A connection structure between an impeller and a turbine shaft
A connection structure, turbine shaft technology, applied in the direction of blade support components, engine components, machines/engines, etc., can solve the problems of time-consuming and expensive manufacturing, low economic benefits of rotor assembly imbalance, and low supercharger life. To achieve the effect of avoiding the risk of rubbing the shell
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Embodiment 1
[0049] A pin tight shaft impeller in this embodiment includes blades, a nose cone 106 and a blind hole 102 arranged at the tail section of the impeller 1, the axis of the blind hole 102 coincides with the axis of the impeller 1, and the tail section of the impeller 1 is evenly opened with Three narrow grooves 104, one end of the narrow groove 104 extends to the end of the impeller 1, and the other end is processed with a round hole with a diameter larger than the width of the narrow groove 104, the round hole is conducive to the compression deformation of the tail section of the impeller 1, making the assembly more convenient, higher efficiency. The narrow groove 104 provides a space for the tail section of the impeller 1 to be deformed under pressure, and limits the axial movement of the impeller 1 to the intake end during operation, thereby avoiding the risk of shell rubbing. Compared with the impeller 1 with threaded blind holes, the pin-tight shaft impeller of this embodim...
Embodiment 2
[0052] The basic structure of a pin-tight shaft impeller of this embodiment and the connection structure between the impeller and the turbine shaft is the same as that of embodiment 1, the difference is that four narrow grooves 104 are evenly opened on the tail section of the impeller 1, and the impeller 1 The material is aluminum alloy, and two pairs of parallel surfaces 203 are processed on the shaft end 202 of the turbine shaft 2 .
Embodiment 3
[0054] The basic structure of a pin-tight shaft impeller of this embodiment and the connection structure between the impeller and the turbine shaft is the same as that of embodiment 1, the difference is that six narrow grooves 104 are evenly opened in the tail section of the impeller 1, and the impeller 1 The material is aluminum alloy, and three pairs of parallel surfaces 203 are processed on the shaft end 202 of the turbine shaft 2 .
[0055] When the intermediate rotor assembly assembly in the present invention is assembled, the impeller 1 is vertically pressed down so that the turbine shaft 2 enters the blind hole 102, because both the blind hole 102 and the shaft end 202 of the turbine shaft 2 are provided with chamfers, so the turbine The shaft 2 can easily enter the blind hole 102, and plastically deform the material in the blind hole 102; at this time, the tail section of the impeller 1 enters the inner cavity 701 of the thrust sleeve 7, is squeezed and deformed, and sn...
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