Transition piece outlet structure enabling to reduce the...

Details Transition piece outlet structure enabling to reduce the... Transition piece outlet structure enabling to reduce the...

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/42 (2006.01) F01D 9/02 (2006.01) F23R 3/60 (2006.01)

Patent

CA 2372070

A gas turbine combustor transition piece outlet structure enabling a reduction in the temperature difference of a flange formed at the transition piece outlet. A flange is formed with a cooling medium channel along the inner circumference, cooling medium channels along the left and right side surfaces, and heating medium channels along the top and bottom surfaces. By cooling the inner circumference or the side surfaces of the flange by a cooling medium or heating the top and bottom surfaces of the flange by a heating medium, the temperature difference of the flange is reduced. Note that as the cooling medium, it is possible to use compressed air, low temperature steam, or fuel, while as the heating medium, it is possible to use high temperature steam or combustion gas.

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