Gas turbine combustor having bypass and annular gas passage...

Details Gas turbine combustor having bypass and annular gas passage... Gas turbine combustor having bypass and annular gas passage...

2005-03-01

2005-03-01

Freay, Charles G. (Department: 3746)

Power plants

Combustion products used as motive fluid

With variable oxidizer control

C060S752000

Reexamination Certificate

active

06860098

ABSTRACT:
There is provided a combustor to burn fuel, comprising a bypass passage connected to one side of the combustor to supply air into the combustor; and an annular passage provided around the combustor and connected to the bypass passage, wherein air supplied through the bypass passage passes in the annular passage in the circumferential direction, and is uniformly supplied into the combustor in the circumferential direction thereof through an opening which connects the combustor and the annular passage. Accordingly, compressed air passing through the bypass passage can be supplied uniformly into a tail portion of the combustor, and unevenness of temperature distribution in a cross section of the combustor tail portion can be reduced.

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