Method for machining turbine rotor with special-shaped center hole

A processing method and technology of turbine rotors, which are applied to the supporting elements of blades, engine elements, machines/engines, etc., can solve problems such as different forces on the center holes at both ends, production limitations, and floating value of the outer circle of the turbine shaft. Improve the dimensional and geometric tolerances of each file, and the effect of strong reliability

Inactive Publication Date: 2020-01-03
CHONGQING JIANGJIN SHIPBUILDING IND
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, due to the needs of assembly and disassembly, the special-shaped central hole at the turbine end and tail of the turbine disc in the turbine rotor adopts a hexagonal inner hole. After long-term tracking and investigation, it is found that during the grinding process, the carbide tip will contact the inner hexagonal hole at the central hole. The sharp edges of the hexagon rub against each other to varying degrees, resulting in fluctuations in the runout value of the outer circle of each gear of the processed turbine shaft, and the circle runout is even as high as 0.1 or more; from a structural point of view, it is impossible to cancel the inner hexagon, or p

Method used

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  • Method for machining turbine rotor with special-shaped center hole
  • Method for machining turbine rotor with special-shaped center hole
  • Method for machining turbine rotor with special-shaped center hole

Examples

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Example Embodiment

[0082] Such as Figure 1 to Figure 14 As shown, a method for processing a turbine rotor with a special-shaped central hole, the method includes the following steps:

[0083] Step 10 solder one

[0084] Take the turbine disc 2, the optical axis of the turbine shaft 1, and after cleaning, weld the compressor end 4 of the turbine disc to the optical axis of the turbine shaft 1. The center hole of the turbine end 3 of the turbine disc is provided with a special-shaped central hole 7;

[0085] Specific processing method: Clean the turbine disc and turbine optical axis with acetone. The welding plane must be free of rust, grease and debris. Weld according to the welding parameters. The beating of the turbine optical axis to the turbine disc shall not exceed 4mm (referring to 29.8 at the outer circle).

[0086] Step 20: Perform the first heat treatment on the welded workpiece;

[0087] Carry out heat treatment according to the company's technical standards and inspect mechanical properties. ...

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Abstract

The invention discloses a method for machining a turbine rotor with a special-shaped center hole. The method for machining the turbine rotor with the special-shaped center hole comprises the followingsteps that a turbine disk and a turbine shaft are welded; heat treatment is conducted; a center hole is drilled, and the turbine disk outer circle and end face margin are removed; semi-finish turningis conducted on end faces of the turbine end of the turbine disk and the special-shaped center hole; turning is conducted on a technological choke plug; semi-finish turning is conducted on end facesof the air-compressing end the turbine disk and the outer circle and end faces of the turbine shaft and the outer circle; a turbine shaft inner hole is drilled; turning is conducted on a turbine shafttool withdrawal groove, chamfering and a shaft stair inner hole; heat treatment is conducted; the technological choke plug and the turbine disk are welded and fixed; the center hole is turned in thetechnological choke plug, and two end faces of the big outer circle of the turbine disk are turned; the big outer circle of the turbine disk and the outer circle M of the turbine shaft are ground; a turbine shaft threaded hole, a stair inner hole and taper are turned, and tapping is conducted; the big outer circle of the turbine disk and end faces, the outer circle of the turbine shaft and end faces, the small outer circle of the turbine disk and the turbine disk D face are ground; an air-sealing groove is turned; and the technological choke plug is removed.

Description

technical field [0001] The invention relates to the technical field of turbine rotor machining, in particular to a machining method of a turbine rotor with a special-shaped center hole. Background technique [0002] The turbine rotor is the main rotating component inside the turbocharger. The turbine rotor uses the steam generated by the heat recovery system to push the turbine blades to work through compression, and the turbine rotor is the most important rotating part that provides power in the entire system. [0003] The supercharger is installed on the exhaust side of the engine, so the working temperature of the supercharger is very high, and the speed of the rotor is very high when the supercharger is working, which can reach hundreds of thousands of revolutions per minute, so the unbalance of the turbine rotor must be very small. In this way, the requirements for the grinding run-out value during the machining process of the turbine rotor are very small. From the pe...

Claims

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Application Information

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IPC IPC(8): B23P15/00F01D5/02
CPCB23P15/00F01D5/02
Inventor 李成科袁华柯益段然杨川华周开松杨意松
Owner CHONGQING JIANGJIN SHIPBUILDING IND
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