Methods, systems, and apparatus for layered and multi-indexed flight management interface
US-9205916-B2 · Dec 8, 2015 · US
Energy protection method and device for an aircraft
US9505488B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9505488-B2 |
| Application number | US-201514922420-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 26, 2015 |
| Priority date | Nov 6, 2014 |
| Publication date | Nov 29, 2016 |
| Grant date | Nov 29, 2016 |
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Abstract
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An energy protection device comprising an activation unit for, in a low energy situation, automatically activating an energy protection function comprising automatically engaging an autothrust and automatically controlling the engines of the aircraft for the engines to supply a maximum thrust, an auxiliary monitoring unit configured to perform a monitoring to detect an absence of activation of a protection mode by at least one of the engines of the aircraft although an activation command has been transmitted, and a disconnection unit to automatically disconnect the autothrust in case of the detection of such a situation, a disconnection of the autothrust resulting in the triggering of the protection function being stopped.
First claim
Opening claim text (preview).
The invention claimed is: 1. An energy protection method for an aircraft which is provided with a plurality of engines and an autothrust, said method having a protection function comprising automatically engaging the autothrust if the autothrust is not already engaged and in automatically increasing a thrust of the engines to a maximum thrust when conditions for triggering the protection function are fulfilled, said method comprising: transmitting an activation command to each of…
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Frequently asked questions
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- What does patent US9505488B2 cover?
- An energy protection device comprising an activation unit for, in a low energy situation, automatically activating an energy protection function comprising automatically engaging an autothrust and automatically controlling the engines of the aircraft for the engines to supply a maximum thrust, an auxiliary monitoring unit configured to perform a monitoring to detect an absence of activation of …
- Who is the assignee on this patent?
- Airbus Operations Sas
- What technology area does this patent fall under?
- Primary CPC classification B64C15/02. Mapped technology areas include Operations & Transport.
- When was this patent published?
- Publication date Tue Nov 29 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
- What related patents are in patentsdb?
- We list 4 related publications on this page (citations in our corpus or others sharing the same primary CPC).