| 摘要 |
PROBLEM TO BE SOLVED: To provide an assembling method for a gas turbine including at least one combustor, and to promote combustion during an engine operation to enhance flame stability in a lean burning area. SOLUTION: The present invention provides a combustor assembly 104. The combustor assembly includes a combustion chamber 128, and one or more of transition parts 130 extended from the combustion chamber to a downstream to introduce easily combustion gas from the combustor assembly. The assembly also includes at least one air control system 200 coupled to the one or more of transition portions. The air control system includes one or more of energizing mechanisms connected to a control part for promoting reduction of emissions resulting from an operation of the combustor assembly. COPYRIGHT: (C)2007,JPO&INPIT
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