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Gas Turbine Engine Combustion System Report

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Added on  2020-03-16

Gas Turbine Engine Combustion System Report

   Added on 2020-03-16

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Running head: GAS TURBINE ENGINE COMBUSTION SYSTEMSGas Turbine Engine Combustion Systems on AircraftName of the student:Name of the university:Author Note
Gas Turbine Engine Combustion System Report_1
1GAS TURBINE ENGINE COMBUSTION SYSTEMS1. SummaryThe report is developed to analyze and examine the developing of the gas turbine engine combustionin aircrafts. It demonstrates the working mechanisms of the combustion system. This also includesits descriptions. The three common types of combustion systems are compared. At last it considersthe other cooling arrangements of airflow that are also used for the cooling combustion system.
Gas Turbine Engine Combustion System Report_2
2GAS TURBINE ENGINE COMBUSTION SYSTEMSTable of Contents2. Introduction:......................................................................................................................................33. Investigating and describing the developing of the gas turbine engine combustion systems:..........34. The working mechanism of combustion system:..............................................................................45. The 'Can' combustion system:...........................................................................................................56. The 'Can-Annular' combustion system:.............................................................................................67. 'Annular' combustion system:............................................................................................................78. A brief comparison of the three combustion systems:.......................................................................89. Other cooling airflow arrangements used to cool combustion systems:.........................................1110. Conclusion:....................................................................................................................................1311. References:....................................................................................................................................14
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3GAS TURBINE ENGINE COMBUSTION SYSTEMS2. Introduction:The gas turbine engine combustion system on the aircraft houses the process of combustion.It raises the temperature of the air by passing through the engine. The main function of the section isto burn the air or fuel mixture adding heat energy to the air. In order to do all this, the combustion chamber is meant to deliver the ways of proper mixingof the air and fuel, assuring a good combustion. They must burn the mixture carefully. Then the hotcombustion products must be cooled to the temperature that the inlet of the turbine guides the bladesor vanes within the operating conditions. Lastly, it delivers the hot gases towards the turbine part.There are three fundamental kinds of combustion chambers currently. They just vary in terms ofdetailing. They are can-combustion, can-annular and annular type. The following report is prepared to describe and investigate the developing of the gas turbineengine combustion. It analyses the working mechanisms of the combustion system along with itsdescriptions. Then the different kinds of combustion systems are discussed. Then, all thesecombustion systems are compared. Lastly, the report discusses the other cooling arrangements ofairflow used for the cooling combustion system. 3. Investigating and describing the developing of the gas turbine engine combustion systems:The industrial revolution came to be the reality as the access to the devices of the energyconversions got dispatched on the demand. For instance, before this innovation, the ships weremoving through sails and so on. The reciprocating design, the original steam engine of Newcomenwas the first breakthrough. After that James Watt added the condenser tripling the efficiency. Then a
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