General Electric Company

Ge Marmara Technology Center Muhendislik Hizmetleri Ltd

Ge Aerospace Poland Sp. Z O.o.

Volkan Ataman

Michael Terry Bucaro

Andrzej Kazimierz Kąkolewski

Fatih Yasar

Emrah Deniz

Mariusz Konopka

Łukasz Filip Tomaszewski

Bartłomiej Tomaszewski

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

A gas turbine engine comprising a combustion section enshrouded by a casing having at least one through passage, the combustion section comprising a dome wall and a liner at least partially defining a combustion chamber; a fuel nozzle connected to the dome wall and having a nozzle tube; and a coupling securing the fuel nozzle with casing and disposed at least partially in the at least one through passage.

Growing community of inventors

Istanbul, Turkey

Volkan Ataman