The design concept of Z3015 is to create a composite wing aircraft with 6-10 hours of flight time, high performance and high cost performance, easy to assemble, modify and expand. Reduce the unit hour cost of UAV to the level of foam aircraft. And expand more blue ocean application scenarios with long flight time.

We used the classic two-brace pneumatic layout which is more common. This layout and 4+1 integration have inherent structural advantages, such as high tail efficiency, concentrated mass distribution, easy to disassemble, etc., but we have also done in-depth potential mining and optimization

1, combined with the key parameters of the previous generation of long-endurance aircraft design experience, redesigned a more suitable airfoil.
2, deep integration of all parts, careful modeling of the surface, the wing tail lift is perfectly distributed.
3, the body is different from the long flow line on the market, easy to place the battery pack and adjust the center of gravity, and as far as possible to do laminar flow optimization, so that the power system intake efficiency is higher
4, the whole machine through several generations of cfd electronic wind tunnel simulation, using curved surface to control the flow line, reduce the resistance of the whole machine
5, the rotor power efficiency is deeply optimized to improve 37%, for example, the hovering power of 14kg aircraft is only 1700W, far lower than the industry's common 2700W. The propeller is placed under, further improving efficiency and reducing noise.

Product data

PNP product configuration

Information Updated version:202501071406

Note:
Production cycle: 7-15 working days (ask customer service about production schedule before ordering)
Prices and freight are for reference only, before purchasing this model, customize the product, no stock, orders need to wait for production time.