Wing full scale strength tests of L410 NG aircraft- MOSTA

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F27174841%3A_____%2F16%3AN0000013" target="_blank" >RIV/27174841:_____/16:N0000013 - isvavai.cz</a>

Výsledek na webu

<a href="http://www.czaerospace.eu/en/2016-02-56.html" target="_blank" >http://www.czaerospace.eu/en/2016-02-56.html</a>

DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

Wing full scale strength tests of L410 NG aircraft- MOSTA

Popis výsledku v původním jazyce

VZLU is involved in project MOSTA which has extraordinary importance by its technical contents and range not for VZLU only from 2010 year. There is significant innovation of L-410 UVP-E aircraft into new generation aircraft, which should be certified according to CS/FAR 23 regulation. The phase testing is largest phase of project and both timely and by technical content overreaches the range of project. The static strength tests of wing which is now designed as full damage tolerant and contains also integral fuel tanks, is one of largest testing campaign in project MOSTA. The target of these static strength tests is a strength proof of the wing with integral fuel tank structure in accordance with regulations CS-23, FAR-23, Amdt. 59. The successfully designed and performed critical load cases as well as structure behaviour during this load conditions anticipate the successful aircraft certification.

Název v anglickém jazyce

Wing full scale strength tests of L410 NG aircraft- MOSTA

Popis výsledku anglicky

VZLU is involved in project MOSTA which has extraordinary importance by its technical contents and range not for VZLU only from 2010 year. There is significant innovation of L-410 UVP-E aircraft into new generation aircraft, which should be certified according to CS/FAR 23 regulation. The phase testing is largest phase of project and both timely and by technical content overreaches the range of project. The static strength tests of wing which is now designed as full damage tolerant and contains also integral fuel tanks, is one of largest testing campaign in project MOSTA. The target of these static strength tests is a strength proof of the wing with integral fuel tank structure in accordance with regulations CS-23, FAR-23, Amdt. 59. The successfully designed and performed critical load cases as well as structure behaviour during this load conditions anticipate the successful aircraft certification.

Druh

J_x - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

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Projekt

<a href="/cs/project/FR-TI2%2F557" target="_blank" >FR-TI2/557: Projekt MOSTA - Modernizace malého dopravního letounu za účelem zvýšení efektivnosti a ekonomie jeho provozu</a><br>

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění

2016

Kód důvěrnosti údajů

C - Předmět řešení projektu podléhá obchodnímu tajemství (§ 504 Občanského zákoníku), ale název projektu, cíle projektu a u ukončeného nebo zastaveného projektu zhodnocení výsledku řešení projektu (údaje P03, P04, P15, P19, P29, PN8) dodané do CEP, jsou upraveny tak, aby byly zveřejnitelné.

Název periodika

Czech Aerospace Proceedings

ISSN

1211-877x

e-ISSN

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Svazek periodika

2016

Číslo periodika v rámci svazku

2

Stát vydavatele periodika

CZ - Česká republika

Počet stran výsledku

4

Strana od-do

42-45

Kód UT WoS článku

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EID výsledku v databázi Scopus

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