General Electric Company

Ge Marmara Technology Center Muhendislik Hizmetleri Ltd

Ge Aerospace Poland Sp. Z O.o.

Mariusz Konopka

Volkan Ataman

Andrzej Kazimierz Kąkolewski

Łukasz Filip Tomaszewski

Bartłomiej Tomaszewski

Fatih Yasar

A gas turbine engine comprising a combustion section having a case and a combustor, the combustor disposed at least partially in the case. The combustor comprises a dome assembly, a liner at least partially defining a combustion chamber, a plurality of mounting arms extending forward from the dome assembly, and a fuel nozzle assembly coupled with the dome assembly and including a mounting base. The mounting base couples with the case and engages with a first mounting arm of the plurality of mounting arms and a second mounting arm of the plurality of mounting arms.

Gas turbine engine and fuel nozzle therefor

Growing community of inventors

Warsaw, Poland

Mariusz Konopka