Gas turbine combustor

Abstract

Abstract PURPOSE:To make it possible to provide a certain allowance for the combustion range of the combustor by connecting a combustion compartment to an exhaust compartment via a bypass pipe provided with a control valve for adjusting the amount of air within the combustion compartment, and exhausting bypass air into the exhaust compartment. CONSTITUTION:The amount of air within a combustion compartment 108 which has been exhausted out of a compressor 101 is controlled from the outside by means of a bypass pipe 112 provided with a control valve 113. Thus, the amount of air which is optimum for continuing to ignite or burn two burners 104 and 106 is secured. As a result, it is possible to reduce the unignition phenomena and load variations to be burdened on the gas turbine at the time of changing a single movement over to a combined operation.

Inventors

• 👤 Yasuhiko Ikegami
• 👤 池上　保彦
• 👤 Fujio Sasamoto
• 👤 笹本　富士男
• 👤 Hirobumi Saeki
• 👤 佐伯　博文

Bibliographic Details