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TRIMIS

Rapid Production of Large Aerospace Components

Project

RAPOLAC - Rapid Production of Large Aerospace Components


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
Project website:
Duration:
Start date: 01/01/2007,
End date: 01/12/2009

Status: Finished
Funding details:
Total cost:
€2 734 683
EU Contribution:
€2 140 650

Overview

Background & policy context:

Shaped metal deposition (SMD) is a prototyping system that allows complex parts to be built directly from a CAD model with minimum finishing. The system builds components layer by layer without the need for tooling. Complex parts can be made with improved material properties and hybrid components can also be created.

The advantage of SMD is that complex parts, or those that need a lot of machining, can be made quickly and cheaply: in some cases lead times have been reduced by 70%. The finished parts can also have improved material qualities, the process has low to zero harmful emissions and it does not require tooling. Uses include rapid prototyping, one-off parts, repair, and complex or hybrid components.

The SMD rig consists of a robot with a TIG welding head and a manipulator, housed inside a sealed chamber with wire fed in from outside. The system welds the wire in an inert argon atmosphere to prevent the substrate, electrode and part reacting with atmospheric gases. Once used, the argon can be safely vented via an extraction system, or re-circulated via a scrubber system. A water-cooled vision system allows the welding arc to be viewed and the size of the bead and weld pool to be monitored in real time. Features can be built in any orientation without the need for support structures.

Objectives:

To exploit SMD technology fully within aerospace, it must be demonstrated that it is a valid and cost-effective manufacturing route. RAPOLAC will produce a business case for SMD to ensure the take-up of this technology. Further work will define material properties, achieve certification for the process and widen the range of materials which can be deposited. RAPOLAC will concentrate on aerospace materials such as titanium, steels and nickel-based alloys, which are costly and difficult to machine. This process has attracted interest from several aerospace companies, but take-up is limited because:

  • weld parameters vary according to the material, substrate, geometry and size
  • the material properties are not well understood, and
  • the benefits of SMD over more traditional processes are not clear.

To validate SMD for commercial aerospace use, samples containing difficult-to-manufacture features will be constructed from a variety of materials. Material characterisation will be performed, and the process modelled using FE and mechanical techniques. A cost-benefit analysis will be carried out to compare SMD construction with traditional manufacturing routes, allowing a business case to be put forward to encourage take-up by SMEs. The time and material savings are expected to make SMD an attractive option for the manufacture of large aerospace parts.

Methodology:

RAPOLAC's aim is to validate SMD to manufacture aerospace parts in a variety of materials. To do this, the properties produced by different materials, geometries and deposition parameters must be catalogued, heat-treatments and machining strategies developed, and the process modelled and controlled.

WP1 will build the parts needed for microstructural analysis, fatigue and stress tests and will provide data for modelling. It will also investigate the effects of different weld parameters, materials, substrates, part sizes and geometries, and test the control strategies developed. It will look at post-heat-treatment and machining strategies for the finished parts.

WP2 will look at the properties of the parts produced, and develop a database of material properties, residual stresses and susceptibility to fracture.

WP3 will develop both local models (optimising weld parameters to give the best material properties) and global robotic models of the SMD process.

WP4 will look at all aspects of the SMD process and quantify its benefits, comparing SMD with traditional manufacturing processes. It will highlight the cost and environmental advantages and develop best practice manufacturing methods, which will indicate where SMD should be used entirely, and where hybrid manufacture is more cost-effective. This will lead to the creation of a business plan for SMD and encourage its take-up in industry.

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