Novel minisize gas turbine

A micro gas turbine, a new type of technology, applied in the direction of gas turbine devices, mechanical equipment, engine components, etc., can solve the problems of reliability, service life reduction, maintainability reduction, etc., and achieve long service life, high reliability and low processing cost Effect

Inactive Publication Date: 2014-12-17
XIAN TONGLING POWER
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This method is a commonly used overall structural scheme in single-axis rotary power machinery, but it has the following disadvantages: due to the distribution of combustion chambers, the main shaft and bearings are in a high-temperature environment, which greatly reduces the reliability and service life of the whole machine Or face a severe test; maintainability is also greatly reduced

Method used

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  • Novel minisize gas turbine
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Examples

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Embodiment Construction

[0023] The present invention will be described in detail below in conjunction with the accompanying drawings.

[0024] Such as figure 1 As shown, the present invention includes a compressor, a turbine and a combustor, the combustor is connected separately with the impeller and the main shaft of the compressor; the impeller and the main shaft are connected through a central tie rod; body join. The air outlet of the compressor is connected with the air inlet of the combustion chamber through a pipeline. The impeller of the compressor and the turbine adopt a back-to-back mode, and are connected and driven through end teeth. The turbine is preferably centripetal; the compressor impeller is preferably centrifugal, and the outer diameter of the compressor impeller is not more than 215.7mm±2mmmm.

[0025] Such as figure 2 , 3 As shown, the present invention is a novel micro gas turbine, the main shaft is fixed by two bearings, the span between the two bearings is 205mm±2mm, and...

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Abstract

A disclosed novel minisize gas turbine comprises a gas compressor, a turbine and a combustion chamber; the combustion chamber is connected with an impeller and a main-shaft divided body; the impeller is connected with a main shaft via a center pull rod; and the combustion chamber is connected with the impeller and the main-shaft divided body via pipes. A 2-0-0 supporting manner is adopted in the overall structure. The gas compressor and the turbine both employ an overhung cantilever end which easily generates relatively large vibration amplitude during working. The axial-direction pre-tightening pulling force generated through cooperation of a locking nut and a turbine pull rod shaft is capable of directly improving the positive pressure of a combination surface of the end tooth, thereby improving the coulomb frictional force between contact surfaces, and further improving the radial rigidity of the shafting overhung cantilever end, so that the radial vibration amplitude of the shafting overhung cantilever end, and also asynchronous radial vibration is avoided between the gas compressor impeller and the turbine. The provided overall structure project has the advantages of simple structure, low processing cost, compact structure and high transmission efficiency.

Description

technical field [0001] The invention relates to gas turbine technology, in particular to a novel micro gas turbine with a shaft power output of 245kW±55kW. Background technique [0002] The micro gas turbine has a series of advanced technical features such as multiple integrated capacity expansion, multiple fuels, low fuel consumption rate, low noise, low emission, low vibration, low maintenance rate, remote control and diagnosis, etc. In addition to distributed power generation, it can also be used for backup Power stations, combined heat and power generation, grid-connected power generation, peak load power generation, etc., are the best way to provide clean, reliable, high-quality, multi-purpose, small-scale distributed power generation and combined heat and power supply, whether for central cities or remote rural areas or even remote areas Both are applicable. [0003] The micro gas turbine is a ground distributed energy power system that my country has focused on resea...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C3/04F02C3/14F02C7/06
Inventor 刘广勤
Owner XIAN TONGLING POWER
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