CC BY
20
UDC 621.43.056
Doi: 10.31772/2587-6066-2020-21-3-356-363
For citation: Baklanov A. V. The influence of the method of fuel supply into the combustion chamber on the quality of mixing and on the carbon oxide formation. Siberian Journal of Science and Technology. 2020, Vol. 21, No. 3, P. 356-363. Doi: 10.31772/2587-6066-2020-21-3-356-363
Для цитирования: Бакланов А. В. Влияние способа подачи топлива в камеру сгорания на качество смешения и образование оксида углерода // Сибирский журнал науки и технологий. 2020. Т. 21, № 3. С. 356-363. Doi: 10.31772/2587-6066-2020-21-3-356-363
THE INFLUENCE OF THE METHOD OF FUEL SUPPLY INTO THE COMBUSTION CHAMBER ON THE QUALITY OF MIXING AND ON THE CARBON OXIDE FORMATION
A. V. Baklanov
Kazan National Research Technical University named after A. N. Tupolev - KAI 10, Marx St., Kazan, 420111, Russian Federation E-mail: [email protected]
The burning offuel in the combustion chamber of a gas turbine engine (GTE) is accompanied by formation of toxic substances. The most dangerous among them are carbon oxides that have a detrimental effect on humans and environment. In this regard the article is solving the urgent problem of determining the optimal method of gaseous fuel supplying in GTE combustion chamber to ensure low carbon-oxide emissions.
The paper presents the design features of injectors that work with a separate supply of air and fuel. Natural gas is used as fuel. One of the considered injectors provides jet fuel supply by means of a perforated spray, and another one provides twisted fuel supply by means of a swirler built into the fuel channel. The main geometric parameters of the injectors are given as well, such as the size of the swirler, the number of blades, and the diameter of the output nozzle.
In this regard the quality of air-fuel mixture preparation in a swirl jet in the outlet of the burner with two types of injector is defined. It is found that the best quality of mixing is ensured by the injector with jet spray.
The design of a heat pipe simulator, in which the tested nozzle is placed, is considered. The design of a stand installation designed for testing injectors in a heat pipe simulator, as well as the modes under which these tests were carried out, are presented. The results were obtained in a heat pipe simulator with installed jet injectors and injectors with a swirling fuel jet. An analysis was conducted, which resulted in conclusions about the effectiveness of using jet injectors. According to the conducted research, the parameters of the injector with a swirling fuel jet are characterized by the presence of high values of CO levels in the combustion products, which is explained by the extremely low quality of mixing fuel with air and, consequently, low efficiency of fuel combustion. Jet fuel injection has low CO values, which indicates good quality of mixing fuel with air and high efficiency of a combustion process. As a result, we have received recommendations on setting the selected type of injectors in a full-size combustion chamber.
Keywords: combustion chamber of gas-turbine engine, emission reduction, diffusion combustion, injector, burner, mixing.
ВЛИЯНИЕ СПОСОБА ПОДАЧИ ТОПЛИВА В КАМЕРУ СГОРАНИЯ НА КАЧЕСТВО СМЕШЕНИЯ И ОБРАЗОВАНИЕ ОКСИДА УГЛЕРОДА
А. В. Бакланов
Казанский национальный исследовательский технический университет им. А. Н. Туполева - КАИ Российская Федерация, 420111, г. Казань, ул. К. Маркса, 10 E-mail: [email protected]
Сжигание топлива в камере сгорания газотурбинного двигателя сопровождается образованием токсичных веществ. Особую опасность среди них представляют окислы углерода, оказывающие вредное воздействие на человека и окружающую среду. В связи с этим в статье решается актуальная задача по определению оптимального способа подачи газообразного топлива в камеру сгорания ГТД для обеспечения низкого выброса СО.
В работе представлены особенности конструкции форсунок, которые работают с раздельной подачей воздуха и топлива. В качестве топлива используется природный газ. Одна из рассмотренных форсунок обеспечивает струйную подачу топлива при помощи перфорированного распылителя, а другая - закрученную подачу топлива при помощи завихрителя, встроенного в топливный канал. Также приведены основные геометрические параметры форсунок, такие как размеры завихрителя, количество лопаток, диаметр выходного сопла.
Произведено определение качества подготовки топливовоздушной смеси в закрученной струе на выходе из горелок с двумя типами форсунок. Установлено, что наилучшее качество смешения обеспечивает форсунка со струйным распылом топлива.
Рассмотрена конструкция имитатора жаровой трубы, в который помещается испытываемая форсунка. Представлена конструкция стендовой установки, предназначенной для испытания форсунок в имитаторе жаровой трубы, а также режимы, при которых данные испытания проводились. Получены результаты в имитаторе жаровой трубы с установленными струйными форсунками и форсунками с подачей закрученной топливной струи. Проведен анализ, по результатам которого сделаны выводы об эффективности применения струйных форсунок. В соответствии с проведенными исследованиями параметры форсунки с подачей закрученной топливной струи характеризуются наличием высоких значений уровня СО в продуктах сгорания, что объясняется крайне низким качеством перемешивания топлива с воздухом и, следовательно, низкой эффективностью сжигания топлива. Форсунка со струйной подачей топлива имеет низкие значения СО, что свидетельствует о хорошем качестве смешения топлива с воздухом и высокой эффективности организации горения. В результате получены рекомендации о постановке выбранного типа форсунок в полноразмерную камеру сгорания.
Ключевые слова: камера сгорания ГТД, снижение выбросов вредных веществ, диффузионное горение, форсунка, горелка, смешение.
Introduction. The quality of the preparation of air-fuel mixture in the combustion chambers of gas turbine engines largely determines the level of emissions of toxic substances, herewith the quality of mixing is ensured by the way fuel is fed into the combustion chamber [1]. For this reason, the issue of the reasonable choice of a fuel supply method and determination of its influence on the formation of toxic substances in the combustion products of gas turbine engines is relevant. The main toxic substances in the combustion of hydrocarbon fuels are nitrogen oxides and carbon monoxide [2], therefore, reducing the level of their concentration is one of the most important tasks of engine manufacturers.
The burner unit of the annular combustion chamber includes an annular plate in which swirling gas burners are installed regularly around the circumference, between the inner and outer shells of the flame tube (fig. 1). In the center of these burners there are injectors that provide fuel supply [3].
in the primary zone of the chamber behind the nozzle heads 4 of each of the swirling burners, flows of the fuel-air mixture are formed, these flows have paraxial circulation areas. The presence of such areas ensures the circulation of hot combustion products and active centers from the combustion zone to the base of the fresh mixture torch, which creates conditions for stable ignition and flame stabilization.
The fuel supply method can be jet in the form of fuel jets and in the form of a swirling fuel jet. This paper considers two injectors operating on gaseous fuel, which differ in the way of fuel supply [4].
The principle of operation of the first one is to supply a swirling gas stream from the center of the burner. The
injector (fig. 2) includes: body 2, (plug) 3 and a throttling washer 4.
screw 1 with a nut
Fig. 1. Burner device of a serial combustion chamber: 1 - injector; 2 - swirler; 3 - mixing chamber; 4 - jet nozzle
Fig. 2. Centrifugal gas injector: 1 - screw; 2 - injector body; 3 - nut (plug); 4 - throttling washer
Рис. 1. Схема горелочного устройства серийной КС: 1 - форсунка; 2 - завихритель; 3 - камера смешения; 4 - сопловой насадок
Рис. 2. Центробежная газовая форсунка: шнек; 2 - корпус форсунки; 3 - гайка (заглушка); 4 - дросселирующая шайба
The fuel supplied by the gas injectors 1 along the axis of each of the burners is mixed in the mixing chamber 3 with the air flow swirling in the swirler 2. As a result,
The body of the injector 2 is made with an internal passage for supplying gas and with the metering holes A for gas outlet. The body has a flange with holes for attach-
1
ing the injector to the combustion chamber body and a threaded channel for installing the screw 1. The throttling orifice 4 is installed to provide the required gas flow through the injector.
The injector operates in the following way: gas flows from the gas collecting main through pipelines to the injectors, passes through the fuel passage in the injector body. Getting on the blades of the screw 1, it twists and leaves the metering holes A. Mixing with the air that goes out of the burner swirler, the gas enters the combustion chamber [4]. Such an injector can be classified as a centrifugal gas injector.
The screw installed inside the injector body (fig. 3) is a swirler with four blades twisted along a helical curve of right-hand thread, stroke - 32 mm, blade thickness -1 mm.
D,
Fig. 3. Injector screw (swirler):
outer screw 10.5 ШШ, Dinner screw 5 ШШ,
ao = 45o; ao = 4 mm; S1 = 5 mm
Рис. 3. Шнек (завихритель) форсунки: Днар.шн.= 10,5 мм; Двнутр.шн= 5 мм; ao = 45o; а0 = 4 мм; S1 = 5 мм
The second injector (fig. 4) differs from the first one in that the screw is excluded from the design, and at the tip of the injector there are four equally spaced holes (instead of one hole) for gas outlet [5].
To check the quality of fuel-air mixing behind the burner with a jet gas injector in comparison with a centrifugal gas injector, additional studies were carried out to determine the quality of the preparation of the fuel-air mixture at the outlet from the burners with these injectors.
Fig. 4. Jet gas injector. Four holes with the diameter d = 2.9 mm
Рис. 4. Струйная газовая форсунка. Четыре отверстия диаметром d = 2,9 мм
The studies were carried out on a testing stand (fig. 5), which includes three systems: air supply, gas supply and measurement system.
The burner is placed on the test-bench equipment as follows: the injector is installed in the receiver body, to the connecting branch of which fuel is supplied. The burner is placed with the sleeve part in the orifice of the receiver cover. The fuel from the jet injectors is fed into the inner cavity of the jet nozzle, as a result, fuel-air mixture is formed at the outlet of the burner. The fuel is supplied to the propellant feed system from the cylinder manifold. Carbon dioxide (CO2) is used as a gas to replace methane. To measure the concentration fields at the outlet of the burner, a coordinate device with a receiver of the gas analyzer called PKU-4-MK-S is installed. This device allows us to move the detector receiver axially and radially. Concentration measurements are made from the center of the burner, for which the nozzle axis "0" is taken, with further movement of the sampling instrument in both directions along the burner nozzle, across the jet every 4 mm. According to this principle, measurements are performed repetitively in seven sections: at the nozzle exit section and every 50 mm up to the distance of 300 mm [6].
The measurements of CO2 concentrations in the burner jets were also aimed at determining the distance at which the concentration pattern is equalized, as well as at fixing the rate of concentration change along the jet axis [7; 8].
To visualize the intensity of the mixing process, fig. 6 shows the characteristics of C02 = f (r), showing in detail the change in the concentration over the cross section of the swirling jet.
According to the data in fig. 6, it can be seen that behind the burner with a centrifugal gas injector, there is no significant expansion of the mixing area, which is associated with the formation of the high flow rate of fuel gas, which leads to the high ejection ability of the jet forming a narrow flow core, in which intensive mixing of fuel
with air occurs. Beyond the relative coordinate r = -r—
r
max
corresponding to the value of 0.5, mixing does not occur, since this area contains practically no fuel.
The burner with a jet gas injector has a wide concentration field and its low level, which is explained by the volumetric recirculation zone provided by the presence of jet fuel supply, which makes it possible to mix fuel with air throughout the entire volume of the swirling jet formed behind the jet nozzle.
The quality of preparation was assessed analyzing the dependence characterizing the maximum relative deviation of concentration from the mean integral value of the concentration field [9]:
- C - C
C — max m
С„
(1)
where Cmax - maximum value in the measured concentration field; Cmi - mean integral value of concentration.
In accordance with this dependence, the indicator of the ideally regular distribution of the concentration of the air-fuel mixture in the section is the value C = 0.
Fig. 7 shows that the best mixing quality in all seven sections is observed for the burner with a jet gas injector. That proves the quality of the mixture preparation.
The measurements of the concentration fields behind the swirl burners confirm that the mixing process is achieved in the burner with a jet gas injector due to the jet fuel supply to the recirculation zone, and in the burner with a centrifugal gas injector due to the high ejection ability of the swirling fuel jet inside the air stream swirled in the opposite direction [10].
Further studies comprised placing the injectors into the combustion chamber in order to determine the emissions of nitrogen oxides and carbon monoxide. The compartment is 1/8 part of a full-size combustion chamber, consisting of an outer and inner shell, a flame tube with a burner unit, in which four burners with injectors are installed. The combustion can is bounded by cooling side-walls on both sides [11].
The combustion chamber compartment is studied on a testing stand, the diagram of which is shown in fig. 8. The stand is equipped with the necessary systems for measuring and registering parameters. The stand includes a gas turbine engine (blowing engine), which is used to supply compressed air to the tested compartment of the combustion chamber 3. Air is taken from the high-pressure compressor, then it enters through the pipeline into the central line 1. Air consumption is measured by a flow meter.
The stand is equipped with a measuring section 2 with recording the readings of a pressure sensor 4, 5; the air temperature is controlled by a chromel-alumel thermocouple 6. The fuel (natural gas) is supplied through the fuel system 7 to the fuel manifold 8 of the combustion chamber compartment, and then it enters the front-line device and injectors. To measure the temperature in the outlet of the compartment, a survey rake 12 is installed at the outlet of it, the data from which is transmitted to the recording equipment 13. To determine the composition of combustion products, a gas sampling probe 9 and a line for transporting combustion products 10 to the gas analyzing equipment 11 are located at the outlet of the compartment.
The gas analyzer testo350 [12] is used to determine the CO content in combustion products.
The compartments were tested under the following conditions: Air pressure Pa = 1.37 kPa, Air flow Ga = 1.72 kg / s, Air temperature Ta = 488 K, superficial velocity speed 1 = 0.28. The change in the excess air ratio was carried out by reducing the fuel consumption.
After determining the component composition of combustion products for carbon monoxide, the emission index EIi is calculated, according to the equation [13]:
EIi(1 — a. • L0) .103.
(2)
Fig. 5. Structure of test stand:
1 - Heater; 2 - outlet reducer; 3 - pressure gauge; 4 - cutoff valve; 5 - flow meter; 6 - tee j oint; 7 - burner; 8 - gas analyzer; 9 - ventilation device for removing carbon dioxide from the working room; 10 - coordinate table; 11 - receiver; 12 - flow meter; 13 - electromagnetic valve; 14 - moisture separator; absolute pressure and C02 temperature sensors installed upstream of the flow meter (throat); sensor for measuring pressure difference across the C02 path; absolute pressure and air temperature sensors installed upstream of the flow meter; and sensor for measuring air pressure difference
installed upstream of the receiver
Рис. 5. Принципиальная схема стенда: 1 - нагреватель; 2 - выходной редуктор; 3 - манометр; 4 - отсечной клапан; 5 - расходомер; 6 - тройник; 7 - горелка; 8 - газоанализатор; 9 - вентиляционное устройство для отвода углекислого газа из рабочего помещения; 10 - координатный стол; 11 - ресивер; 12 - расходомер 13 - электромагнитный клапан; 14 - влагоотделитель
1 -0,8 -0,6 -0,4 -0,2 0 0,2 0,4 0,6 0,8
a
b
Fig. 6. Field of CO2 concentrations in various sections of a swirling jet: а - centrifugal gas injector (CGI); b - with jet injector (JI) ♦ - nozzle cut; ■ - 50 mm; ▲ - 100 mm; x - 150 mm; 0 - 200 mm; □ - 250 mm; A - 300 mm
Рис. 6. Поле концентраций СО2 в различных сечениях закрученной струи: а - ЦБГФ; b - СГФ
♦ - срез сопла; ■ - 50 мм; ▲ - 100 мм; x - 150 мм; 0 - 200 мм; □ - 250 мм; A - 300 мм
Where L0 = 16.7 - stoichiometric coefficient of methane combustion (kg of air / kg of fuel); a; - total or local air-to-fuel ratio; ^ - molar mass of the determined toxic substance; - molar air mass; %i - volume fraction of a toxic substance (ppm). When calculating EIi we have taken the following values of molar masses:
(xco = 28.010 kg / kmol and ^ = 28.964 kg / kmol [14; 15].
According to the results of the measurements (fig. 9), it can be seen that the value of the carbon monoxide emission index in the compartment with a jet gas injector has decreased by half compared to the compartment with a centrifugal gas injector.
The results showed that it is preferable to use gas (by appropriate orientation and range of the jets) to disdistribution with the help of jet feed, which, in contrast tribute fuel over the air flow section with the required to the supply of swirling fuel jets, not only increases concentration profile in the flame tube in a simple and the interface of the mixed media, but it also allows us reliable way.
Fig. 7. The quality of the preparation of the air-fuel mixture in a swirling stream: ■ - the burner with centrifugal gas injector (CGI); □ - the burner with jet injector (JI)
Рис. 7. Качество подготовки топливовоздушной смеси в закрученной струе: ■ - горелка с ЦБГФ; □ - горелка с СГФ
Fig. 8. Stand for testing the sections of a combustion chamber Рис. 8. Стенд для исследования отсеков камеры сгорания
Fig. 9. CO index at the outlet of the compartment: ♦ - JI; ■ - CGI
Рис. 9. Индекс СО на выходе из отсека: ♦ - СГФ; ■ - ЦБГФ
Conclusion.
1. The organization of jet fuel supply will allow us to perform the most efficient combustion of gaseous fuel in comparison with the fuel supply with a swirling jet, which makes it possible to halve the index of carbon monoxide in the combustion products of the combustion chamber compartment.
2. Jet fuel supply provides better preparation of a fuel-air mixture.
3. It is recommended to install a jet gas injector as a measure to reduce carbon monoxide in combustion products of a gas turbine engine.
References
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©Baklanov А. V., 2020
Baklanov Andrey Vladimirovich - Associate Professor; Kazan National Research Technical University named after A. N. Tupolev - KAI. E-mail: [email protected].
Бакланов Андрей Владимирович - доцент; Казанский национальный исследовательского технический университет имени А. Н. Туполева - КАИ. Email: [email protected].
