Patent
Method and system for starting an engine
Youssef Michael,Charest Alexandre,Zingaro Giancarlo,Chahal Jasraj,Lisio Carmine,Mcgrath Darragh +5 more
- 13 Aug 2020
TL;DR: In this article, the engine start request is received on the second channel while the first channel is inactive and it is determined which one of the first channels and second channel was used to conduct a last successful engine start.
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Abstract: Methods and systems for starting an aircraft propulsion engine are described herein. Operation of the engine is controlled by an engine controller having a first channel and a second channel. An engine start request is received on the second channel while the first channel is inactive. It is determined which one of the first channel and the second channel was used to conduct a last successful engine start. Responsive to determining that the last successful engine start was conducted on the second channel, a predetermined time period is waited to elapse and for the first channel to reinitialize before commanding, via the first channel, an engine start based on the engine start request.
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TL;DR: In this article, an exhaust gas purifying apparatus for an internal combustion engine is provided for switching a switching valve at an optimal timing in accordance with an actual activated state of a catalyzer to achieve an optimal exhaust gas characteristic.
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Patent
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Patent
Gas turbine engine bowed rotor avoidance system
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TL;DR: In this article, the authors present a system for a gas turbine engine of an aircraft that includes a bowed rotor prevention motor that drives rotation of a starting spool of the engine through an engine accessory gearbox.
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