Engine mount load for the JA-400 aircraft according to UL-2 and LTF-UL

Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F16%3A00301176" target="_blank" >RIV/68407700:21220/16:00301176 - isvavai.cz</a>
Výsledek na webu
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DOI - Digital Object Identifier
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Jazyk výsledku
angličtina
Název v původním jazyce
Engine mount load for the JA-400 aircraft according to UL-2 and LTF-UL
Popis výsledku v původním jazyce
The report concentrates on the calculation of load on engine mount of the ultralight airplane JA-400. The first part of the report is devoted to a brief description of the structural design of the engine mount and the engine. The following part is a description of the regulatory base, according to which the structure has been designed. Then there is the load calculation and a summary of results for different types of loads occurring in the operation. To reduce the number of future load tests also a calculation of stress in individual rods of the engine mount was done using the finite element method.
Název v anglickém jazyce
Engine mount load for the JA-400 aircraft according to UL-2 and LTF-UL
Popis výsledku anglicky
The report concentrates on the calculation of load on engine mount of the ultralight airplane JA-400. The first part of the report is devoted to a brief description of the structural design of the engine mount and the engine. The following part is a description of the regulatory base, according to which the structure has been designed. Then there is the load calculation and a summary of results for different types of loads occurring in the operation. To reduce the number of future load tests also a calculation of stress in individual rods of the engine mount was done using the finite element method.

Rok uplatnění
2016
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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