Skip to main content
European Commission logo
TRIMIS

Non-rigid geometry variation for fabricated aero structure

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete with results
Geo-spatial type
Other
Total project cost
€449 919
EU Contribution
€337 437
Project Acronym
GeoVar
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Societal/Economic issues,
Safety/Security
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
SP1-JTI-CS-2013-02
Link to CORDIS
Objectives

In traditional 3D variation simulation (stack-up’s) it is common to consider that the parts are rigid. However, often in production forces are applied manually or by different fixturing solutions to assure that requirements on offset are fulfilled before welding parts together in an assembly. This causes the parts to bend and rigid analysis is therefore not valid. Depending on assembly sequences and geometry variation of incoming material, different fixturing forces need to be applied from component to component to assure the right fit in the seam before welding. It may even be necessary to use active fixturing where the forces are varying during the welding process. The welding process itself also contributes with variation that needs to be considered in order to fulfil geometrical requirements.

This project proposed a novel way to combine variation and welding simulation to support the design of future welding fixtures for aircraft engine components. Non-rigid Geometrical Variation Simulation were further developed to optimise locator and support positions in order to minimise geometrical variation in the weld gap and also take fixturing forces into consideration. Computational Welding Mechanics simulations with integrated control functions were further developed to prescribe fixturing forces for maintaining specific tolerances ahead of the weld for a stable weld process.

The simulation areas were combined and integrated to support the design of a physical welding fixture suitable for fabrication of aircraft engine components. The results were demonstrated virtually and physically.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
JTI-CS - Joint Technology Initiatives - Clean Sky
Other Programme
JTI-CS-2013-2-SAGE-02-035 Non-rigid geometry variation simulation for fabricated aero engine structures

Results

Executive Summary:

Green and sustainable aero engines require weight reduction. For the open rotor technology, with rotating Ni-based superalloy components this is enabled by fabrication (welding) methods where a number of small parts, often in different materials, are welded together. In this type of fabricated structures, variation from manufacturing of the individual parts, from the fixturing and assembly process and from the welding process itself accumulates and propagates through the structure and creates geometrical variation in the final subsystem. This in turn has an influence on the ability to meet requirements on aerodynamics and life. It is therefore extremely important to have a reliable process to control how variation affects the final welded geometries. Therefore, the GeoVar project combined state of the art variation simulation with welding metallurgy, welding simulation and fixture design.

The main result in the project was a novel approach on how to combine variation simulation and welding simulation to optimize fixture design and tolerances to meet geometrical requirements. The method contributed to decreased development time and cost and increased product quality for welded areo-structure components.

Partners

Lead Organisation
Organisation
Chalmers Tekniska Hoegskola Ab
Address
41296 GOTHENBURG, Sweden
Organisation website
EU Contribution
€138 751
Partner Organisations
Organisation
Lulea Tekniska Universitet
Address
Universitetsomradet Porson, 971 87 Lulea, Sweden
Organisation website
EU Contribution
€7 732 503
Organisation
Lulea Tekniska Universitet
Address
Universitetsomradet Porson, 971 87 Lulea, Sweden
Organisation website
EU Contribution
€119 936
Organisation
Hogskolan Vast
Address
Hogskolan Vast, 461 86 Trollhattan, Sweden
EU Contribution
€1 861 352
Organisation
Hogskolan Vast
Address
Hogskolan Vast, 461 86 Trollhattan, Sweden
EU Contribution
€56 250
Organisation
Rd&t Technology Ab
Address
STENHYDDEGATAN 5, SE431 64 MOELNDAL, Sweden
EU Contribution
€22 500

Technologies

Technology Theme
Aircraft propulsion
Technology
Aircraft engine conceptual design tools
Development phase
Validation

Contribute! Submit your project

Do you wish to submit a project or a programme? Head over to the Contribute page, login and follow the process!

Submit