Makeflyeasy Pioneer 3200mm UAV Fixed Wing VTOL Drones

The nose section uses a four-point interlocking connection structure, which is sturdy and reliable, and supports quick disassembly.

The nose section has two 9-pin connectors that support communication between the aircraft's flight control system and signals such as image transmission, remote control, and airspeed.

The battery compartment measures 340x220x156mm, and it is recommended to use four 6S 30000mAh semi-solid-state batteries.

The battery cable ties are made of nylon fiber and metal buckles, making them sturdy and durable. The cable tie layout is reasonable and convenient for fixing.

High-strength aluminum alloy and carbon fiber folding landing gear, compact in size when folded.
High ground clearance when deployed, large payload capacity, and tail rotor does not touch the ground.

The aircraft's center of gravity is located at the wing wing swivel.
Before takeoff, always check that the aircraft's center of gravity aligns with the wing swivel.

The power distribution compartment measures 130x45x34 mm.
Optional 200A power distribution board with dual Hall effect current detection on both sides; Dronecan digital communication offers strong anti-interference capabilities; and the wiring is simple and efficient.

The payload compartment measures 395x216x151mm and can hold a lightweight lidar unit weighing 3-5kg.

The cabin features cable trays and removable baffles, making wiring simple and efficient.

The flight control cabin adopts a platform-based open design, compatible with open-source/commercial flight control installations. The optional IND version flight control can greatly optimize the flight path sequence and direction.

The GPS compartment can accommodate dual GPS + compass modules, and the electromagnetic environment is clean.

Two RTK antenna mounting positions are reserved at the front and rear of the fuselage, supporting dual RTK direction finding function.

Optional cruise electronic speed controller (ESC) belly mounting, external aluminum casing for better heat dissipation.

The vertical tail fin can be pre-embedded with a 195mm rat-tail rubber rod antenna, which not only improves the support strength of the vertical tail, but also creates a clean electromagnetic environment.

The horizontal stabilizer features a tool-less quick-release design; a push automatically locks it in place, and a press allows it to be pulled out instantly.

The tail fin can be equipped with an all-metal hollow cup servo, offering greater torque and a more durable metal rocker arm.
The servo requires no pre-installation, making installation convenient.

Extensive flight testing has yielded a configuration featuring 6-series motors and 21-inch propellers, resulting in low power consumption and long endurance.
Power output is precisely matched to cruise aerodynamic requirements.

The wing's overall rigidity is ensured by two pairs of sleeves.
The main sleeve is 20x945mm in diameter, and the inner sleeve is 17x1150mm.
The secondary sleeve is 17x945mm in diameter, and the inner sleeve is 14x1000mm.

The wings and fuselage are separated by two industrial-grade high-current connectors to enhance current carrying capacity and achieve synchronous separation of electrical and mechanical components.

The steering gear bay supports the installation of an airspeed meter, which connects to a dynamic and static airspeed tube to improve airspeed detection accuracy.

The parallel drive design of the twin aileron servos provides safety redundancy and improves stability during high-speed flight.

The control surfaces are reinforced with embedded carbon nanotubes, and the rudder angle fixing plate is enlarged to reduce control surface deformation.
High-strength hinges connect the control surfaces for precise control and reliable connection.

The wingtips are designed with pre-installed navigation light mounting locations to facilitate future modifications and ensure flight safety.

The rotor adopts a regular quadrilateral structure with a side length of 1m, and the center of the rotor coincides with the center of gravity of the fixed wing to ensure a smooth transition during flight transition phases.

Applying a film to the upper and lower surfaces of the wing root enhances the dispersion of wing loads and improves torsional stiffness.

With the optional wiring harness, the entire boom of the vertical lift can be installed and removed, facilitating maintenance.

The middle section of the arm uses 30mm carbon fiber square tubing, which is tightly fitted to the main and auxiliary carbon tubing of the wing with 8 screws to ensure rigidity.

The square and round tubes adopt an aluminum alloy self-locking folding structure, which can be folded with a press and locked with a turn, making them convenient and easy to use.

Extensive testing has led to the selection of a 6-series motor and a 22-inch carbon fiber propeller, achieving a maximum pulling force of 15kg.
The high-power-density motor results in a lighter weight for the same pulling force.

Optional high-power ESC, firmware optimized according to the characteristics of motor and propeller for low heat generation and high efficiency. Large MOS chip for strong power output, tested at 80℃ for durability.