Hybrid brake system
US-12179912-B2 · Dec 31, 2024 · US
Method and system for controlling aircraft braking on a runway
US8972141B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8972141-B2 |
| Application number | US-201313852906-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 28, 2013 |
| Priority date | Mar 30, 2012 |
| Publication date | Mar 3, 2015 |
| Grant date | Mar 3, 2015 |
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Abstract
Official abstract text for this publication.
A method to control braking of an aircraft on a landing runway including: selecting a dummy runway state corresponding to a level of adhesion of wheels of the aircraft to a runway which is lower, over an entire speed range of the aircraft while braking on a runway, than an adhesion level of the wheels of the aircraft to the landing runway; calculating a set point of a deceleration value for the aircraft on the landing runway based on the landing runway for the selected dummy runway state, wherein the calculated set point corresponds to maximum braking value of the aircraft, and controlling the braking of the aircraft using the set point.
First claim
Opening claim text (preview).
The invention claimed is: 1. A method to control braking of an aircraft on a landing runway comprising: storing data regarding dummy runway states wherein the data for each dummy runway state correlates an adhesion level of wheels of the aircraft to landing speeds of the aircraft for a specific weather condition; selecting one of the dummy runway states which corresponds to a level of adhesion of wheels of the aircraft to a runway which is no greater, over an entire speed range…
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Classifications
- B60T8/1703Primary
Operations & Transport · mapped topic
- B64C25/426Primary
Operations & Transport · mapped topic
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Frequently asked questions
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- What does patent US8972141B2 cover?
- A method to control braking of an aircraft on a landing runway including: selecting a dummy runway state corresponding to a level of adhesion of wheels of the aircraft to a runway which is lower, over an entire speed range of the aircraft while braking on a runway, than an adhesion level of the wheels of the aircraft to the landing runway; calculating a set point of a deceleration value for the…
- Who is the assignee on this patent?
- Airbus Operations Sas, Airbus Sa, Airbus Sas
- What technology area does this patent fall under?
- Primary CPC classification B60T8/1703. Mapped technology areas include Operations & Transport.
- When was this patent published?
- Publication date Tue Mar 03 2015 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).