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TRIMIS

Development of an optimized large scale engine CFRP annulus filler

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete with results
Geo-spatial type
Other
Total project cost
€996 397
EU Contribution
€573 132
Project Acronym
ORCA
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Societal/Economic issues,
Environmental/Emissions aspects,
Other specified
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
SP1-JTI-CS-2010-01
Link to CORDIS
Objectives

This proposal described the effort planned by the partners FACC AG, Austria & University of applied sciences (UAS) Rapperswil, Switzerland, for the development of a CFRP annulus filler. Production process was an advanced preform concept with folding techniques and integration of all connection parts, injected with resin by an improved RTM process. Part development started with material tests on coupons, continued by the manufacturing of a prototype design, and finally ending in a close-to-series-production of 56 annulus filler.

In addition, a quality assurance supervisor accompanied the project from the beginning on in order to establish a quality measurement system suitable for a serial production. Material- & process development was led by UAS Rapperswil, while manufacturing, quality assurance and non-destructive testing was be under the responsibility of FACC. FACC AG is Austria’s first-tier aircraft supplier in composite components, UAS Rapperswil is specialised in RTM process improvements and preform technologies.

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-2010-1-SAGE-03-001 Fan annulus filler development

Results

Executive Summary:

An annulus filler is a rotating part on modern jet engines. It smoothens the airstream and is vital for proper functioning of the rotor system. Designed to be as lightweight as possible, yet stable enough for impact of small to medium birds and hailstones, the current state of the art are metallic designs.

The main task of the ORCA project was to design, manufacture and test a composite annulus filler. After several design iterations, a composite design was considered mature enough to be manufactured and tested on the Advanced low pressure system (ALPS) engine of the (sustainable and green engine) SAGE3 project.

The targets set at the beginning of the project were overfulfilled. In comparison to the best existing design, the ORCA filler reduces the weight by over 40%, whilst providing the same excellent impact and fatigue behaviour. Cost wise, the part is competitive to existing designs, with possible further cost reduction summing up to a lighter and less expensive part.

The part had been awarded with the international JEC award on innovation in aeronautics in 2014, and sets a new benchmark for cost- and quality efficient production routes for CFRP parts.

The part had been on display at exhibitions, and several lectures and conference contributions were published. Three patents were filed protecting the generated foreground.

 

Partners

Lead Organisation
Organisation
Fischer Advanced Composite Components Ag*facc Ag
Address
FISCHERSTRASSE, 4910 RIED IM INNKREIS, Austria
Organisation website
EU Contribution
€348 329
Partner Organisations
Organisation
Hsr Hochschule Fur Technik Rapperswil
Address
Oberseestrasse 10, 8640 Rapperswil, Switzerland
EU Contribution
€647 334
Organisation
Hsr Hochschule Fur Technik Rapperswil
Address
Oberseestrasse 10, 8640 Rapperswil, Switzerland
EU Contribution
€224 803

Technologies

Technology Theme
Manufacturing processes
Technology
Smart composite manufacture
Development phase
Demonstration/prototyping/Pilot Production

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