Long-service-life composite bearing for combustion gas turbine

A technology of composite bearings and gas turbines, which is applied in the direction of rotating combined bearings, bearings, bearing components, etc., can solve the problems of unfavorable lubricating oil film formation, shortening the service life of bearings, vibration and noise, etc., achieve a wide and stable working range, and improve bearing load capacity ability, the effect of reducing the starting power

Pending Publication Date: 2018-06-29
HARBIN GUANGHAN GAS TURBINE
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  • Summary
  • Abstract
  • Description
  • Claims
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AI Technical Summary

Problems solved by technology

[0002] Due to the influence of changing working conditions, the ball bearings for gas turbines have large fluctuations in the axial load they bear within a certain range, which is not conducive to the safe operation of the bearings, and the large-scale fluctuations in the axial force are likely to cause a series of vibrations and noises The problem is that it is not conducive to the safe formation of the roller lubricating oil film in the ball bearing, it is not conducive to ensuring the gap between the roller and the i

Method used

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  • Long-service-life composite bearing for combustion gas turbine

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Embodiment Construction

[0009] refer to figure 1 , a long-life composite bearing for a gas turbine, comprising a ball bearing 7 and a thrust bearing, the thrust bearing comprising a thrust bearing pad 11 and a thrust bearing disk 10 installed on a thrust bearing housing 1, the average thickness of the oil film of the thrust bearing passing through the first An adjusting ring 2 is adjusted to adjust the working load of the thrust bearing; the ball bearing 7 is installed on the ball bearing seat 3, and the ball bearing seat 3 is provided with a main elastic ring 9 and an auxiliary elastic ring 6, and the ball bearing 7 and the main elastic ring 9 cooperates with the auxiliary elastic ring 6, and the pre-deformation of the main elastic ring 9 and the auxiliary elastic ring 6 is adjusted and fixed through the second adjustment ring 5 and the stop ring 4, so as to adjust the maximum working load borne by the ball bearing 7, that is, to stabilize Working load; the safety clearance of the ball bearing seat 3 o

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Abstract

The invention belongs to the technical field of combustion gas turbine equipment and particularly relates to a long-service-life composite bearing for a combustion gas turbine. The long-service-life composite bearing comprises a ball bearing and a thrust bearing. The thrust bearing comprises a thrust bearing bush and a thrust bearing disc, wherein the thrust bearing bush and the thrust bearing disc are mounted on a thrust bearing seat. The mean thickness of an oil film of the thrust bearing is adjusted through a first adjustment ring. The ball bearing is mounted on a ball bearing seat. The ball bearing is matched with a main elastic ring and a subsidiary elastic ring. The matching predeformation amount of the main elastic ring and the subsidiary elastic ring is adjusted and fixed through asecond adjustment ring and a check ring. The safety clearance between the thrust bearing disc and the ball bearing seat is set through a third adjustment ring. The ball bearing and the axial thrust bearing are fixed to the end face of a same flange. Compared with a common ball bearing, the maximum bearing capacity of the ball bearing can be set by designing the main elastic ring and the subsidiary elastic ring; and when the bearing load exceeds a set value, the remaining load can be borne by the thrust bearing, so that the service life of the ball bearing is greatly prolonged.

Description

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Claims

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Application Information

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Owner HARBIN GUANGHAN GAS TURBINE
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