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A three-swirl classifying cyclone and its combustion chamber

The technology of swirl classification and swirl device is applied in the field of combustion chamber, which can solve the problems of complex engine structure and fuel supply system, reduce coking of main combustion stage fuel nozzles, and high weight, so as to achieve weight reduction, prevent premature coking, and reduce fuel consumption. System simple effect

Active Publication Date: 2022-03-29
JIANGSU UNIV OF SCI & TECH
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  • Abstract
  • Description
  • Claims
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AI Technical Summary

Problems solved by technology

[0008] Purpose of the invention: The purpose of the present invention is to provide a three-swirl graded cyclone and its combustion chamber. The present invention not only achieves low-pollution combustion chambers and reduces pollutant emissions through the special structural design and arrangement of the cyclone It also simplifies the main fuel supply system of the three-stage swirl combustor, reduces the possibility of coking of the main fuel nozzle, and solves the problem of excessive weight caused by the complexity of the existing engine structure and fuel supply system

Method used

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  • A three-swirl classifying cyclone and its combustion chamber
  • A three-swirl classifying cyclone and its combustion chamber
  • A three-swirl classifying cyclone and its combustion chamber

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Embodiment Construction

[0027] The present invention will be further described below in conjunction with accompanying drawing and embodiment:

[0028] Such as figure 1 and figure 2 As shown, a three-swirl classifying cyclone of the present invention integrates the pre-combustion level obliquely cut hole type cyclone, the main combustion level obliquely cut hole type cyclone and the main combustion level radial cyclone, which includes a shaft To the connecting piece 1 and the radial connecting piece 2, the center of the axial connecting piece 1 is provided with an axial through hole 11, and the radial connecting piece 2 includes a coaxial first venturi tube 21 and a second venturi tube arranged at intervals 22. In the annular space between the first venturi tube 21 and the second venturi tube 22, multiple groups of blades 23 arranged in an annular array are fixedly connected. The installation angle of the blades 23 is between 30 and 45 degrees. The number of blades 23 is 9 Up to 16 groups, the inst...

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Abstract

The invention discloses a three-swirl classifying swirler and its combustion chamber, wherein the swirler includes an axial connecting piece and a radial connecting piece, the center of the axial connecting piece is provided with an axial through hole, the The radial connector includes coaxial first venturi tubes and second venturi tubes arranged at intervals, and the annular space between the first venturi tubes and the second venturi tubes is fixedly connected in an annular array. For the blades provided, both ends of multiple sets of blades are fixedly connected to the first venturi tube and the second venturi tube, and the annular space is evenly divided into a plurality of relatively independent subspaces. Through the special structural design and layout of the swirler, the present invention not only achieves the goal of reducing the discharge of pollutants in the low-pollution combustion chamber, but also simplifies the fuel supply system of the main combustion stage of the combustion chamber and reduces the Possibility of coking.

Description

technical field [0001] The invention belongs to the technical field of combustion chambers, and in particular relates to a three-swirl classifying swirler and a combustion chamber thereof. Background technique [0002] As people pay more and more attention to the living environment and health, people also pay more attention to and strictly control various pollution sources that endanger their own health and damage the environment. Although aeroengines and industrial gas turbines account for a small proportion of the total amount of combustion pollutant emissions, due to their local characteristics, such as near airports and places where industrial gas turbines are used, high concentrations of pollutant emissions will gather. In the air, polluting emissions from all types of aircraft are the only source of high-altitude air pollutants. As a result, emissions from gas turbines, including aero engines and various industrial gas turbines, are increasingly restricted. [0003] ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F23R3/30
CPCF23R3/30
Inventor 肖建昆李明玉
Owner JIANGSU UNIV OF SCI & TECH
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