Ignition system and their purpose in aircraft reciprocating engines

dc.contributor.authorVorlíček, Marek
dc.contributor.authorČerňan, Jozef
dc.date.accessioned2023-11-16T13:44:05Z
dc.date.available2023-11-16T13:44:05Z
dc.date.issued2023
dc.description.abstractThis research describes the function and principles of ignition systems in aircraft reciprocating engines. Physical-chemical processes, which are part of combustion, and the factors affecting them are defined in detail. Types of ignition systems are divided based on main parts and frequency of appearance in aircraft engines. Components of ignition and their function in electric and magnetic circuits are individually described. The future development in ignition systems is defined. The research includes an analysis of the pros and cons of laser ignition in its application in aviation. It presents Low-Temperature Combustion or Volumetric Ignition using Low-Temperature Plasma. An example may be the Microwave-assisted Plasma Ignition System. Engine speed and vacuum in intake are the main parameters influencing the ignition timing curve in Electronic Control Unit Master developed by IMF Soft. This ECU is used in the designed ignition system of testing engine. The designed timing curves were tested, and the results of engine power and torque were compared. In conclusion, the optimal timing curve is evaluated for this reciprocating engine.en_US
dc.identifier.doihttps://doi.org/10.26552/pas.Z.2023.2.01
dc.identifier.urihttp://drepo.uniza.sk/handle/hdluniza/978
dc.language.isoenen_US
dc.publisherUniversity of Žilinaen_US
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectignition systemen_US
dc.subjectignitionen_US
dc.subjectspark plugen_US
dc.subjectaircraft reciprocating engineen_US
dc.subjectlaseren_US
dc.subjectlow temperature combustionen_US
dc.titleIgnition system and their purpose in aircraft reciprocating enginesen_US
dc.typeConference paperen_US

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