Makeflyeasy Hero 2180mm UAV Fixed Wing VTOL Drones – Mapping version Flight for 136 min

A significant amount of high-strength, lightweight carbon fibers, wooden boards, and PC boards are utilized in the materials.

In terms of shape, a multitude of embedded boxstructures are utilized to greatly enhance the structural strength and rigidity of the body.

Based on the 'over-load experiment', considering the structural form and load characteristics of the wing, tail, and fuselage, the structure is optimized with gram precision to reduce unnecessary weight.

The bottom of the fuselageadopts the rear three-pointlanding gear, with high groundclearance, large mountingspace, and the tail rotor doesnot touch the ground.

Aircraft center of gravitybulges under fuselagehooks and wing root plasticstart (same location).

The fuselage's inner side features wire grooves and removable baffles to aid in wire installation, ensuring a simple and efficient cabin wiring.

The nose cabin utilizes a four-point connection struc-ture, providing stability, reliability, and quick release.

A pair of 9-pin connectors in the nose cabin support the connection of signals like image transmission, remote control, and airspeed to the fuselage flight control.

The design file of the nosecabin is open source, and userscan customize the mountingplate according to the installa-tion hole position of the pod.

The dimensions of the battery compartment are 326*110*78mm, with a maximum support of 6S@30000mah solid-state lithium battery. The battery holder is CNC machined from PC board, known for its lightweight nature and excellent impact resistance.

The battery tie is composed of fiber-reinforced plastic, known for its strength and durability. The design of the tie is logical and user-friendly.

The flight control cabin employs a layered design structure to enhance space utilization. The lower layer accommodates the distribution board and landing radar.

The middle layer can instalflight control, which is compat-ible with open source/com-mercial flight control installa-tion.

The top layer can install PPK orimage transmission equipment.

The flight control hatch sup-ports screw fixing to preventforeign objects from fallingwhich is both beautiful anddust-proof.

The GPS and compass modulesare placed above and behindthe flight control cabin, andthe electromagnetic environ-ment is clean.

The position of the PPK anten.na is reserved behind the GPScabin, which is convenient toinstall the PPK antenna andimprove the accuracy of POSdata.

The tail push ESC is placedunder the rear of the flightcontrol cabin, with an exter-nal aluminum shell, which hasa good heat dissipation effect.

The 195mm rat tail glue stickantenna can be pre-buried inthe vertical tail, which notonly improves the supportstrength of the vertical tail,but also has a clean electro-magnetic environment and

The V-tail adopts a tool-freequick-release structure, whichis automatically locked withone push and pulled out im-mediately with one push.

The tail servo does not needto be pre-embedded for easymaintenance.
The servo rocker arm is designed with built-in, even ifthe rocker arm drive columnis loose, the rudder surfacecan be accurately executed.

The wing can be split into awing root segment and a wingtip segment to further reducethe storage volume.

The wing is composed of maincarbon tubes, auxiliary carbontubes, vertical arms, and plas-tic parts to form a framestructure to improve the over-all strength.

The wing root section and thefuselage are separated electri.cally and structurally through5+2 high-current connectors.

The surface of the wing rootsection is reinforced with 3Mstickers, which enhances therigidity of the aircraft and im-proves the torsion resistanceof the wing.

The wing rudder adopts servorocker arm direct drivedesign, simple and durable

The VTOL Rotor Arm is fixedby an aluminum alloy wrap-ping structure, which can beinstalled and removed as awhole for easy maintenance.

The middle section of theVTOL Rotor Arm is open to fa-cilitate the installation of ESCand servo cables.

(Optional) Wiring boardQuick-release wing powersystem

The motor seat supports thelargest outer rotor ф65mmmotor, and the size of the ESCcabin is 67*31*12mm

(Optional) Customized Esc,waterproof and dustproofgood heat dissipation effect,no fear of harsh field environ-ment.