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    • 1. 发明公开
    • 공기 바이패스 시스템 및 가스 터빈 엔진의 효율 개선 방법
    • 用于气体涡轮机入口的空气旁通系统
    • KR1020070121552A
    • 2007-12-27
    • KR1020070060582
    • 2007-06-20
    • 제너럴 일렉트릭 캄파니
    • 칠라르라훌제이스미스라우브와필드스키피오알스톤일포드
    • F02C3/04F02C7/04F02C7/05
    • F02C7/04F02C7/057
    • An air bypass system and a method for improving efficiency of a gas turbine engine is provided to achieve improved allover efficiency and output of the gas turbine engine by reducing a pressure drop during idling of a power increasing system. An air bypass system(110) for a gas turbine inlet filter housing(100) having a power increasing system(40) positioned inside, includes a duct(120) arranged on the inlet filter housing around the power increasing system, and a damper positioned in the duct so as to open/close the duct. A method for improving efficiency of a gas turbine engine, includes a step of increasing an air flow area around the power increasing system, a step of operating the power increasing system, and a step of decreasing the air flow area when the power increasing system operates.
    • 提供一种空气旁路系统和提高燃气轮机的效率的方法,以通过减小功率增加系统的空转时的压降而实现燃气轮机的全效率和输出。 一种用于燃气轮机入口过滤器壳体(100)的空气旁通系统(110),其具有位于内部的功率增加系统(40),包括布置在增压系统周围的入口过滤器壳体上的管道(120) 在管道中打开/关闭管道。 一种用于提高燃气涡轮发动机的效率的方法包括增加增压系统周围的空气流动区域的步骤,操作增压系统的步骤,以及当功率增加系统运行时减小空气流动面积的步骤 。