发明名称 Electrolytic igniter for rocket engines using monopropellants
摘要 The electrolytic ignitor comprises an injector constituting a first electrode, a second electrode that is electrically insulated from the injector and that extends downstream beyond the injector, and a distribution channel to deliver a first mono-propellant to a first mono-propellant injector device constituted by at least one injection hole opening out in the vicinity of the second electrode, and an electrical power supply circuit adapted to raise the second electrode to a potential lying in the range 50 V to 1000 V relative to the potential of the first electrode. The electrical power dissipated by ionic conduction in the free jet of the first mono-propellant is suitable for giving rise to spontaneous decomposition of the first mono-propellant and for producing combustion gas that ensures ignition of jets of a second mono-propellant coming from a main injector situated in the vicinity of the second electrode.
申请公布号 US8387359(B2) 申请公布日期 2013.03.05
申请号 US20080593727 申请日期 2008.03.28
申请人 VALENTIAN DOMINIQUE;SNECMA 发明人 VALENTIAN DOMINIQUE
分类号 F02C7/264 主分类号 F02C7/264
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