Invention Grant
US08387359B2 Electrolytic igniter for rocket engines using monopropellants 有权
使用单一推进剂的火箭发动机电解点火器

  • Patent Title: Electrolytic igniter for rocket engines using monopropellants
  • Patent Title (中): 使用单一推进剂的火箭发动机电解点火器
  • Application No.: US12593727
    Application Date: 2008-03-28
  • Publication No.: US08387359B2
    Publication Date: 2013-03-05
  • Inventor: Dominique Valentian
  • Applicant: Dominique Valentian
  • Applicant Address: FR Paris
  • Assignee: SNECMA
  • Current Assignee: SNECMA
  • Current Assignee Address: FR Paris
  • Agency: Preti Flaherty Beliveau & Pachios LLP
  • Priority: FR0754173 20070330
  • International Application: PCT/FR2008/050543 WO 20080328
  • International Announcement: WO2008/135695 WO 20081113
  • Main IPC: F02C7/264
  • IPC: F02C7/264
Electrolytic igniter for rocket engines using monopropellants
Abstract:
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.
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