Gas turbine engine combustion systems

Details Gas turbine engine combustion systems Gas turbine engine combustion systems

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/08 (2006.01) F02G 3/00 (2006.01)

Patent

CA 2621958

One embodiment is a unique gas turbine engine combustion chamber including primary and secondary burning zones. Other embodiments include unique gas turbine engine apparatuses, systems, methods, and combinations.

Dans une forme de réalisation, l'invention porte sur une chambre de combustion de turbine à gaz spécifique, comprenant une zone de combustion primaire et une zone de combustion secondaire. D'autres formes de réalisation comprennent des dispositifs, des systèmes, des procédés et des combinaisons de turbines à gaz spécifiques. .

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