发明名称 Dual ignition system for a gas turbine engine
摘要 A dual channel ignition circuit (Channel A and a Channel B). In a start sequence in which a successful ignition event occurs, an exciter controller first energizes only a primary ignition channel (Channel A). Once the exciter controller recognizes a success light-off, the alternate channel (Channel B) will also then be excited as the gas turbine engine is accelerated to a self-sustaining speed. The exciter controller will then switch the primary alternative designation of the channels for the next start attempt. In a start sequence in which an unsuccessful ignition event occurs, the exciter controller sets a fail-to-start on the primary ignition channel on a failure to start A/B counter such that a failed ignition channel is diagnosed without dedicated electronic diagnostic circuits while still attempting to excite both circuits to enhance the dependability of a successful engine light-off.
申请公布号 US7509812(B2) 申请公布日期 2009.03.31
申请号 US20040922471 申请日期 2004.08.20
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 MEHRER MICHAEL E.;CHEN DAIH-YEOU
分类号 F02C7/22 主分类号 F02C7/22
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