Steam passage sealing method for steam turbine through-flow portion
A technology for steam turbines and flow parts, which is applied to mechanical equipment, engine components, machines/engines, etc., and can solve problems such as reduced unit efficiency, larger flow gaps, and height loss of steam seal teeth, achieving reduced height loss and excellent performance. High temperature resistance performance, the effect of improving work efficiency
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specific Embodiment approach 1
[0014] Specific embodiment 1: A method for sealing the steam path of the steam turbine flow part described in this embodiment, the method is:
[0015] The stator parts of the high, medium and low pressure passage parts of the steam turbine are sealed with an abradable sealing coating, and the steam seal teeth are arranged between the adjacent two-stage moving blades of the steam turbine and at the end of the steam seal.
[0016] In this embodiment, in order to improve the sealing efficiency of the steam circuit in the flow part of the steam turbine, improve the flow gap, and achieve the purpose of improving the efficiency of the unit, an abradable sealing coating is applied to the stator parts of the high, medium and low pressure flow parts of the steam turbine. The steam seal teeth are inlaid or turned on the top. In this way, when the unit is running, the abradable sealing coating and the steam seal teeth are scraped and rubbed against each other. After the two are scraped, ...
specific Embodiment approach 2
[0017] Specific embodiment 2: This embodiment is a further description of a method for sealing the steam path of the steam turbine flow part described in the specific embodiment 1. In this embodiment, the high, medium and low pressure flow parts of the steam turbine The stator cover is: diaphragm stator vane top shroud, steam seal ring and steam seal arc section.
specific Embodiment approach 3
[0018] Specific embodiment three: this embodiment is a further description of a method for sealing the steam path of a steam turbine flow part described in specific embodiment one. In this embodiment, the abradable sealing coating includes a NiCrAlY bottom layer and NiCrFeAl / hBN / SiO 2 Surface layer.
[0019] In this embodiment, the NiCrAlY bottom layer and NiCrFeAl / hBN / SiO2 surface layer are sprayed on the stator part of the flow part of the steam turbine, and a reasonable coating thickness is designed at the flow position to calculate and define the properties of the coating such as hardness, bonding force and porosity. Index, calculate and reserve the gap, so that the unit will maintain a small gap after the coating and the seal teeth are scraped under the operating environment, and at the same time, the abradable coating system will not be peeled off, corroded and oxidized.
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