Turbine blade of gas turbine

Abstract

The invention discloses a turbine blade of the gas turbine. The turbine blade comprises an outer frame, a gripper frame is arranged in the outer frame, a first threaded box is arranged in the gripperframe, a first rotating shaft is fixedly connected to the left end wall of the first threaded box, a first motor is arranged in the gripper frame, the extending part of the left end of the first rotating shaft is in power connection with the first motor, a first screw rod is in threaded connection with the first threaded box, a gripper cavity is arranged on the right side of the first threaded box, a second rotating shaft which is vertically symmetrical is arranged on the front end wall and the rear end wall in a rotating mode in the gripper cavity, the second rotating shaft is fixedly connected with first straight gears, a first rack is meshed between the first straight gears, the left end of the first rack is fixedly connected with the first screw rod, a clamping disc is rotationally arranged in the left side of the gripper frame, a rack cavity is formed in the left end of the gripper frame, a second rack is arranged in the rack cavity in a sliding manner, the second rack is fixedlyconnected with the clamping disc.

Description

technical field [0001] The invention relates to the field of maintenance of turbine blades of a gas turbine, in particular to a turbine blade of a gas turbine. Background technique [0002] As the most widely used power unit in factories and military at present, gas turbine plays a very important role, and the turbine blade inside the gas turbine plays an important role as one of its most important components, but most gas turbines exist after long-term use. Detailed rust will affect the use. In view of the above situation, the current rust removal method on the market is friction rust removal. This method has great instability for turbine blades with high precision requirements. Improvements are made to address the above problems. Contents of the invention [0003] Aiming at the deficiencies of the above technologies, the present invention proposes a turbine blade of a gas turbine. [0004] A turbine blade of a gas turbine according to the present invention comprises an ...

AI Technical Summary

Problems solved by technology

[0002] As the most widely used power unit in factories and military at present, gas turbine plays a very important role, and the turbine blade inside the gas turbine plays an important role as one of its most important components, but most gas turbines exist after long-term use. Detailed rust will affect the use. In view of the above situation, the current rust removal method on the market is friction rust removal. This method has great instability for turbine blades with high precision requirements. Improvements are made to address the above problems

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