References — Ultralight Aircraft

VL-3

VL-3 homepage

Manufacturer:
Aveko, Brno, Czech Republic

VL-3 aircraft, S/N 2
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This ultralight is an aerodynamically clean low-wing single-engine aircraft manufactured from composite materials with two side-by-side seats, a bow-type hydraulic actuated retractable or fixed undercarriage and cruising speed up to 270 kph (168 mph, 146 kt) CAS.

3D geometric model of engine installation
3D geometric model of engine installation

This aircraft has been developed from the beginning in our design office as a virtual prototype in the SolidWorks package, where all works, inclusive of mechanism simulations (controls, undercarriage, etc.), are made in digital environment of the computer only.

Manufacturer of this aircraft has made laminating moulds from our CAD drawings near end of the development phase and consecutively also dummy prototype for verification and testing of all mechanisms and manufacturing process, such as is usuall in the “big” aviation.

The result of all such effort was achieving of empty weight of the equipped aircraft 301 kg (664 lb) at the first manufactured aircraft, e.g. inclusive of retractable undercarriage and rich instrument equipment.

Fixed undercarriage installation

VL-3 with fixed U/C
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VL-3 aircraft with fixed undercarriage

The VL-3 aircraft with fixed composite undercarriage was made in April 2006. This variant brings exept of custommer's financial savings also lover weight of empty aircraft. In this case it was achieved 291 kg (641.5 lb) at fully equipped aircraft with three-blade electric variable-pitch propeller, position light installation and other extra equipment.

VL-3 with fixed U/C
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VL-3 aircraft with fixed undercarriage

Furthermore, design arrangement of the undercarriage attachment allows to the aircraft owner to have retrofit his aircraft by hydraulic actuated retractable U/C by means of an upgrade kit at manufacturer's facility.

Technical data

Following table shows dimensions and performance of average VL-3 aircraft.
The MTOW value depends on certification basis of a given aircraft and on its equipment.

Technical data
Metric unitsImperial units
Wing span8,44 m27.7 ft
Length6,24 m20.5 ft
Height2,05 m6.7 ft
Wing area9,77 sq m105 sq ft
Stalling speed65 kph35 kts
Max. horizontal speed280 kph151 kts
Cruising speed210-270 kph113-145 kts
Never-exceed speed300 kph162 kts
Engine power output
(Rotax 912 ULS)
73,5 kW100 hp
Climbing6 mps1200 ft/min
Fuel consumption8 – 12 l/h2 – 3 gal/hr
Total tanks volume90 l24 gal
MTOW
(depending on version)
450-472-560 kg992-1040-1235 lb



Copyright © 2007 Vanessa Air, spol. s r. o.
Last update: 1 March 2007