CN218559177U - Drive bird unmanned aerial vehicle rack construction - Google Patents
Drive bird unmanned aerial vehicle rack construction Download PDFInfo
- Publication number
- CN218559177U CN218559177U CN202222701318.5U CN202222701318U CN218559177U CN 218559177 U CN218559177 U CN 218559177U CN 202222701318 U CN202222701318 U CN 202222701318U CN 218559177 U CN218559177 U CN 218559177U
- Authority
- CN
- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- bird
- rotor wing
- frame
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Catching Or Destruction (AREA)
Abstract
The utility model belongs to the technical field of the bird equipment is driven to the electric wire netting, especially, relate to a drive bird unmanned aerial vehicle rack construction. Comprises a stander component, a rotor wing component and a functional component; the rack assembly comprises a rectangular supporting framework, a box-type positioning frame, a machine shell and a connecting shaft; the rotor wing assembly comprises a U-shaped connecting frame, a rotor wing arm, a motor base, a motor and a rotor wing; the functional components comprise a medicine box arranged in the medicine bin and a battery pack arranged in the battery bin; the front side of the medicine box is provided with a mounting port for mounting the spray head, and the top of the medicine box is provided with a filling pipe. The utility model provides a drive bird unmanned aerial vehicle rack construction mainly is applicable to each type and drives bird unmanned aerial vehicle's structural design, and its overall structure is succinct light, and complete machine spare part is small in quantity, can effectively reduce the degree of difficulty that the plant maintenance used, and it does not need professional take off and land equipment, requires lowly to the environment of taking off and land, is favorable to popularizing and applying in the bird operation of driving in all kinds of middle-size and small-size or remote areas.
Description
Technical Field
The utility model belongs to the technical field of the bird equipment is driven to the electric wire netting, especially, relate to a drive bird unmanned aerial vehicle rack construction.
Background
Bird unmanned aerial vehicle mainly used solves distribution network overhead line, regional birds such as pole perch or the problem of nesting, current partial unmanned aerial vehicle product structure is complicated, rack construction uses multiple connection fixed mode, the organism uses multilayer casing and interior outer frame, complete machine spare part is many, on the one hand the assembly is used the step and is heavy and complicated, preparation and maintenance work volume around using are great, on the other hand more spare part leads to unmanned aerial vehicle built-in trouble hidden danger source to increase, the overall stability descends, requirement to take off and land and control increases, unmanned aerial vehicle has restricted the further application in the medium-size and small-size bird operation that drives.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a succinct compactness of structure, stability is good, and complete machine spare part is small in quantity, and assembly, maintenance and use are more convenient, drive bird unmanned aerial vehicle rack construction that the environmental requirement is low to take off and land.
In order to achieve the above purpose, the utility model adopts the following technical scheme.
A bird repelling unmanned aerial vehicle rack structure comprises a rack component 1, a rotor wing component 2 and a functional component 3;
the rack assembly 1 comprises a rectangular supporting framework 10, a box type positioning frame 11, a machine shell 12 and a connecting shaft 13;
the outer side surface of the rectangular supporting framework 10 is provided with a rotor wing connecting hole group 10a, and four corners of the top of the rectangular supporting framework are provided with connecting holes 10b; the box type positioning frame 11 is of a box body structure with an opening at the top, an inner cavity of the box type positioning frame 11 is divided into a medicine bin 11a at the front side and a battery bin 11b at the rear side through a vertically arranged isolation rib plate, and a spraying opening 11c is dug at the front side of the medicine bin 11 a; the outer edge of the top opening of the box-type positioning frame 11 extends outwards to form a rectangular connecting skirt 11d, the rectangular connecting skirt 11d is buckled on the upper side of the rectangular supporting framework 10, and a through hole 11e coaxially opposite to the connecting hole 10b is formed in the rectangular connecting skirt 11 d; the casing 12 is arranged on the upper side of the rectangular support framework 10, and the casing 12 is provided with a fixing hole 12a coaxially opposite to the connecting hole 10b; the connecting shaft 13 is inserted into the connecting hole 10b for fixing after being inserted into the fixing hole 12a and passing through the through hole 11e;
the rotor wing assembly 2 comprises a U-shaped connecting frame 20, a rotor wing arm 21, a motor base 22, a motor 23 and a rotor wing 24;
the U-shaped connecting frame 20 is provided with a hole group corresponding to the rotor wing connecting hole group 10a, and the U-shaped connecting frame 20 is connected to the outer side of the rectangular supporting framework 10 through a bolt group arranged in the hole group; one end of the rotor arm 21 is connected to the U-shaped connecting frame 20, the other end extends outwards, and the motor base 22 is fixed at the extended end; the motor 23 is fixedly arranged on the motor base 22 and used for driving the rotor 24 to rotate;
the functional assembly 3 comprises a medicine box 30 arranged in the medicine bin 11a and a battery pack 31 arranged in the battery bin 11 b; the cartridge 30 is provided at the front side with a mounting port 30a for mounting a nozzle and at the top with a fill pipe 30b.
To the further improvement or preferred embodiment of the aforesaid bird repellent unmanned aerial vehicle rack structure, functional component 3 still includes the stock frame 32 that sets up in the outside of group battery 31, stock frame 32 comprises two U-shaped elastic strips 32a and two elastic connection strip 32b that are located two U-shaped elastic strips 32a front and back sides that set up side by side; the upper ends of the two U-shaped elastic strips 32a extend outward and are snapped on the rectangular connecting skirt 11 d.
To the aforesaid drive bird unmanned aerial vehicle rack construction's further improvement or preferred embodiment, casing 12 is the ship shape structure of back-off, and the position just right with rotor connection punch combination 10a on the lateral wall of casing 12 is provided with keeps away empty notch 12b, and the top of casing 12 is provided with operation window 12c respectively with medicine storehouse 11a and battery compartment 11b just right position.
To the aforesaid drive bird unmanned aerial vehicle rack construction's further improvement or preferred embodiment, the part thickening at connecting hole 10b place on casing 12 forms after widening and strengthens connecting platform 12d, and connecting hole 10b digs out from strengthening connecting platform 12 d.
In a further improvement or preferred embodiment of the bird repelling unmanned aerial vehicle rack structure, a connecting piece 25 is arranged between the rotor arm 21 and the motor base 22;
the connecting piece 25 comprises a sleeve connecting part 250 which can be sleeved on the rotor arm 21 and a rotating shaft part 251 which is connected with the sleeve connecting part 250; two ends of the rotating shaft part 251 horizontally extend to form a short shaft 252; the bottom of the motor base 22 is provided with a connecting port 220, and the inner wall of the connecting port 220 is provided with a hole sleeved with the short shaft 252.
The bird-repelling unmanned aerial vehicle frame structure further improves or optimizes the implementation scheme, and further comprises a buffer structure arranged on the rotor arm 21;
the buffer structure comprises a connecting sleeve 26, a supporting rod 27, an elastic beam 28 and a cushion 29;
the connecting sleeve 26 is composed of a horizontal sleeve 260 extending horizontally and arranged on the rotor arm 21 and a vertical sleeve 261 arranged vertically; the middle part of the elastic beam 28 is provided with a support sleeve 280 which extends upwards; the upper end and the lower end of the support rod 27 are respectively inserted into the vertical sleeve 261 and the support sleeve 280; two cushions 29 are respectively arranged at the lower sides of the two ends of the elastic beam 28.
The beneficial effects are that:
the utility model provides a drive bird unmanned aerial vehicle rack construction mainly is applicable to each type and drives bird unmanned aerial vehicle's structural design, and its overall structure is succinct light, and complete machine spare part is small in quantity, can effectively reduce the degree of difficulty that the plant maintenance used, and it does not need professional take off and land equipment, requires lowly to the environment of taking off and land, is favorable to popularizing and applying in the bird operation of driving in all kinds of middle-size and small-size or remote areas.
Drawings
Fig. 1 is a front view of a bird repelling drone rack structure;
fig. 2 is a side view of a bird repellent drone airframe structure;
fig. 3 is an oblique view of a bird repellent drone airframe structure;
fig. 4 is an assembly view of the bird repelling unmanned aerial vehicle rack structure rack and functional components;
fig. 5 is an assembly view of the bird repelling drone rack structure rotor.
Detailed Description
The present invention will be described in detail with reference to the following specific examples.
The utility model provides a drive bird unmanned aerial vehicle rack construction, the main objective provides a structure comparatively simple, and complete machine spare part is few, and the erection joint is simple, reduces the equipment use and maintains the degree of difficulty and cost, and the basic unit personnel of being convenient for use, reduce the use cost in the bird operation of driving of well low work load to in the messenger drive bird unmanned aerial vehicle and drive bird and further use in using in the basic unit.
As shown in fig. 1 to 3, the main structure of the bird repelling unmanned aerial vehicle rack structure of the present application includes a rack assembly 1, a rotor assembly 2, and a functional assembly 3;
wherein frame subassembly 1 constitutes the basic structure of unmanned aerial vehicle body, and its characteristics lie in that overall structure is compact indirect, use more succinctly spare part less to construct unmanned aerial vehicle skeleton texture, under the prerequisite of guaranteeing unmanned aerial vehicle stability, reduce unmanned aerial vehicle assembly, use and the work load and the technical degree of difficulty of maintaining, make as far as possible that the basic unit personnel who does not possess professional maintenance technique also can be convenient maintain the use.
The rack component 1 comprises a rectangular supporting framework 10, a box-type positioning frame 11, a machine shell 12 and a connecting shaft 13;
the outer side surface of the rectangular supporting framework 10 is provided with a rotor wing connecting hole group 10a, and four corners of the top of the rectangular supporting framework are provided with connecting holes 10b; the box type positioning frame 11 is of a box body structure with an opening at the top, an inner cavity of the box type positioning frame 11 is divided into a medicine bin 11a at the front side and a battery bin 11b at the rear side through a vertically arranged isolation rib plate, and a spraying opening 11c is dug at the front side of the medicine bin 11 a; the outer edge of the opening at the top of the box-type positioning frame 11 extends outwards to form a rectangular connecting skirt 11d, the rectangular connecting skirt 11d is buckled on the upper side of the rectangular supporting framework 10, and a through hole 11e coaxially opposite to the connecting hole 10b is formed in the rectangular connecting skirt 11 d; the casing 12 is arranged on the upper side of the rectangular supporting framework 10, and the casing 12 is provided with a fixing hole 12a coaxially opposite to the connecting hole 10b; the connecting shaft 13 is inserted into the connecting hole 10b for fixing after being inserted into the fixing hole 12a and passing through the through hole 11e;
in this embodiment, casing 12 is the ship shape structure of back-off to air current environment when optimizing unmanned aerial vehicle flight, taking place the structure for avoiding rotor structure and casing and interfering, being provided with rotor connection punch combination 10a just right position on the lateral wall of casing 12 and keeping away empty notch 12b, the top of casing 12 is just right the position with medicine storehouse 11a and battery compartment 11b and is provided with operation window 12c respectively.
In the practical implementation process, the connecting shaft 13 may be fixed by interference fit, adhesion, or bolt connection, the connecting hole needs to connect and fix the casing 12, the rectangular supporting frame 10, and the box-type positioning frame 11 through the connecting shaft to form a relatively fixed whole, so as to ensure the connection strength and prevent the deformation of the connecting hole, in this embodiment, the portion of the casing 12 where the connecting hole 10b is located is thickened and widened to form the reinforced connecting platform 12d, and the connecting hole 10b is dug out from the reinforced connecting platform 12 d.
The rotor wing assembly 2 provides power for the movement of the human-machine, the current rotor wing structure generally adopts a multi-rotor wing structure, the basic structure and the control scheme of the multi-rotor wing structure are very mature, and the basic structure comprises a U-shaped connecting frame 20, a rotor wing arm 21, a motor base 22, a motor 23 and a rotor wing 24; consider that to drive bird unmanned aerial vehicle at the sprinkling irrigation operation in-process, can form the spraying region near the organism, receive the influence for avoiding motor in the rotor, set up the rotor arm and can select different length according to its user demand, realize the coordination of control performance and security performance.
The U-shaped connecting frame 20 is provided with a hole group corresponding to the rotor wing connecting hole group 10a, and the U-shaped connecting frame 20 is connected to the outer side of the rectangular supporting framework 10 through a bolt group arranged in the hole group; one end of the rotor arm 21 is connected to the U-shaped connecting frame 20, the other end extends outwards, and the motor base 22 is fixed at the extended end; the motor 23 is fixedly arranged on the motor base 22 and used for driving the rotor 24 to rotate;
particularly, in order to increase the flexibility of unmanned aerial vehicle control and provide a structural foundation for the unmanned aerial vehicle rotor wing to be matched with each other to realize the change of the rotor wing angle, an optional improved structure is also provided, and the improved structure comprises a connecting piece 25 arranged between a rotor wing arm 21 and a motor base 22;
the connecting piece 25 comprises a sleeve connecting part 250 which can be sleeved on the rotor arm 21 and a rotating shaft part 251 which is connected with the sleeve connecting part 250; two ends of the rotating shaft part 251 horizontally extend to form a short shaft 252; the bottom of the motor base 22 is provided with a connecting port 220, and the inner wall of the connecting port 220 is provided with a hole sleeved with the short shaft 252.
In order to further improve the applicability of the unmanned aerial vehicle, reduce the requirements on the taking-off and landing environment of the unmanned aerial vehicle and protect the unmanned aerial vehicle, the unmanned aerial vehicle further comprises a buffer structure arranged on the rotor arm 21 in the embodiment;
the buffer structure comprises a connecting sleeve 26, a supporting rod 27, an elastic beam 28 and a cushion 29;
the connecting sleeve 26 is composed of a horizontal sleeve 260 extending horizontally and arranged on the rotor arm 21 and a vertical sleeve 261 arranged vertically; the middle part of the elastic beam 28 is provided with a support sleeve 280 which extends upwards; the upper end and the lower end of the support rod 27 are respectively inserted into the vertical sleeve 261 and the support sleeve 280; two cushions 29 are respectively provided on the lower sides of both ends of the elastic beam 28.
As driving bird unmanned aerial vehicle, what kind of bird mode of adoption drives the influence of bird to the unmanned aerial vehicle structure is very big, and the bird unmanned aerial vehicle that drives that traditional adoption acousto-optic system relies on the inside acousto-optic emission system of self, and its structure is complicated with high costs, and the bird effect that drives that obtains after birds are familiar with a period will descend rapidly, and birds can return once more after unmanned aerial vehicle flies away. The application refers to the functional characteristics of an agricultural unmanned aerial vehicle, and provides a scheme for realizing bird repelling by spraying irritant substances on key positions in a control area to enable corresponding point positions to form a continuous and stable environment atmosphere which is not suitable for birds to inhabit and multiply; in practical use, the used irritant substance is a biological preparation processed from pure natural raw materials (or equivalent natural raw materials), and after being distributed for use, the irritant substance slowly and persistently releases a special faint scent affecting the nervous system and the respiratory system of birds and birds, birds and birds can fly away after smelling the special faint scent, and the faint scent cannot come again in the memory period of birds and birds, and the irritant substance is generally prepared from crude oil extracts capable of being naturally and slowly degraded.
In order to facilitate the use, the internal space is reasonably distributed, and the mass distribution of the unmanned aerial vehicle is realized, in the utility model, the functional component 3 comprises a medicine box 30 arranged in a medicine bin 11a and a battery pack 31 arranged in a battery bin 11 b; the cartridge 30 is provided at the front side with a mounting port 30a for mounting a nozzle and at the top with a fill pipe 30b.
In order to avoid the problems of poor contact and the like of the battery pack caused by vibration and the like, in the embodiment, the functional assembly 3 further comprises a shaping frame 32 arranged outside the battery pack 31, and the shaping frame 32 is composed of two U-shaped elastic strips 32a arranged side by side and two elastic connecting strips 32b positioned on the front and rear sides of the two U-shaped elastic strips 32 a; the upper ends of the two U-shaped elastic strips 32a extend outward and snap over the rectangular connecting skirt 11 d.
It should be finally noted that the above embodiments are only intended to illustrate the technical solutions of the present invention, and not to limit the scope of the present invention, and although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that the technical solutions of the present invention can be modified or replaced with equivalents without departing from the spirit and scope of the technical solutions of the present invention.
Claims (6)
1. A bird-repelling unmanned aerial vehicle rack structure is characterized by comprising a rack assembly (1), a rotor wing assembly (2) and a functional assembly (3);
the rack assembly (1) comprises a rectangular supporting framework (10), a box-type positioning frame (11), a machine shell (12) and a connecting shaft (13);
the outer side surface of the rectangular supporting framework (10) is provided with a rotor wing connecting hole group (10 a), and four corners of the top of the rectangular supporting framework are provided with connecting holes (10 b); the box type positioning frame (11) is of a box body structure with an opening at the top, an inner cavity of the box type positioning frame (11) is divided into a medicine bin (11 a) at the front side and a battery bin (11 b) at the rear side through a vertically arranged isolation rib plate, and a spraying opening (11 c) is dug at the front side of the medicine bin (11 a); the outer edge of an opening at the top of the box-shaped positioning frame (11) extends outwards to form a rectangular connecting skirt edge (11 d), the rectangular connecting skirt edge (11 d) is buckled at the upper side of the rectangular supporting framework (10), and a through hole (11 e) coaxially opposite to the connecting hole (10 b) is formed in the rectangular connecting skirt edge (11 d); the shell (12) is arranged on the upper side of the rectangular supporting framework (10), and a fixing hole (12 a) coaxially opposite to the connecting hole (10 b) is formed in the shell (12); the connecting shaft (13) is inserted into the connecting hole (10 b) from the fixing hole (12 a) and passes through the through hole (11 e) for fixing;
the rotor wing assembly (2) comprises a U-shaped connecting frame (20), a rotor wing arm (21), a motor base (22), a motor (23) and a rotor wing (24);
the U-shaped connecting frame (20) is provided with a hole group corresponding to the rotor wing connecting hole group (10 a), and the U-shaped connecting frame (20) is connected to the outer side of the rectangular supporting framework (10) through a bolt group arranged in the hole group; one end of the rotor arm (21) is connected to the U-shaped connecting frame (20), the other end of the rotor arm extends outwards, and the motor base (22) is fixed at the extending end; the motor (23) is fixedly arranged on the motor base (22) and is used for driving the rotor wing (24) to rotate;
the functional component (3) comprises a medicine box (30) arranged in the medicine bin (11 a) and a battery pack (31) arranged in the battery bin (11 b); the front side of the medicine box (30) is provided with a mounting opening (30 a) for mounting the spray head, and the top is provided with a filling pipe (30 b).
2. A bird repelling unmanned aerial vehicle frame structure according to claim 1, wherein the functional assembly (3) further comprises a sizing frame (32) arranged outside the battery pack (31), the sizing frame (32) is composed of two U-shaped elastic strips (32 a) arranged side by side and two elastic connecting strips (32 b) positioned at the front and rear sides of the two U-shaped elastic strips (32 a); the upper ends of the two U-shaped elastic strips (32 a) extend outwards and are buckled on the rectangular connecting skirt (11 d).
3. A bird-repelling unmanned aerial vehicle rack structure according to claim 1, wherein the housing (12) is of an inverted boat-shaped structure, a clearance notch (12 b) is formed in a position on the side wall of the housing (12) opposite to the rotor wing connecting hole group (10 a), and operation windows (12 c) are respectively formed in positions on the top of the housing (12) opposite to the medicine bin (11 a) and the battery bin (11 b).
4. A bird-scaring unmanned aerial vehicle frame structure according to claim 1, wherein the part of the connecting hole (10 b) on the casing (12) is thickened and widened to form a reinforced connecting platform (12 d), and the connecting hole (10 b) is dug out from the reinforced connecting platform (12 d).
5. A bird scaring drone frame structure according to claim 1, characterised in that a connection (25) is provided between the rotor arm (21) and the motor base (22);
the connecting piece (25) comprises a sleeve connecting part (250) which can be sleeved on the rotor arm (21) and a rotating shaft part (251) connected with the sleeve connecting part (250); two ends of the rotating shaft part (251) horizontally extend out to form a short shaft (252); the bottom of the motor base (22) is provided with a connecting port (220), and the inner wall of the connecting port (220) is provided with a hole sleeved with the short shaft (252).
6. A bird scaring drone frame structure according to claim 1, further including a buffer structure provided on the rotor arm (21);
the buffer structure comprises a connecting sleeve (26), a supporting rod (27), an elastic beam (28) and a cushion (29);
the connecting sleeve (26) consists of a horizontal sleeve (260) which extends horizontally and is arranged on the rotor arm (21) and a vertical sleeve (261) which is arranged vertically; the middle part of the elastic beam (28) is provided with a supporting sleeve (280) which extends upwards; the upper end and the lower end of the support rod (27) are respectively inserted into the vertical sleeve (261) and the support sleeve (280); two soft pads (29) are respectively arranged at the lower sides of the two ends of the elastic beam (28).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222701318.5U CN218559177U (en) | 2022-10-13 | 2022-10-13 | Drive bird unmanned aerial vehicle rack construction |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222701318.5U CN218559177U (en) | 2022-10-13 | 2022-10-13 | Drive bird unmanned aerial vehicle rack construction |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218559177U true CN218559177U (en) | 2023-03-03 |
Family
ID=85317185
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222701318.5U Active CN218559177U (en) | 2022-10-13 | 2022-10-13 | Drive bird unmanned aerial vehicle rack construction |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218559177U (en) |
-
2022
- 2022-10-13 CN CN202222701318.5U patent/CN218559177U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206984376U (en) | A kind of agricultural chemicals of plant protection unmanned plane is finished warning device | |
| CN218559177U (en) | Drive bird unmanned aerial vehicle rack construction | |
| CN203544370U (en) | Agricultural multi-rotor unmanned helicopter | |
| CN210869508U (en) | Be used for crops disease and pest control device | |
| CN209634724U (en) | A kind of agricultural plant protection unmanned plane | |
| CN205884500U (en) | A six rotor unmanned aerial vehicle for spray insecticide | |
| CN204846380U (en) | Agricultural plant protection unmanned aerial vehicle takes precautions against earthquakes and swings medical kit | |
| CN210338295U (en) | Plant protection unmanned aerial vehicle capable of compensating free end of spray rod | |
| CN209581876U (en) | It can VTOL fixed-wing fog machine | |
| CN217496543U (en) | Unmanned aerial vehicle remote control sprinkler convenient to dismantle | |
| CN203512034U (en) | Multi-rotor wing unmanned aerial vehicle (UAV) for agriculture and forestry plant protection | |
| CN207665875U (en) | A kind of fog machine liquid case that automatic anti-earthquake is swung | |
| CN210391563U (en) | Spraying unmanned aerial vehicle | |
| CN213921507U (en) | Multi-functional locust fixed wing unmanned aerial vehicle that kills | |
| CN212797327U (en) | Unmanned aerial vehicle electrostatic spraying device | |
| CN210445442U (en) | Unmanned aerial vehicle device of spraying insecticide | |
| CN204228737U (en) | The wind speed measuring device of agricultural depopulated helicopter | |
| CN209553493U (en) | A kind of more rotor plant protection drones based on adaptive multiinjector grouping spray application | |
| CN104304222B (en) | Spray equipment | |
| CN208165255U (en) | A kind of more rotor plant protection drones | |
| CN219545086U (en) | Multipurpose deinsectization unmanned aerial vehicle | |
| CN211055399U (en) | Unmanned aerial vehicle mosquito trap | |
| CN211543897U (en) | Unmanned aerial vehicle for agricultural | |
| CN220494019U (en) | Agricultural planting insect expelling device | |
| CN210149565U (en) | Easily-installed medicine box for plant protection unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |