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Smart Aircraft in Emergency Situations

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete with results
Geo-spatial type
Other
Total project cost
€5 732 493
EU Contribution
€3 828 125
Project website
Project Acronym
SMAES
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Safety/Security,
Digitalisation
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
FP7-AAT-2010-RTD-1
Link to CORDIS
Background & Policy context

For large transport aircraft, ditching analysis is requested by EASA. The respective requirements are primarily devoted to a minimisation of risks for immediate injuries and the provision of fair chances for an evacuation. A significant part of average air travel is over water and historically a planned or unplanned water-landing event occurs grossly speaking every 5 years.

Objectives

The objectives of the SMAES project are "Aircraft Safety" and "Aircraft Development Cost". The primary outcome of the project will be advanced methodologies and simulation tools to support aircraft development from pre-project phase to certification. These will enhance future innovation in aircraft design through ensuring that innovative designs are compliant with safety requirements.

Methodology

The key developments addressed in the work programme are:

  • Improved models for the calculation of ditching loads including both analytical and detailed fluid dynamics models. Inclusion of the effects of the complex flow physics in ditching is critical to prediction of ditching loads;
  • Reliable and predictive aircraft models for structural behaviour under dynamic fluid loads;
  • Demonstration of the methods on representative future aircraft design concepts.

The consortium brings together aircraft manufacturers, analysis software developers, research organisations and universities. The consortium partners form a strong team covering the required expertise in aircraft design, numerical methods and simulation, ditching analysis and supporting experimental methods to achieve the project objectives.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
The European Commission
Type of funding
Public (EU)
Specific funding programme
FP7-TRANSPORT

Results

New tools to ensure aircraft stays afloat during ditching

EU-funded researchers developed a set of simulation tools that should permit cost-effective design of aircraft able to protect passengers in emergency situations such as ditching. The team addressed problems of passenger survival during all phases of a water landing: from the moment of approaching water up to the actual floating.

The current drive towards greener, safer and lower-cost aircraft requires manufacturers to come up with innovative design solutions and new structural concepts. Empirical methods traditionally used to design aircraft with respect to emergency situations are becoming obsolete. New methodologies and predictive numerical tools are necessary to mitigate safety and economical risks.

Within the project http://www.smaes.eu/ (SMAES) (Smart aircraft in emergency situations), researchers developed advanced simulation tools for use at different stages of the design and certification processes. Through optimising the ditching response, these newly developed tools should reduce design and test costs, increasing innovation to create safer, lighter and less expensive structures.

The ditching process can be categorised into four phases: approach, impact, landing and floatation. Ditching generates high hydrodynamic loads on the structure. Because of the high forward velocity, effects such as cavitation and ventilation influence hydrodynamic loads.

Amongst project achievements was the development of improved analytical and numerical models for predicting fluid loads and local pressures acting on aircraft during ditching. Researchers produced complex fluid models that can represent important physical phenomena such as air cushioning, ventilation, cavitation and suction force.

Another part of the work focused on the successful development of reliable models predicting an aircraft's structural behaviour and rupture under dynamic fluid loads. The deformable structural models were then coupled with the improved fluid models. The outcomes of this task were validated methodologies for performing fluid-structure coupled with aircraft ditching simulations.

The SMAES team established a new experimental high-speed water impact facility that can support future research and development in water impact response. An extensive set of test data was produced, covering high-speed water impact and the response of composite structures.

Apart from upgrading safety, SMAES is expected to contribute to the competitiveness and primacy of the European aeronautics industry thanks to an array of novel tools for aircraft design. Finally, improved understanding of the complex physical phenomena that occur during aircraft ditching will be useful in other structure-fluid applications such as landing rotorcraft on water and high-speed planning.

Partners

Lead Organisation
Organisation
Cranfield Aerospace Limited
Address
Cranfield University Campus Hangar 2, Cranfield, MK43 0AL, United Kingdom
Organisation website
EU Contribution
€437 501
Partner Organisations
Organisation
University Of East Anglia
Address
Earlham Road, Norwich, NR4 7TJ, United Kingdom
EU Contribution
€212 138
Organisation
Technische Universitat Hamburg
Address
Am Schwarzenberg Campus 1, 21073 Hamburg, Germany
Organisation website
EU Contribution
€144 000
Organisation
Esi Group
Address
Avenue De Suffren 100-102, 75008 Paris, France
Organisation website
EU Contribution
€195 000
Organisation
Office National D' Etudes Et De Recherches Aérospatiales
Address
29, avenue de la Division Leclerc, BP72 CHÂTILLON CEDEX, France
Organisation website
EU Contribution
€401 915
Organisation
Deutsches Zentrum Fr Luft Und Raumfahrt E.v
Address
Linder Hoehe, 51147 KOELN, Germany
Organisation website
EU Contribution
€441 352
Organisation
Airbus Deutschland Gmbh
Address
Kreetslag 10, 950109 HAMBURG, Germany
Organisation website
EU Contribution
€26 300
Organisation
Consiglio Nazionale Delle Ricerche
Address
Piazzale Aldo Moro, 185 Roma, Italy
Organisation website
EU Contribution
€0
Organisation
Dassault Aviation
Address
9, Rond-Point des Champs-Elysées - Marcel Dassault, 75008 PARIS, France
Organisation website
EU Contribution
€360 000
Organisation
Centro Italiano Ricerche Aerospaziali Scpa
Address
Via Maiorise s/n, 81043 CAPUA (CE), Italy
Organisation website
EU Contribution
€235 580
Organisation
Alenia Aermacchi Spa
Address
Viale Dell'aeronautica Snc, 80038 Pomigliano D'arco (Na), Italy
Organisation website
EU Contribution
€175 000
Organisation
Airbus Defence And Space Sa
Address
Avenida De Aragon 404, 28022 Madrid, Spain
EU Contribution
€155 607
Organisation
Altair Development France
Address
Centre D'affaires, Rue De La Renaissance Bat A 2, 92160 Antony, France
Organisation website
EU Contribution
€127 500
Organisation
Istituto Nazionale Per Studi Ed Esperienze Di Architettura Navale
Address
VIA DI VALLERANO 139, 00128 ROMA, Italy
Organisation website
EU Contribution
€567 670
Organisation
Panepistimio Patron
Address
University Campus- Rio, 26500 Patras, Greece
Organisation website
EU Contribution
€215 922
Organisation
Technische Universitaet Dresden
Address
Helmholtzstrasse 10, 1069 Dresden, Germany
Organisation website
EU Contribution
€132 640

Technologies

Technology Theme
Aircraft design and manufacturing
Technology
Aircraft design model
Development phase
Research/Invention

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