Functional drop tests of L-410 UVP-E20 and L-410 NG (MOSTA) landing gears on platform and rotating drum

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F12%3A%230001294" target="_blank" >RIV/00010669:_____/12:#0001294 - isvavai.cz</a>

Výsledek na webu

<a href="http://www.czaerospace.eu/en/2012-3-45.html" target="_blank" >http://www.czaerospace.eu/en/2012-3-45.html</a>

DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

Functional drop tests of L-410 UVP-E20 and L-410 NG (MOSTA) landing gears on platform and rotating drum

Popis výsledku v původním jazyce

The relatively large functional drop tests of main landing gear of L-410 UVP-E20 and subsequently L-410 NG aircraft designated for innovated aircraft which is subject of MOSTA national project were performed. The tests were completed on great multi-purpose drop test machine and their purpose was measurement of dynamic forces during landing shock. During the test the wide measurement of vertical and for and aft forces in order to get comparison under various adhesive conditions according to CS ? 23 and Russian AP- 23 airworthiness requirements was provided. The test results confirmed possibility to utilize the L-410 UVP-E20 landing gear for L-410 NG innovated aircraft.

Název v anglickém jazyce

Functional drop tests of L-410 UVP-E20 and L-410 NG (MOSTA) landing gears on platform and rotating drum

Popis výsledku anglicky

The relatively large functional drop tests of main landing gear of L-410 UVP-E20 and subsequently L-410 NG aircraft designated for innovated aircraft which is subject of MOSTA national project were performed. The tests were completed on great multi-purpose drop test machine and their purpose was measurement of dynamic forces during landing shock. During the test the wide measurement of vertical and for and aft forces in order to get comparison under various adhesive conditions according to CS ? 23 and Russian AP- 23 airworthiness requirements was provided. The test results confirmed possibility to utilize the L-410 UVP-E20 landing gear for L-410 NG innovated aircraft.

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

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Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2012

Kód důvěrnosti údajů

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

Název periodika

Czech Aerospace Proceedings / Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Svazek periodika

3/2012

Číslo periodika v rámci svazku

3

Stát vydavatele periodika

CZ - Česká republika

Počet stran výsledku

6

Strana od-do

20-25

Kód UT WoS článku

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EID výsledku v databázi Scopus

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