Community Research and Development Information Service - CORDIS

Horizon 2020 project information and now also report summaries are available on CORDIS. All H2020 projects can be downloaded from the EU Open Data Portal .

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ID: AER20030
Start date: 1993-01-01, End date: 1995-12-31
The main objectives of this crashworthiness research programme are to increase the level of safety in moderate commercial aircraft crashes, to enhance European knowledge and capabilities with respect to crashworthiness of commercial aircraft, and to enable European partners to...
Programme: FP3-AERO 1C
Record Number: 5475
Last updated on: 1994-04-21
[PROJECT] LARA - Laminar Flow Research Action
ID: AER30054
Start date: 1993-01-01, End date: 1994-10-31
Aircraft engine nacelles make a significant contribution to the skin friction drag of aircraft and as such are an attractive candidate for the application of drag reducing laminar flow technology. At the beginning of 1993 two European, EC supported collaborative programmes wer...
Programme: FP3-AERO 1C
Record Number: 6002
Last updated on: 1994-04-21
ID: AER20037
Start date: 1993-01-01, End date: 1995-12-31
It was the intention of the Pilot Phase programme to demonstrate the feasibility of producing high integrity Electrically Powered Actuators (EPA) for Primary Flight Controls applications. This objective has been fulfilled both for the Electromechanic Actuator (EMA) and the Ele...
Programme: FP3-AERO 1C
Record Number: 5492
Last updated on: 1994-04-21
ID: AER20044
Start date: 1992-12-01, End date: 1996-09-30
The research programme has the following principal objectives. Better understanding of, and ability to control wake/blade interaction effects in highly loaded HP turbines. Resolution of the effects on turbine performance of coolant injection in Nozzle Guide Vanes (NGV) and ...
Programme: FP3-AERO 1C
Record Number: 5499
Last updated on: 1994-04-21
ID: AER20041
Start date: 1993-01-01, End date: 1995-12-31
Aircraft engine nacelles make a significant contribution to the skin friction drag of aircraft and as such are an attractive candidate for the application of drag reducing laminar flow technology. At the beginning of 1993 two European, EC supported collaborative programmes wer...
Programme: FP3-AERO 1C
Record Number: 5493
Last updated on: 1994-04-21
ID: AER20035
Start date: 1993-01-01, End date: 1995-12-31
This Focused Fundamental Research project is aimed at developing and validating PDF/CFD based methods for low emission combustors. Combustion sub-models currently in use by the gas-turbine manufacturer CFD codes do not incorporate finite rate chemical kinetics effects. While t...
Programme: FP3-AERO 1C
Record Number: 5495
Last updated on: 1994-07-05
ID: AER20043
Start date: 1993-01-01, End date: 1995-12-31
The IMAGES 2000 project deals with the improvement to Dependability features of avionics systems in an advanced IMA context. The study is focused on the modules of the cabinets and on the application software. The purpose is to know how to enhance the dependability of these co...
Programme: FP3-AERO 1C
Record Number: 5498
Last updated on: 1994-04-21
ID: AER20042
Start date: 1992-11-01, End date: 1995-10-31
The application of advanced materials in fuselage structures is seen as an important contribution to increase the composite content in aircraft structures. This will have an advantageous effect on the structural weight of the aircraft and consequently on the Direct Operating C...
Programme: FP3-AERO 1C
Record Number: 5535
Last updated on: 1994-04-21
ID: AERA0004
Start date: 1994-12-01, End date: 1996-08-31
The thermal behavior of the actuator has been excellent in flight with only some minor concerns when the actuator is a long time energized on the ground. This has been checked in several flights with very different flight profiles both in duration and external temperature. ...
Programme: FP3-AERO 1C
Record Number: 23738
Last updated on: 1995-02-22
ID: AER30055
Start date: 1993-03-01, End date: 1995-07-31
The objectives of the GAAS study is to define an open ATM system architecture based on a generic kernel. Thanks to the Client-Server model, the main advantage of such a study will be to federate the other ATM projects providing them interface standards. This Research and Devel...
Programme: FP3-AERO 1C
Record Number: 5983
Last updated on: 1994-04-21
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List retrieved on: 2017-11-25
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