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Development of an advanced rotor for tilt-rotor

Project

DART - Development of an advanced rotor for tilt-rotor


Funding origin:
European
European Union
STRIA Roadmaps:
Vehicle design and manufacturing (VDM)
Vehicle design and manufacturing
Network and traffic management systems (NTM)
Network and traffic management systems
Transport mode:
Airborne
Airbone
Transport sectors:
Passenger transport
Passenger transport
Freight transport
Freight transport
Duration:
Start date: 01/03/2002,
End date: 01/01/2006

Status: Finished
Funding details:

Overview

Background & policy context:

As the air passenger traffic continues to grow, by at least 5% per year, airport congestion becomes a mounting problem in Europe. Because of environmental constraints, airport extensions are more and more difficult to achieve and there is an increasing pressure for finding innovative solutions to cope with the air traffic growth expected within the next 20 years.

As already evidenced during the AIRPORT-IV study sponsored mid 90's by DG-VII, one of these innovative solutions could be the use of Rotorcraft for some of the hub-feeder missions which are today achieved with turboprop aircraft.

Indeed, thanks to their inherent Vertical Takeoff and Landing (VTOL) capability, Rotorcraft are able to reach airports without using the main runways which, in that case, could be reserved for large capacity medium/long haul jet airplanes.

The Tilt-Rotor is a relatively new configuration of Rotorcraft combining the operational capabilities and advantages of the propeller-driven airplane and of the helicopter.

Objectives:

The DART project goal was to significantly contribute to the development of a flying tilt-rotor demonstrator by achieving the following objectives:

  • to define, design, manufacture and test an advanced rotor hub for future implementation on a tilt-rotor aircraft;
  • to gain a better understanding of the technological issues associated with tilt-rotor rotor hub design;
  • to bring significant improvements compared to existing design with respect to external noise, vibration, dynamic loads, safety and costs.



 

Methodology:

The design of such an advanced rotor hub for very unconventional operations has been possible thanks to the strong effort put on the calculations methods and methodology for loads and dynamic. The definition of the requirements, the Xcross correlations between several codes performed within this project and the method developments secure the hub concept definition. This effort provides a unique expertise for the partners and increase European knowledge. Next development phases towards serial product will start basically on those methodology.

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