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Combustor mixing head for liquid rocket engine comprising vertical separate plate and horizontal separate plate
Combustor mixing head for liquid rocket engine comprising vertical separate plate and horizontal separate plate
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机译:用于液体火箭发动机的燃烧器混合头,包括垂直分隔板和水平分隔板
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摘要
The present invention relates to a liquid rocket engine combustor head having vertical and horizontal separation plate separating plate , more specifically in the combustor head for liquid rocket engine is installed on the inlet side of the oxidant , the oxidant is a plurality of domes and the junction hole is formed in the distribution plate and perpendicular to the cylindrical inlet oxidant is passed through an oxidizer inlet; Surrounding the outer circumferential surface of the vertical separating plate provided with a horizontal separation plate of a plurality of disk-like holes are formed to the inlet oxidant is passed through the oxidant inlet . ; According to the present invention , LRE it is possible to prevent damage due to the increase in the local heat flux by the wall of the combustor to the oxidant is evenly distributed to the side of the inlet for the burner head .
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