Calculated A/F Ratio via Exhaust Gas Temperature Measurement for Small Engine Control

2001 ◽  
Author(s):  
Joseph R. Griffin ◽  
Todd J. Ferguson ◽  
Hamid Servati ◽  
Mark Swanson
Keyword(s):  
Temperature Measurement ◽  
Exhaust Gas ◽  
Engine Control ◽  
Gas Temperature ◽  
Exhaust Gas Temperature

scholarly journals Exhaust gas temperature measurements in diagnostic examination of naval gas turbine engines

2011 ◽  
Vol 18 (4) ◽  
pp. 49-53 ◽  
Author(s):  
Zbigniew Korczewski
Keyword(s):  
Normal Distribution ◽  
Gas Turbine ◽  
Temperature Measurements ◽  
Initial Time ◽  
Turbine Engines ◽  
Exhaust Gas ◽  
Engine Control ◽  
Gas Turbine Engines ◽  
Gas Temperature ◽  
Exhaust Gas Temperature

Exhaust gas temperature measurements in diagnostic examination of naval gas turbine engines The third part of the article presents a method for detecting failures of the automatic engine control system with the aid of an exhaust gas temperature setter, specially designed and machined for this purpose. It also presents a procedure of identifying the operating tolerances and determining the diagnostic tolerances for the exhaust gas temperature recorded in the naval turbine engine during the start-up and acceleration processes. The diagnostic tolerances were determined using the statistic inference, based on the hypothesis about the normal distribution of the starting exhaust gas temperature dispersion at the initial time of engine operation. The above hypothesis was verified using the non-parametric statistic test χ2 for examining the consistency of the empirical distribution with the assumed normal distribution. As a result of the examination, satisfactory convergence of the compared distributions was obtained which made the basis for assuming the three-sigma limits of the diagnostic tolerance for the analysed engine control parameter.

scholarly journals Analisa Waktu Operasi Terhadap Temperatur dan Tekanan pada Mesin Diesel

Jurnal METTEK ◽  
2021 ◽  
Vol 7 (1) ◽  
pp. 39
Author(s):  
Nasmi Herlina Sari ◽  
Suteja Suteja ◽  
Yudi Ahmad Efendi
Keyword(s):  
The Other ◽  
Control Panel ◽  
Exhaust Gas ◽  
Engine Control ◽  
Pressure Measurements ◽  
Gas Temperature ◽  
Temperature And Pressure ◽  
Engine Components ◽  
Exhaust Gas Temperature ◽  
Temperature Side

Studi ini bertujuan untuk menganalisa temperatur, dan tekanan pada setiap komponen mesin Mesin diesel Sulzer 16 ZAV 40S selama beroperasi 8 jam. Penelitian ini dilakukan di PT. Iradat Aman Sektor Pringgabaya Lombok. Engine Control Panel (ECP) dan Generator Control Panel (GCP) telah digunakan untuk menentukan nilai dari tekanan, dan temperatur berdasarkan sensor yang telah dipasang pada komponen mesin. Pengukuran temperatur dan tekanan dilakukan setiap jam selama 8 jam. Hasil penelitian menunjukan bahwa setelah mesin beroperasi selama 4 jam sampai 7 jam; temperatur stator, temperatur gas buang, temperature silinder sisi A dan silider sisi B mengalami penurunan yang signifikan dikarenakan kebocoran pada silinder A dan B. Sedangkan tekanan pada mesin masih normal dan tidak mengalami perubahan yang signifikan. This study aims to analyze the temperature and pressure of each component of the Sulzer 16 ZAV 40S diesel engine for 8 hours of operation. This research was conducted at PT. Iradat Aman Sector Pringga Baya Lombok. The Engine Control Panel (ECP) and Generator Control Panel (GCP) have been used to determine the value of pressure and temperature based on sensors that have been installed on engine components. Temperature and pressure measurements were carried out every hour for 8 hours. The results showed that after the machine operated for 4 hours to 7 hours; stator temperature, exhaust gas temperature, cylinder temperature side A and side cylinder B experienced a significant decrease due to leaks in cylinders A and B. On the other hand, the pressure on the engine was still normal and did not experience a significant change.

scholarly journals Multifunctional Signal Generator for Calibration System of Jet Engine Exhaust Gas Temperature Measurement

2017 ◽  
Vol 47 (1) ◽  
pp. 25-28 ◽  
Author(s):  
Premysl Janu ◽  
Sang Van Doan
Keyword(s):  
Temperature Measurement ◽  
Measurement System ◽  
Power Supply ◽  
Low Voltage ◽  
Proper Function ◽  
Exhaust Gas ◽  
Gas Temperature ◽  
Jet Engine ◽  
Temperature Measurement System ◽  
Exhaust Gas Temperature

One of the most important systems of an aircraft jet engine is exhaust gas temperature measurement system that ensure right function of the engine. Temperature of the gas flowing from the engine turbine is quite high. There is one way, how to measure high temperature and it is by thermocouple. So the main aim of the paper is to describe creation and correct function analysis of a thermocouple simulator. Thermocouple generates very low voltage depending on a temperature that ranges from units micro-volts to several tens of millivolts. Generating of such low voltage using simulator is not easy, because this voltage may move at levels of noise. Voltage generation is performed by digital-analogue converter, which is controlled by a microcontroller via SPI bus. The generated voltage is further reduced to a level corresponding to the voltage output of the thermocouple. Several calibration waveforms are performed belonging to appropriate thermocouple type for multifunctional use. Only positive temperatures are generated, because exhaust gas temperature measurement system is aimed at high temperatures. The power supply circuit offers two options. It is supply from accumulator for its portability or from the laboratory power supply. Surface mounted devices are selected in terms of module miniaturization. The newest device base is chosen for modern design of the module. The temperature waveform is generated by the way of polynomial approximation with correction. Dependence of real generated voltage on the voltage, which is defined by appropriate thermocouple type standard and errors evaluation, is used as a proof of proper function.

Fast Response Exhaust Gas Temperature Measurement in IC Engines

2006 ◽  
Author(s):  
Robert J. Kee ◽  
Peter Hung ◽  
Bryan Fleck ◽  
George Irwin ◽  
Robert Kenny ◽  
...  
Keyword(s):  
Temperature Measurement ◽  
Fast Response ◽  
Exhaust Gas ◽  
Gas Temperature ◽  
Ic Engines ◽  
Exhaust Gas Temperature

Lime kiln conversion from coke to natural gas operation – an option in direction of sustainable energy

2020 ◽  
pp. 431-434
Author(s):  
Oliver Arndt
Keyword(s):  
Natural Gas ◽  
New Technology ◽  
Exhaust Gas ◽  
Gas Temperature ◽  
Gaseous Fuels ◽  
Lime Kiln ◽  
Lime Kilns ◽  
Co2 Balance ◽  
Exhaust Gas Temperature

This paper deals with the conversion of coke fired lime kilns to gas and the conclusions drawn from the completed projects. The paper presents (1) the decision process associated with the adoption of the new technology, (2) the necessary steps of the conversion, (3) the experiences and issues which occurred during the first campaign, (4) the impacts on the beet sugar factory (i.e. on the CO2 balance and exhaust gas temperature), (5) the long term impressions and capabilities of several campaigns of operation, (6) the details of available technologies and (7) additional benefits that would justify a conversion from coke to natural gas operation on existing lime kilns. (8) Forecast view to develop systems usable for alternative gaseous fuels (e.g. biogas).

scholarly journals Exhaust Gas Temperature Measurements in Diagnostics of Turbocharged Marine Internal Combustion Engines Part I Standard Measurements

2015 ◽  
Vol 22 (1) ◽  
pp. 47-54 ◽  
Author(s):  
Zbigniew Korczewski
Keyword(s):  
Internal Combustion Engines ◽  
Internal Combustion ◽  
Technical Condition ◽  
Temperature Measurements ◽  
Injection System ◽  
Exhaust Gas ◽  
Combustion Engines ◽  
Gas Temperature ◽  
Measuring Signal ◽  
Exhaust Gas Temperature

Abstract The article discusses the problem of diagnostic informativeness of exhaust gas temperature measurements in turbocharged marine internal combustion engines. Theoretical principles of the process of exhaust gas flow in turbocharger inlet channels are analysed in its dynamic and energetic aspects. Diagnostic parameters are defined which enable to formulate general evaluation of technical condition of the engine based on standard online measurements of the exhaust gas temperature. A proposal is made to extend the parametric methods of diagnosing workspaces in turbocharged marine engines by analysing time-histories of enthalpy changes of the exhaust gas flowing to the turbocompressor turbine. Such a time-history can be worked out based on dynamic measurements of the exhaust gas temperature, performed using a specially designed sheathed thermocouple. The first part of the article discusses possibilities to perform diagnostic inference about technical condition of a marine engine with pulse turbocharging system based on standard measurements of exhaust gas temperature in characteristic control cross-sections of its thermal and flow system. Selected metrological issues of online exhaust gas temperature measurements in those engines are discusses in detail, with special attention being focused on the observed disturbances and thermodynamic interpretation of the recorded measuring signal. Diagnostic informativeness of the exhaust gas temperature measurements performed in steady-state conditions of engine operation is analysed in the context of possible evaluations of technical condition of the engine workspaces, the injection system, and the fuel delivery process.

Energetic Based Organic Fluid Selection for a Solid Oxide Fuel Cell-Organic Rankine Cycle Combined System

2012 ◽  
Vol 622-623 ◽  
pp. 1162-1167
Author(s):  
Han Fei Tuo
Keyword(s):  
Fuel Cell ◽  
Solid Oxide Fuel Cell ◽  
Heat Recovery ◽  
Waste Heat ◽  
Solid Oxide ◽  
Exhaust Gas ◽  
Oxide Fuel ◽  
Gas Temperature ◽  
Selection For ◽  
Exhaust Gas Temperature

In this study, energetic based fluid selection for a solid oxide fuel cell-organic rankine combined power system is investigated. 9 dry organic fluids with varied critical temperatures are chosen and their corresponding ORC cycle performances are evaluated at different turbine inlet temperatures and exhaust gas temperature (waste heat source) from the upper cycle. It is found that actual ORC cycle efficiency for each fluid strongly depends on the waste heat recovery performance of the heat recovery vapor generator. Exhaust gas temperature determines the optimal fluid which yields the highest efficiency.

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