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Large-sized turbine generator shaft bushing and method for machining bore of shaft bushing

A technology for turbogenerators and processing methods, which is applied to shafts and bearings, bearing components, mechanical equipment, etc., and can solve the problems of clamping and fixing errors of bearing bushes, extremely high requirements for symmetry and perpendicularity between the joint surface and the reference plane, etc. , to achieve the effect of reducing the requirements for level and verticality and improving efficiency

Active Publication Date: 2008-10-01
上海电气集团上海电机厂有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the prior art, the upper and lower bearing bushes are processed separately, which requires a special car mold for processing. The car model must have high precision to ensure the eccentric value, and there will be large errors in the clamping and fixing of the bearing bushes. The symmetry and perpendicularity between the surface and the reference plane are extremely demanding, so how to process the inner hole of the bearing bush has become a subject of intensive research by the industry.

Method used

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  • Large-sized turbine generator shaft bushing and method for machining bore of shaft bushing
  • Large-sized turbine generator shaft bushing and method for machining bore of shaft bushing
  • Large-sized turbine generator shaft bushing and method for machining bore of shaft bushing

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Embodiment Construction

[0020] see figure 1 and figure 2 , a spherical bearing for a large steam turbine generator according to the present invention, comprising an upper bearing 1 and a lower bearing 2, an arc-shaped oil wedge 22 is arranged at the center of the inner surface of the lower bearing 2, the upper bearing 1 and the lower The inner holes of the bearing bush 2 are all eccentric circles with a diameter of a, the center of the inner semicircle of the upper bearing bush 1 is δ from the joint surface 11, the center of the inner semicircle of the lower bearing bush 2 is η from the joint surface 21, and the center of the oil wedge 22 is It is located on the joint surface 21 of the lower valve bearing bush 2, and its surface diameter is b, and its arc length is d, wherein a>b, η>δ, a-b>η, η>(a-b) / 2.

[0021] see again Figure 3 to Figure 6 , a method for machining the inner hole of a large turbogenerator spherical bearing bush of the present invention, comprising the following steps:

[0022]...

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Abstract

The invention discloses a large size turbo generator bush and a bore processing method, wherein the bore of the upper and the lower bush has an eccentric circle with the diameter a, the center distance of the inner semicircle of the upper bush has a distance delta from the joint surface, the center distance of the inner semicircle of the lower bush has a distance eta from the joint surface. The center of the oil wedge is arranged on the joint surface of the lower bush and the superficial diameter is b. The bore process of the bush has the following steps: processing the base level of the upper and the lower bush; revising the verticality of the joint surface of the upper and the lower bushes and the base level; assembling the upper and the lower bushes, using the center of the joint surface as the centre of a circle and processing the inner bore of the bush with the diameter b; disconnecting the upper and the lower bushes, underlaying a pad with the thickness delta plus eta between the joint surface, then assembling the upper and the lower bushes; finding out the symmetric center O, then adjusting the eccentricity and finding our the processing center O', at last processing the bush inner circle with the center O' as the processing center.

Description

technical field [0001] The invention relates to a processing method for a bearing bush of a generator, in particular to a method for processing an inner hole of a bearing bush of a steam turbine generator. technical background [0002] The 390KW gas turbine generator is an F-class heavy-duty gas turbine generator with the most advanced technology in the world today. Under the same power generation, the carbon dioxide gas emission of the F-class gas turbine GTCC combined cycle system is about 42% of that of a coal-fired power plant. Nitrogen oxide emissions are less than 20% of coal-fired power plants, emissions of sulfur dioxide gas and ash are equivalent to 1% to 3% of coal-fired units with the same power generation, and water consumption is equivalent to 33% of coal-fired units with the same power generation. The plant covers an area equivalent to 54% of the coal-fired units with the same power generation capacity, so it has the characteristics of less pollution and less r...

Claims

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Application Information

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IPC IPC(8): F16C23/04F16C33/10F16C33/14
Inventor 赵钰姮柯益昌
Owner 上海电气集团上海电机厂有限公司
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