Aero-engine labyrinth tight-sealing structure
A technology of aero-engine and sealing structure, applied in the direction of engine components, machines/engines, mechanical equipment, etc., can solve the problems of difficult to achieve circumferential blockage and small flow resistance.
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[0018] The present invention will be described in further detail below in conjunction with the accompanying drawings and specific embodiments.
[0019] The aero-engine grate sealing structure as shown in the figure includes a sealing bush 1 and a rotating shaft 2. There are 5 stages of grating teeth on the rotating shaft 2, the first-stage grate teeth are 3, the second-stage grate teeth are 5, and the third-stage grate teeth 7. Four-stage grate teeth 9, five-stage grate teeth 11; grate tooth chambers are formed between two adjacent grate teeth, the first grate tooth chamber 4, the second grate tooth chamber 6, the third grate tooth chamber 8, The fourth grate tooth cavity 10; the circumferential tooth cavity partitions 12 are arranged in the grate tooth cavity, distributed in a circular array with an interval of 60°, and the tooth cavity partitions 12 in two adjacent grate tooth cavities are distributed at an interval of 30°.
[0020] The tooth chamber partition 12 is parallel...
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