CN220263110U - Unmanned aerial vehicle portable coupling assembling - Google Patents
Unmanned aerial vehicle portable coupling assembling Download PDFInfo
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- CN220263110U CN220263110U CN202322142517.1U CN202322142517U CN220263110U CN 220263110 U CN220263110 U CN 220263110U CN 202322142517 U CN202322142517 U CN 202322142517U CN 220263110 U CN220263110 U CN 220263110U
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- 230000008878 coupling Effects 0.000 title claims description 6
- 238000010168 coupling process Methods 0.000 title claims description 6
- 238000005859 coupling reaction Methods 0.000 title claims description 6
- 230000007246 mechanism Effects 0.000 claims abstract description 12
- 230000000694 effects Effects 0.000 abstract description 4
- 230000003139 buffering effect Effects 0.000 abstract description 3
- 230000002035 prolonged effect Effects 0.000 abstract description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
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- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses a portable connection assembly of an unmanned aerial vehicle, which comprises a machine body, four groups of connection frames and four groups of power devices, wherein the connection frames comprise a first frame body and a second frame body, the power devices comprise a motor and two groups of rotary blades, a protection mechanism is arranged outside the connection frames and comprises a protection assembly and a fixing assembly, the protection assembly comprises a protection ring, a sponge ring is fixedly arranged outside the protection ring, a rubber ring is fixedly arranged outside the sponge ring, the fixing assembly comprises a lantern ring and two groups of inclined plates, and screw holes are formed in the inclined plates; according to the utility model, through the designed protection mechanism, the connecting frame can be conveniently protected in use, deformation and damage caused by the fact that the connecting frame is mistakenly touched with external foreign matters are prevented, the protection effect is achieved through the protection ring, the rubber ring and the sponge ring play a buffering role, the service life of the connecting frame is prolonged, and the use cost is reduced.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle connectors, and particularly relates to a portable connecting assembly of an unmanned aerial vehicle.
Background
The unmanned plane is an unmanned plane, is a unmanned plane operated by using radio remote control equipment and a self-provided program control device, or is operated completely or intermittently and autonomously by a vehicle-mounted computer, the unmanned plane is flown by a power device on the unmanned plane, and a fuselage on the unmanned plane is connected with the power device by a connecting frame.
The current unmanned aerial vehicle portable coupling assembling is in the time of using, when the unmanned aerial vehicle is by mistake when touching external object in the flight, causes link and object to produce the collision easily, leads to the link to produce deformation or damage, reduces link life, influences unmanned aerial vehicle flight's problem, for this we propose an unmanned aerial vehicle portable coupling assembling.
Disclosure of Invention
The utility model aims to provide an unmanned aerial vehicle portable connecting assembly, which solves the problem that when the conventional unmanned aerial vehicle portable connecting assembly is used, a connecting frame is easy to collide with an external object in the flight process of the unmanned aerial vehicle to cause deformation or damage.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an unmanned aerial vehicle portable coupling assembling, includes fuselage, four link and four power pack of group, the link includes support body one and support body two, power pack includes motor and two sets of spiral vane, the outside of link is provided with protection machanism, protection machanism includes protection component and fixed subassembly, protection component includes the protection ring, the outside of protection ring is fixed and is provided with the sponge ring, the outside of sponge ring is fixed and is provided with the rubber ring.
Preferably, the fixing component comprises a lantern ring and two groups of inclined plates, and screw holes are formed in the inclined plates.
Preferably, a screw is arranged in the screw hole, and the working end of the screw extends to the outer wall of the lantern ring.
Preferably, the screw rod is connected with the screw hole through screw thread screwing, and a rotating handle is fixedly arranged at the end part of the screw rod.
Preferably, the sloping plate is fixed on the protection ring, and the lantern ring is fixed outside the second frame body.
Preferably, a disassembly and assembly mechanism is arranged between the second frame body and the first frame body, the disassembly and assembly mechanism comprises an external thread ring and an internal thread ring, two groups of baffles are fixedly arranged on the second frame body, and the external thread ring is connected with the internal thread ring through thread screwing.
Preferably, the external thread ring is fixed on the second frame body, and the internal thread ring is fixed on the first frame body.
Preferably, four groups of clamping plates are fixedly arranged on the machine body, and the clamping plates are fixedly connected with the first frame body through screws.
Compared with the prior art, the utility model has the beneficial effects that:
(1) According to the utility model, through the designed protection mechanism, the connecting frame can be conveniently protected in use, deformation and damage caused by the fact that the connecting frame is mistakenly touched with external foreign matters are prevented, the protection effect is achieved through the protection ring, the rubber ring and the sponge ring play a buffering role, the service life of the connecting frame is prolonged, and the use cost is reduced.
Drawings
FIG. 1 is a schematic diagram of the structure of the present utility model;
FIG. 2 is an enlarged schematic view of the portion A of FIG. 1 according to the present utility model;
FIG. 3 is a schematic cross-sectional view of the swash plate according to the present utility model;
FIG. 4 is a schematic cross-sectional view of a rubber ring sponge ring according to the present utility model;
FIG. 5 is a schematic view of the assembly and disassembly mechanism according to the present utility model;
in the figure: 100. a rubber ring; 101. a sponge ring; 102. a guard ring; 111. a collar; 112. a sloping plate; 113. a rotary handle; 114. a screw; 115. a screw hole; 200. a body; 300. a first frame body; 301. a second frame body; 400. a clamping plate; 500. rotating leaves; 501. a motor; 600. an external threaded ring; 601. an internally threaded ring; 602. and a baffle.
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 can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Examples
Referring to fig. 1-5, the present utility model provides a technical solution: the utility model provides an unmanned aerial vehicle portable connection subassembly, including fuselage 200, four link and four power pack of group, the link includes support body one 300 and support body two 301, power pack includes motor 501 and two sets of spiral vane 500, the outside of link is provided with protection machanism, protection machanism includes protection component and fixed subassembly, protection component includes protection ring 102, protection ring 102 is located the outside of link in the time of using, protection ring 102's outside is fixed and is provided with sponge ring 101, sponge ring 101's outside is fixed and is provided with rubber ring 100, rubber ring 100 and sponge ring 101 can play the cushioning effect in the time of using, fixed subassembly includes lantern ring 111 and two sets of swash plate 112, screw 115 has been seted up to the inside of swash plate 112, the inside of screw 115 is provided with screw 114, through threaded connection between screw 114 and the screw 115, the work end of screw 114 extends to the outer wall of lantern ring 111, through the screw thread spin-in connection between screw 114 and the screw 115, the tip of screw 114 is fixed to be provided with the knob 113, can conveniently rotate screw 114 in the time of using through knob 113, the fixed on protection ring 102, the effect of protecting ring 102 can be played the outside through the design of two sets of swash plate 112, the life-span is reduced in the use, the life-time of can be reached through the frame is connected with the frame is fixed to the outside through the screw ring 111, the frame is convenient for use, the life-to have been realized, the life has been reduced and can be damaged in the life has been used, and can be used to protect the frame has been realized, and has been used in the life has been used, and has been used to the life has been used.
In this embodiment, preferably, a dismounting mechanism is provided between the second frame 301 and the first frame 300, the dismounting mechanism includes an external thread ring 600 and an internal thread ring 601, when in use, the external thread ring 600 can be in threaded connection with the internal thread ring 601, two groups of baffles 602 are fixedly provided on the second frame 301, when in use, the baffles 602 can play a limiting role, the external thread ring 600 and the internal thread ring 601 are connected through threaded engagement, the external thread ring 600 is fixed on the second frame 301, the internal thread ring 601 is fixed on the first frame 300, and through the dismounting mechanism, the dismounting mechanism is convenient to use, when the first frame 300 or the second frame 301 on the connecting frame is damaged, the damaged first frame 300 or the second frame 301 can be replaced independently, the replacement cost is reduced, the waste of materials is also reduced, and the use is convenient.
In this embodiment, preferably, four groups of clamping plates 400 are fixedly arranged on the machine body 200, the clamping plates 400 are fixedly connected with the first frame body 300 through screws, the connecting frame can be disassembled and assembled through the screws when the machine is used, and the connecting frame can be disassembled from the machine body 200 by unscrewing the screws, so that the occupied space of the connecting frame is reduced, and the connecting frame is convenient to carry.
The working principle and the using flow of the utility model are as follows:
when the utility model is used, the protecting ring 102 on the protecting component is sleeved on the connecting frame from the end part of the first frame body 300 on the connecting frame, at the moment, the end part of the inclined plate 112 is positioned outside the lantern ring 111, at the moment, the rotary handle 113 is rotated towards the direction close to the lantern ring 111 to drive the screw 114 to rotate, then the end part of the screw 114 contacts and clamps the lantern ring 111, at the moment, the protecting component can be arranged, at the moment, the protecting component can protect the connecting frame, when the connecting frame quickly touches external foreign matters, at the moment, the external foreign matters contact with the rubber ring 100, the rubber ring 100 and the sponge ring 101 can play a role of buffering, and the protecting ring 102 can play a role of protecting the connecting frame, thereby playing a protecting role on the connecting frame;
when the first frame 300 or the second frame 301 in the connecting frame is damaged, the first frame 300 can be rotated in a direction away from the second frame 301 to drive the inner threaded ring 601 to rotate, then the inner threaded ring 601 is separated from the outer threaded ring 600, the first frame 300 and the second frame 301 can be separated, and then a new first frame 300 or second frame 301 can be taken out for replacement according to the reverse principle.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (8)
1. The utility model provides an unmanned aerial vehicle portable coupling assembling, includes fuselage (200), four link and four power pack of group, the link includes support body one (300) and support body two (301), power pack includes motor (501) and two sets of whirl vane (500), its characterized in that: the outside of link is provided with protection machanism, protection machanism includes protection subassembly and fixed subassembly, protection subassembly includes protection ring (102), the outside of protection ring (102) is fixed and is provided with sponge ring (101), the outside of sponge ring (101) is fixed and is provided with rubber ring (100).
2. The unmanned aerial vehicle portable connection assembly of claim 1, wherein: the fixing assembly comprises a lantern ring (111) and two groups of inclined plates (112), and screw holes (115) are formed in the inclined plates (112).
3. The unmanned aerial vehicle portable connection assembly of claim 2, wherein: the screw hole (115) is internally provided with a screw rod (114), and the working end of the screw rod (114) extends to the outer wall of the lantern ring (111).
4. A portable unmanned aerial vehicle connection assembly according to claim 3, wherein: the screw (114) is connected with the screw hole (115) through threaded screwing, and a rotary handle (113) is fixedly arranged at the end part of the screw (114).
5. The unmanned aerial vehicle portable connection assembly of claim 4, wherein: the inclined plate (112) is fixed on the protection ring (102), and the lantern ring (111) is fixed outside the second frame body (301).
6. The unmanned aerial vehicle portable connection assembly of claim 1, wherein: the novel lifting frame comprises a frame body II (301) and a frame body I (300), wherein a dismounting mechanism is arranged between the frame body II (301) and the frame body I (300), the dismounting mechanism comprises an external thread ring (600) and an internal thread ring (601), two groups of baffles (602) are fixedly arranged on the frame body II (301), and the external thread ring (600) is connected with the internal thread ring (601) through thread screwing.
7. The unmanned aerial vehicle portable connection assembly of claim 6, wherein: the external thread ring (600) is fixed on the second frame body (301), and the internal thread ring (601) is fixed on the first frame body (300).
8. The unmanned aerial vehicle portable connection assembly of claim 1, wherein: four groups of clamping plates (400) are fixedly arranged on the machine body (200), and the clamping plates (400) are fixedly connected with the first frame body (300) through screws.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202322142517.1U CN220263110U (en) | 2023-08-09 | 2023-08-09 | Unmanned aerial vehicle portable coupling assembling |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202322142517.1U CN220263110U (en) | 2023-08-09 | 2023-08-09 | Unmanned aerial vehicle portable coupling assembling |
Publications (1)
Publication Number | Publication Date |
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CN220263110U true CN220263110U (en) | 2023-12-29 |
Family
ID=89318231
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202322142517.1U Active CN220263110U (en) | 2023-08-09 | 2023-08-09 | Unmanned aerial vehicle portable coupling assembling |
Country Status (1)
Country | Link |
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CN (1) | CN220263110U (en) |
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2023
- 2023-08-09 CN CN202322142517.1U patent/CN220263110U/en active Active
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