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Micro-rocket operating with periodic explosive combustion, includes distributor, combustion chamber, igniter and flame traps in supply lines

机译:带有周期性爆炸燃烧的微型火箭,包括分配器,燃烧室,点火器和供应管线中的火焰收集器

摘要

The distributor (6) has openings introducing fuel supplied (3), into the micro-combustion chamber (1), which also includes an igniter (7). Flame traps (9) are included in the supply lines. All components are constructed as microstructures in a substrate. Preferred features: The two supply lines introduce different media. A pressure buffer volume (11) is provided close to the supplies (3). The mixing zone (5) is similarly constructed as a microstructure, and intervenes between supplies and distributor. The nozzle (2) delivers the combustion products. Flame traps comprise micro-nozzles (9). In an otherwise similar variant of the design, the fuel is introduced in water-encapsulated form. Fuels comprise gases, gas mixtures or atomized liquids. Numerous micro-rockets can be coupled (see also: use).
机译:分配器(6)具有将供应的燃料(3)引入微燃烧室(1)的开口,该微燃烧室还包括点火器(7)。进料管中包括火焰收集器(9)。所有组件都被构造为衬底中的微结构。首选功能:两条供应线引入不同的介质。在气源(3)的附近设有一个压力缓冲空间(11)。混合区(5)类似地构造成微结构,并介于供应源和分配器之间。喷嘴(2)输送燃烧产物。火焰收集器包括微喷嘴(9)。在设计的其他类似变体中,燃料以水包封形式引入。燃料包括气体,气体混合物或雾化液体。可以耦合许多微型火箭(另请参见:使用)。

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