مقاتلة Makeflyeasy 2430mm بدون طيار ذات جناح ثابت

A large number of high-strengthlight PC boards are used in mate-rials, and a large number of em-bedded box structures are usedin figure to improve the structur-al strength and rigidity of thebody in many ways

Based on the "Overload Test"according to the structure andload characteristics of thewing, tail and fuselage, thestructure was optimized as"g" precision to minimize un-necessary weight

The wing and tail adopt a toolless quick-release structure, which reduces the installationsteps and shortens the disassembly and assembly time

The head cabin cover adoptsan integral umbrella structureto prevent rainwater from en-tering the cabin

The fuselage cabin cover isspecially designed with awater channel and a wateroutlet to ensure that the air-craft has normal flight capa-bilities in little rain

The inside of the fuselage isequipped with a wire groove anda removable baffle, which ismatched with nylon braidedsleeves to ensure simple and effi-cient wiring in the cabin

Streamlined EVA cushionsare designed on both sidesof the bottom of the fuse-lage, which does not blockthe camera hole, shock ab-sorption and wear resis-tance, and improve the air-craft's course stability

The center of gravity of the air-craft is under the raised positionof fuselage hook and the wingroot plastic (same position)

The center of gravity of thehand-held lanyard duringheavy load, and the centerof gravity of the hand-liftedwing during light load

Battery cabin supports 26s@16000/22000mAh(Li-Po)whitch provides strong power forlong endurance

The battery fixed seat ismade of PC board and CNCmachined, with light weightand good impact resistance
The dual battery cable tie hasa reasonable layout, whicheffectively avoids entangle-ment

The distribution cabin cover isreserved with data transmissionantenna holes, which is conve-nient for the assembly and dis-assembly of the antenna

The design of the distributioncabin shortens the wire pathand improves the electromag.netic environment of the air-craft
With the power distributionboard, the power system ofthe fuselage can be quickly re.placed

Load cabin size:280x160x110mm

A7R/A7R2,five-lenshalf-frame tilt camera canbe placed in the main cabin

The auxiliary carbon tube adoptsa toolless quick-release design.After disassembly, it can openthe main and auxiliary cabin.ltcan be equipped with a five-lensfull-frame tilt camera or a 1.5kglightweight lidar

The open platform design of theflight control cabin facilitates theinstallation of open source /com-mercial flight control installation
Cooperating with the center boardcan make full use of the spacelayout, greatly optimizing the linesequence and direction

The double-sided roundholes ensure the accurateheight measurement of theflight control barometer andalso facilitate the installationand use of safety switches

Cooperate with the flight con-trol protective cover to pre-vent foreign matter from fall-ing, beautiful and dustproof

The RTK/PPK antenna positionis reserved at the rear of theflight control cabin, and with theRTK/PPK module,it can im-prove the POS data accuracy

The GPS module is located atthe rear of the fuselage, witha size of 69 x 63 x 18mm,which can accommodateflight control GPS and com-pass modules. The electro-magnetic environment isclean

The size of the parachute cabin is172 x 113 x52mm, which caneasily place 6-8kg parachute

The horizontal tail adopts atool-less quick-release structurewhich is automatically lockedwhen it is pushed and pulled outimmediately when pressed

The left and right horizontaltails are designed with inde.pendent control of dualservo. Even if one side fails,the aircraft can return,which improves the safetyof the aircraft

Horizontal tail servos do notneed to be buried in advance,which is convenient for servomaintenance
The rocker arm of servoadopts an embedded design,even if the rocker arm transmission column is loose, therudder surface is also accu-rately executed

Carbon tubes are embeddedin the rudder surface of thehorizontal tail to increasethe strength of the ruddersurface
Four hinges connect therudder surface, reduce therotation resistance and in-crease the accuracy ofrudder surface execution

ф12x1000mm Outer coveringф14x560mm Main carbon tubeф12x600mm Auxiliary carbon tubeEnsure the overall rigidity ofthe wing.

The wing and fuselage withthe embedded box struc-ture enhance the contor-tion resistance of the wing

Dual connector can realizesignal line redundancy,im-prove system stability, reducewiring difficulty, and is com-patible with 4 + 2 layout

The wing wiring cabin facil-itates the installation ofpower signal cables. Withthe wiring board, the wingpower system can bequickly disassembled andassembled

The aileron servo cabin notonly facilitates replacingservo, but also can beequipped with an airspeedmeter module to improve theairspeed detection accuracy

Embedded carbon tubes onthe Aileron rudder surfaceincrease the strength ofrudder surface,increase therudder angle fixing plate, andincrease the rudder surfaceresponse speed
Four hinges connect therudder surface, reduce therotation resistance and in-crease the accuracy of

Double forward-pull motor,embedded reinforced boardconnects the wing carbon tubeand the motor frame to ensurethe strength and rigidity of themotor frame