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PULSE DETONATION COMBUSTION CHAMBER HAVING DETONATION GAS ENERGY DISTRIBUTION SMOOTH STRUCTURE

机译:脉冲爆震燃烧室具有爆轰气体能量分布平滑结构

摘要

A pulse detonation combustion chamber (12) having a detonation gas energy distribution smooth structure. The pulse detonation combustion chamber comprises a combustion chamber air inlet channel (1), the pulse detonation combustion chamber (12), a pulse detonation fuel gas energy distribution adjusting device (15), and a transition section (17) which are sequentially communicated. An air inlet cone (2) is mounted in the combustion chamber air inlet channel (1); an atomized air channel (5), a fuel channel (6), and a conical swirl nozzle (11) are provided in the air inlet cone (2); the atomized air channel (5) is connected to a high-pressure atomized air inlet pipeline (3) extending into the air inlet cone (2) from the outside of the combustion chamber air inlet channel (1), and the fuel channel (6) is connected to a fuel supply pipeline (4) extending into the air inlet cone (2) from the outside of the combustion chamber air inlet channel (1); the conical swirl nozzle (11) is connected to the atomized air channel (5) and the fuel channel (6), and a pneumatic valve (8) is mounted at the tail end of the air inlet cone (2); a spark plug mounting base (14) is provided on the pulse detonation combustion chamber (12), and a spark plug (13) is mounted on the spark plug mounting base (14). The pulse detonation combustion chamber (12) solves the problems that pulse detonation combustion high-temperature gas energy flow density is concentrated, the detonation gas energy conversion and extraction efficiency of a turbine is low, and detonation combustion wave pressure is transmitted back.
机译:具有爆轰气体能量分布平滑结构的脉冲爆震燃烧室(12)。脉冲爆震燃烧室包括燃烧室空气入口通道(1),脉冲爆轰燃烧室(12),脉冲爆震燃料气体能量分布调节装置(15),以及顺序地传送的过渡部分(17)。空气入口锥(2)安装在燃烧室空气入口通道(1)中;雾化空气通道(5),燃料通道(6)和锥形旋流喷嘴(11)设置在进气锥(2)中;雾化空气通道(5)连接到从燃烧室空气入口通道(1)的外部延伸到空气入口锥(2)中的高压雾化空气入口管道(3),以及燃料通道(6 )连接到从燃烧室空气入口通道(1)的外部延伸到空气入口锥(2)中的燃料供应管道(4);锥形旋流喷嘴(11)连接到雾化空气通道(5)和燃料通道(6),气动阀(8)安装在进气口锥(2)的尾端;火花塞安装基座(14)设置在脉冲爆震燃烧室(12)上,并且火花塞(13)安装在火花塞安装基座(14)上。脉冲爆炸燃烧室(12)解决了脉冲爆炸燃烧高温气体能量流密密度集中的问题,涡轮机的爆轰气体能量转换和提取效率低,并透射爆炸燃烧波压力。

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