Abstract
The morphing trailing edge system or flap
system, CRTEF, has been developed over
the last 10 years at DTU Wind Energy. After
a promising wind tunnel test of the system
in 2009 the INDUFLAP project has been
carried out from 2011-2014 to transfer the
technology from laboratory to industrial
manufacturing and application.
To narrow the gap between wind tunnel
testing and full scale prototype testing we
developed the rotating test rig. The overall
objectives with the rotating test rig are: 1) to
test the flap system in a realistic rotating
environment with a realistic g-loading; 2) to
measure the flap performance in real
turbulent inflow and 3) to test the flap
system in a realistic size and Reynolds
number when comparing with full scale
applications..
The rotating test rig consists of a 2.2m
blade section attached to a 10m boom and
mounted on a 100kW turbine platform. It
was installed in June 2014 and a short
measurement campaign was conducted in
the autumn 2014.
An important result of testing the flap
system on the rotating test rig was
operation of the flap system up to 30 rpm.
which a g-loading of 9-10g comparable with
the conditions on a 2-3MW turbine.
Another important result was the measured
performance of the flap system. We found
that about 5.0deg. flap angle gives the
same load change as 1deg. pitch. This is
somewhat lower than simulations have
shown which are in the range of 2 to 3 deg.
flap angle to 1deg. pitch angle for a 15%
flap. The realistic, turbulent inflow is
probably a major cause of this lower
performance.
Original language | English |
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Title of host publication | Scientific Proceedings. EWEA Annual Conference and Exhibition 2015 |
Publisher | European Wind Energy Association (EWEA) |
Publication date | 2015 |
Pages | 26-30 |
ISBN (Print) | 9782930670003 |
Publication status | Published - 2015 |
Event | EWEA Annual Conference and Exhibition 2015 - Paris, France Duration: 17 Nov 2015 → 20 Nov 2015 |
Conference
Conference | EWEA Annual Conference and Exhibition 2015 |
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Country/Territory | France |
City | Paris |
Period | 17/11/2015 → 20/11/2015 |
Keywords
- Controllable Rubber Trailing Edge Flap
- CRTEF
- Flap testing
- Morphing airfoil
- Rotating test rig
- Pressure measurements