"Design, development and manufacturing of an electro-mechanical actuator and test rig for AiRcrafts Main LandIng Gear acTuation systems."

Projektinformationen

ARMLIGHT

ID Finanzhilfevereinbarung: 298176

Abgeschlossenes Projekt

Startdatum 1 Juli 2012

Enddatum 30 Juni 2016

Finanziert unter

• Specific Programme "Cooperation": Joint Technology Initiatives

Gesamtkosten € 748 030,00

EU-Beitrag € 473 692,75

Koordiniert durch

COMPANIA ESPANOLA DE SISTEMAS AERONAUTICOS SA
Spain

Ziel

"The ARMLIGhT project will design, manufacture, tune and validate an innovative and smart Electro-Mechanical Actuator for the study and validation of a future complete all-electric landing gear actuation system. ARMLIGhT actuator will be based on a modular and efficient approach that will integrate easily exchangeable electric and mechanical components with sensors and control strategies that will allow automatic and autonomous safety control.

The ARMLIGhT Electro-Mechanical Actuator will include its dedicated Electronic Control Unit, a Built In Test equipment to detect potential failures and a disable device to guarantee compatibility with emergency actuation. Different configurations will be studied and evaluated to determine the optimum system architecture from a technical point of view. Volume, mass, electrical consumption, power to mass ratio, reliability, durability and safety are concepts that will drive the development.

The ARMLIGhT system will be tested and validated at several stages: Virtual validation at model level and finally actual experimental validations of the complete system through both on-ground and in-flight test campaigns. These sequential and complementary validations will assure thus a reliable, safe and efficient performance of the prototype and will provide data for a deep concept evaluation.
For this validation purpose, the ARMLIGhT project will also design, manufacture and tune a Test Rig for ARMLIGhT Electro-Mechanical Actuator validation. ARMLIGhT Test Rig will allow installation both in Copper Bird® and in the ATR (Avions de Transport Regional) passenger cabin. The test bench will also include its own control system, inertia load simulation of the Main Landing Gear involved weight and counter-load actuator with its hydraulic and electric power supply systems."

Wissenschaftliches Gebiet

• engineering and technology › electrical engineering, electronic engineering, information engineering › electrical engineering › electric energy
• engineering and technology › electrical engineering, electronic engineering, information engineering › electronic engineering › control systems
• engineering and technology › mechanical engineering › vehicle engineering › aerospace engineering › aircraft
• engineering and technology › electrical engineering, electronic engineering, information engineering › electronic engineering › sensors

Programm/Programme

• FP7-JTI - Specific Programme "Cooperation": Joint Technology Initiatives

Thema/Themen

• JTI-CS-2011-2-GRA-03-005 - Design, development and manufacturing of EMA and Test Set-up for advanced Landing Gear System actuation

Aufforderung zur Vorschlagseinreichung

SP1-JTI-CS-2011-02
Andere Projekte für diesen Aufruf anzeigen

Finanzierungsplan

JTI-CS - Joint Technology Initiatives - Clean Sky

Koordinator

COMPANIA ESPANOLA DE SISTEMAS AERONAUTICOS SA

Kontakt Verwaltung

Esmeralda Campillo (Ms.)

• EU-Beitrag: € 174 659,00
• Adresse: PASEO JOHN LENNON 4 GETAFE ; 28906 Madrid ; Spanien
• Region: Comunidad de Madrid › Comunidad de Madrid › Madrid
• Aktivitätstyp: Private for-profit entities (excluding Higher or Secondary Education Establishments)
• Gesamtkosten: Keine Daten

Beteiligte (1)

FUNDACION TECNALIA RESEARCH & INNOVATION

Spanien

Kontakt Verwaltung

Francisco Estensoro (Mr.)

• EU-Beitrag: € 299 033,75
• Adresse: PARQUE CIENTIFICO Y TECNOLOGICO DE GIPUZKOA, PASEO MIKELETEGI 2 ; 20009 DONOSTIA-SAN SEBASTIAN (GIPUZKOA)
• Region: Noreste › País Vasco › Gipuzkoa
• Aktivitätstyp: Research Organisations
• Gesamtkosten: Keine Daten