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TRIMIS

Thermal Overall Integrated Conception of Aircraft

Project

TOICA - Thermal Overall Integrated Conception of Aircraft


Funding origin:
European
European Union
STRIA Roadmaps:
Vehicle design and manufacturing (VDM)
Vehicle design and manufacturing
Transport mode:
Airborne
Airbone
Transport sectors:
Passenger transport
Passenger transport
Freight transport
Freight transport
Duration:
Start date: 01/09/2013,
End date: 30/09/2016

Status: Finished
Funding details:
Total cost:
€26 483 333
EU Contribution:
€15 166 972

Overview

Background & policy context:

The thermal behaviour of aircrafts has recently become a crucial subject due to many factors: increasing numbers of complex systems required by modern, more electric, commercial aircrafts, the introduction of hotter engines with higher by-pass ratios, the increased use of composite materials in aircraft structures, or the confinement of highly dissipative equipment and systems to smaller areas to earn space for passengers and cargo. New advanced techniques to manage the aircraft thermal behaviour at the very early stages of development are essential to take the right figuration decisions while meeting market demands. To work efficiently and to work on emerging innovative solutions, it is essential to perform thermal management at the global aircraft level. Today, thermal studies are performed for sizing and risk analyses.

Objectives:

The TOICA project intends to radically change the way thermal studies are performed within aircraft design processes. It will create and manage a thermal aircraft architecture which does not yet exist today. This will be shared in the extended enterprise with design partners through a collaborative environment supporting the new advanced capabilities developed by the project, namely the architect cockpit, which will allow the architects and experts to monitor the thermal assessment of an aircraft and to perform trade-off studies. Supra integration will support a holistic view of the aircraft and allow traditional design views and the related simulation cascade to be challenged. Six cases of use illustrating new thermal strategies will demonstrate the benefits of the TOICA approach on realistic aircraft figurations. Plateaus will be organised with architects for the definition, selection and evaluation of thermally optimised aircraft figurations. These plateaus will stimulate the project. In parallel, technology readiness evaluations will assess the maturity of the developed technologies and support the deployment and exploitation of the TOICA results.

Methodology:

The research tasks are organised in four technical sub-projects corresponding to the main TOICA research domains (BDA capabilities, multidisciplinary M&S capabilities, new thermal strategies, thermal trade-off). Six user-cases illustrating the thermal strategies, jointly defined between architects and experts, will demonstrate the benefits of the TOICA approach on two realistic aircraft configurations.

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