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Combustion chamber of a micro gas turbine with double wall structure

A micro gas turbine and combustion chamber technology, which is applied in combustion chambers, continuous combustion chambers, combustion methods, etc., can solve the problems of low combustion efficiency, short gas residence time, and poor flame stability of micro combustion chambers, and achieve very high combustion efficiency and The effect of flame stability, temperature reduction, and heat dissipation loss reduction

Active Publication Date: 2019-08-02
BEIHANG UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, compared with the conventional combustion chamber, due to the influence of the scale effect, the micro combustion chamber faces the unfavorable factors of short gas residence time, high heat loss and incomplete combustion, which will make the combustion efficiency of the micro combustion chamber low and the flame stable poor sex

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  • Combustion chamber of a micro gas turbine with double wall structure

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Embodiment Construction

[0021] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0022] The combustor of a micro gas turbine with a double-wall structure described in this embodiment uses methane gas fuel. Such as figure 1 As shown, the combustion chamber is mainly composed of the combustion chamber outer casing 6, the flame cylinder outer ring 12, the flame cylinder inner ring 13, the combustion chamber casing 14, the ignition needle 5, the combustion chamber outlet outer casing 7 and the combustion chamber outlet inner casing 9 constitute. The outer ring 12 of the flame tube is made of porous sintered material, the inner ring 13 of the flame tube, the outer casing 7 of the combustion chamber outlet, and the inner casing 9 of the combustion chamber outlet are made of superalloy materials, and the outer casing 6 of the combustion chamber and the casing 14 of the combustion chamber are made of stainless steel . The comp...

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Abstract

The invention discloses a micro combustion chamber with a double-walled structure of a combustion gas turbine. The micro combustion chamber consists of a combustion chamber outer case, a flame barrel outer ring, a flame barrel inner ring, a combustion chamber inner case and the like. The flame barrel outer ring is made of a porous sintered material; the flame barrel inner ring is made of a high-temperature alloy material; and the inner case and the outer case are made of a stainless steel material. After being subjected to diffusion by a diffusion section, high-pressure air enters the combustion chamber in two streams, wherein one stream flows to an outer ring cavity between the flame barrel outer ring and the combustion chamber outer case, and is fixed with fuels to participate in combustion; and the other stream flows to an inner ring cavity between the flame barrel inner ring and the combustion chamber inner case, flows into the flame barrel through mixing holes, and is mixed with head high-temperature fuel gas. The air is divided into streams, so that a working condition close to a stoichiometric ratio is kept in a combustion area of the flame barrel, and therefore, combustion efficiency is improved, and stable working range of the combustion chamber is improved. A flame stabilization way adopting porous medium plane flames is adopted, so that remarkable effect on reducing wall temperature, strengthening stability of the combustion chamber and improving efficiency of the combustion chamber is achieved.

Description

technical field [0001] The invention relates to the technical field of micro-scale combustion, in particular to a combustion chamber of a micro-gas turbine with a double-wall structure. Background technique [0002] In recent years, with the gradual development of Micro-Electro-Mechanical Systems (MEMS) technology, the miniaturization of mechanical structures has become a new trend in technology trends. Micro-devices and their systems, such as sensors, micro-scale aircraft, micro-medical devices, micro-pumps, micro-motors, etc., are widely used in the fields of national defense, scientific research, medical treatment, and industry. In addition, personal portable systems including mobile office and communicator tools are also widely used developed rapidly. For the above-mentioned devices, systems and products, the development of micro-energy systems with small volume, light weight, high energy density and continuous energy supply will have an important impact on their perfor...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F23R3/08F23R3/52
CPCF23R3/08F23R3/52
Inventor 张弛张良薛鑫林宇震张馨桐
Owner BEIHANG UNIV
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