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Sliding arc plasma combustion-supporting exciter without relying on external gas supply of combustion chamber

A technology of plasma and sliding arc, which is applied in the direction of plasma, gas turbine devices, electrical components, etc., can solve problems such as differences in external shape and structural features, and achieve the effects of small size, strong versatility, and enhanced stability

Active Publication Date: 2020-01-17
AIR FORCE UNIV PLA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In summary, the plasma igniter and the plasma combustion actuator are two different combustion chamber devices. The application background and working principle of the two are different, which also leads to differences in the external shape and structural characteristics of the two.

Method used

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  • Sliding arc plasma combustion-supporting exciter without relying on external gas supply of combustion chamber
  • Sliding arc plasma combustion-supporting exciter without relying on external gas supply of combustion chamber
  • Sliding arc plasma combustion-supporting exciter without relying on external gas supply of combustion chamber

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Embodiment Construction

[0048] This embodiment is a sliding-arc plasma combustion-supporting exciter that does not rely on the external gas supply of the combustion chamber, including an anode sleeve 1 , an outer ring cavity sleeve 2 , an electrode mounting seat 3 , a cathode electrode rod 4 and a cathode cone 5 . Wherein, the electrode mounting seat 3 is installed in the anode casing 1 through threads, and is positioned by a positioning step at the upper end of the electrode mounting seat. One end of the cathode electrode rod 4 passes through the central hole of the electrode mounting base, and is threadedly connected with the cathode cone 5 located on the lower end face of the electrode mounting base. The outer ring cavity cover 2 is installed between the radial two-layer annular bosses on the outer circumferential surface of the anode sleeve 1, and the inner circumferential surface of the outer ring cavity cover and the outer circumferential surface of the anode sleeve An outer ring cavity 8 is fo...

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Abstract

The invention relates to a sliding arc plasma combustion-supporting exciter without relying on external gas supply of a combustion chamber. An electrode mounting seat is installed in an anode casing pipe; and an inner annular cavity is formed between the outer surface of a cathode cone connecting section at the lower end of the electrode mounting seat and the inner surface of the anode casing pipe. One end of a cathode electrode rod penetrates through the electrode mounting seat to be connected with a cathode cone. An outer annular cavity is formed between the inner circumferential surface ofan outer ring cavity sleeve and the outer circumferential surface of the anode casing pipe. The outer ring cavity is in communication with the inner ring cavity through inner layer air inlet holes located in the anode casing pipe. The inner layer air inlet holes are axially distributed in the pipe body of the anode casing pipe. According to the sliding arc plasma combustion-supporting exciter, two-strand channel gas of the combustion chamber serves as a working medium gas, the technical bottleneck that an existing plasma combustion-supporting technology is not good for improving the performance of the combustion chamber is broken through, and the sliding arc plasma combustion-supporting exciter has the characteristics of being simple in structure, suitable for conversion and application inthe field of combustion of aviation engines and strong in universality.

Description

technical field [0001] The invention relates to plasma combustion-supporting technology in the field of aerodynamics, in particular to a sliding-arc plasma combustion-supporting exciter for an aeroengine combustion chamber that does not depend on the external air supply of the combustion chamber. Background technique [0002] Plasma combustion-supporting technology is one of the effective means to improve the performance of aero-engine combustors. It can enhance the stability of combustion, broaden the stable combustion range of the combustor, improve the combustion efficiency of the aero-engine combustor, and also improve the outlet of the combustor Uniformity has been widely concerned by experts at home and abroad in recent years. [0003] As an important form of plasma generation, sliding arc discharge has unique and significant advantages in enhancing combustion reactions. The application of the sliding arc plasma burner in the field of aero-engine combustion is not onl...

Claims

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Application Information

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IPC IPC(8): F02C7/264H05H1/48
CPCF02C7/264H05H1/48F05D2240/35Y02T10/12
Inventor 陈一费力何立明邓俊雷健平陈高成赵子晨代胜吉
Owner AIR FORCE UNIV PLA
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