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Statements

Subject Item
n2:7E11025
rdf:type
n18:Projekt
rdfs:seeAlso
http://www.isvav.cz/projectDetail.do?rowId=7E11025
dcterms:description
Today’s design and certification procedures of aircrafts are mainly based on conservative static loading which leads to additional weight and, potentially, to a structurally unsafe aircraft. The overall objective of the DAEDALOS project is to develop methods and procedures to determine dynamical loads considering the effects of dynamic buckling, material damping and mechanical hysteresis during aircraft service. Use of advanced analysis and design principles from DAEDALOS will partly remove the uncertainty and the conservatism of today’s design and certification procedures. DAEDALOS work will hence form the basis for improved common design practices by: 1. Determining accurate dynamic load spectra to be used for structural sizing. 2. Reducing the added weight of aircraft structural components due to conservative design in compliance with quasi-static loads by using more realistic equivalent dynamic loads. This goal will be achieved through improved introduction of the structure damping capacity and detailed analysis. 3. Increasing structural safety using more realistic loading scenarios. 4. Establishing new procedures for the definition of loads to be used during aircraft design and certification by authorities. Today’s design and certification procedures of aircrafts are mainly based on conservative static loading which leads to additional weight and, potentially, to a structurally unsafe aircraft. The overall objective of the DAEDALOS project is to develop methods and procedures to determine dynamical loads considering the effects of dynamic buckling, material damping and mechanical hysteresis during aircraft service. Use of advanced analysis and design principles from DAEDALOS will partly remove the uncertainty and the conservatism of today’s design and certification procedures. DAEDALOS work will hence form the basis for improved common design practices by: 1. Determining accurate dynamic load spectra to be used for structural sizing. 2. Reducing the added weight of aircraft structural components due to conservative design in compliance with quasi-static loads by using more realistic equivalent dynamic loads. This goal will be achieved through improved introduction of the structure damping capacity and detailed analysis. 3. Increasing structural safety using more realistic loading scenarios. 4. Establishing new procedures for the definition of loads to be used during aircraft design and certification by authorities.
dcterms:title
Dynamics in Aircraft Engineering Design and Analysis for Light Optimized Structures Dynamics in Aircraft Engineering Design and Analysis for Light Optimized Structures
skos:notation
7E11025
n4:aktivita
n12:7E
n4:celkovaStatniPodpora
n14:celkovaStatniPodpora
n4:celkoveNaklady
n14:celkoveNaklady
n4:datumDodatniDoRIV
2014-06-30+02:00
n4:druhSouteze
n19:RP
n4:duvernostUdaju
n15:S
n4:fazeProjektu
n16:100705763
n4:hlavniObor
n6:JU
n4:hodnoceniProjektu
n21:U
n4:kategorie
n13:AP
n4:klicovaSlova
Structures, design, dynamic loads, damping, buckling, composites
n4:partnetrHlavni
n11:orjk%3A26210
n4:pocetKoordinujicichPrijemcu
0
n4:pocetPrijemcu
1
n4:pocetSpoluPrijemcu
0
n4:pocetVysledkuRIV
0
n4:pocetZverejnenychVysledkuVRIV
0
n4:posledniUvolneniVMinulemRoce
2013-03-27+01:00
n4:prideleniPodpory
n7:13595%2F2011+%E2%80%93+321
n4:sberDatUcastniciPoslednihoRoku
n8:2013
n4:sberDatUdajeProjZameru
n8:2014
n4:statusZobrazovaneFaze
n17:DUU
n4:typPojektu
n10:P
n4:ukonceniReseni
2013-10-31+01:00
n4:zahajeniReseni
2011-01-01+01:00
n4:zhodnoceni+vysledku+projektu+dodavatelem
Following the condition that the candidate of financial contribution was evaluated and afterwards selected by international provider in accordance with the rules of the program the Ministry of Education, Youth ans Sports does not realize the evaluation of project results. The project is evaluated only after its approval by an international provider. Hodnocení výsledků řešení ministerstvo neprovádí, neboť podmínkou podpory je, že uchazeč byl vybrán mezinárodním poskytovatelem v souladu s pravidly příslušného programu. Projekt je hodnocen až po jeho schválení mezinárodním poskytovatelem.
n4:zivotniCyklusProjektu
n22:ZBKU
n4:vyzva
n20:FP7-AAT-2010-RTD-1
n4:klicoveSlovo
Structures buckling design damping dynamic loads