CN112170055A - High-end fixed wing unmanned aerial vehicle application rotary platform equipment - Google Patents
High-end fixed wing unmanned aerial vehicle application rotary platform equipment Download PDFInfo
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- CN112170055A CN112170055A CN202011039316.3A CN202011039316A CN112170055A CN 112170055 A CN112170055 A CN 112170055A CN 202011039316 A CN202011039316 A CN 202011039316A CN 112170055 A CN112170055 A CN 112170055A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B13/00—Machines or plants for applying liquids or other fluent materials to surfaces of objects or other work by spraying, not covered by groups B05B1/00 - B05B11/00
- B05B13/02—Means for supporting work; Arrangement or mounting of spray heads; Adaptation or arrangement of means for feeding work
- B05B13/0221—Means for supporting work; Arrangement or mounting of spray heads; Adaptation or arrangement of means for feeding work characterised by the means for moving or conveying the objects or other work, e.g. conveyor belts
- B05B13/0228—Means for supporting work; Arrangement or mounting of spray heads; Adaptation or arrangement of means for feeding work characterised by the means for moving or conveying the objects or other work, e.g. conveyor belts the movement of the objects being rotative
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B13/00—Machines or plants for applying liquids or other fluent materials to surfaces of objects or other work by spraying, not covered by groups B05B1/00 - B05B11/00
- B05B13/02—Means for supporting work; Arrangement or mounting of spray heads; Adaptation or arrangement of means for feeding work
- B05B13/0278—Arrangement or mounting of spray heads
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B15/00—Details of spraying plant or spraying apparatus not otherwise provided for; Accessories
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Abstract
The invention relates to unmanned aerial vehicle coating rotary platform equipment, in particular to high-end fixed wing unmanned aerial vehicle coating rotary platform equipment which comprises a lifting mechanism, a fixing mechanism, a rotating mechanism, a water circulation mechanism, a pressurizing paint spraying mechanism and an unmanned aerial vehicle model mechanism.
Description
Technical Field
The invention relates to unmanned aerial vehicle coating rotary platform equipment, in particular to high-end fixed wing unmanned aerial vehicle coating rotary platform equipment.
Background
When the fixed wing unmanned aerial vehicle application, often need rise for unmanned aerial vehicle rotatory, but do not have better unmanned aerial vehicle application rotary platform equipment on the market, so designed this kind of high-end fixed wing unmanned aerial vehicle application rotary platform equipment.
Disclosure of Invention
The invention mainly solves the technical problem of providing high-end fixed wing unmanned aerial vehicle coating rotary platform equipment, which can lift an unmanned aerial vehicle, fix the unmanned aerial vehicle when the unmanned aerial vehicle is lifted, rotate the fixed unmanned aerial vehicle, pressurize and spray paint through a spray nozzle, and prevent static electricity from being generated through water circulation under a microporous plate when the equipment is used for spraying paint.
In order to solve the technical problem, the invention relates to an unmanned aerial vehicle coating rotary platform device, in particular to a high-end fixed wing unmanned aerial vehicle coating rotary platform device which comprises a lifting mechanism, a fixing mechanism, a rotating mechanism, a water circulation mechanism, a pressurizing paint spraying mechanism and an unmanned aerial vehicle model mechanism.
The lifting mechanism is connected with the fixing mechanism, the fixing mechanism is connected with the rotating mechanism, the rotating mechanism is connected with the lifting mechanism, the water circulation mechanism is connected with the lifting mechanism, the pressurizing paint spraying mechanism is connected with the lifting mechanism, and the water circulation mechanism is connected with the pressurizing paint spraying mechanism.
As a further optimization of the technical scheme, the invention relates to high-end fixed wing unmanned aerial vehicle coating rotary platform equipment, wherein a lifting mechanism comprises a motor mounting plate, a motor shaft bearing plate, a lifting gear, a lifting rack, a rack connecting plate, a rubber elastic strip, a reverse shaft a, a reverse gear b, a reverse shaft b, a mounting plate a, a mounting plate b, a mounting plate c, a mounting plate d, a mounting plate e and a mounting plate f, the motor mounting plate is connected with the motor, the motor is connected with the motor shaft, the motor shaft is connected with the motor shaft bearing plate, the motor shaft bearing plate is connected with the mounting plate a, the lifting gear is connected with the motor shaft, the lifting rack is meshed with the lifting gear, the rack connecting plate is connected with the lifting rack, two ends of the rubber elastic strip are connected with the rack, the reverse gear a is connected with the reverse shaft a, the reverse gear b is meshed with the reverse gear a, the reverse shaft b is connected with the reverse gear b, the mounting plate a is connected with the mounting plate b, the mounting plate b is connected with the mounting plate c, the mounting plate c is connected with the mounting plate d, the mounting plate d is connected with the mounting plate a, the mounting plate e is connected with the mounting plate a, the mounting plate f is connected with the mounting plate a, the motor mounting plate is connected with the mounting plate a, the lifting rack is slidably connected with the mounting plate a, the reverse shaft b is connected with the motor shaft bearing plate, the mounting plate b is connected with the mounting plate e, the mounting plate c is connected with the mounting plate e, the mounting plate d is connected with the mounting plate e, the mounting plate b is connected with the mounting plate f, the mounting plate c is connected with the mounting plate f.
As a further optimization of the technical scheme, the high-end fixed wing unmanned aerial vehicle coating rotary platform device comprises a connecting belt a, a connecting shaft a, a connecting gear a, a connecting friction wheel, a connecting shaft b, a pressing shaft, a limiting connecting plate a, a limiting block, a connecting shaft b bearing plate, a connecting belt b, a limiting connecting plate b, a resetting shaft, a resetting limiting plate, a resetting spring, a resetting block, a resetting groove a and a resetting groove b, wherein the connecting belt a is in friction connection with the reverse shaft b, the connecting shaft a is in friction connection with the connecting belt a, the connecting gear a is in friction connection with the connecting belt a, the connecting friction wheel connecting shaft b is connected with the connecting gear a, the pressing shaft is in friction connection with the connecting friction wheel, the limiting connecting plate a is connected with the pressing shaft, the limiting block is connected with the limiting connecting plate a, and the connecting shaft b bearing plate is in bearing connection with the, connecting belt b and motor shaft friction coupling, spacing connecting plate b is connected with the oppression axle of opposite side, the axle that resets and spacing connecting plate b sliding connection, the limiting plate that resets is connected with the axle that resets, reset spring cover is epaxial and spacing in spacing connecting plate b and the limiting plate that resets, the piece that resets is connected with the axle that resets, reset groove an is connected with the piece that resets, it is connected with spacing connecting plate b to reset groove b, the connecting axle b bearing plate and the mounting panel e of one side are connected, the connecting axle b bearing plate and the mounting panel f of opposite side are connected, the oppression axle and the mounting panel e sliding connection of one side, the oppression axle and the mounting panel f sliding.
As a further optimization of the technical scheme, the rotary mechanism comprises a rotary motor, a rotary motor shaft, a rotary belt a, a rotary belt b, a rotary transmission shaft a, a rotary belt c, a rotary transmission shaft b and a rotary belt d, wherein the rotary motor is connected with the rotary motor shaft, the rotary motor shaft is in friction connection with the rotary belt a, the rotary belt a is in friction connection with the rotary belt b, the rotary belt b is in friction connection with the rotary transmission shaft a, the rotary transmission shaft a is in friction connection with the rotary belt c, the rotary belt c is in friction connection with the rotary transmission shaft b, the rotary transmission shaft b is in friction connection with the rotary belt d, a pressing shaft at one side is in friction connection with the rotary belt b, a pressing shaft at one side is in friction connection with the rotary belt d, and the rotary motor is connected with an installation plate f, the rotating motor shaft is connected with the mounting plate f through a bearing, the rotating transmission shaft a is connected with the mounting plate e through a bearing, the rotating transmission shaft a is connected with the mounting plate f through a bearing, and the rotating transmission shaft b is connected with the mounting plate e through a bearing.
As a further optimization of the technical scheme, the invention relates to a high-end fixed wing unmanned aerial vehicle coating rotary platform device, wherein a water circulation mechanism comprises a water circulation motor, a water circulation motor shaft, a water circulation belt a, a water circulation transmission shaft a, a water circulation belt b, a water circulation transmission shaft b, a water circulation belt c, a water circulation transmission shaft c, a water circulation friction wheel, a propeller transmission shaft, a reaction force propeller, an air suction duct, an air suction conical duct, a water suction pipe, a water discharge pipe, a connecting plate a, a connecting plate b, a connecting plate c and a connecting plate d, the water circulation motor is connected with the water circulation motor shaft, the water circulation motor shaft is connected with the water circulation belt a in a friction manner, the water circulation belt a is connected with the water circulation transmission shaft a in a friction manner, the water circulation transmission shaft a is connected with the water circulation belt b in a friction manner, the water circulation belt b is connected with the water circulation transmission shaft b in, the water circulation belt c is in friction connection with the water circulation transmission shaft c, the water circulation transmission shaft c is in friction connection with the water circulation friction wheel, the water circulation friction wheel is connected with the propeller transmission shaft, the propeller transmission shaft is connected with the reaction force propeller, the reaction force propeller is in sliding connection with the air suction duct, the air suction conical duct is connected with the air suction duct, the water suction pipe is connected with and connected with the connecting plate a, the connecting plate a is connected with the connecting plate b, the connecting plate b is connected with the connecting plate c, the connecting plate c is connected with the connecting plate d, the water circulation motor is connected with the mounting plate f, the water circulation transmission shaft a is in bearing connection with the connecting plate c, the water circulation transmission shaft b is in bearing connection with the connecting plate a, the propeller transmission shaft is in bearing connection with the connecting plate b, the air suction duct is connected with the connecting plate d, the water suction pipe penetrates through the mounting plate a and is connected with the mounting plate a, the water discharge pipe penetrates through the connecting plate d and is connected with the connecting plate d, the water discharge pipe penetrates through the mounting plate a and is connected with the mounting plate a, the connecting plate a is connected with the connecting plate c, the connecting plate a is connected with the connecting plate d, the connecting plate d is connected with the mounting plate e, and the connecting plate d is connected with the mounting plate f.
As a further optimization of the technical scheme, the invention relates to a high-end fixed wing unmanned aerial vehicle coating rotary platform device, wherein a pressurized paint spraying mechanism comprises a device mounting hole, a pressurized connecting plate, a pressurized barrel, a pressurized propeller connecting shaft, a pressurized propeller connecting shaft limiting plate, a paint spraying pipe, a pressurized hole, a spray nozzle, a paint box connecting plate a, a paint box connecting plate b and a paint box connecting plate c, the device mounting hole is formed in the paint box connecting plate a and is connected with the pressurized barrel, the pressurized connecting plate is connected with the pressurized barrel in a sliding manner, the pressurized barrel is connected with and communicated with the paint spraying pipe, the pressurized propeller connecting shaft is connected with the pressurized connecting plate, the pressurized propeller is connected with the pressurized propeller connecting shaft limiting plate, the pressurized propeller connecting shaft bearing is connected with the pressurized propeller connecting shaft, the paint spraying pipe is connected with the pressurized hole, the pressurized hole is, paint case connecting plate an is connected with paint case connecting plate b, and paint case connecting plate b is connected with paint case connecting plate c, and paint case connecting plate c is connected with paint case connecting plate a, and the pressure boost connecting plate is connected with hydrologic cycle transmission shaft a, and the pressure boost connecting plate is connected with the pressure boost screw connecting axle, and pressure boost bucket and pressure boost screw connecting axle limiting plate are connected, and the pipe that sprays paint passes mounting panel a, and paint case connecting plate c is connected with mounting panel c.
According to the high-end fixed wing unmanned aerial vehicle coating rotary platform equipment, the unmanned aerial vehicle model mechanism comprises a nose skin, wings, a body skin, a tail wing skin, a rear undercarriage and a front undercarriage, wherein the nose skin is connected with the wings, the body skin is connected with the nose skin, the tail wing skin is connected with the body skin, the rear undercarriage is connected with the body skin, and the front undercarriage is connected with the head skin.
As a further optimization of the technical scheme, the high-end fixed wing unmanned aerial vehicle coating rotary platform equipment is characterized in that the paint spraying pipe is a rubber hose.
As a further optimization of the technical scheme, the coating rotary platform equipment for the high-end fixed-wing unmanned aerial vehicle is characterized in that the surface of the mounting plate a is provided with micropores.
The coating rotary platform equipment for the high-end fixed-wing unmanned aerial vehicle has the beneficial effects that:
according to the high-end fixed wing unmanned aerial vehicle coating rotary platform equipment, the equipment can lift the unmanned aerial vehicle, the equipment can fix the unmanned aerial vehicle when the unmanned aerial vehicle is lifted, the equipment can rotate the fixed unmanned aerial vehicle, the equipment can pressurize and spray paint through the spray nozzle, and the equipment can prevent static electricity from being generated through water circulation under the microporous plate when the paint is sprayed.
Drawings
The invention is described in further detail below with reference to the accompanying drawings and specific embodiments.
Fig. 1 is a schematic structural diagram of a high-end fixed-wing unmanned aerial vehicle painting rotary platform device according to the present invention.
Fig. 2 is a schematic structural diagram of a second high-end fixed-wing unmanned aerial vehicle painting rotary platform device of the invention.
Fig. 3 is a first structural schematic diagram of a lifting mechanism 1 of a high-end fixed-wing unmanned aerial vehicle painting rotary platform device of the invention.
Fig. 4 is a schematic structural diagram of a second lifting mechanism 1 of the coating rotary platform device of the high-end fixed-wing unmanned aerial vehicle of the invention.
Fig. 5 is a third schematic structural diagram of the lifting mechanism 1 of the coating rotary platform device of the high-end fixed-wing unmanned aerial vehicle of the invention.
Fig. 6 is a first schematic structural diagram of a fixing mechanism 2 of a high-end fixed-wing drone painting rotary platform device according to the present invention.
Fig. 7 is a second schematic structural diagram of the fixing mechanism 2 of the high-end fixed-wing unmanned aerial vehicle painting rotary platform device of the invention.
Fig. 8 is a third schematic structural diagram of the fixing mechanism 2 of the high-end fixed-wing unmanned aerial vehicle painting rotary platform device of the invention.
Fig. 9 is a schematic structural diagram of a first rotating mechanism 3 of the painting rotating platform device of the high-end fixed-wing drone of the present invention.
Fig. 10 is a schematic structural diagram of a second rotating mechanism 3 of the painting rotating platform device of the high-end fixed-wing drone of the present invention.
Fig. 11 is a schematic structural diagram of a water circulation mechanism 4 of a high-end fixed-wing drone painting rotary platform device according to the present invention.
Fig. 12 is a schematic structural diagram of a water circulation mechanism 4 of a high-end fixed-wing drone painting rotary platform device according to the present invention.
Fig. 13 is a third schematic structural diagram of a water circulation mechanism 4 of the high-end fixed-wing drone painting rotary platform device of the present invention.
Fig. 14 is a fourth schematic structural diagram of the water circulation mechanism 4 of the high-end fixed-wing drone painting rotary platform device according to the present invention.
Fig. 15 is a first structural schematic diagram of a pressurized paint spraying mechanism 5 of a painting rotary platform device of a high-end fixed-wing drone according to the present invention.
Fig. 16 is a second structural schematic diagram of the pressurized paint spraying mechanism 5 of the painting rotary platform equipment of the high-end fixed-wing drone of the present invention.
Fig. 17 is a third schematic structural diagram of a pressurized paint spraying mechanism 5 of a painting rotary platform device of a high-end fixed-wing drone according to the present invention.
Fig. 18 is a fourth schematic structural diagram of the pressurized paint spraying mechanism 5 of the high-end fixed-wing drone painting rotary platform equipment according to the present invention.
Fig. 19 is a schematic structural view of an equipment mounting hole 5-1 of the high-end fixed-wing drone painting rotary platform equipment of the present invention.
Fig. 20 is a schematic structural diagram of an unmanned aerial vehicle model mechanism 6 of a high-end fixed-wing unmanned aerial vehicle painting rotary platform device according to the present invention.
In the figure: a lifting mechanism 1; a motor mounting plate 1-1; a motor 1-2; a motor shaft 1-3; a motor shaft bearing plate 1-4; 1-5 of a lifting gear; 1-6 of lifting racks; 1-7 rack connecting plates; 1-8 parts of rubber elastic strips; reverse axis a 1-9; reverse gear a 1-10; reverse gear b 1-11; a reverse shaft b 1-12; mounting plate a 1-13; mounting plate b 1-14; mounting plate c 1-15; mounting plate d 1-16; mounting plate e 1-17; mounting plate f 1-18; 1-19 of a lifting belt; a fixing mechanism 2; a connecting belt a 2-1; connecting shaft a 2-2; connecting gear a 2-3; connecting friction wheels 2-4; connecting shaft b 2-5; 2-6 of a compression shaft; a limit connecting plate a 2-7; 2-8 parts of a limiting block; connecting shaft b bearing plates 2-9; a connecting belt b 2-10; a limit connecting plate b 2-11; 2-12 of a reset shaft; resetting the limit plates 2-13; 2-14 parts of a return spring; 2-15 of a reset block; reset grooves a 2-16; reset grooves b 2-17; a rotating mechanism 3; a rotating electrical machine 3-1; a rotating motor shaft 3-2; the rotating belt a 3-3; a rotating belt b 3-4; a rotary transmission shaft a 3-5; rotating belt c 3-6; a rotary transmission shaft b 3-7; rotating belt d 3-8; a water circulation mechanism 4; a water circulation motor 4-1; 4-2 of a water circulation motor shaft; a water circulation belt a 4-3; a water circulation transmission shaft a 4-4; a water circulation belt b 4-5; a water circulation transmission shaft b 4-6; a water circulation belt c 4-7; a water circulation transmission shaft c 4-8; 4-9 parts of water circulation friction wheel; 4-10 parts of a propeller transmission shaft; 4-11 of a reaction force propeller; 4-12 of an air suction duct; 4-13 of a suction conical duct; 4-14 parts of a suction pipe; 4-15 parts of a drain pipe; connection board a 4-16; connecting plate b 4-17; connecting plate c 4-18; connecting plates d 4-19; a pressurized paint spraying mechanism 5; an equipment mounting hole 5-1; a pressurizing connecting plate 5-2; 5-3 of a pressurizing barrel; a supercharging propeller connecting shaft 5-4; 5-5 parts of a pressurizing propeller; a booster propeller connecting shaft limiting plate 5-6; 5-7 parts of a paint spraying pipe; 5-8 of pressurizing holes; 5-9 parts of a spray head; a paint box connecting plate a 5-10; a paint box connecting plate b 5-11; a paint box connecting plate c 5-12; an unmanned aerial vehicle model mechanism 6; 6-1 of nose skin; wing 6-2; 6-3 of fuselage skin; 6-4 parts of tail wing skin; a rear landing gear 6-5; nose gear 6-6.
Detailed Description
The first embodiment is as follows:
the present invention relates to a rotary platform device for painting unmanned aerial vehicles, and more particularly to a rotary platform device for painting high-end fixed wing unmanned aerial vehicles, which includes a lifting mechanism 1, a fixing mechanism 2, a rotating mechanism 3, a water circulation mechanism 4, a pressurized painting mechanism 5, and an unmanned aerial vehicle model mechanism 6, and can lift the unmanned aerial vehicle, fix the unmanned aerial vehicle when the unmanned aerial vehicle is lifted, rotate the fixed unmanned aerial vehicle, pressurize and spray paint through a nozzle, and prevent static electricity from being generated by water circulation under a micropore plate when the device is used for painting.
The lifting mechanism 1 is connected with the fixing mechanism 2, the fixing mechanism 2 is connected with the rotating mechanism 3, the rotating mechanism 3 is connected with the lifting mechanism 1, the water circulation mechanism 4 is connected with the lifting mechanism 1, the pressurizing paint spraying mechanism 5 is connected with the lifting mechanism 1, and the water circulation mechanism 4 is connected with the pressurizing paint spraying mechanism 5.
The second embodiment is as follows:
the following describes the present embodiment with reference to fig. 1, fig. 2, fig. 3, fig. 4, fig. 5, fig. 6, fig. 7, fig. 8, fig. 9, fig. 10, fig. 11, fig. 12, fig. 13, fig. 14, fig. 15, fig. 16, fig. 17, fig. 18, fig. 19, and fig. 20, and the present embodiment further describes the present embodiment, where the lifting mechanism 1 includes a motor mounting plate 1-1, a motor 1-2, a motor shaft 1-3, a motor shaft bearing plate 1-4, a lifting gear 1-5, a lifting rack 1-6, a rack connecting plate 1-7, a rubber elastic strip 1-8, a reverse shaft a1-9, a reverse gear a1-10, a reverse gear b1-11, a reverse shaft b1-12, a mounting plate a1-13, a mounting plate b1-14, a mounting plate c1-15, a mounting plate d1-16, a mounting plate e1-17, a mounting, Mounting plate f1-18, motor mounting plate 1-1 is connected with motor 1-2, motor 1-2 is connected with motor shaft 1-3, motor shaft 1-3 is connected with motor shaft bearing plate 1-4, motor shaft bearing plate 1-4 is connected with mounting plate a1-13, lifting gear 1-5 is connected with motor shaft 1-3, lifting rack 1-6 is engaged with lifting gear 1-5, rack connecting plate 1-7 is connected with lifting rack 1-6, two ends of rubber elastic strip 1-8 are connected with rack connecting plate 1-7, reverse shaft a1-9 is connected with motor shaft bearing plate 1-4, reverse gear a1-10 is connected with reverse shaft a1-9, reverse gear b1-11 is engaged with reverse gear a1-10, the reverse shaft b1-12 is connected with a reverse gear b1-11, the mounting plates a1-13 are connected with mounting plates b1-14, the mounting plates b1-14 are connected with mounting plates c1-15, the mounting plates c1-15 are connected with mounting plates d1-16, the mounting plates d1-16 are connected with mounting plates a1-13, the mounting plates e1-17 are connected with mounting plates a1-13, the mounting plates f1-18 are connected with mounting plates a1-13, the motor mounting plates 1-1 are connected with mounting plates a1-13, the lifting racks 1-6 are slidably connected with the mounting plates a1-13, the reverse shaft b1-12 is connected with a motor shaft bearing plate 1-4, the mounting plates b1-14 are connected with mounting plates e1-17, the mounting plates c1-15 are connected with mounting plates e1-17, the mounting plates d1-16 are connected with mounting plates e1-17, the mounting plate b1-14 is connected with the mounting plate f1-18, the mounting plate c1-15 is connected with the mounting plate f1-18, the mounting plate d1-16 is connected with the mounting plate f1-18, the lifting belts 1-19 are in friction connection with the motor shafts 1-3, the lifting belts 1-19 are in friction connection with the reverse shaft a1-9, the device can lift the unmanned aerial vehicle, the motors 1-2 work to drive the motor shafts 1-3 to rotate, the motor shafts 1-3 rotate to drive the lifting gears 1-5 to rotate, the lifting gears 1-5 rotate to drive the lifting racks 1-6 to ascend or descend, the motor shafts 1-3 simultaneously drive the reverse shaft a1-9 to rotate through the lifting belts 1-19, the reverse shaft a1-9 rotates to drive the reverse gear a1-10 to rotate, the reverse gear a1-10 rotates to drive the reverse gear b1-11 to rotate reversely, the reverse gear b1-11 rotates to drive the reverse shaft b1-12 to rotate, the reverse shaft b1-12 rotates to drive the lifting gear 1-5 on the reverse shaft b1-12 to rotate in the direction, the lifting gear 1-5 rotating in the direction drives the lifting rack 1-6 to ascend or descend, the lifting rack 1-6 moves to drive the rubber elastic strip 1-8 to move through the rack connecting plate 1-7, the fixed wing unmanned aerial vehicle is placed on the rubber elastic strip 1-8, the rubber elastic strip 1-8 on one side close to the mounting plate e1-17 is supported between the wing 6-2 and the front landing gear 6-6, the rubber elastic strip 1-8 on the other side is supported between the wing 6-2 and the rear landing gear 6-5, at this time, the ascending or descending of the rubber elastic strips 1-8 can support the unmanned aerial vehicle to ascend or descend.
The third concrete implementation mode:
the embodiment is described below with reference to fig. 1, fig. 2, fig. 3, fig. 4, fig. 5, fig. 6, fig. 7, fig. 8, fig. 9, fig. 10, fig. 11, fig. 12, fig. 13, fig. 14, fig. 15, fig. 16, fig. 17, fig. 18, fig. 19, and fig. 20, and the embodiment further describes the embodiment, where the fixing mechanism 2 includes a connecting belt a2-1, a connecting shaft a2-2, a connecting gear a2-3, a connecting friction wheel 2-4, a connecting shaft b2-5, a pressing shaft 2-6, a limit connecting plate a2-7, a limit block 2-8, a connecting shaft b bearing plate 2-9, a connecting belt b2-10, a limit connecting plate b2-11, a reset shaft 2-12, a reset limit plate 2-13, a reset spring 2-14, a reset block 2-15, a reset groove a2-16, a reset groove b2-10, A reset groove b2-17, a connecting belt a2-1 is in frictional connection with a reverse shaft b1-12, a connecting shaft a2-2 is in frictional connection with a connecting belt a2-1, a connecting gear a2-3 is in frictional connection with a connecting belt a2-1, a connecting shaft b2-5 of a connecting friction wheel 2-4 is connected, a connecting shaft b2-5 is connected with a connecting gear a2-3, a pressing shaft 2-6 is in frictional connection with a connecting friction wheel 2-4, a limit connecting plate a2-7 is connected with a pressing shaft 2-6, a limit block 2-8 is connected with a limit connecting plate a2-7, a connecting shaft b bearing plate 2-9 is in bearing connection with a connecting shaft b2-5, a connecting belt b2-10 is in frictional connection with a motor shaft 1-3, a limit connecting plate b2-11 is connected with a pressing shaft 2-6 on the other, reset shafts 2-12 are connected with limit connecting plates b2-11 in a sliding way, reset limit plates 2-13 are connected with reset shafts 2-12, reset springs 2-14 are sleeved on the reset shafts 2-12 and limited on the limit connecting plates b2-11 and the reset limit plates 2-13, reset blocks 2-15 are connected with the reset shafts 2-12, reset grooves a2-16 are connected with the reset blocks 2-15, reset grooves b2-17 are connected with the limit connecting plates b2-11, connecting shaft b bearing plates 2-9 at one side are connected with mounting plates e1-17, connecting shaft b bearing plates 2-9 at the other side are connected with mounting plates f1-18, pressing shafts 2-6 at one side are connected with mounting plates e1-17 in a sliding way, pressing shafts 2-6 at the other side are connected with mounting plates f1-18 in a sliding way, the device can fix the unmanned aerial vehicle when the unmanned aerial vehicle is lifted, the motor 1-2 works to drive the motor shaft 1-3 to rotate, the motor shaft 1-3 also drives the reverse shaft a1-9 to rotate through the lifting belt 1-19, the reverse shaft a1-9 rotates to drive the connecting shaft a2-2 to rotate through the connecting belt a2-1, the connecting belt a2-1 also drives the connecting gear a2-3 to rotate when moving along with the connecting belt a2-1, the connecting gear a2-3 rotates to drive the connecting shaft b2-5 to rotate, the connecting shaft b2-5 rotates to drive the connecting friction wheel 2-4 to rotate, the connecting friction wheel 2-4 rotates to drive the compression shaft 2-6 on the same side to move transversely, the compression shaft 2-6 on the other side synchronously moves under the action of the connecting belt b2-10 and the motor shaft 1, two pressing shafts 2-6 move towards the center of the equipment or the outside of the equipment simultaneously, when the pressing shafts 2-6 move towards the center of the equipment, the pressing shafts 2-6 move to drive two limiting blocks 2-8 through limiting connecting plates a2-7, the grooves on the limiting blocks 2-8 move to be contacted with the curved beams of the nose landing gear 6-6, the relative position of the nose landing gear 6-6 is limited, the limiting blocks 2-8 continue to move to be completely propped against the curved beams of the nose landing gear 6-6, meanwhile, the pressing shafts 2-6 on the other side move to drive limiting connecting plates b2-11 to move synchronously, the limiting connecting plates b2-11 move to drive limiting connecting plates a2-7 to move, when the limiting connecting plates a2-7 move to be contacted with the rear landing gear 6-5, the limiting connecting plates a2-7 continue to move and under the action of return springs 2-14, the return grooves a2-16 and b2-17 completely restrict the rear landing gear 6-5 of the column, and the pressing shaft 2-6 on the other side stops moving, so that the rear landing gear 6-5 and the nose landing gear 6-6 are fixed simultaneously.
The fourth concrete implementation mode:
referring to fig. 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, the embodiment is further described, and the embodiment includes a rotating mechanism 3 including a rotating motor 3-1, a rotating motor shaft 3-2, a rotating belt a3-3, a rotating belt b3-4, a rotating transmission shaft a3-5, a rotating belt c3-6, a rotating transmission shaft b3-7, a rotating belt d3-8, the rotating motor 3-1 is connected to the rotating motor shaft 3-2, the rotating motor shaft 3-2 is frictionally connected to the rotating belt a3-3, the rotating belt a3-3 is frictionally connected to the rotating belt b3-4, the rotating belt b3-4 is frictionally connected to the rotating transmission shaft a3-5, the rotary transmission shaft a3-5 is in frictional connection with a rotary belt c3-6, the rotary belt c3-6 is in frictional connection with a rotary transmission shaft b3-7, the rotary transmission shaft b3-7 is in frictional connection with a rotary belt d3-8, the pressing shaft 2-6 at one side is in frictional connection with a rotary belt b3-4, the pressing shaft 2-6 at one side at the other side is in frictional connection with a rotary belt d3-8, the rotary motor 3-1 is connected with an installation plate f1-18, the rotary motor shaft 3-2 is in bearing connection with an installation plate f1-18, the rotary transmission shaft a3-5 is in bearing connection with an installation plate e1-17, the rotary transmission shaft a3-5 is in bearing connection with an installation plate f1-18, the rotary transmission shaft b3-7 is in bearing connection with an installation plate e1-17, and the device can, the fixed wing unmanned aerial vehicle is fixed, the rotating motor 3-1 works to drive the rotating motor shaft 3-2 to rotate, the rotating motor shaft 3-2 rotates to drive the compression shaft 2-6 on one side to rotate through the rotating belt b3-4, the rotating motor shaft 3-2 simultaneously drives the rotating transmission shaft a3-5 to rotate through the rotating belt a3-3, the rotating transmission shaft a3-5 rotates to drive the rotating transmission shaft b3-7 to rotate through the rotating belt c3-6, the rotating transmission shaft b3-7 rotates to drive the compression shaft 2-6 on the other side to rotate through the rotating belt d3-8, and the equipment rotates when the two compression shafts 2-6 simultaneously rotate in the same direction.
The fifth concrete implementation mode:
the embodiment is further described by combining the following figures 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19 and 20. the embodiment 4 comprises a water circulation motor 4-1, a water circulation motor shaft 4-2, a water circulation belt a4-3, a water circulation transmission shaft a4-4, a water circulation belt b4-5, a water circulation transmission shaft b4-6, a water circulation belt c4-7, a water circulation transmission shaft c4-8, a water circulation friction wheel 4-9, a propeller transmission shaft 4-10, a reaction propeller 4-11, an air suction duct 4-12, an air suction tapered duct 4-13, a water suction pipe 4-14, 14 and 20, 4-15 parts of drain pipe, 4-16 parts of connecting plate a4-16 part, 4-17 parts of connecting plate b4-17 part, c4-18 part and d4-19 part, 4-1 part of water circulation motor is connected with 4-2 part of water circulation motor shaft, 4-2 part of water circulation motor shaft is connected with 4-3 part of water circulation belt a4-3 part, 4-3 part of water circulation belt a is connected with 4-4 part of water circulation driving shaft a, 4-4 part of water circulation driving shaft a is connected with 4-5 part of water circulation belt b, 4-5 part of water circulation belt b is connected with 4-6 part of water circulation driving shaft b, 4-6 part of water circulation driving shaft b is connected with 4-7 part of water circulation belt c, 4-7 part of water circulation belt c4-8 part of water circulation driving shaft c4-8 part of water circulation driving shaft c is connected with 4-, the water circulation friction wheel 4-9 is connected with the propeller transmission shaft 4-10, the propeller transmission shaft 4-10 is connected with the reaction force propeller 4-11, the reaction force propeller 4-11 is connected with the air suction duct 4-12 in a sliding way, the air suction tapered duct 4-13 is connected with the air suction duct 4-12, the water suction pipe 4-14 is connected with the connecting plate a4-16, the connecting plate a4-16 is connected with the connecting plate b4-17, the connecting plate b4-17 is connected with the connecting plate c4-18, the connecting plate c4-18 is connected with the connecting plate d4-19, the water circulation motor 4-1 is connected with the mounting plate f1-18, the water circulation transmission shaft a4-4 is connected with the connecting plate c4-18 by bearing, the water circulation transmission shaft b4-6 is connected with the connecting plate a4-16 by bearing, the water circulation transmission shaft c4-8 is connected with a connecting plate a4-16 through a bearing, the propeller transmission shaft 4-10 is connected with a connecting plate b4-17 through a bearing, the air suction duct 4-12 is connected with a connecting plate d4-19, the water suction pipe 4-14 penetrates through a connecting plate d4-19 and is connected with a connecting plate d4-19, the water suction pipe 4-14 penetrates through a mounting plate a1-13 and is connected with a mounting plate a1-13, the water discharge pipe 4-15 penetrates through a connecting plate d4-19 and is connected with a connecting plate d4-19, the water discharge pipe 4-15 penetrates through a mounting plate a1-13 and is connected with a mounting plate a1-13, the connecting plate a4-16 is connected with a connecting plate c4-18, the connecting plate a4-16 is connected with a connecting plate d4-19, the connecting plate d4-19 is connected with a mounting plate e1-17, and the connecting.
The sixth specific implementation mode:
referring to fig. 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19 and 20, the present embodiment will be further described, wherein the pressurized paint spraying mechanism 5 comprises an equipment mounting hole 5-1, a pressurized connecting plate 5-2, a pressurized barrel 5-3, a pressurized propeller connecting shaft 5-4, a pressurized propeller 5-5, a pressurized propeller connecting shaft limiting plate 5-6, a paint spraying pipe 5-7, a pressurized hole 5-8, a spraying head 5-9, a paint box connecting plate a5-10, a paint box connecting plate b5-11 and a paint box connecting plate c5-12, the equipment mounting hole 5-1 is opened on the paint box connecting plate a5-10 and connected with the pressurized barrel 5-3, the pressurizing connecting plate 5-2 is connected with the pressurizing barrel 5-3 in a sliding way, the pressurizing barrel 5-3 is connected and communicated with a paint spraying pipe 5-7, a pressurizing propeller connecting shaft 5-4 is connected with the pressurizing connecting plate 5-2, the pressurizing propeller 5-5 is connected with the pressurizing propeller connecting shaft 5-4, a pressurizing propeller connecting shaft limiting plate 5-6 is connected with a pressurizing propeller connecting shaft 5-4 bearing, the paint spraying pipe 5-7 is connected with a pressurizing hole 5-8, the pressurizing hole 5-8 is arranged on the pressurizing barrel 5-3, a spray head 5-9 is connected with the paint spraying pipe 5-7, a paint box connecting plate a5-10 is connected with a paint box connecting plate b5-11, a paint box connecting plate b5-11 is connected with a paint box connecting plate c5-12, a paint box connecting plate c5-12 is connected with a paint box connecting plate a5-10, the pressurizing connecting plate 5-2 is connected with a water circulation transmission shaft a4-4, the pressurizing connecting plate 5-2 is connected with a pressurizing propeller connecting shaft 5-4, the pressurizing barrel 5-3 is connected with a pressurizing propeller connecting shaft limiting plate 5-6, the paint spraying pipe 5-7 penetrates through a mounting plate a1-13, a paint box connecting plate c5-12 is connected with a mounting plate c1-15, the paint can be sprayed out through a sprayer in a pressurizing mode, the equipment can prevent static electricity from being generated through water circulation under a microporous plate during paint spraying, water is filled in a space formed by the mounting plate a1-13, the mounting plate b1-14, the mounting plate c1-15, the mounting plate d1-16, the mounting plate f 1-17 and the mounting plate f1-18, the water circulation motor shaft 4-1 works to drive the water circulation motor shaft 4-2 to rotate, and the water circulation motor shaft 4-2 rotates to drive the water circulation transmission shaft a4-4 rotation, the water circulation transmission shaft a4-4 rotation drives the water circulation transmission shaft b4-6 rotation through the water circulation belt b4-5, the water circulation transmission shaft b4-6 rotation drives the water circulation transmission shaft c4-8 rotation through the water circulation belt c4-7, the water circulation belt c4-7 rotation also drives the water circulation friction wheel 4-9 rotation when following the movement, the water circulation friction wheel 4-9 rotation drives the propeller transmission shaft 4-10 rotation, the propeller transmission shaft 4-10 rotation drives the reaction force propeller 4-11 rotation, the reaction force propeller 4-11 clockwise rotation sucks the air at the lower side to be discharged upwards, namely the water at the lower part of the water suction pipe 4-14 is sucked to move upwards, and the sucked water is discharged to the mounting plates a1-13, b1-14, c1-15, d1-16 and the mounting plates through the water discharge pipe 4-15 e1-17 and a mounting plate f1-18 form a space to form water circulation, static electricity generated during coating can be avoided under the action of micropores on the surface of the mounting plate a1-13, the water circulation transmission shaft a4-4 also drives the pressurizing connecting plate 5-2 to rotate, the pressurizing connecting plate 5-2 rotates to drive the pressurizing propeller connecting shaft 5-4 to rotate, the pressurizing propeller connecting shaft 5-4 rotates to drive the pressurizing propeller 5-5 to rotate, the pressurizing propeller 5-5 rotates to discharge paint in the space formed by the paint box connecting plate a5-10, the paint box connecting plate b5-11 and the paint box connecting plate c5-12 to the paint spraying pipe 5-7 through a hole in the pressurizing barrel 5-3, and the paint in the paint spraying pipe 5-7 is discharged through a nozzle 5-9.
The seventh embodiment:
the present embodiment will be described below with reference to fig. 1, fig. 2, fig. 3, fig. 4, fig. 5, fig. 6, fig. 7, fig. 8, fig. 9, fig. 10, fig. 11, fig. 12, fig. 13, fig. 14, fig. 15, fig. 16, fig. 17, fig. 18, fig. 19, and fig. 20, and the first embodiment will be further described, the unmanned aerial vehicle model mechanism 6 comprises a nose skin 6-1, wings 6-2, a fuselage skin 6-3, a tail wing skin 6-4, a rear undercarriage 6-5 and a front undercarriage 6-6, wherein the nose skin 6-1 is connected with the wings 6-2, the fuselage skin 6-3 is connected with the nose skin 6-1, the tail wing skin 6-4 is connected with the fuselage skin 6-3, the rear undercarriage 6-5 is connected with the fuselage skin 6-3, and the front undercarriage 6-6 is connected with the nose skin 6-1.
The specific implementation mode is eight:
the present embodiment will be described below with reference to fig. 1, fig. 2, fig. 3, fig. 4, fig. 5, fig. 6, fig. 7, fig. 8, fig. 9, fig. 10, fig. 11, fig. 12, fig. 13, fig. 14, fig. 15, fig. 16, fig. 17, fig. 18, fig. 19, and fig. 20, and the first embodiment will be further described, in which the paint spray pipes 5 to 7 are rubber hoses.
The specific implementation method nine:
the following describes the present embodiment with reference to fig. 1, fig. 2, fig. 3, fig. 4, fig. 5, fig. 6, fig. 7, fig. 8, fig. 9, fig. 10, fig. 11, fig. 12, fig. 13, fig. 14, fig. 15, fig. 16, fig. 17, fig. 18, fig. 19, and fig. 20, and the present embodiment further describes the first embodiment in which the surfaces of the mounting plates a1-13 have micropores.
The working principle of the device is as follows: the device can lift an unmanned aerial vehicle, the motor 1-2 works to drive the motor shaft 1-3 to rotate, the motor shaft 1-3 rotates to drive the lifting gear 1-5 to rotate, the lifting gear 1-5 rotates to drive the lifting rack 1-6 to ascend or descend, the motor shaft 1-3 simultaneously drives the reverse shaft a1-9 to rotate through the lifting belt 1-19, the reverse shaft a1-9 rotates to drive the reverse gear a1-10 to rotate, the reverse gear a1-10 rotates to drive the reverse gear b1-11 to rotate reversely, the reverse gear b1-11 rotates to drive the reverse shaft b1-12 to rotate, the reverse shaft b1-12 rotates to drive the lifting gear 1-5 on the reverse shaft b1-12 to rotate in the direction, the lifting gear 1-5 rotating in the direction drives the lifting rack 1-6 to ascend or descend, the lifting rack 1-6 moves to drive the rubber elastic strips 1-8 to move through the rack connecting plate 1-7, the fixed wing unmanned aerial vehicle is placed on the rubber elastic strips 1-8, the rubber elastic strips 1-8 close to one side of the mounting plate e1-17 are supported between the wings 6-2 and the front landing gears 6-6, the rubber elastic strips 1-8 on the other side are supported between the wings 6-2 and the rear landing gears 6-5, at the moment, the rising or falling of the rubber elastic strips 1-8 can support the unmanned aerial vehicle to rise or fall, the equipment can fix the unmanned aerial vehicle when the unmanned aerial vehicle rises, the motor 1-2 works to drive the motor shaft 1-3 to rotate, and the motor shaft 1-3 simultaneously drives the reverse shaft a1-9 to rotate through the lifting belt 1-19, the reverse shaft a1-9 rotates to drive the connecting shaft a2-2 to rotate through the connecting belt a2-1, the connecting belt a2-1 also drives the connecting gear a2-3 to rotate when moving along with the connecting belt a2-1, the connecting gear a2-3 rotates to drive the connecting shaft b2-5 to rotate, the connecting shaft b2-5 rotates to drive the connecting friction wheel 2-4 to rotate, the connecting friction wheel 2-4 rotates to drive the pressing shafts 2-6 on the same side to move transversely, the pressing shafts 2-6 on the other side synchronously move under the action of the connecting belt b2-10 and the motor shaft 1-3, the two pressing shafts 2-6 simultaneously move towards the center of the equipment or the outside of the equipment, when the pressing shafts 2-6 move towards the center of the equipment, the pressing shafts 2-6 move to drive the two limiting blocks 2-8 through the limiting connecting plate a2-, when the grooves on the limiting blocks 2-8 move to be in contact with the curved beam of the nose landing gear 6-6, the relative position of the nose landing gear 6-6 is limited, the limiting blocks 2-8 continue to move to be completely propped against the curved beam of the nose landing gear 6-6, meanwhile, the pressing shaft 2-6 on the other side drives the limiting connecting plate b2-11 to move synchronously when moving towards the center of the equipment, the limiting connecting plate b2-11 moves to drive the limiting connecting plate a2-7 to move, the limiting connecting plate a2-7 moves to be in contact with the rear landing gear 6-5, the limiting connecting plate a2-7 continues to move, under the action of the return springs 2-14, the return grooves a2-16 and the return grooves b2-17 completely limit the post rear landing gear 6-5, the pressing shaft 2-6 on the other side stops moving, and the rear landing gear 6-5 and the nose landing gear 6-6 are, the device can rotate the fixed unmanned aerial vehicle, fix the fixed wing unmanned aerial vehicle, work the rotating motor 3-1 to drive the rotating motor shaft 3-2 to rotate, the rotating motor shaft 3-2 rotates to drive the pressing shaft 2-6 at one side to rotate through the rotating belt b3-4, the rotating motor shaft 3-2 simultaneously drives the rotating transmission shaft a3-5 to rotate through the rotating belt a3-3, the rotating transmission shaft a3-5 rotates and drives the rotating transmission shaft b3-7 to rotate through the rotating belt c3-6, the rotating transmission shaft b3-7 rotates to drive the pressing shaft 2-6 at the other side to rotate through the rotating belt d3-8, the device rotates when the two pressing shafts 2-6 simultaneously rotate in the same direction, and the device can pressurize and spray paint through the spray head, the device can prevent static electricity from being generated by water circulation under the microporous plate when spraying paint, water is put into a space formed by the mounting plate a1-13, the mounting plate b1-14, the mounting plate c1-15, the mounting plate d1-16, the mounting plate e1-17 and the mounting plate f1-18, the water circulation motor 4-1 works to drive the water circulation motor shaft 4-2 to rotate, the water circulation motor shaft 4-2 rotates to drive the water circulation transmission shaft a4-4 to rotate through the water circulation belt a4-3, the water circulation transmission shaft a4-4 rotates to drive the water circulation transmission shaft b4-6 to rotate through the water circulation belt b4-5, the water circulation transmission shaft b4-6 rotates to drive the water circulation transmission shaft c4-8 to rotate through the water circulation belt c4-7, and the water circulation belt c4-7 also drives the water circulation friction wheel 4-9 to rotate when moving along with the water, the water circulation friction wheel 4-9 rotates to drive the propeller transmission shaft 4-10 to rotate, the propeller transmission shaft 4-10 rotates to drive the reaction force propeller 4-11 to rotate, the reaction force propeller 4-11 rotates clockwise to suck air on the lower side into the air and discharge the air upwards, namely the water on the lower part of the water suction pipe 4-14 is adsorbed and moves upwards, the adsorbed water is discharged into a space formed by the mounting plate a1-13, the mounting plate b1-14, the mounting plate c1-15, the mounting plate d1-16, the mounting plate e1-17, the mounting plate f1-18 through the water discharge pipe 4-15 to form water circulation, under the action of micropores on the surface of the mounting plate a1-13, static electricity generated during coating can be avoided, the water circulation transmission shaft a4-4 also drives the pressurizing connecting plate 5-2 to rotate during rotation, the pressurizing connecting plate 5-2 rotates to drive the pressurizing propeller connecting shaft 5-4 to rotate, the pressurizing propeller connecting shaft 5-4 rotates to drive the pressurizing propeller 5-5 to rotate, the pressurizing propeller 5-5 rotates, paint in a space formed by the paint box connecting plate a5-10, the paint box connecting plate b5-11 and the paint box connecting plate c5-12 is discharged into the paint spraying pipe 5-7 through a hole in the pressurizing barrel 5-3, and the paint in the paint spraying pipe 5-7 is discharged through the spray head 5-9.
It is to be understood that the above description is not intended to limit the present invention, and the present invention is not limited to the above examples, and that various changes, modifications, additions and substitutions which are within the spirit and scope of the present invention and which may be made by those skilled in the art are also within the scope of the present invention.
Claims (9)
1. The utility model provides a high-end fixed wing unmanned aerial vehicle application rotary platform equipment, includes elevating system (1), fixed establishment (2), rotary mechanism (3), hydrologic cycle mechanism (4), pressure boost mechanism of spraying paint (5), unmanned aerial vehicle model mechanism (6), its characterized in that: elevating system (1) be connected with fixed establishment (2), fixed establishment (2) are connected with rotary mechanism (3), rotary mechanism (3) are connected with elevating system (1), water circulation mechanism (4) are connected with elevating system (1), pressure boost mechanism of spraying paint (5) are connected with elevating system (1), water circulation mechanism (4) are connected with pressure boost mechanism of spraying paint (5).
2. The high-end fixed-wing drone painting rotating platform apparatus according to claim 1, characterized in that: the lifting mechanism (1) comprises a motor mounting plate (1-1), a motor (1-2), a motor shaft (1-3), a motor shaft bearing plate (1-4), a lifting gear (1-5), a lifting rack (1-6), a rack connecting plate (1-7), a rubber elastic strip (1-8), a reverse shaft a (1-9), a reverse gear a (1-10), a reverse gear b (1-11), a reverse shaft b (1-12), a mounting plate a (1-13), a mounting plate b (1-14), a mounting plate c (1-15), a mounting plate d (1-16), a mounting plate e (1-17), a mounting plate f (1-18) and a lifting belt (1-19), wherein the motor mounting plate (1-1) is connected with the motor (1-2), the motor (1-2) is connected with the motor shaft (1-3), the motor shaft (1-3) is connected with the bearing plate (1-4) of the motor shaft through a bearing, the bearing plate (1-4) of the motor shaft is connected with the mounting plate a (1-13), the lifting gear (1-5) is connected with the motor shaft (1-3), the lifting rack (1-6) is meshed with the lifting gear (1-5), the rack connecting plate (1-7) is connected with the lifting rack (1-6), two ends of the rubber elastic strip (1-8) are connected with the rack connecting plate (1-7), the reverse shaft a (1-9) is connected with the bearing plate (1-4) of the motor shaft, the reverse gear a (1-10) is connected with the reverse shaft a (1-9), the reverse gear b (1-11) is meshed with the reverse gear a (1-10), the reverse shaft b (1-12) is connected with the reverse gear b (1-11), the mounting plate a (1-13) is connected with the mounting plate b (1-14), the mounting plate b (1-14) is connected with the mounting plate c (1-15), the mounting plate c (1-15) is connected with the mounting plate d (1-16), the mounting plate d (1-16) is connected with the mounting plate a (1-13), the mounting plate e (1-17) is connected with the mounting plate a (1-13), the mounting plate f (1-18) is connected with the mounting plate a (1-13), the motor mounting plate (1-1) is connected with the mounting plate a (1-13), the lifting rack (1-6) is connected with the mounting plate a (1-13) in a sliding manner, the reverse shaft b (1-12) is connected with a bearing plate (1-4) of a motor shaft, the mounting plate b (1-14) is connected with the mounting plate e (1-17), the mounting plate c (1-15) is connected with the mounting plate e (1-17), the mounting plate d (1-16) is connected with the mounting plate e (1-17), the mounting plate b (1-14) is connected with the mounting plate f (1-18), the mounting plate c (1-15) is connected with the mounting plate f (1-18), the mounting plate d (1-16) is connected with the mounting plate f (1-18), the lifting belt (1-19) is in friction connection with the motor shaft (1-3), and the lifting belt (1-19) is in friction connection with the reverse shaft a (1-9).
3. The high-end fixed-wing drone painting rotating platform apparatus according to claim 1, characterized in that: the fixing mechanism (2) comprises a connecting belt a (2-1), a connecting shaft a (2-2), a connecting gear a (2-3), a connecting friction wheel (2-4), a connecting shaft b (2-5), a pressing shaft (2-6), a limiting connecting plate a (2-7), a limiting block (2-8), a connecting shaft b bearing plate (2-9), a connecting belt b (2-10), a limiting connecting plate b (2-11), a reset shaft (2-12), a reset limiting plate (2-13), a reset spring (2-14), a reset block (2-15), a reset groove a (2-16) and a reset groove b (2-17), wherein the connecting belt a (2-1) is in friction connection with the reverse shaft b (1-12), the connecting shaft a (2-2) is in friction connection with the connecting belt a (2-1), a connecting gear a (2-3) is in friction connection with a connecting belt a (2-1), a connecting friction wheel (2-4) is connected with a connecting shaft b (2-5), the connecting shaft b (2-5) is connected with the connecting gear a (2-3), a pressing shaft (2-6) is in friction connection with the connecting friction wheel (2-4), a limiting connecting plate a (2-7) is connected with the pressing shaft (2-6), a limiting block (2-8) is connected with the limiting connecting plate a (2-7), a bearing plate (2-9) of the connecting shaft b is in bearing connection with the connecting shaft b (2-5), a connecting belt b (2-10) is in friction connection with a motor shaft (1-3), a limiting connecting plate b (2-11) is connected with the pressing shaft (2-6) at the other side, a reset shaft (2-12) is in sliding connection with the limiting connecting plate b (2-11), the reset limiting plate (2-13) is connected with the reset shaft (2-12), the reset spring (2-14) is sleeved on the reset shaft (2-12) and limited on the limit connecting plate b (2-11) and the reset limiting plate (2-13), the reset block (2-15) is connected with the reset shaft (2-12), the reset groove a (2-16) is connected with the reset block (2-15), the reset groove b (2-17) is connected with the limit connecting plate b (2-11), the connecting shaft b bearing plate (2-9) on one side is connected with the mounting plate e (1-17), the connecting shaft b bearing plate (2-9) on the other side is connected with the mounting plate f (1-18), the compression shaft (2-6) on one side is connected with the mounting plate e (1-17) in a sliding mode, and the compression shaft (2-6) on the other side is connected with the mounting plate f (1-18) in a sliding mode.
4. The high-end fixed-wing drone painting rotating platform apparatus according to claim 1, characterized in that: the rotating mechanism (3) comprises a rotating motor (3-1), a rotating motor shaft (3-2), a rotating belt a (3-3), a rotating belt b (3-4), a rotating transmission shaft a (3-5), a rotating belt c (3-6), a rotating transmission shaft b (3-7) and a rotating belt d (3-8), wherein the rotating motor (3-1) is connected with the rotating motor shaft (3-2), the rotating motor shaft (3-2) is in friction connection with the rotating belt a (3-3), the rotating belt a (3-3) is in friction connection with the rotating belt b (3-4), the rotating belt b (3-4) is in friction connection with the rotating transmission shaft a (3-5), and the rotating transmission shaft a (3-5) is in friction connection with the rotating belt c (3-6), the rotary belt c (3-6) is in friction connection with the rotary transmission shaft b (3-7), the rotary transmission shaft b (3-7) is in friction connection with the rotary belt d (3-8), the pressing shaft (2-6) on one side is in friction connection with the rotary belt b (3-4), the pressing shaft (2-6) on one side on the other side is in friction connection with the rotary belt d (3-8), the rotary motor (3-1) is connected with the mounting plate f (1-18), the rotary motor shaft (3-2) is in bearing connection with the mounting plate f (1-18), the rotary transmission shaft a (3-5) is in bearing connection with the mounting plate e (1-17), the rotary transmission shaft a (3-5) is in bearing connection with the mounting plate f (1-18), and the rotary transmission shaft b (3-7) is in bearing connection with the mounting plate e (1-17).
5. The high-end fixed-wing drone painting rotating platform apparatus according to claim 1, characterized in that: the water circulation mechanism (4) comprises a water circulation motor (4-1), a water circulation motor shaft (4-2), a water circulation belt a (4-3), a water circulation transmission shaft a (4-4), a water circulation belt b (4-5), a water circulation transmission shaft b (4-6), a water circulation belt c (4-7), a water circulation transmission shaft c (4-8), a water circulation friction wheel (4-9), a propeller transmission shaft (4-10), a reaction force propeller (4-11), an air suction duct (4-12), an air suction conical duct (4-13), a water suction pipe (4-14), a drain pipe (4-15), a connecting plate a (4-16), a connecting plate b (4-17), a connecting plate c (4-18) and a connecting plate d (4-19), the water circulation motor (4-1) is connected with the water circulation motor shaft (4-2), the water circulation motor shaft (4-2) is in friction connection with the water circulation belt a (4-3), the water circulation belt a (4-3) is in friction connection with the water circulation transmission shaft a (4-4), the water circulation transmission shaft a (4-4) is in friction connection with the water circulation belt b (4-5), the water circulation belt b (4-5) is in friction connection with the water circulation transmission shaft b (4-6), the water circulation transmission shaft b (4-6) is in friction connection with the water circulation belt c (4-7), the water circulation belt c (4-7) is in friction connection with the water circulation transmission shaft c (4-8), the water circulation transmission shaft c (4-8) is in friction connection with the water circulation friction wheel (4-9), the water circulation friction wheel (4-9) is connected with the propeller transmission shaft (4-10), the propeller transmission shaft (4-10) is connected with the reaction force propeller (4-11), the reaction force propeller (4-11) is connected with the air suction duct (4-12) in a sliding way, the air suction conical duct (4-13) is connected with the air suction duct (4-12), the water suction pipe (4-14) is connected with the connecting plate a (4-16), the connecting plate a (4-16) is connected with the connecting plate b (4-17), the connecting plate b (4-17) is connected with the connecting plate c (4-18), the connecting plate c (4-18) is connected with the connecting plate d (4-19), the water circulation motor (4-1) is connected with the mounting plate f (1-18), the water circulation transmission shaft a (4-4) is connected with the connecting plate c (4-18) in a bearing way, a water circulation transmission shaft b (4-6) is in bearing connection with a connecting plate a (4-16), a water circulation transmission shaft c (4-8) is in bearing connection with the connecting plate a (4-16), a propeller transmission shaft (4-10) is in bearing connection with a connecting plate b (4-17), an air suction duct (4-12) is connected with a connecting plate d (4-19), a water suction pipe (4-14) penetrates through the connecting plate d (4-19) and is connected with the connecting plate d (4-19), the water suction pipe (4-14) penetrates through a mounting plate a (1-13) and is connected with a mounting plate a (1-13), a water discharge pipe (4-15) penetrates through the connecting plate d (4-19) and is connected with the connecting plate d (4-19), the water discharge pipe (4-15) penetrates through the mounting plate a (1-13) and is connected with the mounting plate a (1-13), the connecting plates a (4-16) are connected with the connecting plates c (4-18), the connecting plates a (4-16) are connected with the connecting plates d (4-19), the connecting plates d (4-19) are connected with the mounting plates e (1-17), and the connecting plates d (4-19) are connected with the mounting plates f (1-18).
6. The high-end fixed-wing drone painting rotating platform apparatus according to claim 1, characterized in that: the pressurized paint spraying mechanism (5) comprises an equipment mounting hole (5-1), a pressurized connecting plate (5-2), a pressurized barrel (5-3), a pressurized propeller connecting shaft (5-4), a pressurized propeller (5-5), a pressurized propeller connecting shaft limiting plate (5-6), a paint spraying pipe (5-7), a pressurized hole (5-8), a spray head (5-9), a paint box connecting plate a (5-10), a paint box connecting plate b (5-11) and a paint box connecting plate c (5-12), wherein the equipment mounting hole (5-1) is formed in the paint box connecting plate a (5-10) and is connected with the pressurized barrel (5-3), the pressurized connecting plate (5-2) is in sliding connection with the pressurized barrel (5-3), and the pressurized barrel (5-3) is connected and communicated with the paint spraying pipe (5-7), a pressurizing propeller connecting shaft (5-4) is connected with a pressurizing connecting plate (5-2), a pressurizing propeller (5-5) is connected with the pressurizing propeller connecting shaft (5-4), a pressurizing propeller connecting shaft limiting plate (5-6) is connected with a bearing of the pressurizing propeller connecting shaft (5-4), a paint spraying pipe (5-7) is connected with a pressurizing hole (5-8), the pressurizing hole (5-8) is arranged on a pressurizing barrel (5-3), a spray nozzle (5-9) is connected with the paint spraying pipe (5-7), a paint box connecting plate a (5-10) is connected with a paint box connecting plate b (5-11), the paint box connecting plate b (5-11) is connected with a paint box connecting plate c (5-12), the paint box connecting plate c (5-12) is connected with the paint box connecting plate a (5-10), the pressurizing connecting plate (5-2) is connected with the water circulation transmission shaft a (4-4), the pressurizing connecting plate (5-2) is connected with the pressurizing propeller connecting shaft (5-4), the pressurizing barrel (5-3) is connected with the pressurizing propeller connecting shaft limiting plate (5-6), the paint spraying pipe (5-7) penetrates through the mounting plate a (1-13), and the paint box connecting plate c (5-12) is connected with the mounting plate c (1-15).
7. The high-end fixed-wing drone painting rotating platform apparatus according to claim 1, characterized in that: the unmanned aerial vehicle model mechanism (6) comprises a nose skin (6-1), wings (6-2), a body skin (6-3), a tail wing skin (6-4), a rear undercarriage (6-5) and a front undercarriage (6-6), wherein the nose skin (6-1) is connected with the wings (6-2), the body skin (6-3) is connected with the nose skin (6-1), the tail wing skin (6-4) is connected with the body skin (6-3), the rear undercarriage (6-5) is connected with the body skin (6-3), and the front undercarriage (6-6) is connected with the nose skin (6-1).
8. The high-end fixed-wing drone painting rotating platform apparatus according to claim 1, characterized in that: the paint spraying pipe (5-7) is a rubber hose.
9. The high-end fixed-wing drone painting rotating platform apparatus according to claim 1, characterized in that: the surface of the mounting plate a (1-13) is provided with micropores.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011039316.3A CN112170055B (en) | 2020-09-28 | 2020-09-28 | High-end fixed wing unmanned aerial vehicle application rotary platform equipment |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011039316.3A CN112170055B (en) | 2020-09-28 | 2020-09-28 | High-end fixed wing unmanned aerial vehicle application rotary platform equipment |
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| CN112170055A true CN112170055A (en) | 2021-01-05 |
| CN112170055B CN112170055B (en) | 2021-06-15 |
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| CN202011039316.3A Active CN112170055B (en) | 2020-09-28 | 2020-09-28 | High-end fixed wing unmanned aerial vehicle application rotary platform equipment |
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Cited By (1)
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| CN113769940A (en) * | 2021-09-15 | 2021-12-10 | 毛凤香 | Medical instrument antibacterial coating spraying equipment for medical treatment |
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| CN206454828U (en) * | 2017-01-11 | 2017-09-01 | 烟台金驰科技有限公司 | A kind of robot spray painting automatic regulating apparatus |
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| Publication number | Publication date |
|---|---|
| CN112170055B (en) | 2021-06-15 |
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