Media

System overview

System overview of the V3, with optional launch mast. Made by: “Salma, V., Friedl, F., Schmehl, R.: Improving Reliability and Safety of Airborne Wind Energy Systems. Wind Energy 23(2), 340–356 (2019). doi: 10.1002/we.2433”

Flight path illustration

[30]: Friedl, F.: Fault-Tolerant Design of a Pumping Kite Power Flight Control System. M.Sc. Thesis, FH Joanneum, University of Applied Sciences, Graz, Austria, 9 Feb 2015. http://resolver.tudelft.nl/uuid:e704e8aa-2371-437b-8de9-80b3b7067241 [31]: Salma, V., Friedl, F., Schmehl, R.: Improving Reliability and Safety of Airborne Wind Energy Systems. Wind Energy 23(2), 340–356 (2019). doi: 10.1002/we.2433

Kite

The TU Delft V3 kite with 25 m2 wing surface area is a custom development by kite designer Martial Camblong, creator of the brand Genetrix, in close collaboration with TU Delft team members John van den Heuvel and Rolf van der Vlugt.

The kite also deforms heavily, although the right photo here is not representative for nominal flight operation but caused by an extreme steering input in combination with an only lightly loaded wing during a launching maneuver from an upside-down hanging position.

System Components

An illustration of the system components, their labels and general dimensions.
Property TUDELFT_V3_KITE
Flat area (m²) 25
Number of struts (-) 8
Flat wing span (m) 11.18
Flat maximum chord (m) 2.63
Flat aspect ratio (-) 5
Projected area (m²) 19.753
Projected wing span (m) 8.32
Projected wing height (m) 3.13
Projected aspect ratio (-) 3.498
Side view area (m²) 5.646
Leading edge 3D length (m) 11.302
Trailing edge 3D length (m) 11.249
CoG wing in x-dir. (%) 54
CoG wing in z-dir. (%) 34.3
Ixx wing (kgm²) 84.79
Iyy wing (kgm²) 13.23
Izz wing (kgm²) 83.01
Ixz wing (kgm²) -0.66
Bridle height (m) 9.60
Number of bridle lines (-) 82
Total length bridle lines (m) 96
Number of pulleys in bridle 0
Wing and bridle mass (kg) 10.6
Nominal pulling force (N) 5800

KCU details

The height (with tape guide), width and length of the KCU without exterior foam padding, as displayed in Fig. 15, is 32.7, 24.4 and 30.5 cm. Because of the space constraints under the shorter cover, the longer cover was quickly used on both sides, which increased the length without foam padding to 39 cm. With exterior foam padding this elongated but symmetric design had a height, width and length of 36, 30 and 53 cm, which takes into account the storage pouch for the progressive-tearing energy absorber.

CAD view of the KCU

In the considered time frame from 2010 until 2015, the mass of the KCU increased from initially 5 to 8.4 kg. The mass of the KCU including weak link and entire bridle line system, but excluding wing-mounted sensors and Pitot sensor, is 9 kg. The KCU is connected with the ground control computer via a fast and a separate slow wireless link. The link quality (latency) was recorded during the test flights. A fixed data rate of 20 Hz in both directions was used. The data from the angular encoders were recorded, as were the motor temperatures and the battery voltage.

Tether details

The tether is a 16-strand plaited hollow braid rope made of Dyneema® SK75, with a diameter of 4 mm, a mean breaking load of 13.5 kN, a mean breaking strain of 3.5% and a mass of 0.91 kg per 100 m.

Other

flight-path-animation

threejs model, with a “save to SVG” button