CN210555571U - Intelligent unmanned aerial vehicle lifting cargo carrying device - Google Patents
Intelligent unmanned aerial vehicle lifting cargo carrying device Download PDFInfo
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- CN210555571U CN210555571U CN201921591889.XU CN201921591889U CN210555571U CN 210555571 U CN210555571 U CN 210555571U CN 201921591889 U CN201921591889 U CN 201921591889U CN 210555571 U CN210555571 U CN 210555571U
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Abstract
The utility model relates to an intelligence unmanned aerial vehicle lift cargo carrier, including flap retaining ring and storage disc, radially be equipped with a plurality of horn in the flap retaining ring, every horn is respectively through the storage disc of a storage disc pillar connection below, all be equipped with the ESC electricity on every storage disc pillar and transfer, flap retaining ring centre of a circle department is equipped with the horn connecting plate, horn one end is fixed in on the horn connecting plate, the other end is fixed in on the inner wall of flap retaining ring, there is the infrared obstacle-avoiding sensor on the flap retaining ring outer wall, be fixed with the external compass of GPS on the horn connecting plate and press from both sides the line wheel on with, it is connected with the lower line wheel that presss from both sides that is fixed in the storage disc below through following the spool to. And the surrounding environment is monitored in real time during working to ensure safety. The storage tray is used for placing the transported objects. After constructor goes up the eminence, put down the rope, fixed rope both ends respectively pass unmanned aerial vehicle with the rope, and lift platform operates from top to bottom along the rope, and easy operation is easily handed, can decide the high accurate location of realization through atmospheric pressure.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to intelligent unmanned aerial vehicle goes up and down to carry cargo ware.
Background
For high-altitude operation personnel, generally, goods are transported up and down under various limitations, most of high-altitude operations are transported upwards only by workers through ropes when transporting goods, and people are unsafe to stand at high altitude, so that the intelligent unmanned aerial vehicle lifting cargo loader is invented for solving the problem.
Disclosure of Invention
An object of the utility model is to provide an intelligence unmanned aerial vehicle goes up and down to carry cargo ware alleviates high altitude construction personnel's intensity of labour, improves the operation security.
The utility model provides a technical scheme that its technical problem adopted is: the utility model provides an intelligence unmanned aerial vehicle lift cargo carrier, including flap retaining ring and storage disc, radially be equipped with a plurality of horn in the flap retaining ring, every horn is located the storage disc of flap retaining ring below through a storage disc pillar connection respectively, all be equipped with ESC electricity on every storage disc pillar and transfer, the centre of a circle department of flap retaining ring is equipped with the horn connecting plate, the one end of horn is fixed in on the horn connecting plate, the other end is fixed in on the inner wall of flap retaining ring, the infrared obstacle sensor of keeping away of fixedly connected with on the outer wall of the flap retaining ring relative with the horn, be equipped with brushless motor on the horn, brushless motor is connected with the screw, be fixed with external compass of GPS and last wire clamping wheel on the horn connecting plate, it is connected with the lower wire clamping wheel that is fixed in the storage disc below through following the spool to go up the wire clamping wheel, the bottom.
Specifically, the horn connecting plate comprises a horn connecting top plate and a horn connecting bottom plate, the end of the horn is located between the horn connecting top plate and the horn connecting bottom plate, and the horn is fixed on the horn connecting top plate and the horn connecting bottom plate through bolts. And a cradle head mounting hole is reserved on the arm connecting bottom plate, and a cradle head camera can be mounted according to the use requirement.
Specifically, the GPS external compass and the upper wire clamping wheel are fixed on the upper surface of the machine arm connecting top plate, a through hole is formed in the center of the machine arm connecting top plate and the center of the machine arm connecting bottom plate, and one end of the downwind pipe penetrates through the through holes of the machine arm connecting top plate and the machine arm connecting bottom plate to be connected with the upper wire clamping wheel; the center of the storage disc is also provided with a through hole, and the other end of the line arranging pipe penetrates through the through hole of the storage disc to be connected with the lower line clamping wheel.
Specifically, the horn is connected with the flap retaining ring through the retaining ring fixing clamping groove, a rubber pad is further arranged between the retaining ring fixing clamping groove and the flap retaining ring, the rubber pad plays a role in connection on one hand, and the rubber pad plays a role in buffering on the other hand.
Specifically, a motor base is fixed on the horn, and the brushless motor is fixed on the motor base.
Specifically, go up the wire clamping wheel and press from both sides the wire wheel structure the same down, all include two wire clamping wheels, every wire clamping wheel passes through the roller bearing and connects on fixed buckle, and the roller bearing below is equipped with the encoder, and the bottom of fixed buckle is equipped with the mounting hole for on being connected roof or storage dish through the bolt fastening in horn.
Specifically, the rubber buffering landing leg is consistent with the horn, the quantity of storing dish pillar, and the rubber buffering landing leg is located the below of storing dish pillar.
Specifically, the bottom of the storage tray is provided with a groove for embedding the rubber buffering supporting legs, and the rubber buffering supporting legs are connected with the storage tray through interference fit.
Specifically, the storage tray adopts a honeycomb-hole hollow-out structure.
Specifically, the storage disc, the horn connecting plate and the motor base are all made of carbon fiber materials; the protective wing retainer ring is made of light and soft plastic; the storage tray pillar is made of aluminum alloy materials.
The utility model discloses following beneficial effect has: the utility model discloses based on unmanned aerial vehicle, provide power for whole device through six rotors. Different with ordinary six rotor unmanned aerial vehicle designs, through the horn extension externally newly-increased flap retaining ring, the flap retaining ring increases infrared obstacle avoidance sensor with the horn junction outside, has ensured the security of this device at during operation real-time supervision surrounding environment. In addition, a storage tray is additionally arranged at the lower part of the product and is used for placing transported articles. After constructor goes up the eminence, put down the rope, fixed rope both ends respectively pass unmanned aerial vehicle with the rope, and lift platform operates from top to bottom along the rope, and easy operation is easily handed, can decide the high accurate location of realization through atmospheric pressure.
Drawings
Fig. 1 is the utility model discloses intelligent unmanned aerial vehicle goes up and down to carry cargo aircraft's spatial structure sketch map one.
Fig. 2 is the utility model discloses intelligent unmanned aerial vehicle goes up and down to carry cargo aircraft's spatial structure schematic diagram two.
Fig. 3 is the utility model discloses intelligent unmanned aerial vehicle goes up and down to carry cargo aircraft's front view.
Fig. 4 is the utility model discloses intelligent unmanned aerial vehicle goes up and down to carry the top view of cargo aircraft.
Fig. 5 is the utility model discloses intelligent unmanned aerial vehicle goes up and down horn and flap retaining ring connection structure sketch map of cargo aircraft.
Fig. 6 is the utility model discloses intelligent unmanned aerial vehicle goes up and down to carry the rubber buffering landing leg structure schematic diagram of cargo ware.
Fig. 7 is the utility model discloses intelligence unmanned aerial vehicle goes up and down the horn of cargo aircraft and connects roof and horn connection bottom plate connection structure sketch map.
Fig. 8 is the utility model discloses intelligent unmanned aerial vehicle goes up and down to carry cargo aircraft's last trapping mechanism wheel schematic structure.
In the figure, 1, a brushless motor, 2, a wing retainer ring, 3, a storage disc, 4, a machine arm, 5, a machine arm connecting top plate, 6, a retainer ring fixing clamping groove, 7, a machine arm connecting bottom plate, 8, a consequent line pipe, 9, a storage disc retainer ring, 10, a lower wire clamping wheel, 11, a GPS external compass, 12, an upper wire clamping wheel, 13, a propeller, 14, ESC electric regulation, 15, an infrared obstacle avoidance sensor, 16, a storage disc support column, 17, a rubber buffering support leg, 18, a motor base, 19, a rolling shaft, 20, a fixing buckle, 21, a mounting hole, 22, a bolt, 23 and a rubber pad.
Detailed Description
The present invention will now be described in further detail with reference to the accompanying drawings.
As shown in fig. 1-4, an intelligent unmanned aerial vehicle lifting cargo loader comprises a wing retainer ring 2 and a storage tray 3, wherein a plurality of horn 4 are radially arranged in the wing retainer ring 2, in this embodiment, six horn 4 are provided, each horn 4 is connected with the storage tray 3 below the wing retainer ring 2 through a storage tray pillar 16, each storage tray pillar 16 is provided with an ESC electronic controller 14, a horn connecting plate is arranged at the center of the wing retainer ring 2, as shown in fig. 7, the horn connecting plate is composed of a horn connecting top plate 5 and a horn connecting bottom plate 7, one end of the horn 4 is arranged between the horn connecting top plate 5 and the horn connecting bottom plate 7, and is fixed on the horn connecting top plate 5 and the horn connecting bottom plate 7 through bolts 22(M3 hexagon socket head bolts), the other end of the horn 4 is fixed on the inner wall of the wing retainer ring 2, an infrared obstacle avoidance sensor 15 is fixedly connected on the outer wall of the wing retainer ring 2 opposite to the horn 4 through bolts, the flight areas in six directions can be monitored in real time, and the safety performance of the aircraft is ensured. Be fixed with motor cabinet 18 on the horn 4, motor cabinet 8 and storing dish pillar 16 are installed through the stay bolt with the hole on the horn 4, brushless motor 1 passes through the bolt fastening on motor cabinet 8, brushless motor 1 passes through the nut and is connected with screw 13 with fastening structure, be fixed with the external compass 11 of GPS and go up pinch roller 12 on the horn connecting plate, go up pinch roller 12 through being connected with the lower pinch roller 10 that is fixed in storing dish 3 below along line pipe 8, the bottom of storing dish 3 is equipped with a plurality of rubber buffering landing legs 17. The number of the rubber buffer supporting legs 17 is the same as that of the machine arms 4 and the storage tray supporting columns 16, and the rubber buffer supporting legs 17 are positioned below the storage tray supporting columns 16. The bottom of the storage tray 3 is provided with a groove for embedding the rubber buffering supporting leg 17, and the rubber buffering supporting leg 17 is connected with the storage tray 3 through interference fit, as shown in fig. 6.
In a preferred embodiment, as shown in fig. 5, the horn 4 is connected to the wing retainer ring 2 through the retainer ring fixing groove 6, the horn 4 is connected to the retainer ring fixing groove 6 by bolts, the retainer ring fixing groove 6 is connected to the wing retainer ring 2 in a snap-fit manner, the wing retainer ring 2 can be directly clamped in the T-shaped groove of the retainer ring fixing groove 6, a rubber pad 23 is further disposed between the retainer ring fixing groove 6 and the wing retainer ring 2, and the rubber pad 23 plays a role in connection on one hand and a role in buffering on the other hand.
The GPS external compass 11 and the upper wire clamping wheel 12 are fixed on the upper surface of the machine arm connecting top plate 5, a through hole is arranged in the center of the machine arm connecting top plate 5 and the center of the machine arm connecting bottom plate 7, and one end of the fairing pipe 8 penetrates through the through holes of the machine arm connecting top plate 5 and the machine arm connecting bottom plate 7 to be connected with the upper wire clamping wheel 12; the center of the storage disc 3 is also provided with a through hole, and the other end of the line arranging pipe 8 penetrates through the through hole of the storage disc 3 to be connected with the lower line clamping wheel 10. And a cradle head mounting hole is reserved on the arm connecting bottom plate 7, and a cradle head camera can be mounted according to the use requirement.
As shown in fig. 8, the upper wire clamping wheel 12 and the lower wire clamping wheel 10 have the same structure and both comprise two wire clamping wheels, each wire clamping wheel is connected to the fixed buckle 20 through a rolling shaft 19, an encoder is arranged below the rolling shaft 19, the working condition of the cargo loader is judged according to the rotating speed of the wire clamping wheels, and if the rotating speed is increased suddenly, the fault falling is judged. The bottom of the fixing buckle 20 is provided with a mounting hole 21 for being fixed on the top plate 5 or the storage tray 3 through a bolt. Go up wire clamping wheel 12 and lower wire clamping wheel 10 and carry the cargo device in the lift extremely important, it uses with following the spool 8 cooperatees, passes lift cargo carrier, purpose with the rope through last wire clamping wheel 12, following spool 8, lower wire clamping wheel 10: firstly, in order to simplify the operation steps of an operator, the operator only needs to control a lifting switch of a lifter, and the lifting cargo loader moves up and down along a rope in the lifting process; secondly, the operation stability of the lifting cargo carrying device is improved, the direction of the lifting cargo carrying device does not need to be adjusted in real time, so that the working efficiency of workers is improved, thirdly, when the lifting cargo carrying device breaks down, the upper wire clamping wheel 12 and the lower wire clamping wheel 10 can be locked at the same time, and the falling of the lifting cargo carrying device is avoided. After constructor goes up the eminence, put down the rope, fixed rope both ends respectively pass unmanned aerial vehicle lift platform with the rope and operate from top to bottom along the rope, easy operation is easily got up, can decide the high accurate location of realization through atmospheric pressure.
In addition, the bottom storage plate is connected with the machine arm through bolts, and a user can selectively install the bottom storage plate according to actual conditions. In the requirement of working from non-straight up to straight down, the unmanned aerial vehicle or an omnidirectional aircraft operator can operate the unmanned aerial vehicle to fly in an omnidirectional manner by using a remote controller. And the design of this unmanned aerial vehicle is safer compared with other unmanned aerial vehicles.
The utility model discloses the unsettled static method of intelligent unmanned aerial vehicle lift cargo carrier as follows: the unmanned aerial vehicle hovers in the air under the lifting force of six wing units (propellers), meanwhile, under the action of wind force and other interference factors, the unmanned aerial vehicle can shake, the carried objects are fixed in the storage disc, the flight control unit calculates and adjusts the rotating speed of the rotor motor according to the shaking condition of the frame, and rapidly makes corresponding posture adjustment to offset the shaking trend in real time, thereby achieving the effect of frame balance,
the utility model discloses intelligent unmanned aerial vehicle goes up and down cargo carrier descending method as follows: unmanned aerial vehicle is when arriving appointed place, hover above earlier, there is not barrier through the outer infrared obstacle avoidance sensor analysis of self flap retaining ring, at this in-process, unmanned aerial vehicle will receive external wind-force or some other interferences, unmanned aerial vehicle's stability is guaranteed constantly according to unsettled quiescent method to unmanned aerial vehicle, a plurality of brushless motor of horn can reduce the rotational speed simultaneously in the in-process that descends, thereby slow reduction lift, make unmanned aerial vehicle slow descend to ground, the infrared obstacle avoidance sensor of six positions on the descending in-process flap retaining ring can guarantee unmanned aerial vehicle's security, after arriving ground, unmanned aerial vehicle can close brushless motor by oneself. And the safety switch is turned on to prevent the rotary wing from rotating to accidentally injure people in the unloading process.
The utility model discloses intelligent unmanned aerial vehicle goes up and down cargo carrier gesture adjustment method as follows: unmanned aerial vehicle hovers in the air under the lift effect of six wing units (propellers), is installed on the horn by thing storage dish device, and six wing units are controlled respectively one by one to the flight control unit, through the different rotational speed of propeller to realize the lift of different wings, the storage dish of bottom adopts the design of honeycomb hole fretwork, can effectually offset rotor reaction, guarantees the stability of system.
The above-described embodiments are merely illustrative of the preferred embodiments of the present invention and are not intended to limit the spirit and scope of the present invention. Under the prerequisite that does not deviate from the design concept of the utility model, the ordinary person in the art should fall into the protection scope of the utility model to the various changes and improvements that the technical scheme of the utility model made.
The technology, shape and construction parts which are not described in detail in the present invention are all known technology.
Claims (10)
1. The utility model provides an intelligence unmanned aerial vehicle lift cargo carrier, a serial communication port, including flap retaining ring and storage dish, radially be equipped with a plurality of horn in the flap retaining ring, every horn is located the storage dish of flap retaining ring below through a storage dish pillar joint respectively, all be equipped with ESC electricity on every storage dish pillar and transfer, the centre of a circle department of flap retaining ring is equipped with the horn connecting plate, the one end of horn is fixed in on the horn connecting plate, the other end is fixed in on the inner wall of flap retaining ring, fixedly connected with infrared obstacle avoidance sensor on the outer wall of the flap retaining ring relative with the horn, be equipped with brushless motor on the horn, brushless motor is connected with the screw, be fixed with external compass of GPS and last wire clamping wheel on the horn connecting plate, go up the wire clamping wheel through being connected with the lower wire clamping wheel that is fixed in storage dish below along the spool, the bottom of storage dish is equipped with.
2. The intelligent unmanned aerial vehicle elevating cargo loader of claim 1, wherein the horn connecting plate is comprised of a horn connecting top plate and a horn connecting bottom plate, an end of the horn is located between the horn connecting top plate and the horn connecting bottom plate, and the horn is fixed to the horn connecting top plate and the horn connecting bottom plate by bolts.
3. The intelligent unmanned aerial vehicle elevating cargo loader of claim 2, wherein the GPS external compass and the upper wire clamping wheel are fixed on the upper surface of the arm connecting top plate, a through hole is arranged in the center of the arm connecting top plate and the arm connecting bottom plate, and one end of the line guiding pipe penetrates through the through holes of the arm connecting top plate and the arm connecting bottom plate to be connected with the upper wire clamping wheel; the center of the storage disc is also provided with a through hole, and the other end of the line arranging pipe penetrates through the through hole of the storage disc to be connected with the lower line clamping wheel.
4. The intelligent unmanned aerial vehicle elevating cargo loader of claim 1, wherein the horn is connected with the flap retainer ring through a retainer ring fixing groove, and a rubber pad is further arranged between the retainer ring fixing groove and the flap retainer ring.
5. The intelligent unmanned aerial vehicle elevating cargo loader of claim 1, wherein a motor mount is fixed to the horn, and a brushless motor is fixed to the motor mount.
6. The intelligent unmanned aerial vehicle elevating cargo loader of claim 1, wherein the upper wire clamping wheel and the lower wire clamping wheel are the same in structure and each comprise two wire clamping wheels, each wire clamping wheel is connected to a fixing buckle through a roller, an encoder is arranged below the roller, and a mounting hole is formed in the bottom of the fixing buckle and used for being fixed on a machine arm connecting top plate or a storage disc through a bolt.
7. The intelligent unmanned aerial vehicle elevating cargo loader of claim 1, wherein the rubber buffer legs are in accordance with the number of the horn and the storage tray support, and the rubber buffer legs are located below the storage tray support.
8. The intelligent unmanned aerial vehicle elevating cargo loader of claim 1 or 7, wherein the bottom of the storage tray is provided with a groove for embedding a rubber buffering leg, and the rubber buffering leg is connected with the storage tray through interference fit.
9. The intelligent unmanned aerial vehicle elevating cargo loader of claim 1, wherein the storage tray is of a cellular hollow structure.
10. The intelligent unmanned aerial vehicle elevating cargo loader of claim 1, wherein the storage tray, the horn connecting plate, and the motor base are made of carbon fiber material; the protective wing retainer ring is made of light and soft plastic; the storage tray pillar is made of aluminum alloy materials.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921591889.XU CN210555571U (en) | 2019-09-23 | 2019-09-23 | Intelligent unmanned aerial vehicle lifting cargo carrying device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921591889.XU CN210555571U (en) | 2019-09-23 | 2019-09-23 | Intelligent unmanned aerial vehicle lifting cargo carrying device |
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| CN210555571U true CN210555571U (en) | 2020-05-19 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201921591889.XU Active CN210555571U (en) | 2019-09-23 | 2019-09-23 | Intelligent unmanned aerial vehicle lifting cargo carrying device |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113911355A (en) * | 2021-07-10 | 2022-01-11 | 山东交通学院 | Portable unmanned aerial vehicle and using method thereof |
| CN113942637A (en) * | 2020-07-15 | 2022-01-18 | 深圳市卓派自动化技术有限公司 | Unmanned plane |
-
2019
- 2019-09-23 CN CN201921591889.XU patent/CN210555571U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113942637A (en) * | 2020-07-15 | 2022-01-18 | 深圳市卓派自动化技术有限公司 | Unmanned plane |
| CN113911355A (en) * | 2021-07-10 | 2022-01-11 | 山东交通学院 | Portable unmanned aerial vehicle and using method thereof |
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