains 23.3% oxygen by weight with the remainder being nitrogen (not quite true, but near enough), then 52 [Type here] ACADEMIC YEAR 2014-2015 units of acetylene will need 160/0.233 units of air for complete combustion. So we have that 52 units of acetylene require 686.7 units of air for complete combustion. This analysis being based upon weight. If we now divide the units of air by the units of acetylene we will obtain the air:fuel ratio by weight. Air:fuel ratio for acetylene is 13.206:1 for complete combustion. This ideal ratio is called the stoichiometric air:fuel ratio. NOTE Calculating the air:fuel ratio by volume is sometimes used. Just as a simple example, if we used the information above we would find that 13.206N of air is needed to give complete combustion to 1N of acetylene. By dividing both sides by 9.81 we can refer to masses, which makes our understanding a bit easier. Therefore 13.206kg of air is needed to give complete combustion to 1kg of acetylene. At sea level, 150C and normal atmospheric pressure (101325N/m2) the density of air is 1.2kg/m3. Therefore 13.206kg of air occupy 13.206/1.2 m3 = 11.005m3 (11005 litres) [Type here] ACADEMIC YEAR 2014-2015 As acetylene is a gas at this temperature, we can make use of the fact presented to us by Avogadro, that the gm molecular weight of any gas occupies 22.4 litres at standard conditions. (As above) I found this confusing! Which gas? So 52g of acetylene occupy 22.4 litres. 52kg will occupy 22 400 litres. 1kg will occupy 22 400/52 litres, which equals 430.77 litres Air:fuel ratio by volume = 11005/430.77 = 25.55:1 QUITE A DIFFERENCE! SELF-TEST 6.5b Ensure that you know whether the air:fuel ratio is needed by weight or volume. A fuel has the formula C4H4. Produce a diagram to show all the possible arrangement of bonding of the carbon atoms that will meet this formula. Determine the stoichiometric air:fuel ratios by weight and In the previous examples the fuel has been a pure hydrocarbon, that is only the elements carbon and hydrogen have been present in the compound. Some fuels contain oxygen within their structure, and this is available for combustion as well as the oxygen in the air. The presence of this oxygen will clearly affect the air:fuel ratios. Example 6.5a Determine the stoichiometric air:fuel ratios by weight and volume for the fuel shown in the diagram below. [Type here] ACADEMIC YEAR 2014-2015 H O O H C C C H H C O Solution This fuel has the composition C4H4O3. Note how each carbon atom uses four bonds, each oxygen two bonds and the hydrogen one bond. For complete combustion the products will be CO2 and H2O. The four atoms of carbon need eight atoms of oxygen. The four atoms of hydrogen need two atoms of oxygen. The total requirement is for ten atoms of oxygen. However there are already three present in the fuel, so the net requirement for additional oxygen is seven atoms. We know that oxygen exists as a di-atomic molecule so we need to double up on these quantities. The combustion equation becomes 2 C4H4O3 + 7O2 = 8CO2 +4H2O By mass 2(48+4+48) + 7x32 = 8(12+32) + 4x18 200 [Type here] + 224 = 352 + 72 ACADEMIC YEAR 2014-2015 so 200kg of fuel need 224kg of oxygen, which equates to 224/.233kg of air. Air:fuel ratio by weight 961.37:200, or 4.8:1 By volume Using the molecular weights in kg, and assuming that the fuel is gaseous at these temperatures 2x22400 litres of fuel need 7x22400/(0.233x1.2) litres of air. Air:fuel ratio by volume is 12.518:1 SELF-TEST 6.5.c A lot of fuels contain Sulphur. Sulphur burns completely in air to produce a gas called sulphur dioxide, SO2. Page 105 will show that sulphur has atomic number 18 (2,8,8) with an atomic weight (=molecular weight) of 36. Why is the atomic weight the same as the molecular weight? If Benzine sulphonic acid, C6H5SO3H was to burn completely in air, what would be the air:fuel ratio by mass? 6.6 EXCESS/RESTRICTED AIR So far we have looked at the exact amount of air required for complete combustion. In practice the amount of air might be less [Type here] ACADEMIC YEAR 2014-2015 than that, and incomplete combustion will occur. When that happens the carbon may form carbon monoxide as well as carbon dioxide. CARBON DIOXIDE O C O CARBON MONOXIDE O C C O Our combustion equations would change, for example, from CH4 + 2O2 to = CO2 2CH4 + 3O2 = + 2H2O 2 CO + 4H2O SELF-TEST 6.6a The hydrocarbon fuel shown below is burnt to produce a. CO2 only as well as water vapour. b. CO only as well as water vapour. c. 50% CO2 and 50% CO as well as water vapour. Determine the air:fuel ratios by weight in each case. [Type here] ACADEMIC YEAR 2014-2015 H O O O C C C C H H C O H Practically excess air needs to be supplied to ensure that complete combustion occurs. There is a time delay involved in the burning of a fuel and in many practical situations the combustion process may be inhibited by the other constituents of air. In a gas turbine excess air is provided to ensure complete mixing of the air and fuel, so that a uniform temperature distribution at entry to the turbine is obtained. The excess air is also used to keep the temperature in the combustion chambers down so that dissociation of CO2 into CO is minimised. Excess air does mean that useful heat is lost as the temperature of elements not involved in the combustion process is also increased. Example 6.6a An analysis of a sample of coal reveals that it contains by percentage of weight carbon: 84, hydrogen: 5, sulphur: 3,oxygen: 6 and ash: 2. Air is supplied to this fuel at the ratio of 20:1 by weight. What is the percentage excess air supplied? [Type here] ACADEMIC YEAR 2014-2015 Solution Consider 1 kg of the fuel. There will be 0.84kg of carbon. As C + O2 = CO2, then using molecular weights (masses) we deduce that 12kg of carbon will need 32kg of oxygen for complete combustion. Therefore 0.84kg of carbon will need 2.24kg of oxygen for complete combustion. There will be 0.05kg of hydrogen. As 2H2 + O2 = 2H2O, then our molecular weights (masses) show that 4kg of hydrogen needs 32kg of oxygen for complete combustion. Therefore 0.05kg of hydrogen will need 0.4kg of oxygen for complete combustion. There will be 0.03kg of sulphur. As S + O2 = SO2, then our molecular weights (masses) indicate that 32kg of sulphur need 32kg of oxygen for complete combustion. Therefore 0.03kg of sulphur will need 0.03kg of oxygen for complete combustion. There will be 0.06kg of oxygen. This is present in the fuel, and will reduce the amount necessary from the air. Ash is inert. It plays no part in the process of combustion. So 1kg of this coal needs 2.61kg of oxygen. For 2.61kg of oxygen we need 2.61/0.233kg of air = 11.202kg. Air supplied is 20kg. Excess air is 20 – 11.202 = 8.796kg [Type here] ACADEMIC YEAR 2014-2015 Percentage excess = 8.796/11.202 = 78.52% SELF-TEST 6.6b An analysis of a fuel reveals that it contained 76% carbon, 7% hydrogen, 6% oxygen, 7% sulphur, 3%nitrogen by weight, the remainder being ash. Determine the air supply rate needed (kg air: kg fuel) to give 100% excess air by weight. [Type here] ACADEMIC YEAR 2014-2015 7. ENERGY OF COMBUSTION 7.1 CALORIFIC VALUES We have met the term calorific value previously. Hydrocarbon fuels release energy in the form of heat when burnt. Clearly the amount of heat released by a fuel will determine how useful it is. The obvious conclusion that the higher the calorific value the better the fuel may not be the case. Too large a heat release may produce temperatures that cause damage to the arrangement that is containing the combustion. Some typical calorific values of fuels are shown below. COAL 35Mj/kg WOOD 20Mj/kg PETROL 45Mj/kg COAL GAS 20Mj/kg NATURAL GAS 38Mj/kg It is important at this stage to note the fact that there are two calorific values that can be defined. a) Higher Calorific Value (HCV)also known as the Gross Calorific Value b) Lower Calorific Value (LCV) also known as the Net Calorific Value. The HCV is the energy released when the products of combustion are cooled to the original fuel temperature. As fuels contain hydrogen one of the principal products of combustion is water. It is also possible that there may be a small amount of moisture present in the fuel anyway. On combustion the water will appear as water vapour in the exhaust or flue. Only if this exhaust is cooled to the original fuel temperature will the water vapour condense and then release its enthalpy of evaporation. [Type here] ACADEMIC YEAR 2014-2015 It is more usual for the water to remain as vapour and consequently this heat is lost to the plant. The adjustment for the loss of this heat indicates that the fuel calorific value is less than in the case where the water vapour condenses. In most cases it is more appropriate to use this lower value. 7.2. DETERMINATION OF CALORIFIC VALUES. The calorific value of the fuel is determined in a container called a calorimeter. These are especially designed to deal with the differing rates of burning, so for solid fuels and some liquid fuels the bomb calorimeter is used. For other liquid fuels and gaseous fuels the gas calorimeter is used. A bomb calorimeter. [Type here] ACADEMIC YEAR 2014-2015 A bomb calorimeter is used to measure the energy that is given out when a substance is completely burned in oxygen. A known amount of the substance is placed in the crucible, oxygen is added at 20 atmospheres pressure, and then the substance is ignited using the heated wire. As the calorimeter heats, it heats the water. The rise in water temperature is measured and from this the heat generated by the burning substance is calculated. The assumption is that the mass of fuel multiplied by its calorific value will generate the heat required to raise the temperature of the bomb (the steel? container), the water and any peripherals through the recorded temperature rise. Clearly accurate temperature measurement is required as is confidence that equilibrium has been reached. It is usual to calibrate the bomb calorimeter before evaluation of a new fuel. This enables the thermal equivalent (mass x specific heat) of the equipment to be confirmed by using a fuel of known calorific value. A file of a powerpoint slideshow of this process is included. It is the work of Dr Roger Latham, Faculty of Applied Sciences, De Montfort University. calibration of a bomb calorimeter The usual calorimeter used to evaluate the calorific value of a gaseous fuel is Boys calorimeter. The Boys Gas Calorimeter has been developed, from apparatus designed by the late Sir Charles Boys F.R.S., to provide a simple but accurate method of ascertaining the calorific values of a wide range of gaseous fuels currently in use. The principle of operation is that gas is supplied at a regulated pressure at a constant rate, which is metered. This gas is then ignited at burners located at the base of the calorimeter, with the [Type here] ACADEMIC YEAR 2014-2015 hot gases passing upwards over a set of cooling tubes through which a controlled flow of water is passing. The water vapour in the exhaust can be condensed and collected to enable the LCV to be determined as well. The simple relationship that the heat gained by the cooling water is equal to the heat given up by the fuel enables the determination of the calorific value. 7.3 EFFICIENCY OF POWER PLANT AND COMBUSTION PROCESS The efficiency is usually simply defined as the ratio of what was got out compared with what was put in. When dealing with power plant as a whole it is necessary to consider the efficiency of the method of producing heat, which involves whether or not the fuel is being completely burnt, and whether the conditions are at an optimum. An overall thermal efficiency therefore relates to the work output compared to the energy stored within the fuel. If the power plant is an open system with steady flow, then fuel and air enter, exhaust products leave and there may be both work and heat transfer te tf W fuel air [Type here] Q exhaust product s ACADEMIC YEAR 2014-2015 If the fuel and air enter at atmospheric temperature the maximum value of the energy transferred will occur when all the fuel is burnt completely, when inlet and outlet temperatures are equal and when water products in the exhaust have condensed. Under these conditions it is accepted that the efficiency can be represented by = W H.C.V In practice it is not possible to reduce the exhaust product’s temperature to inlet level. The condensing water would absorb the sulphur dioxide that is a product of most solid fuels, to form sulphuric acid. As the combustion process is denied the enthalpy of evaporation of the water, it may be more appropriate to define efficiency as = W L.C.V In the case of a boiler, for example, the heat supplied to the water is determined by the difference in enthalpies between the feed water and the steam at exit. The boiler efficiency can therefore be assessed by = Δh L.C.V [Type here] ACADEMIC YEAR 2014-2015 8 PRODUCTS OF COMBUSTION 8.1 VOLUMETRIC ANALYSIS If a fuel is a pure hydrocarbon the products of combustion when, burnt completely in air, would be carbon dioxide and water vapour. However under conditions when there is excess air present there will be some excess oxygen present in the exhaust products. In a similar way, if the amount of air is restricted, then not all the carbon will form carbon dioxide and carbon monoxide will be present. An analysis of the products of combustion can lead to a determination of the effectiveness of the combustion process. By taking samples at stages through a reaction it is possible to find variations of air-fuel distribution. Analysis of the products of combustion also allows an air:fuel ratio to be computed. The most common way to analyse the exhaust gases is by means of the Orsat apparatus. t ap measuring buret t e gas levelling bot t le reagent bot t le t ubes t o increase wet t ed surface wat er bat h [Type here] ACADEMIC YEAR 2014-2015 The Orsat apparatus is used to measure volumes of carbon dioxide, oxygen and carbon monoxide within a fixed volume of a sample gas (100cc). However it is not particularly accurate at detecting very low concentrations. The Orsat apparatus works using a very simple method. To find the volume of a particular gas within the sample a fixed volume of the sampled gas is passed through a specific solution which absorbs only the required gas. The remaining volume of the gas can then be remeasured and compared with the original volume to find the proportion of a specific gas within the sample. The sampled gas is passed through a sequence of solutions each removing one of the gases and the remaining volume calculated afterwards. A solution of caustic potash is used to absorb the carbon dioxide, a mixture of pyrogallic acid, caustic potash and water is used to absorb the oxygen, and to remove the carbon monoxide a solution of cuprous chloride is used. 8.1 PRODUCT PROPORTIONS AND AIR:FUEL RATIO As has been mentioned before the air:fuel ratio can be an indicator of the effectiveness of mixing of air and fuel, as well as a measure of the efficiency of the combustion process. The analysis of the products of combustion by the Orsat method, or any other, can give valuable information about the combustion process. For any hydrocarbon fuel the hydrogen will appear in the exhaust as water vapour. The carbon will be either carbon dioxide or carbon monoxide, or both. If too little air is supplied the initial air:fuel ratio is low indicating a rich mixture. Generally the hydrogen will be burnt off first leaving [Type here] ACADEMIC YEAR 2014-2015 too little air for complete combustion of the carbon. Nitrogen from the air will also appear in the exhaust products If too much air is provided the air:fuel ratio will be high indicating a weak mixture. Again the hydrogen will burn off first as water vapour, the carbon will burn to carbon dioxide and there will be some oxygen left in the exhaust along with the nitrogen. This then explains the reasoning behind the Orsat analysis. The water vapour is nearly always burnt off and consequently the degree to which the products carbon dioxide, carbon monoxide and oxygen appear will be the indicators of combustion efficiency. Nitrogen in the air tends to get in the way of direct contact between oxygen and the fuel. Improved combustion efficiency is obtained by the introduction of turbulence in the combustion zone. This can be effected by many methods – flare plates in the Olympus 301 engine, secondary and tertiary air holes in annular combustion chambers, piston head designs to encourage rotation of the mixture, etc, etc. Similarly, any attempt to reduce the fuel droplet size will aid burning in that the surface area will become larger in comparison to the volume. Therefore fuel spraying or injection will generally improve efficiency. It will seem fairly safe to say that the efficiency of the combustion process can be indicated by the level of CO. If the air content is increased then the CO content will be reduced, until the point is reached where excess oxygen is detected and the excess air condition is reached. The following diagram shows the percentage variation of CO 2, CO and O2 against air:fuel ratio. [Type here] ACADEMIC YEAR 2014-2015 C 02 O2 CO FUEL : AIR RATIO [Type here] ACADEMIC YEAR 2014-2015 ANSWERS TO SELF-TEST QUESTIONS. 6.2a There is no set answer here. Your choices should be discussed with your tutor to determine the likelihood of their validity. It is probable that checks will be made to confirm suggestions. 6.3a Name Molecular weight Boiling point 0C Methane 16 -164 Ethane Propane Butane 30 44 58 -89 -44.5 -0.5 Pentane 72 36 BOILING TEMP verses MOLECULAR WEIGHT 50 0 0 10 -50 -100 -150 -200 6.3b [Type here] 20 30 40 50 60 70 80 ACADEMIC YEAR 2014-2015 Name Ethylene Propylene Butylene Pentylene Molecular Weight 26 42 56 70 Boiling Point 0C -105 -40 -6.1 30.2 MOLECULAR WEIGHT verses BOILING POINT 40 20 0 0 10 20 30 40 50 60 70 80 -20 -40 -60 -80 -100 -120 combined 50 0 0 10 20 30 40 50 60 70 -50 -100 -150 -200 A linear correlation would be appropriate here! 6.5a 16kW [Type here] 80 ACADEMIC YEAR 2014-2015 6.5b 13.206 by weight 25.547 by volume 6.5c 6.085 6.6a a 4.292 b 1.609 c If 50% by volume then 2.95 If 50% by mass then 2.673 6.6b 11.44 [Type here]