Gas turbine combustor

Details Gas turbine combustor Gas turbine combustor

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/02 (2006.01) F23R 3/00 (2006.01) F23R 3/04 (2006.01)

Patent

CA 2380914

An internal cylinder which has the opening section from which combustion gas is blown out is inserted into the tail cylinder which becomes a flow path of the combustion gas, and is engaged with the tail cylinder, while securing a clearance between the edge of the opening section and the internal wall surface of the tail cylinder. Air compressed with a compressor is jetted from the clearance along the internal wall surface of the tail cylinder, and a film of cooling air is formed on the internal wall surface of the tail cylinder.

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