Dual ignition system for a gas turbine engine

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 7509812
APP PUB NO 20060037326A1
SERIAL NO

10922471

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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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.

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First Claim

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Patent Owner(s)

Patent OwnerAddress
HAMILTON SUNDSTRAND CORPORATIONONE HAMILTON ROAD WINDSOR LOCKS CT 06096

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Chen, Daih-Yeou San Diego , US 19 207
Mehrer, Michael E San Diego, US 11 155

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