Purpose of the development: A drone aircraft with the original design of the combined wing, which reduces the operating load and increase flight safety system was developed.

Recommended application field: Design and construction of aircraft.

Advantages over analogues: Due to the combined structure of the wing lower operating loads acting on the structure, thereby enabling the use of thinner power elements, which makes it possible to reduce the weight of the wing. Also, due to deformation of the back of improved flight safety in critical conditions of flight.

The development stage readiness: Finishing off is required

Description of the development:
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In the developed unmanned aircraft back of the soft combined wing formed compartments made of vozduhoneproduvaemogo material. They are filled with air, the incoming flow through the air inlets located in front of the wing. Thus the wing-filled compartments form the shape of the outer surface, which is identical to the classical form. The aircraft with the combined wings can be folded to a compact size, it is easy and convenient for transportation.

corresponds technical description
Reguires revision

Possibility of transfer abroad:
Licence's sale
Combinated reduction to industrial level

Photo

Country Ukraine

For additional information turn to:
E-mail: gal@uintei.kiev.ua