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    • 1. 发明公开
    • GASTURBINE MIT EINER KÜHLUNG DER LETZTEN TURBINENSTUFE
    • GASTURBINE麻省理工学院EINERKÜHLUNGDER LETZTEN TURBINENSTUFE
    • EP3172407A1
    • 2017-05-31
    • EP15794884.5
    • 2015-11-11
    • Siemens Aktiengesellschaft
    • WAGNER, Michael
    • F01D5/08F01D11/00F01D11/04
    • F01D11/001F01D5/082F01D11/04F05D2220/3215F05D2240/55F05D2270/3013Y02T50/673Y02T50/676
    • The invention relates to an exhaust-gas section (12) for a gas turbine (1), comprising a surrounding shroud (42, 44) having a first opening (48), which is arranged in a region of the exhaust-gas section (12) that has a pressure lower than the air pressure of the outer environment of the gas turbine (1) in an operating state of the gas turbine (1) and which forms the outlet of an air channel (50), the inlet of which is connected to the outer environment of the gas turbine (1). The problem addressed by the invention is that of, by means of said exhaust-gas section, ensuring especially flexible operation of the gas turbine by reliably avoiding exhaust-gas leaks in all operating states. This problem is solved in that the air channel (50) has a chamber (62) at the outlet-side end of the air channel, which chamber has a second opening (64), through which a specified gas mass flow is admitted into the chamber (62).
    • 本发明涉及一种用于燃气轮机(1)的排气区段(12),该排气区段包括具有第一开口(48)的周围护罩(42,44),该第一开口布置在排气区段 在燃气轮机(1)的运行状态下具有比燃气轮机(1)的外部环境的气压低的压力并形成空气通道(50)的出口的空气通道(50)(图12) 连接到燃气轮机(1)的外部环境。 本发明解决的问题在于,通过所述排气部分,通过可靠地避免所有运行状态下的排气泄漏来确保燃气涡轮机的特别灵活的运行。 该问题通过如下方式解决:空气通道(50)在空气通道的出口侧端部具有腔室(62),该腔室具有第二开口(64),特定气体质量流通过该第二开口 室(62)。