6 European Projects Found
Searched on 125080 European Projects
FINISHED
Efficient ice protection Systems and simulation Techniques Of ice Release on propulsive systeMs (STORM)
Start date: Oct 1, 2013, End date: Mar 31, 2017,
Icing conditions are one of the most severe for aircraft and engines as experienced in the certification process and in-service events. Certification tests are never simple because icing phenomena is a very complex domain and designers have access to a very low level of prediction capability compare to other fields, mainly relying on a very fragmented knowledge based on empirical past experience. ...
Read Project
15
Partners Participants
FINISHED
Electro-thermal Laminar Wing Ice Protection System Demonstrator (ELWIPS)
Start date: Oct 1, 2012, End date: Dec 31, 2016,
This proposal regards designing, building and testing a functional prototype of part of a laminar wing fitted with electro-thermal ice protection (ETIPS) for a business jet. The aim is to show innovation in the use of composite materials for the fixed leading edge, (e.g. Fibre/Metal Laminates), which are thermally efficient, can be manufactured to tight laminar wing tolerances and comparable to a ...
Read Project
4
Partners Participants
FINISHED
Design and manufacture of a flight worthy intake system (scoop/NACA divergent intake) SCOOP AND NACA DIVERGENT INTAKE TRIAL (SANDIT) (SANDIT)
Start date: Jan 1, 2013, End date: Mar 31, 2016,
"This proposal supports the supply of an innovative scoop and NACA divergent intake, qualified to a sufficientlevel to support flight trial activities.With a successful pedigree in intake design, coupled with a wealth of experience in complex structures andhaving gained a detailed understanding of scoop intake design from successful delivery of the original JTI funded scoop program, GKN and its pa ...
Read Project
4
Partners Participants
FINISHED
Hybrid WIPS Design code (HETEMS)
Start date: Jan 4, 2010, End date: Jan 3, 2015,
"In this propsal we will develop a hyrbid low power ice proection modellisation tool. This will consist of combining our existing knwoledge on separate electrothermal and electromechancial ice proections systems into a single, integrated, computer code. We will also test (but not manufacture, which is a separate CfP) a hybrid Wing Ice Protection System (WIPS) in an icing wind tunnel. The data gath ...
Read Project
1
Partner Participant
FINISHED
Development and Manufacture Scoop Intake and Channel incl. ice and debris protection and acoustic absorbers (SIPAL)
Start date: Jan 1, 2010, End date: Mar 31, 2011,
"B.1.1 Concept and Objectives The concept of this project is to design and build a composite prototype scoop intake, incorporating the following key aspects of design • Acoustic panelling • Electro thermal ice protection • Lightning protection (if necessary) • Erosion protection • Temperature sensing The objective of the consortium team is to effectively trade the various design requirements to pr ...
Read Project
2
Partners Participants
FINISHED
SLD and Icing tests on an Ice Protected Scoop Intake and Channel (SLD_scoop)
Start date: Jan 1, 2010, End date: Mar 31, 2011,
...conditions including in-flight icing (CS-25 Appendix C), freezing fog, super-cooled large droplets (FAR 25 Appendix X) and snow (ice crystal) conditions. Our proposal if fully compliant with the CfP. AeroTex is an SME specialising in Aircraft Icing Consultancy and has over 28 years combined staff experience in icing wind tunnel testing. A commericial icing wind tunnel will be hired for the period ...
Read Project
