首页> 外国专利> METHOD OF SEALING A ROTOR SHAFT RELATIVE TO A TURBO-SET CASING AND A TURBO-SET FORM MAKING THE SAME

METHOD OF SEALING A ROTOR SHAFT RELATIVE TO A TURBO-SET CASING AND A TURBO-SET FORM MAKING THE SAME

机译:相对于涡轮固定套密封转子轴的方法和使涡轮固定套相同的方法

摘要

The proposed method of sealing a rotor shaft (2) with respect to a casing (1) of a turbo-set working in a piping (16) for transported gas with a dry gas sealing system between the rotor shaft (2) and the casing (1) is characterized in that in the gas sealing system (3) a closing medium is introduced from both inner and outer sides of the casing, i.e. from the casing (1) inner side a purified transported gas and from the casing (1) outer side a closing gas and a mixture containing escaping transported gas and closing gas occurring in the gas sealing system (3) on the casing (1) outer side is exhausted. The mixture containing escaping transported gas and closing gas occurring in the gas sealing system (3) on the casing (1) outer side is exhausted and introduced on air suction side into a gas engine (19, 20) being otherwise fed with the transported gas. The turbo-set for carrying this method is provided with a turbo-machine (15) working in the piping (16) for transporting gas, which contains the casing (1) in which the rotor shaft (2) is mounted. Between the rotor shaft (2) and the casing (1) there is arranged a dry gas sealing system (3) in front of which there is from the casing (1) inner and outer sides arranged at least one partition wall (6, 7, 29). The first space (9) extending between the first partition wall (6) on the casing (1) inner side and the gas sealing system (3) is provided with an inlet (10) for transported gas, while the third space (13) extending between the partition wall (7) on the casing (1) outer side and the gas sealing system (3) is provided with a second outlet (14) for a mixture of escaping transported gas with closing gas. The turbo-set contains at least one gas engine (19, 20) with an exhaust piping (35) for combustion products, a supply piping (21) of combustion gas and a suction piping (24) for combustion air. The suction piping (24) for combustion air is connected with the second outlet (14) of the mixture containing escaping transported gas and closing gas from the turbo-machine (15).
机译:所提出的利用转子轴(2)和壳体之间的干气密封系统将转子轴(2)相对于涡轮机组的壳体(1)密封在用于输送气体的管道(16)中的方法(1)的特征在于,在气体密封系统(3)中,从壳体的内侧和外侧引入封闭介质,即从壳体(1)的内侧引入净化的输送气体,并从壳体(1)引入封闭介质。在壳体1的外侧的气体密封系统3中,排出封闭气体和包含逸出的输送气体和封闭气体的混合物的外部气体。在壳体(1)外侧的气体密封系统(3)中产生的,包含逸出的输送气体和封闭气体的混合物被排出,并在吸气侧被引入到燃气发动机(19、20)中,否则该输送气体被供给。用于执行该方法的涡轮机组具有在用于输送气体的管道(16)中工作的涡轮机(15),该涡轮机包含壳体(1),转子轴(2)安装在该壳体中。在转子轴(2)和壳体(1)之间布置有干燥气体密封系统(3),在该干燥气体密封系统的前方,从壳体(1)的内侧和外侧布置有至少一个分隔壁(6、7)。 ,29)。在壳体(1)内侧的第一分隔壁(6)和气体密封系统(3)之间延伸的第一空间(9)设置有用于输送气体的入口(10),而第三空间(13)在壳体(1)外侧上的分隔壁(7)和气体密封系统(3)之间延伸的第二出口(14)设有用于将所输送的气体与关闭的气体逸出的混合物。该涡轮机组包括至少一个燃气发动机(19、20),其具有用于燃烧产物的排气管道(35),燃烧气体的供应管道(21)和用于燃烧空气的吸入管道(24)。燃烧空气的吸入管(24)与混合物的第二出口(14)相连,混合物的第二出口(14)包含逸出的输送气体和来自涡轮机(15)的封闭气体。

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