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    • 1. 发明授权
    • Combustion chamber/venturi configuration and assembly method
    • 燃烧室/文丘里配置和装配方法
    • US06865892B2
    • 2005-03-15
    • US10248079
    • 2002-12-17
    • Miguel GarridoShawn Miller
    • Miguel GarridoShawn Miller
    • F23R3/00F23R3/60F02C7/20
    • F23R3/60F23R3/005F23R2900/00017
    • A two-stage gas turbine combustor is disclosed that incorporates an improved assembly and disassembly methodology that results in improved inspection and repair techniques. The combustor includes an upper liner, lower liner, cap assembly, and a venturi assembly that directs cooling air into the combustion chamber for use in the combustion process, wherein a venturi assembly is inserted within an upper liner and an upper liner is then inserted in a lower liner. The venturi assembly, upper liner, and lower liner are fixed together with a plurality of easily removable retaining pins. The improved assembly allows for easier inspection and repair of the upper liner, lower liner, and venturi assembly.
    • 公开了一种两级燃气轮机燃烧器,其包括改进的组装和拆卸方法,其导致改进的检查和修复技术。 燃烧器包括上衬套,下衬套,盖组件和文丘里组件,其将冷却空气引导到燃烧室中以用于燃烧过程,其中文丘里组件插入上衬垫内,然后将上衬管插入 下层衬里 文丘里组件,上衬套和下衬套与多个容易拆卸的保持销固定在一起。 改进的组件允许更容易地检查和修理上衬套,下衬套和文氏管组件。