Annular combustor with tangential cooling air injection

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

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60746, 60755, 60756, 60760, F02C 308

Patent

active

RE0349623

ABSTRACT:
The combustion dynamics and efficiency of gas turbine having an annular combustor 26 provided with fuel injection nozzles 50 that inject fuel generally tangentially is improved by providing the walls 32, 34, 39 of the combustion 26 with cooling air film injectors 70, 86; 72, 88; 74, 90 at substantially equally angularly spaced locations about each such wall and which are oriented to generally tangentially inject a film-like air stream on the associated wall 32, 34, 39.

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