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Vertical streamline tunnel wheel gas turbine

A gas turbine and streamline technology, which is applied in gas turbine devices, liquid fuel engines, mechanical equipment, etc., can solve the problems of reducing structural strength and power consumption, and achieve the effects of improving stability, reducing losses, and reducing axial loads

Inactive Publication Date: 2020-12-18
萍乡北京理工大学高新技术研究院
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] Horizontal gas turbine support bearings are usually oil film bearings or rolling bearings, the mechanism for delivering lubricating oil needs to consume a certain amount of power, and the opened oil passage will also reduce the structural strength

Method used

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  • Vertical streamline tunnel wheel gas turbine
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Examples

Experimental program
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Effect test

Embodiment 1

[0023] Such as figure 1 As shown, a vertical streamlined tunnel gas turbine includes a compressor 1, a gas turbine 2, a shaft 3, and a combustion chamber 4; the compressor 1 and the gas turbine 2 are respectively installed at the upper and lower ends of the shaft 3 to form a gas turbine The rotor; the combustion chamber 4 is located between the compressor 1 and the gas turbine 2; the shaft 3 is placed vertically to form a vertical structure.

[0024] In order to make the compressor 1 have a reasonable layout, further, the compressor 1 can be arranged in a single stage or in multiple stages, and in case of multiple stages, multiple streamline tunnel compressor wheels 5 are installed on the shaft 3 in sequence.

[0025] In order to make the gas turbine 2 have a reasonable arrangement, further, the gas turbine 2 can be arranged in a single stage or multi-stage, and in case of multi-stage, multiple streamline tunnel turbines 6 are installed on the shaft 3 in sequence.

[0026] In...

Embodiment 2

[0030] Such as figure 2 As shown, with respect to Embodiment 1, in this embodiment, the vertical streamline tunnel gas turbine also includes a regenerator 9 installed downstream of the outlet of the streamline tunnel turbine 6, and the regenerator 9 utilizes the heat of exhaust gas after the turbine to The incoming air is heated, and the preheated air is combusted in the combustor 4 with the fuel ejected from the fuel nozzle 10, thereby improving the efficiency of the gas turbine; the regenerator 9 has various arrangements, including but not limited to as figure 2 structure shown.

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Abstract

The invention discloses a vertical streamline tunnel wheel gas turbine, and belongs to the field of gas turbines. The vertical streamline tunnel wheel gas turbine comprises a gas compressor, a combustion turbine, a shaft and a combustion chamber, wherein the gas compressor and the combustion turbine are installed at the upper end and the lower end of the shaft to form a gas turbine rotor, the combustion chamber is located between the gas compressor and the combustion turbine, and the shaft is vertically arranged to form a vertical structure. The vertical streamline tunnel wheel gas turbine adopts streamline tunnel turbines and gas compressor wheels, is mounted in a vertical structure in cooperation with an external contour type air bearing, and can achieve the beneficial effects of improving the rotating speed, improving the reliability, reducing the leakage loss, reducing the size and the weight and the like.

Description

technical field [0001] The invention relates to the field of gas turbines, in particular to a vertical streamlined tunnel wheel gas turbine. Background technique [0002] Gas turbines can convert the energy of fuel into mechanical energy and directly output rotational motion. They are often used in generators, ship power, aviation power, etc. Its working process is that the compressor continuously compresses air and sends it into the combustion chamber, and the high-temperature gas formed after being mixed with fuel flows into the turbine to expand and do work, driving the turbine and driving the coaxial compressor to rotate. [0003] Traditional open and semi-open blade structure impellers have tip clearances, and the number and thickness of blades are limited by the level of material technology and there is no room for optimization, which limits the further improvement of the aerodynamic performance of turbines and compressors. At the same time, the tip clearance leakage ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C3/08F02C3/14F01D5/04F01D25/00F04D29/28F04D29/02F02C7/06F02C7/08F01D25/04
CPCF01D5/04F01D25/005F01D25/04F02C3/085F02C3/14F02C7/06F02C7/08F04D29/023F04D29/284F05D2300/20
Inventor 黄若郭文杰高泽黄仕豪
Owner 萍乡北京理工大学高新技术研究院
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