CN207843321U - A kind of 6 axis unmanned plane structures - Google Patents

Abstract

The utility model discloses a kind of 6 axis unmanned plane structures, it is combined including lower lotus disk, center bearing bracket, upper cover and active flight arm, the bottom of the lower centrally disposed holder of lotus disk, the centrally disposed cradle top of upper cover, there are six the combination of active flight arm is set, side wall of the equidistantly distributed in center bearing bracket, upper cover and lower lotus disk form a cavity, inside cavity is equipped with LED controller, power supervisor, flight controller, IMU modules and power supply, upper lid is equipped with GPS modules, close structure implements simple, low cost.

Description

A kind of 6 axis unmanned plane structures

Technical field

The utility model is related to unmanned plane field, more particularly to a kind of 6 axis unmanned plane structures.

Background technology

In unmanned vehicle field, pine and aerial dispensing are removed in the air transport of especially light weight object, and agricultural protection is answered With in the process, realizing that the flight of light structure quick and stable and the control of multi-pose quick shift is necessary；The present invention provides one 6 axis unmanned plane structures of kind, use 6 spiral power wing distribution equalizing structures, compact-sized, while meeting multi-pose control and requiring.

Utility model content

The technical problem to be solved by the utility model is to provide a kind of 6 axis unmanned plane architecture implementations, close structure, Implement simple, low cost, to solve the above-mentioned many defects caused by the prior art.

To achieve the above object, the utility model provides technical solution below：A kind of 6 axis unmanned plane structures, including under Lotus disk, center bearing bracket, upper cover and the combination of active flight arm, the bottom of the lower centrally disposed holder of lotus disk, upper cover setting exist At the top of center bearing bracket, there are six the combination of active flight arm is set, equidistantly distributed is in the side wall of center bearing bracket, upper cover and lower lotus disk group At a cavity, inside cavity is equipped with LED controller, power supervisor, flight controller, IMU modules and power supply, is set on upper lid There are GPS modules.

Preferably, active flight arm combination include center fixed seat, be connected by power arm, Rotor mount, motor and Rotary wings group；The both ends of be connected by power arm connect center fixed seat and Rotor mount by elastic fixing clamp, and motor setting exists In rotor fixed seat, motor drives the rotation of rotary wings group.

Preferably, the elastic fixing clamp is made of 1 circular arc shrapnel riveted, 2 locking card columns, and locking card column setting exists The both ends of circular arc shrapnel.

Preferably, the rotor fixed seat is equipped with mounting hole, is equipped with cooling fin in mounting hole, rotor fixed seat is being installed It is equipped with upper installation sheet above and below hole and lower installation sheet, the motor are fixed on fixinig plate.

Preferably, the rotary wings group includes upper loading board and lower loading board, and rotary wings are symmetricly set on loading board and lower loading board Between.

Preferably, the center bearing bracket is double-layer scaffold, and the center fixed arm setting of active flight arm combination is propped up in bilayer It is screwed between frame, lower lotus disk and upper cover are separately fixed at lower layer's center bearing bracket and upper layer center bearing bracket by screw On.

Preferably, the LED controller, power supervisor, flight controller, IMU modules, power supply and GPS modules use Gum is pasted and band bundled fixed.

It is using the advantageous effect of above technical scheme：The utility model structure proposes a kind of 6 axis unmanned plane structures Embodiment, it is compact-sized, implement simple；6 active flight arm combination installation distributions use hexagonal isogonism array structure, Power arm can quick-snap installation；Framework simple and compact optimizes product cost, improves resource utilization, and is beneficial to society It can environment.

Description of the drawings

Fig. 1 is the unmanned plane structural schematic diagram of the utility model；

Fig. 2 is the structural schematic diagram of active flight arm combination；

Fig. 3 is the structural schematic diagram of elastic fixing clamp.

Specific implementation mode

The preferred embodiment that according to the present invention will be described in detail below with reference to the accompanying drawings.

Fig. 1 and Fig. 2 show specific embodiment of the present utility model：It is an object of the invention to provide a kind of 6 axis unmanned planes Structure；The unmanned plane structure combines 10 by a lower lotus disk 1, two center bearing brackets 2, a upper cover 8, six active flight arms, One power supply 7 and power supervisor 4, a LED controller 3, a flight controller 5, a GPS module 9, an IMU Module 6 forms；The bottom of the 1 centrally disposed holder 2 of lower lotus disk, 8 centrally disposed holder of upper cover, 2 top, active flight There are six arm combination 10 is set, for equidistantly distributed in the side wall of center bearing bracket 2, upper cover 8 and lower lotus disk 1 form a cavity, cavity It is internally provided with LED controller 3, power supervisor 4, flight controller 5, IMU modules 6 and power supply 7, upper cover 8 is equipped with GPS modules 9。

The program combines 10 installation distributions by 6 active flight arms and uses hexagonal isogonism array structure, active flight Arm combination 10 can quick-snap installation, to reach a kind of unmanned plane structure simple and compact for structure.

Wherein each active flight arm combination 10 is by a center fixed seat 101, and two elastic fixing clamps 102, one dynamic Power linking arm 103, a Rotor mount 104, a lower installation sheet 105, a radiator 106, a upper installation sheet 107, One motor 108 and a rotary wings group 109 form, and the both ends of be connected by power arm 103 connect center by elastic fixing clamp 102 Fixed seat 101 and Rotor mount 104, motor 108 are arranged in rotor fixed seat 104, and motor 108 drives rotary wings group 109 Rotation；Rotor fixed seat 109 is equipped with mounting hole, is equipped with cooling fin 106 in mounting hole, rotor fixed seat 109 is in mounting hole Above and below be equipped with upper installation sheet 107 and lower installation sheet 105, the motor 108 and be fixed on fixinig plate 107；Rotary wings Group 109 includes upper loading board 1092 and lower loading board 1093, rotary wings 1091 be symmetricly set on loading board 1092 and lower loading board 1093 it Between.

Center bearing bracket 2 is preferentially closed using aviation duralumin metal plate or stainless steel materials punching punch forming or duralumin in the present invention Golden casting and forming；Lower lotus disk 1 and upper cover 8 use injection molding, material secondary to select ABS, ABS+ preferably with materials such as carbon fibers PC；It instantly, can be by HDPE, PET, PVC blow moldings when load plate 2 needs to cover into liquid container.The combination combination of active flight arm In, center fixed seat 101, a Rotor mount 104 and a radiator 106 are by duralumin, hard alumin ium alloy casting and forming；One power Linking arm 103 is fabricated by tube and pipe of aluminium alloy；Lower installation sheet 105 and upper installation sheet 107 are molded by stainless steel metal plate punching；

When the present invention is implemented by 6 active flight arm combination installations using hexagonal isogonism array structure, upper and lower 2 layers of center Holder 2 is fixed by 6 101 lock screws of center fixed seat；The center mounting hole 1011 of 6 center fixed seats 101 will be with 6 groups of mounting holes 21 of upper and lower 2 layers of center bearing bracket 2 are implemented to fix by screw.Other structures component is fixedly connected using screw, electricity Submodule group is pasted using gum and band bundled fixed.

In active flight arm of the present invention combination combination, center fixed seat 101 and a Rotor mount 104 and be connected by power Arm 103 is connected and fixed, and will be realized by elastic fixing clamp 102；Elastic fixing clamp 102 is by 1 1021 riveted 2 of circular arc shrapnel A locking card column 1022 forms；Elastic fixing clamp 102 is pre-loaded into the card hole 1031 of be connected by power arm 103；When center fixed seat 101 When being inserted in be connected by power arm 103 with Rotor mount 104, precompressed locking card column 1022 and 103 outer tube wall of be connected by power arm are needed Outer surface 1033 is equal to continue to be inserted in, and card hole 1013 and be connected by power arm are fixed when locking card column 1022 moves to be connected by power arm It can bounce and be locked in fixed card hole hole when fixed card hole 1041, to ensure connection locking.When dismounting, it is only necessary to push lock When determining card column 1022 and sinking to be connected by power arm and fix card hole 1013 and be connected by power arm and fix the internal face 1042 of card hole 1041, i.e., Be connected by power arm 103 can be extracted out.

Lower lotus disk 1 includes shell 12, and 12 inside of shell is equipped with fixed screw position 11 and is used for fixed center holder 2, shell bottom Portion is equipped with shaping integrated 4 support legs 13, plays unmanned plane supporting role when rising and falling；The side wall of upper cover 8 is equipped with multiple shields The gap shielding of double-layered central holder 2 is protected internal electronic module, upper cover 8 to be equipped with screw position 82 by plate 83, backplate 83, For fixed center holder 2.

Power supply after PMU progress power managements to LED controller and flight controller by powering；IMU includes storage unit Or grafting removable memory module and carry video and digital information processing Circumscribing port mouth；Flight controller is formed with IMU With motor, PMU, LED controller and GPS module wired connections after main controller, and communicated wirelessly with unmanned controller；It is main Power information of the device according to PMU is controlled, GPS information and gyroscope information carry out the automatic safe flight control for comparing goal-selling task It manages and the timely dynamic of flight motor is adjusted to realize the automatic flight management of unmanned plane, and given by LED controller Go out corresponding fluorescent tube instruction；Flight controller, which can synchronize, simultaneously receives the instruction from remote controler to carry out flight regulation and control.

The utility model structure proposes a kind of 6 axis unmanned plane architecture implementations, and compact-sized, implementation is simple；6 A active flight arm combination installation distribution uses hexagonal isogonism array structure, and power arm can quick-snap installation；Framework is simple Compact and optimized product cost, improves resource utilization, and be beneficial to social environment.

Above-described is only preferred embodiments of the present invention, it is noted that for the ordinary skill of this field For personnel, without departing from the concept of the present invention, various modifications and improvements can be made, these all belong to In the scope of protection of the utility model.

Claims (1)

1. a kind of 6 axis unmanned plane structures, which is characterized in that it is combined including lower lotus disk, center bearing bracket, upper cover and active flight arm, The bottom of the lower centrally disposed holder of lotus disk, the centrally disposed cradle top of upper cover, active flight arm combination set there are six, For equidistantly distributed in the side wall of center bearing bracket, upper cover and lower lotus disk one cavity of composition, inside cavity are equipped with LED controller, electricity Source manager, flight controller, IMU modules and power supply, upper lid are equipped with GPS modules；

The active flight arm combination includes center fixed seat, be connected by power arm, Rotor mount, motor and rotary wings group；It is dynamic The both ends of power linking arm connect center fixed seat and Rotor mount by elastic fixing clamp, and motor is arranged in rotor fixed seat Interior, motor drives the rotation of rotary wings group；The elastic fixing clamp is made of 1 circular arc shrapnel riveted, 2 locking card columns, locking card Column is arranged at the both ends of circular arc shrapnel；The rotor fixed seat is equipped with mounting hole, is equipped with cooling fin in mounting hole, rotor is fixed Seat is equipped with upper installation sheet above and below mounting hole and lower installation sheet, the motor are fixed on fixinig plate；The rotation Rotor group includes upper loading board and lower loading board, and rotary wings are symmetricly set between loading board and lower loading board；The center bearing bracket is double The center fixed arm setting of layer holder, the combination of active flight arm is screwed between double-layer scaffold, lower lotus disk and upper cover It is separately fixed on lower layer's center bearing bracket and upper layer center bearing bracket by screw；The LED controller, power supervisor, flight Controller, IMU modules, power supply and GPS modules are pasted using gum and band bundled fixed.