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A Hydrogen Combustor Based on Axial Vortex-to-column Mixing

A combustion chamber, axial technology, applied in the direction of combustion chamber, continuous combustion chamber, combustion method, etc., can solve the problem of complex structure of transverse jet micro-mixing combustion chamber, difficulty in burning high-concentration hydrogen and pure hydrogen, high design and test costs, etc. problem, to achieve the effect of increasing the combustion power per unit volume, fast processing speed and cheap geometric shape

Active Publication Date: 2022-05-31
INST OF ENGINEERING THERMOPHYSICS - CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The low-pollution combustion chamber modified based on this combustion technology can only burn part of the hydrogen, and it is difficult to burn high-concentration hydrogen and pure hydrogen
At the same time, the modified dry-low combustion chamber has a more complex structure, high design and test costs, and a large number of modifications to the combustion chamber will cause changes in the overall layout of the machine and increase research and development costs.
In addition, the existing pure hydrogen combustor adopts lean oil direct injection technology, which has high combustion temperature and high pollutant emissions; the structure of the transverse jet micro-mixing combustor is complicated, and the processing cost is high

Method used

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  • A Hydrogen Combustor Based on Axial Vortex-to-column Mixing
  • A Hydrogen Combustor Based on Axial Vortex-to-column Mixing
  • A Hydrogen Combustor Based on Axial Vortex-to-column Mixing

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Embodiment Construction

[0061] Hereinafter, embodiments of the present disclosure will be described with reference to the accompanying drawings. It should be understood, however, that these descriptions are exemplary only

[0062] The terminology used herein is for the purpose of describing particular embodiments only and is not intended to limit the present disclosure. use here

[0065] The present disclosure provides a blended hydrogen combustor based on an axial vortex row arrangement, as shown in FIGS. 1 to 3, comprising:

[0070] The above-mentioned trailing edge 62 includes at least one fuel hole 63. As shown in FIG. 9, the axis of the fuel hole 63 is parallel with the trailing edge 62.

[0072] The above-mentioned axial vortex generator 60 locally mixes the air axial vortex with the jet hydrogen fuel to realize diffusion combustion.

[0077] The above-mentioned circumferentially aligned arrangement enhances the blending effect, improves the combustion power per unit volume, and further reduces the...

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Abstract

The present disclosure provides a hydrogen combustor based on an axial vortex pairing arrangement, including: a flame tube, the flame tube includes an outer ring and an inner ring; an outer casing, and the outer ring of the flame tube encloses an air circulation outer channel ; The inner casing is fixedly connected to the inside of the outer casing, and the inner casing and the inner ring of the flame tube form an air circulation inner channel; at least two axial vortex generators, and the axial vortex generator is a tetrahedral cavity The axial vortex generators are fixedly connected to the outer ring and the inner ring of the flame tube respectively, and are suitable for providing axial vortex to make fuel mixed and burned. The hydrogen combustor based on the axial vortex arrangement in this disclosure for blending proposes a design scheme combining the axial vortex and the tiny tangential jet. The tetrahedral structure is used to generate the axial vortex for blending. Compared with the non-reflux zone and low-velocity zone, the combustion chamber of the recirculator can effectively burn pure hydrogen, and overcome the problems of flashback, self-ignition and combustion instability.

Description

A hybrid hydrogen combustion chamber based on axial vortex row arrangement technical field [0001] The present disclosure relates to the field of gas turbines, and in particular, to a hybrid hydrogen combustor based on an axial vortex in-line arrangement. Background technique As the international and domestic requirements for low-carbon and clean energy are gradually improved, the pressure of carbon emission is increasing day by day, and hydrogen is used as an energy source. As the representative of low-carbon and clean energy in the future, it is of strategic significance to study the conversion and utilization of hydrogen energy. Hydrogen is a low-carbon clean energy, Using gas turbine to burn hydrogen is a typical hydrogen energy utilization method. Compared with natural gas fuel, hydrogen flame spreads faster. It is extremely fast and the flame surface is more prone to wrinkling, thermoacoustic oscillation and tempering, which leads to the It is difficult to burn...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F23R3/28F23R3/36F23R3/42F23R3/58
CPCF23R3/36F23R3/58F23R3/286F23R3/42Y02E20/34
Inventor 杨旸余志健
Owner INST OF ENGINEERING THERMOPHYSICS - CHINESE ACAD OF SCI
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