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Modular testing device for cyclone combustion thermo-acoustic oscillation characteristic research

A test device and thermoacoustic oscillation technology, which is applied in the field of modular test devices for the study of swirling combustion thermoacoustic oscillation characteristics, can solve the problems of limited test parameter range and single function, and save test preparation period and test cost Effect

Pending Publication Date: 2018-08-17
HUNAN AIRTOPS INTELLIGENT TECH CO LTD
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The purpose of the present invention is to provide a swirl combustion thermoacoustic oscillation test device for overcoming the problems of single function, limited range of test parameters, and risk of backfire of premixed fuel in the existing technology. A modular test device for characteristic research, which can simulate the flow field characteristics of swirling combustion and the thermoacoustic oscillation characteristics of swirling combustion under premixed combustion state, diffusion combustion state and mixed combustion state, and can effectively prevent flame back propagation. Modular design, the main functional components can be replaced, and the test parameters, sound field conditions, and injection positions can be flexibly adjusted

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  • Modular testing device for cyclone combustion thermo-acoustic oscillation characteristic research
  • Modular testing device for cyclone combustion thermo-acoustic oscillation characteristic research
  • Modular testing device for cyclone combustion thermo-acoustic oscillation characteristic research

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Embodiment Construction

[0067] The specific embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings. It should be understood that the specific embodiments described here are only used to illustrate and explain the present invention, and the protection scope of the present invention is not limited to the following specific embodiments. .

[0068] figure 1 It is a schematic diagram of the appearance of an embodiment of the test device of the present invention. The main part of the test device is installed vertically, including speaker section 5, air chamber section 1, swirler section 4, window combustion section 3, and combustion chamber extension section 2 from bottom to top. The sections are connected by flanges for easy loading and unloading. Each part of each section can be provided with installation holes in advance, and monitoring devices such as temperature measurement and pressure measurement can be arranged to obtain internal flow ...

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Abstract

The invention relates to the field of aero-engine and gas turbine basic combustion test research, and discloses a modular testing device for cyclone combustion thermo-acoustic oscillation characteristic research. The device is composed of a loudspeaker section, an air plenum chamber section, a cyclone section, a windowing combustion section and a combustion chamber lengthening section from bottomto top. After air flows through an air supply pipeline to enter a plenum chamber, through the excitation effect of a loudspeaker, after the air flows through an axial flow type cyclone, a needed soundfield environment and a needed cyclone flow field environment can be obtained. Fuel jetting at different positions can be achieved through three paths of fuel supply pipelines, and premixed combustion, diffusive combustion, the mixed mode of premixed combustion and diffusive combustion and other cyclone combustion flow field characteristics are obtained. Modular design is adopted for the testingdevice, the main functional parts can be detached and replaced, testing working condition parameters, sound field conditions and jetting positions can be flexibly adjusted, and flame passback can be avoided. A rectangular four-face windowing combustion chamber can be compatible with various kinds of advanced optical equipment, and combustion diagnosis data can be measured and obtained.

Description

technical field [0001] The invention relates to the research field of basic combustion tests of aero-engines and gas turbines, in particular to a modular test device for the research of swirl combustion thermoacoustic oscillation characteristics. Background technique [0002] At present, the world is facing increasingly serious environmental degradation problems, and countries around the world have reached a high degree of consensus on the concept of pollution source governance. Human beings' excessive consumption of fossil energy is an important reason for the current environmental pollution. Diffusion combustion is widely used in the current energy utilization field, which produces thermal nitrogen oxides (NO X ) is one of the main sources. With the increasingly stringent emission standards of gas turbines and aero engines, the huge market demand promotes the rapid development of advanced low-emission combustion organization technology. The three low-pollution combustio...

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Application Information

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IPC IPC(8): G01M15/14G01M10/00
CPCG01M10/00G01M15/14
Inventor 罗世彬
Owner HUNAN AIRTOPS INTELLIGENT TECH CO LTD
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