发明名称 Igniter/thruster with catalytic decomposition chamber
摘要 An ignition system and method of igniting the ignition system includes a main catalyst section in a staged relationship with a pilot-catalyst section to stage a decomposition though the pilot-catalyst section which preheats the main catalyst section.
申请公布号 US8814562(B2) 申请公布日期 2014.08.26
申请号 US200812131840 申请日期 2008.06.02
申请人 Aerojet Rocketdyne of DE, Inc. 发明人 Jensen Jeff;Claflin Scott
分类号 F23C3/00;F23Q9/08;F23Q11/00;F41F3/04;F02C7/26;C06D5/00 主分类号 F23C3/00
代理机构 代理人 Landau Joel G.
主权项 1. An ignition system comprising: a pilot-catalyst section along a longitudinal axis; a pilot inlet in communication with said pilot-catalyst section to receive a propellant; a main catalyst section in a staged relationship with said pilot-catalyst section along said longitudinal axis; a main inlet in communication with said main catalyst section to receive the propellant; wherein said pilot-catalyst section includes a pilot catalyst bed; wherein a pilot outlet is downstream of said pilot catalyst bed relative to said longitudinal axis, said main catalyst section in communication with said pilot outlet; wherein said pilot-catalyst section includes a pilot regenerative cooling jacket, said pilot catalyst bed in communication with said pilot inlet via said pilot regenerative cooling jacket; and wherein the main catalyst section includes a main catalyst bed, and wherein the main catalyst section includes a main regenerative cooling jacket, said main catalyst bed in communication with said main inlet via said main regenerative cooling jacket, and wherein said main catalyst bed is in communication with said pilot outlet.
地址 Canoga Park CA US