AIRCRAFT LEADING EDGES MINOR DAMAGES DETECTION BASED ON THERMOGRAPHIC SURVEY OF ELECTRICAL ANTI-ICING SYSTEM

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F18%3APU129828" target="_blank" >RIV/00216305:26210/18:PU129828 - isvavai.cz</a>

Výsledek na webu

<a href="http://dx.doi.org/10.13164/conf.read.2018.2" target="_blank" >http://dx.doi.org/10.13164/conf.read.2018.2</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.13164/conf.read.2018.2" target="_blank" >10.13164/conf.read.2018.2</a>

Jazyk výsledku

angličtina

Název v původním jazyce

AIRCRAFT LEADING EDGES MINOR DAMAGES DETECTION BASED ON THERMOGRAPHIC SURVEY OF ELECTRICAL ANTI-ICING SYSTEM

Popis výsledku v původním jazyce

Aircraft leading edge is one of the most important subjects of aircraft scheduled maintenance. Leading edge as part of the slot on transport aircraft is not critical to fatigue stress in most of the cases. However, leading edge is extremely vulnerable to the accidental damage in combination with environmental damage. Maintenance is usually provided by visual inspection before every flight. Nevertheless, development of anti-icing system based on contact electrical heating opens possibility to thermographic NDT methods usage. These methods could detect minor damages, which are visually undetectable especially in the case of composite materials. This paper describes possibility of thermographic methods (using anti-icing system) application as mean of leading edge minor damage detection.

Název v anglickém jazyce

AIRCRAFT LEADING EDGES MINOR DAMAGES DETECTION BASED ON THERMOGRAPHIC SURVEY OF ELECTRICAL ANTI-ICING SYSTEM

Popis výsledku anglicky

Aircraft leading edge is one of the most important subjects of aircraft scheduled maintenance. Leading edge as part of the slot on transport aircraft is not critical to fatigue stress in most of the cases. However, leading edge is extremely vulnerable to the accidental damage in combination with environmental damage. Maintenance is usually provided by visual inspection before every flight. Nevertheless, development of anti-icing system based on contact electrical heating opens possibility to thermographic NDT methods usage. These methods could detect minor damages, which are visually undetectable especially in the case of composite materials. This paper describes possibility of thermographic methods (using anti-icing system) application as mean of leading edge minor damage detection.

Druh

D - Stať ve sborníku

CEP obor

—

OECD FORD obor

20304 - Aerospace engineering

Projekt

<a href="/cs/project/EF16_019%2F0000826" target="_blank" >EF16_019/0000826: Centrum pokročilých leteckých technologií</a><br>

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)<br>O - Projekt operacniho programu

Rok uplatnění

2018

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

13th Research and Education in Aircraft Design Conference

ISBN

978-80-214-5696-9

ISSN

—

e-ISSN

—

Počet stran výsledku

7

Strana od-do

15-22

Název nakladatele

Neuveden

Místo vydání

neuveden

Místo konání akce

Brno

Datum konání akce

7. 11. 2018

Typ akce podle státní příslušnosti

EUR - Evropská akce

Kód UT WoS článku

000460498600002