DAEDALOS

Dynamics in Aircraft Engineering Design and Analysis for Light Optimized Structures

 Coordinatore POLITECNICO DI MILANO 

 Organization address address: PIAZZA LEONARDO DA VINCI 32
city: MILANO
postcode: 20133

contact info
Titolo: Dr.
Nome: Francesco Giovanni
Cognome: Cecchet
Email: send email
Telefono: +39 02 2399 8331
Fax: +39 02 2399 8334

 Nazionalità Coordinatore Italy [IT]
 Totale costo 5˙857˙183 €
 EC contributo 3˙962˙468 €
 Programma FP7-TRANSPORT
Specific Programme "Cooperation": Transport (including Aeronautics)
 Code Call FP7-AAT-2010-RTD-1
 Funding Scheme CP-FP
 Anno di inizio 2010
 Periodo (anno-mese-giorno) 2010-11-01   -   2014-04-30

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    POLITECNICO DI MILANO

 Organization address address: PIAZZA LEONARDO DA VINCI 32
city: MILANO
postcode: 20133

contact info
Titolo: Dr.
Nome: Francesco Giovanni
Cognome: Cecchet
Email: send email
Telefono: +39 02 2399 8331
Fax: +39 02 2399 8334

IT (MILANO) coordinator 551˙259.00
2    DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV

 Organization address address: Linder Hoehe
city: KOELN
postcode: 51147

contact info
Titolo: Mr.
Nome: Michael
Cognome: Renker
Email: send email
Telefono: +49 531 295 2119
Fax: +49 531 295 2875

DE (KOELN) participant 488˙264.00
3    ALENIA AERMACCHI SPA

 Organization address address: Via Ing. P. Foresio 1
city: VENEGONO SUPERIORE
postcode: 21040

contact info
Titolo: Dr.
Nome: Carlo Oreste
Cognome: Valerio
Email: send email
Telefono: 390332000000
Fax: 390332000000

IT (VENEGONO SUPERIORE) participant 323˙809.00
4    TECHNION - ISRAEL INSTITUTE OF TECHNOLOGY

 Organization address address: TECHNION CITY - SENATE BUILDING
city: HAIFA
postcode: 32000

contact info
Titolo: Mr.
Nome: Jack
Cognome: Lavan
Email: send email
Telefono: +972 4 8293097
Fax: +972 4 8232958

IL (HAIFA) participant 322˙375.00
5    TOTALFORSVARETS FORSKNINGSINSTITUT

 Organization address address: Gullfossgatan 6
city: STOCKHOLM
postcode: 164 90

contact info
Titolo: Mr.
Nome: Rolf
Cognome: Jarlas
Email: send email
Telefono: +46 8 55 50 31 44
Fax: +46 8 55 50 33 97

SE (STOCKHOLM) participant 316˙100.00
6    SMR ENGINEERING & DEVELOPMENT SA

 Organization address address: Rue Dufour 109 b
city: BIENNE
postcode: 2502

contact info
Titolo: Dr.
Nome: Silvio
Cognome: Merazzi
Email: send email
Telefono: 41323452121
Fax: 41323452120

CH (BIENNE) participant 301˙800.00
7    ISRAEL AEROSPACE INDUSTRIES LTD.

 Organization address address: BEN GURION INTERNATIONAL AIRPORT
city: LOD
postcode: 70100

contact info
Titolo: Ms.
Nome: Gila
Cognome: Ghilai
Email: send email
Telefono: +972 3 9358685
Fax: +972 3 9355055

IL (LOD) participant 295˙000.00
8    ADVANCED LIGHTWEIGHT ENGINEERING BV

 Organization address address: ROTTERDAMSEWEG 145
city: DELFT
postcode: 2628AL

contact info
Titolo: Mr.
Nome: Jan-Jaap
Cognome: Koppert
Email: send email
Telefono: +31 15 2513430
Fax: +31 15 2513439

NL (DELFT) participant 285˙250.00
9    AERNNOVA ENGINEERING SOLUTIONS SA

 Organization address address: "Parque Tecnologico de Alava, C/ Leonardo da Vinci 13"
city: MINANO ALAVA
postcode: 1510

contact info
Titolo: Mr.
Nome: Francisco
Cognome: Molas
Email: send email
Telefono: +39 945 185 672
Fax: +34 945 185 685

ES (MINANO ALAVA) participant 267˙500.00
10    RHEINISCH-WESTFAELISCHE TECHNISCHE HOCHSCHULE AACHEN

 Organization address address: Templergraben 55
city: AACHEN
postcode: 52062

contact info
Titolo: Prof.
Nome: Ernst
Cognome: Schmachtenberg
Email: send email
Telefono: +49 241 8090490
Fax: +49 241 8092490

DE (AACHEN) participant 225˙000.00
11    GOTTFRIED WILHELM LEIBNIZ UNIVERSITAET HANNOVER

 Organization address address: Welfengarten 1
city: HANNOVER
postcode: 30167

contact info
Titolo: Prof.
Nome: Raimund
Cognome: Rolfes
Email: send email
Telefono: +49 511 762 2992
Fax: +49 511 762 2236

DE (HANNOVER) participant 218˙191.00
12    LATECOERE CZECH REPUBLIC SRO

 Organization address address: BERANOVYCH 65 LETNANY
city: PRAHA
postcode: 19902

contact info
Titolo: Mr.
Nome: Josef
Cognome: Krena
Email: send email
Telefono: 420234000000
Fax: +420 234 312 082

CZ (PRAHA) participant 200˙000.00
13    Vysoke uceni technicke v Brne

 Organization address address: ANTONINSKA 548/1
city: BRNO
postcode: 60190

contact info
Nome: Jiri
Cognome: Hlinka
Email: send email
Telefono: 420541000000
Fax: 420541000000

CZ (BRNO) participant 167˙920.00
14    ALENIA AERMACCHI SPA

 Organization address address: PIAZZA MONTE GRAPPA 4
city: ROMA
postcode: 195

contact info
Titolo: Dr.
Nome: Carlo Oreste
Cognome: Valerio
Email: send email
Telefono: 390332000000
Fax: 390332000000

IT (ROMA) participant 0.00

Mappa


 Word cloud

Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.

daedalos    service    weight    real    loads    uncertainty    components    dynamic    hysteresis    material    load    realistic    remove    unsafe    structures    mechanical    dissipation    energy    conservatism    models    fuselage    loading    quasi    basis    buckling    team    standards    aircraft    structural    static    damping    model    full    certification    transport    conservative    additional   

 Obiettivo del progetto (Objective)

'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.'

Introduzione (Teaser)

The European aircraft industry and transport policy are demanding safer and greener transport systems. EU researchers in the DAEDALOS project have taken an innovative design approach for aerospace structures that will result in aircraft weight reduction with corresponding fuel saving and lower emissions and operating costs.

Descrizione progetto (Article)

Current design standards based on conservative static loading often lead to additional and unnecessary weight. Without adequate understanding and consideration of dynamic loads, resulting designs may even be unsafe. The 'Dynamics in aircraft engineering design and analysis for light optimized structures' (http://www.daedalos-fp7.eu/ (DAEDALOS)) project has characterised dynamic loads during aircraft service. Incorporation of effects of material damping, dynamic buckling and mechanical hysteresis stand to remove the uncertainty and conservatism of present-day aircraft certification procedures.

Conventional design practice considers the fuselage as a beam on which a load is statically applied. It is a highly simplified model assuming that no energy is absorbed from the fuselage by the stringer/frame/skin constructions. It assumes that the full load propagates along the fuselage without attenuation from structural damping.

This is not the case in the real system. In addition, dynamic buckling can be much greater than static buckling, meaning that the fuselage could theoretically absorb more energy without breaking under a higher load than is predicted in the static case. The end result of these assumptions is a heavier design that may not address real-life dynamic loading conditions.

DAEDALOS developed a mid-size business jet model for the analysis. The team developed full finite element and hybrid models at various scales. Various methods for evaluating structural energy dissipation via damping were developed and implemented. These included a strain energy method, as well as quasi-linear viscoelastic material and generalised Maxwell viscous material damping models.

A rigorous campaign of experimental testing supported model development. The team evaluated materials damping of an aluminium alloy and two carbon-epoxy composites at coupon level using a variety of techniques. Panels and shells representative of typical components were also tested subjected to static and dynamic loads. Furthermore, the components were assessed in terms of weight benefits.

Through its advanced models, simulation tools and databases, the DAEDALOS project established a scientific basis for new aircraft design and certification standards reflecting energy dissipation during dynamic loading. Dynamic analysis is part of the design process in many industries and DAEDALOS deliverables could therefore be appropriate in a wide range of applications and fields.

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