Intelligent control multi-flame combustion chamber, aero-engine and control method

The invention relates to the technical field of aviation industry, and provides an intelligent control multi-flame combustion chamber, an aero-engine and a control method.The multi-flame combustion chamber comprises a combustion unit, an intelligent temperature control valve assembly and a plurality...

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Bibliographische Detailangaben
Hauptverfasser: WANG XUDAN, EOM HEE-SUNG, LI HONGAO, ZHANG CHI, WANG JIANCHEN
Format: Patent
Sprache:chi ; eng
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Zusammenfassung:The invention relates to the technical field of aviation industry, and provides an intelligent control multi-flame combustion chamber, an aero-engine and a control method.The multi-flame combustion chamber comprises a combustion unit, an intelligent temperature control valve assembly and a plurality of main combustion stage fuel oil supply parts, and the combustion unit comprises a combustion chamber body and a plurality of main combustion stage assemblies arranged on the combustion chamber body; the main combustion stage assembly comprises at least one main combustion stage element part; the multiple main combustion stage fuel oil supply parts are connected with the multiple main combustion stage assemblies in a one-to-one correspondence mode. The intelligent temperature control valve assembly is provided with a medium inlet and a plurality of medium outlets, and the multiple medium outlets are connected with the multiple main combustion stage fuel oil supply components in a one-to-one correspondence mode. T