CN220786179U - Novel protection architecture that unmanned aerial vehicle wing was used - Google Patents
Novel protection architecture that unmanned aerial vehicle wing was used Download PDFInfo
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- CN220786179U CN220786179U CN202321467042.7U CN202321467042U CN220786179U CN 220786179 U CN220786179 U CN 220786179U CN 202321467042 U CN202321467042 U CN 202321467042U CN 220786179 U CN220786179 U CN 220786179U
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- 230000001681 protective effect Effects 0.000 claims description 8
- 238000009434 installation Methods 0.000 abstract description 11
- 238000000034 method Methods 0.000 abstract description 7
- 230000008569 process Effects 0.000 abstract description 5
- 230000003014 reinforcing effect Effects 0.000 abstract description 5
- 230000000694 effects Effects 0.000 description 7
- 230000007246 mechanism Effects 0.000 description 4
- 230000009471 action Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a novel protection structure for an unmanned aerial vehicle wing, which comprises a shell component, wherein a plurality of grooves are formed in the top end of the shell component, mounting grooves are formed in the inner two walls of the plurality of grooves, compression bars are arranged in the two mounting grooves, the improved novel protection structure for the unmanned aerial vehicle wing is realized during the use of the unmanned aerial vehicle through the cooperation of a protection frame, a reinforcing plate and a fixed block, the problem that the unmanned aerial vehicle is damaged due to collision with an object or branches in the flight process of the unmanned aerial vehicle is solved, the situation that the unmanned aerial vehicle is crashed is avoided, the unmanned aerial vehicle wing protection structure is quickly installed and dismantled by utilizing the cooperation of the compression bars, the return springs and the push blocks, the convenience of the unmanned aerial vehicle wing protection structure during the installation is greatly improved, and the installation efficiency is improved, so that the protection requirement of the unmanned aerial vehicle wing is met.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a novel protection structure for an unmanned aerial vehicle wing.
Background
Unmanned plane is unmanned plane for short, is the unmanned plane that utilizes radio remote control equipment and self-contained program control device to operate, perhaps operate independently by on-vehicle computer is complete or intermittent type, unmanned plane is according to the application, can divide into for military use and civilian, for military use aspect, unmanned plane divide into reconnaissance aircraft and target aircraft, for civilian aspect, unmanned plane + trade use, be unmanned plane real just need, in the field of taking photo by plane, agriculture, plant protection, miniature self-timer shooting, express delivery transportation, disaster relief, observe wild animal, monitor infectious disease, survey, news report, electric power inspection, disaster relief, film and television shooting, make romantic etc. the use of unmanned plane itself has been greatly extended.
Unmanned aerial vehicle wing protection architecture carries out effective guard action to unmanned aerial vehicle's wing, can promote unmanned aerial vehicle's security in the flight by a wide margin, leads to unmanned aerial vehicle to appear damaging because of the wing directly ground when preventing unmanned aerial vehicle to drop, therefore unmanned aerial vehicle wing protection architecture is indispensable.
The prior patent (publication number: CN 218368294U) discloses an unmanned aerial vehicle, which comprises a body and a power supply mechanism detachably mounted on the body, wherein a first connecting structure and a second connecting structure are arranged between the body and the power supply mechanism, the power supply mechanism and the body can selectively form a locking effect or release the locking effect through the first connecting structure in a first direction, and the power supply mechanism and the body can selectively form the locking effect or release the locking effect through the second connecting structure in a second direction. Through set up first connection structure and second connection structure between fuselage and power supply unit, first connection structure can form locking or unblock effect to fuselage and power supply unit in first direction, and second connection structure can form locking or unblock effect to fuselage and power supply unit in the second direction, namely, forms locking or structure effect to fuselage and power supply unit in two different directions respectively through two connection structure, is favorable to power supply unit's dismouting. The inventors found that the following problems exist in the prior art in the process of implementing the present utility model: 1. the traditional unmanned aerial vehicle lacks a wing protection structure, and when the unmanned aerial vehicle collides with an unknown object or branch in the flight process, the wing of the unmanned aerial vehicle is easily damaged, so that the unmanned aerial vehicle is crashed; 2. the part unmanned aerial vehicle wing protection architecture needs to install it through multiple appurtenance when the installation, and is consuming time and consuming power, and the operation is comparatively loaded down with trivial details to reduce unmanned aerial vehicle's practicality.
Disclosure of Invention
The utility model aims to provide a novel protection structure for an unmanned aerial vehicle wing, so as to solve the problems that the traditional unmanned aerial vehicle lacks a wing protection structure, when an unmanned aerial vehicle collides with an unknown object or branch in the flying process, the wing of the unmanned aerial vehicle is easily damaged, so that the unmanned aerial vehicle crashes, and part of unmanned aerial vehicle wing protection structures are required to be installed through various auxiliary tools during installation, so that the problems of time and labor consumption and complex operation are solved.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a novel protection architecture that unmanned aerial vehicle wing was used, includes housing assembly, a plurality of recess has been seted up on housing assembly's top, and a plurality of the mounting groove has been seted up to the inside both walls of recess, two the inside of mounting groove is provided with the depression bar, two the one end of depression bar is provided with the ejector pad, two the outside of depression bar is provided with the clamp plate, two one side of clamp plate is provided with reset spring, two the both ends of clamp plate all are provided with the slider, a plurality of peg graft in the inside of recess has the fixed block, a plurality of the fluting has been seted up to one side bottom of fixed block, a plurality of grooved inside both walls are provided with two slide bars respectively, two the outside of slide bar is provided with two fixture blocks, two connect through the spring between the fixture block, a plurality of one side of fixed block is provided with protection frame, a plurality of protection frame's inner wall is provided with the reinforcing plate.
Preferably, the shell assembly comprises an unmanned aerial vehicle body, two connecting rods are respectively arranged on two sides of the unmanned aerial vehicle body, and wing fans are arranged at one ends, away from the unmanned aerial vehicle body, of the connecting rods.
Preferably, a sliding groove is formed in two inner walls of the mounting groove, and the sliding groove is connected with the sliding block in a sliding mode.
Preferably, a clamping structure is arranged between the clamping block and the mounting groove.
Preferably, the sliding rod is in sliding connection with the clamping block.
Preferably, the compression bar, the pushing block and the return spring are symmetrical with respect to the vertical center line of the connecting rod.
Preferably, the grooves are provided as trapezoidal structures.
Compared with the prior art, the utility model has the beneficial effects that:
through the cooperation of protective frame, enhancement version and fixed block, make unmanned aerial vehicle in the use period, realize protecting unmanned aerial vehicle wing, solved unmanned aerial vehicle in the flight, because of bump with object or branch, lead to unmanned aerial vehicle to appear damaging the problem, avoid unmanned aerial vehicle to appear the condition of crash to accord with the protection demand of unmanned aerial vehicle wing.
Through the cooperation of depression bar, reset spring and ejector pad, make unmanned aerial vehicle in the use, realize quick installation and dismantlement to unmanned aerial vehicle wing protection architecture, promote unmanned aerial vehicle wing protection architecture convenience when the installation by a wide margin, increase installation effectiveness to promote unmanned aerial vehicle's practicality by a wide margin.
Drawings
FIG. 1 is a schematic elevational view of the present utility model;
FIG. 2 is a schematic diagram of the internal structure of the front view of the present utility model;
FIG. 3 is a schematic diagram of the side view of the connecting rod of the present utility model in an enlarged internal structure;
fig. 4 is an enlarged schematic view of the structure of fig. 3 a according to the present utility model.
In the figure: 1. a housing assembly; 101. an unmanned aerial vehicle body; 102. a connecting rod; 103. wing fans; 2. a groove; 3. a mounting groove; 4. a compression bar; 5. a pushing block; 6. a pressing plate; 7. a return spring; 8. a slide block; 9. a fixed block; 10. slotting; 11. a slide bar; 12. a clamping block; 13. a spring; 14. a protective frame; 15. reinforcing plate.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which are obtained by a worker of ordinary skill in the art without creative efforts, are within the protection scope of the present utility model based on the embodiments of the present utility model.
Referring to fig. 1 to 4, the present utility model provides a technical solution: the utility model provides a novel protection architecture that unmanned aerial vehicle wing was used, including housing assembly 1, a plurality of recess 2 has been seted up on housing assembly 1's top, mounting groove 3 has been seted up to the inside both walls of a plurality of recess 2, the inside of two mounting grooves 3 is provided with depression bar 4, the one end of two depression bars 4 is provided with pusher 5, the outside of two depression bars 4 is provided with clamp plate 6, one side of two clamp plates 6 is provided with reset spring 7, the both ends of two clamp plates 6 all are provided with slider 8, fixed block 9 has been pegged graft to the inside of a plurality of recess 2, fluting 10 has been seted up to one side bottom of a plurality of fixed block 9, the inside both walls of a plurality of fluting 10 are provided with two slide bars 11 respectively, the outside of two slide bars 11 is provided with two fixture blocks 12, be connected through spring 13 between two fixture blocks 12, one side of a plurality of fixed block 9 is provided with protection frame 14, the inner wall of a plurality of protection frame 14 is provided with reinforcing plate 15.
In this embodiment, as shown in fig. 1, the housing assembly 1 includes an unmanned aerial vehicle body 101, two sides of the unmanned aerial vehicle body 101 are respectively provided with two connecting rods 102, and one end of the two connecting rods 102 away from the unmanned aerial vehicle body 101 is provided with a wing fan 103.
In this embodiment, as shown in fig. 4, two walls of the inside of the installation groove 3 are provided with sliding grooves, and the sliding grooves are in sliding connection with the sliding blocks 8; the stability of the platen 6 during movement is increased, thereby avoiding the occurrence of deflection of the platen 6 during movement.
In this embodiment, as shown in fig. 3 and 4, a clamping structure is set between the clamping block 12 and the mounting groove 3, so as to fix the wing protection frame 14 of the unmanned aerial vehicle, and avoid the shaking of the protection frame 14 during use.
In this embodiment, as shown in fig. 4, the sliding rod 11 and the clamping block 12 are slidably connected, so that stability of the clamping block 12 during movement is increased, the movement direction of the clamping block 12 is single, and the problem of inclination of the clamping block 12 during movement is prevented.
In this embodiment, as shown in fig. 3, the compression bar 4, the push block 5 and the return spring 7 are symmetrical with respect to the vertical center line of the connecting rod 102; realize quick installation and dismantlement to unmanned aerial vehicle wing protection architecture, promote unmanned aerial vehicle wing protection architecture convenience when the installation by a wide margin, increase installation effectiveness.
In this embodiment, as shown in fig. 3, the groove 2 is a trapezoid structure, so that the two clamping blocks 12 are more smoothly clamped with the inside of the mounting groove 3 under the action of the spring 13.
The application method and the advantages of the utility model are as follows: this kind of novel protection architecture that unmanned aerial vehicle wing was used when using, the working process is as follows:
as shown in fig. 1, fig. 2, fig. 3 and fig. 4, firstly, when needing to protect unmanned aerial vehicle wing, through driving the inside of protection frame 14 and reinforcing plate 15 grafting and recess 2 with fixed block 9, two fixture blocks 12 compress spring 13 under the extrusion of recess 2, when fixture block 12 moves to mounting groove 3 department, utilize spring 13's elastic structure, drive the inside of two fixture block 12 joint and mounting groove 3, make fixture block 12 and mounting groove 3 form the joint structure, realize the fixed to unmanned aerial vehicle wing protection frame 14, avoid protection frame 14 to appear rocking the condition during the use, realize protecting unmanned aerial vehicle wing, the unmanned aerial vehicle is in flight in-process because of bump with object or branch, and the problem that damage appears in unmanned aerial vehicle is avoided unmanned aerial vehicle, avoid unmanned aerial vehicle to appear the condition of crash, when need dismantle to protection frame 14, press two 4, depression bar 4 drive clamp plate 6 and push away from each other 5 and carry out synchronous movement under the cooperation of slider 8 and spout, and release spring 7 carries out compression spring 7 when the depression plate 6 moves, thereby make push away from clamp plate 12 with the compression block 3 and make the condition that push away from the inside of 3 to make the compression plate 12 and make the inside of clamping plate 3 and detach, thereby realize the demand of the improvement of protection frame to install the frame to the side of 3, and the demand of the unmanned aerial vehicle is high-lift the safety device, and the demand is increased, and the demand is realized to the improvement to the safety device is realized, and the safety device is improved.
The foregoing has shown and described the basic principles, principal features and advantages of the utility model. It will be understood by those skilled in the art that the present utility model is not limited to the above-described embodiments, and that the above-described embodiments and descriptions are only preferred embodiments of the present utility model, and are not intended to limit the utility model, and that various changes and modifications may be made therein without departing from the spirit and scope of the utility model as claimed. The scope of the utility model is defined by the appended claims and equivalents thereof.
Claims (7)
1. Novel protection architecture that unmanned aerial vehicle wing was used, including shell subassembly (1), its characterized in that: the utility model discloses a protection device for the automobile, including shell subassembly (1), mounting groove (3) have been seted up on the top of shell subassembly (1), a plurality of mounting groove (2)'s inside both walls have been seted up, two the inside of mounting groove (3) is provided with depression bar (4), two the one end of depression bar (4) is provided with ejector pad (5), two the outside of depression bar (4) is provided with clamp plate (6), two one side of clamp plate (6) is provided with reset spring (7), two the both ends of clamp plate (6) all are provided with slider (8), a plurality of peg graft in the inside of recess (2) has fixed block (9), a plurality of fluting (10) have been seted up to one side bottom of fixed block (9), a plurality of fluting (10) inside both walls are provided with two slide bar (11) respectively, two the outside of slide bar (11) is provided with two fixture block (12), two be connected through spring (13) between fixture block (12), a plurality of one side of fixed block (9) is provided with protection frame (14), a plurality of protection frame (14) inner wall (15).
2. The novel protective structure for an unmanned aerial vehicle wing according to claim 1, wherein: the shell assembly (1) comprises an unmanned aerial vehicle body (101), two connecting rods (102) are respectively arranged on two sides of the unmanned aerial vehicle body (101), and wing fans (103) are arranged at one ends, far away from the unmanned aerial vehicle body (101), of the connecting rods (102).
3. The novel protective structure for an unmanned aerial vehicle wing according to claim 1, wherein: the two walls inside the mounting groove (3) are provided with sliding grooves, and the sliding grooves are connected with the sliding blocks (8) in a sliding mode.
4. The novel protective structure for an unmanned aerial vehicle wing according to claim 1, wherein: the clamping block (12) and the mounting groove (3) are arranged into a clamping structure.
5. The novel protective structure for an unmanned aerial vehicle wing according to claim 1, wherein: the sliding rod (11) is connected with the clamping block (12) in a sliding way.
6. The novel protective structure for an unmanned aerial vehicle wing according to claim 1, wherein: the compression bar (4), the pushing block (5) and the return spring (7) are respectively symmetrical with respect to the vertical center line of the connecting rod (102).
7. The novel protective structure for an unmanned aerial vehicle wing according to claim 1, wherein: the groove (2) is a trapezoid structure body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321467042.7U CN220786179U (en) | 2023-06-08 | 2023-06-08 | Novel protection architecture that unmanned aerial vehicle wing was used |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321467042.7U CN220786179U (en) | 2023-06-08 | 2023-06-08 | Novel protection architecture that unmanned aerial vehicle wing was used |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220786179U true CN220786179U (en) | 2024-04-16 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321467042.7U Active CN220786179U (en) | 2023-06-08 | 2023-06-08 | Novel protection architecture that unmanned aerial vehicle wing was used |
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| Country | Link |
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| CN (1) | CN220786179U (en) |
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2023
- 2023-06-08 CN CN202321467042.7U patent/CN220786179U/en active Active
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240705 Address after: 211400 Building A3, West of Mintai Avenue, Economic Development Zone, Yizheng City, Yangzhou City, Jiangsu Province Patentee after: Yangzhou Hangwei Technology Co.,Ltd. Country or region after: China Address before: 430000 Leke Workshop Incubator, Building 1, Lianchuang Technology Center, No. 55 Haitang Road, Wuhan Economic and Technological Development Zone, Wuhan City, Hubei Province (Ji-LKGC-B53) Patentee before: Wuhan Heyi Technology Co.,Ltd. Country or region before: China |
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| TR01 | Transfer of patent right |