Dual-Cam Bellcrank Mechanism
US-2016258385-A1 · Sep 8, 2016 · US
US9109538B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9109538-B2 |
| Application number | US-201113578270-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 3, 2011 |
| Priority date | Feb 10, 2010 |
| Publication date | Aug 18, 2015 |
| Grant date | Aug 18, 2015 |
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Official abstract text for this publication.
The invention relates to a system ( 10 ) for controlling an aircraft propelled by at least one jet engine housed in a nacelle, characterised in that said system includes: a full authority electronic control unit ( 100 ) of the jet engine, intended for monitoring the jet engine, suitable for monitoring and controlling at least one electrical device of the nacelle; and an electric power unit ( 200 ) of the nacelle, external to said full authority electronic control unit of the jet engine for monitoring the jet engine, suitable for managing the electric power supply of said electrical device of the nacelle.
Opening claim text (preview).
The invention claimed is: 1. A control system of an aircraft propelled by at least one jet engine housed in a nacelle, the control system comprising: a full authority digital engine control unit of the at least one jet engine, the full authority digital engine control unit monitoring the at least one jet engine, and directly monitoring and controlling at least one electrical device of the nacelle; and an electric power unit of the nacelle external to the full authority digital e…
Mechanical Engineering · mapped topic
Cross-Sectional Technologies · mapped topic
Mechanical Engineering · mapped topic
Cross-Sectional Technologies · mapped topic
Cross-Sectional Technologies · mapped topic
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