Runoff type supercharger turbine rotating shaft structure and molding process thereof

A turbocharger turbine and shaft structure technology, which is applied in the direction of machines/engines, blade support components, engine components, etc., can solve the difficult problems of reliable connection of turbocharger turbine shafts, so as to improve the allowable operating speed, reliable Connection, the effect of improving the connection rigidity

Inactive Publication Date: 2017-07-28
CHINA NORTH ENGINE INST TIANJIN
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, when the turbocharger turbine is made of new materials such as ceramics and titanium-aluminum alloys, it is difficult to use friction welding or electron beam welding to achieve reliable connection of the turbocharger turbine shaft

Method used

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  • Runoff type supercharger turbine rotating shaft structure and molding process thereof
  • Runoff type supercharger turbine rotating shaft structure and molding process thereof
  • Runoff type supercharger turbine rotating shaft structure and molding process thereof

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Embodiment Construction

[0028] A radial supercharger turbine shaft structure, including a turbine 1, a shaft 2 and a self-locking ring 3, such as figure 1 As shown, one end of the turbine 1 connected to the rotating shaft 2 is provided with a turbine internal thread blind hole 4, and the bottom of the turbine internal thread blind hole 4 is provided with a process ring groove, and the thread of the internal thread blind hole 4 of the turbine 1 The direction of rotation is opposite to the direction of rotation when the turbine shaft works; a section of turbine light hole 5 is provided between the end surface of the turbine 1 close to the shaft 2 and the blind hole 4 of the internal thread of the turbine, and the turbine light hole 5 is provided with a hole for assembling The turbine ring groove 6 of the lock ring 3, the diameter of the turbine light hole 5 is larger than the internal thread bottom diameter of the turbine internal thread blind hole 4, and the end surface of the turbine light hole 5 nea...

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Abstract

The invention relates to a turbine shaft structure of a radial supercharger and its forming process, including a turbine, a shaft and a self-locking ring. The turbine has internal threaded blind holes, light holes, ring grooves and guide chamfers. The shaft There are external threads, positioning shaft shoulders, optical shafts, and ring grooves. The self-locking ring is an elastic split ring and has guiding chamfers. By reasonably determining the structural dimensions of the turbine, shaft and self-locking ring, and processing the turbine, shaft and self-locking ring, and then assembling the turbine, shaft and self-locking ring together, a complete turbine shaft is formed. The invention can effectively solve the problem of turbine shaft connection when the turbocharger turbine adopts new materials such as ceramics and titanium-aluminum alloy, and can realize reliable connection of the turbocharger shaft, fully ensuring the connection strength and rigidity of the turbine shaft.

Description

technical field [0001] The invention belongs to the structural design field of a turbocharger, and in particular relates to a radial turbocharger turbine shaft structure and a forming process thereof. Background technique [0002] The turbocharger is one of the key components of the turbocharged engine, and the turbine shaft is the core component of the turbocharger, which is mainly connected by the turbine and the shaft. At present, the supercharger turbine is generally made of cast nickel-based superalloy K418 material (the material density is 8.0×10 3 kg / m 3 ), the shaft is made of 42CrMo alloy steel. For the turbocharger turbine made of K418 material and the shaft made of 42CrMo alloy steel, friction welding or electron beam welding technology can be used to realize the reliable connection between the turbine and the shaft to form the shaft of the turbine. However, due to the high density of the K418 alloy material, the moment of inertia of the turbine made of the K41...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F01D5/02B23P15/00
CPCF01D5/025B23P15/00
Inventor 王正王增全邢卫东王阿娜
Owner CHINA NORTH ENGINE INST TIANJIN
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