Unlock instant, AI-driven research and patent intelligence for your innovation.

Combustion instability active inhibition method based on autoregressive moving average model

A self-regressive sliding, combustion unstable technology, applied in the combustion method, burner, control combustion and other directions, can solve the problems of unstable combustion, oscillating combustion of the combustion system, not considering the actual feedback of pressure pulsation, etc.

Inactive Publication Date: 2020-08-28
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
View PDF5 Cites 3 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When the pressure and equivalence ratio pulsation meet certain conditions, the strong coupling process will lead to serious oscillating combustion in the combustion system
[0006] At present, there have been certain research results on the suppression of unstable combustion abroad, and passive and active suppression methods for unstable combustion have been developed. The typical passive control method is to use structures such as Helmholtz resonators and quarter-wavelength tubes. To suppress unstable pressure pulsation, but in the process of its engineering, it faces the disadvantages of fixed pressure pulsation frequency and small controllable range.
An active control method is to apply a disturbance pressure signal to the combustion system during the combustion process. This control method does not consider the actual feedback of the pressure pulsation after the combustion system is controlled. It is an open-loop control

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Combustion instability active inhibition method based on autoregressive moving average model
  • Combustion instability active inhibition method based on autoregressive moving average model
  • Combustion instability active inhibition method based on autoregressive moving average model

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0049] In order to make the object, technical solution and effect of the present invention clearer and clearer, the following examples are given to further describe the present invention in detail. It should be pointed out that the specific implementations described here are only used to explain the present invention, not to limit the present invention.

[0050] The purpose of the present invention is to propose an adaptive active suppression method to suppress combustion instability, combustion instability control system such as figure 1 shown. The combustion system can be the combustion chamber of the engine or the combustion furnace, etc. figure 1 The combustion chamber in the middle represents the combustion system. Usually, the combustion system requires inlet air and fuel supply. The fuel supply is realized by the fuel pump. The control system suppresses combustion instability according to the output control fuel signal and pressure sampling signal. The method of the p...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention provides a combustion instability self-adaptive closed-loop active control method, and belongs to the field of combustion. The method comprises the following steps that firstly, online identification is carried out on a system through a fuel oil flow supply flow signal and a dynamic pressure signal by using recursive least square algorithm; and indirect self-correction active controlis carried out by using minimum variance, the fuel oil flow at each moment is decided, so that the combustion pulsation pressure is controlled. The invention relates to the self-adaptive closed-loopactive control method, the method comprises the following steps that a current control signal and a combustion pressure pulsation feedback signal after control are comprehensively considered in a control process, structural parameters of the system are continuously updated, and variance of combustion pressure pulsation is taken as a target function, and a control signal, namely fuel flow, of the system is given under the condition of ensuring that the variance of the pressure pulsation is minimum.

Description

technical field [0001] The invention belongs to the field of combustion, and relates to a method for actively suppressing combustion instability based on an autoregressive moving average model (CARMA) with a control quantity. Background technique [0002] Unstable combustion in the combustion system is manifested as a large pressure pulsation during combustion, which not only has an adverse effect on the hardware structure of the combustion system, but also greatly increases the capital investment and development cycle of the equipment. [0003] In recent years, the international attention to environmental pollution has increased, and the development of low-pollution combustion technology is imminent. A low-pollution combustion technology that is prevalent at present—lean oil premixed combustion technology, has shown good characteristics of low pollution emissions. However, due to the use of lean fuel combustion technology, the combustion is more sensitive to the pulsation ...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): F23D11/46F23N5/00F23N1/00G06F17/18
CPCF23D11/46F23N1/00F23N5/00G06F17/18
Inventor 田泽民刘云鹏颜应文刘勇李井华
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS