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Ramjet Solid Fuel with Ignition Support for Gun-Propelled Ramjet Shell

机译:带有点火支持的Ramjet固体燃料,适用于机枪式Ramjet外壳

摘要

The present invention relates to a ramjet fuel applied to an extended range sub caliber where a ramjet engine is mounted, which can rapidly actuate the ramjet engine by applying an ignition assisting unit to the solid fuel of a jet engine in the extended range sub caliber on which the ramjet engine is mounted to extend the range of 105 mm, 155 mm and 8-inch howitzer shells or 3-inch and 5-inch naval shells launched for fire support. The present invention provides the ramjet solid fuel applied to the extended range sub caliber where the ramjet engine is mounted to extend the range of shells and is arranged between an inlet and an injection nozzle of the ramjet engine, comprising: a fuel body (10) composed of a ring shaped solid body; and an ignition assisting material with which the fuel body (10) is covered to ignite the fuel body, wherein the fuel body (10) contains: 40-90 wt% of an HTPB fuel; 5-15 wt% of an AP oxidant; 5-15 wt% of first metal particles composed of aluminum (Al) or magnesium (Mg); 0-30 wt% of second metal particles composed of at least one metal among boron (B), boron carbide (B_4C), zirconium (Zr) and zirconium carbide (ZrC); and unavoidable impurities.
机译:冲压燃料技术领域本发明涉及一种应用于安装有冲压喷气发动机的扩展范围子口径的冲压燃料,该冲压燃料可以通过将点火辅助单元施加到扩展子级口径的喷气发动机的固体燃料上来快速致动冲压发动机。装有冲压喷气发动机的发动机可以扩展105毫米,155毫米和8英寸榴弹炮弹或3英寸和5英寸海军炮弹的射程,以提供火力支持。本发明提供了应用于扩展范围子口径的冲压发动机固体燃料,其中冲压发动机被安装以延伸壳体的范围,并且布置在冲压发动机的入口和喷嘴之间,包括:燃料主体(10)由环形固体组成;覆盖有燃料体(10)以点燃燃料体的点火辅助材料,其中燃料体(10)包含:40-90重量%的HTPB燃料;和5-15wt%的AP氧化剂; 5-15重量%的由铝(Al)或镁(Mg)组成的第一金属颗粒; 0-30重量%的第二金属颗粒由硼(B),碳化硼(B_4C),锆(Zr)和碳化锆(ZrC)中的至少一种金属组成;和不可避免的杂质。

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