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TRIMIS

GURNEY FLAP ACTUATOR AND MECHANISM FOR A FULL SCALE HELICOPTER ROTOR BLADE

Project

PT656 - GURNEY FLAP ACTUATOR AND MECHANISM FOR A FULL SCALE HELICOPTER ROTOR BLADE


Funding origin:
European
European Union
STRIA Roadmaps:
Vehicle design and manufacturing (VDM)
Vehicle design and manufacturing
Transport mode:
Airborne
Airbone
Transport sectors:
Passenger transport
Passenger transport
Freight transport
Freight transport
Duration:
Start date: 01/05/2011,
End date: 01/10/2015

Status: Finished
Funding details:
Total cost:
€660 615
EU Contribution:
€371 063

Overview

Objectives:

Microtecnica SrL (MT) have brought together industry leading expertise to support the design and development of a full scale Active Gurney Flap (AGF) system. The team have a combination of relevant experience in blade actuation across a range of technologies together with significant capabilities in fundamental engineering analysis to support a comprehensive review of potential solutions. The proposal reflected the joint desire of offering a risk managed baseline approach as well as ensuring all potential candidate solutions are assessed as part of the initial development task.

The consortium was lead by MT who provide the technical and programme management and the detail design and manufacture of the wind tunnel and whirl test hardware. MT was supported by Microtecnica Actuation Technologies (MAT), University of Bristol and the “Politecnico di Torino” based in Turin. The team ensured a balance of technical depth together with a commitment and capability to exploit technology for commercial gain.

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