CN216994885U - Automatic quick-witted nest that charges of retrieving of VTOL fixed wing unmanned aerial vehicle - Google Patents
Automatic quick-witted nest that charges of retrieving of VTOL fixed wing unmanned aerial vehicle Download PDFInfo
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- CN216994885U CN216994885U CN202220608631.1U CN202220608631U CN216994885U CN 216994885 U CN216994885 U CN 216994885U CN 202220608631 U CN202220608631 U CN 202220608631U CN 216994885 U CN216994885 U CN 216994885U
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Abstract
The utility model relates to the technical field of unmanned aerial vehicle machine nests, in particular to a vertical take-off and landing fixed wing unmanned aerial vehicle automatic recovery charger nest which comprises a machine body and four adjusting devices, wherein a placing plate is arranged on the inner wall of the machine body, two machine covers are arranged on the upper surface of the machine body, a circuit is arranged on one side of the machine body, the adjusting devices are arranged on the surface of the machine body, each adjusting device comprises a placing sleeve, the number of the placing sleeves is four, the placing sleeves are fixedly connected with the surface of the machine body, a supporting rod is connected to the inner wall of each placing sleeve in a sliding mode, a sliding hole is formed in the surface of each placing sleeve, a hollow block is fixedly connected to the surface of each supporting rod and is connected with the inner wall of the corresponding sliding hole in a sliding mode, and a fixing rod is fixedly connected to the inner wall of the sliding hole in the surface of each placing sleeve. According to the utility model, the adjusting device is arranged, so that the equipment can be conveniently adjusted and placed, the phenomenon that the equipment is placed unevenly on a low-lying ground can be effectively reduced, the influence of the equipment on the recovery of the unmanned aerial vehicle is reduced, and the integral stability of the equipment is further improved.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle nests, in particular to an automatic recycling charger nest of a vertical take-off and landing fixed-wing unmanned aerial vehicle.
Background
Vertical take-off and landing fixed wing unmanned aerial vehicle retrieves to charge often and uses automatic recovery machine nest that charges, and present most equipment is when carrying out the use, because equipment is placed on low-lying road surface, easily appears placing uneven phenomenon, leads to equipment to collapse and the uneven condition that influences unmanned aerial vehicle and park of equipment, need improve this.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the defects that equipment collapses and the parking of an unmanned aerial vehicle is influenced by uneven equipment due to the fact that the equipment is placed on a low-lying road surface in the prior art, and provides an automatic recovery charger nest for a vertical take-off and landing fixed wing unmanned aerial vehicle.
In order to achieve the purpose, the utility model adopts the following technical scheme: a vertical take-off and landing fixed wing unmanned aerial vehicle automatic recovery charger nest comprises a machine body and an adjusting device, wherein a placing plate is arranged on the inner wall of the machine body, two machine covers are arranged on the upper surface of the machine body, a circuit is arranged on one side of the machine body, the adjusting device is arranged on the surface of the machine body and comprises four placing sleeves, the placing sleeves are fixedly connected with the surface of the machine body, a supporting rod is connected with the inner wall of each placing sleeve in a sliding manner, a sliding hole is formed in the surface of each placing sleeve, a hollow block is fixedly connected with the surface of each supporting rod and is connected with the inner wall of each sliding hole in a sliding manner, a fixing rod is fixedly connected with the inner wall of each sliding hole in the surface of each placing sleeve, a round hole is formed in the surface of each clamping block, the fixing rod is connected with the inner wall of each round hole in a sliding manner, and the inner wall of each hollow block is connected with the clamping block in a sliding manner, the draw-in groove has been seted up on the surface of dead lever, fixture block and draw-in groove joint through setting up the fixture block, can restrict bracing piece and hollow block, and the convenience supports the bracing piece, can reduce equipment effectively and place the condition that uneven influence unmanned aerial vehicle parks.
Preferably, the number of dead lever surface draw-in groove has a plurality ofly, a plurality of draw-in grooves are equidistant setting, through setting up a plurality of draw-in grooves, conveniently adjust the position of bracing piece, are convenient for place on low-lying road surface.
Preferably, a circular hole is formed in one side of the hollow block, a pull rod is fixedly connected to one side of the fixture block, the pull rod is connected with the inner wall of the circular hole in a sliding mode, the fixture block is convenient to control to move through the pull rod, and the whole usability is improved.
Preferably, the surface cover of pull rod is equipped with first spring, the both ends of first spring respectively with the inner wall fixed connection of fixture block and hollow block, through setting up first spring, be convenient for control fixture block resets, improves the constraint effect of fixture block.
Preferably, one side that the organism is close to the circuit is provided with the anticreep device, the anticreep device is including solid fixed ring, gu fixed ring is connected with the fixed surface of organism, gu fixed ring's surface has seted up the ring channel, the inner wall of ring channel rotates and is connected with the control ring, the fixed surface of control ring is connected with two kellies, the fixed surface of circuit is connected with the spacing ring, two recesses have been seted up on the surface of spacing ring, kellies and groove joint cooperate through kellies and spacing ring, can reduce the circuit atress condition of droing, influences the normal charge of equipment.
Preferably, the connecting hole has been seted up on the surface of control ring, the inner wall sliding connection of connecting hole has the inserted bar, the slot has been seted up on solid fixed ring's surface, inserted bar and slot joint through setting up the inserted bar, can restrict control ring and kelly, improve holistic stability.
Preferably, the surface cover of inserted bar is equipped with the second spring, the both ends of second spring respectively with inserted bar and control ring fixed connection, through setting up the second spring, can control the inserted bar and reset, improve the constraint effect of inserted bar.
Compared with the prior art, the utility model has the advantages and positive effects that:
1. according to the utility model, through the arrangement of the adjusting device, when the equipment needs to be used, the pull rod is pulled, the pull rod drives the fixture block to move, the first spring is stressed and deformed to generate elastic force, the fixture block loses the constraint on the clamping groove in the surface of the fixed rod, the position of the support rod is adjusted in the placing sleeve, when the adjustment is completed, the pull rod is loosened, the first spring releases the elastic force, the fixture block is inserted into the clamping groove in the surface of the fixed rod, through the arrangement of the adjusting device, the equipment is conveniently adjusted and placed, the phenomenon that the equipment is not placed flatly on the low-lying ground can be effectively reduced, the influence of the equipment on the unmanned aerial vehicle recovery is reduced, and the overall stability of the equipment is further improved.
Drawings
Fig. 1 is a schematic perspective view of an automatic recovery charger nest of a vertical take-off and landing fixed wing unmanned aerial vehicle according to the present invention;
fig. 2 is a schematic structural diagram of an adjusting device for an automatic recovery charger nest of a vertical take-off and landing fixed wing unmanned aerial vehicle, according to the utility model;
fig. 3 is a schematic cross-sectional structural view of an adjusting device for an automatic recovery charger nest of a vertical take-off and landing fixed wing unmanned aerial vehicle according to the utility model;
fig. 4 is a schematic structural diagram of a position a in fig. 3, showing an automatic recovery charger nest of a vertical take-off and landing fixed wing unmanned aerial vehicle according to the present invention;
fig. 5 is a schematic structural view of an anti-disengaging device for an automatic recovery charger nest of a vertical take-off and landing fixed wing unmanned aerial vehicle provided by the utility model.
Illustration of the drawings:
1. a body; 2. placing the plate; 3. a machine cover; 4. a line; 5. an adjustment device; 51. placing a sleeve; 52. a support bar; 53. a hollow block; 54. fixing the rod; 55. a clamping block; 56. a pull rod; 57. a first spring; 6. an anti-drop device; 61. a fixing ring; 62. a control loop; 63. a clamping rod; 64. a limiting ring; 65. inserting a rod; 66. a second spring.
Detailed Description
Referring to fig. 1-5, the present invention provides a technical solution: the utility model provides an automatic quick-witted nest that charges of retrieving of VTOL fixed wing unmanned aerial vehicle, includes organism 1 and adjusting device 5, and the inner wall of organism 1 is provided with places board 2, and the upper surface of organism 1 is provided with two covers 3, and one side of organism 1 is provided with circuit 4, and adjusting device 5 sets up at organism 1 on the surface, and one side that organism 1 is close to circuit 4 is provided with anticreep device 6.
The specific arrangement and function of the adjusting device 5 and the anti-slip device 6 will be described in detail below.
In this embodiment: adjusting device 5 is including placing cover 51, the number of placing cover 51 has four, place the fixed surface that cover 51 and organism 1 and be connected, the inner wall sliding connection who places cover 51 has bracing piece 52, the surface of placing cover 51 has seted up the slide opening, the fixed surface of bracing piece 52 is connected with hollow block 53, the inner wall sliding connection of hollow block 53 and slide opening, the inner wall fixedly connected with dead lever 54 of placing cover 51 surface slide opening, the round hole has been seted up on the surface of fixture block 55, the inner wall sliding connection of dead lever 54 and round hole, the inner wall sliding connection fixture block 55 of hollow block 53, the draw-in groove has been seted up on the surface of dead lever 54, fixture block 55 and draw-in groove joint, through setting up fixture block 55, can restrict bracing piece 52 and hollow block 53, it supports bracing piece 52 conveniently, the condition that equipment placed unevennesses and influence unmanned aerial vehicle parking can be reduced effectively.
Specifically, the number of dead lever 54 surface draw-in groove has a plurality ofly, and a plurality of draw-in grooves are equidistant setting, through setting up a plurality of draw-in grooves, conveniently adjust the position of bracing piece 52, are convenient for place on low-lying road surface.
Specifically, a circular hole is formed in one side of the hollow block 53, a pull rod 56 is fixedly connected to one side of the fixture block 55, and the pull rod 56 is slidably connected with the inner wall of the circular hole.
In this embodiment: through setting up pull rod 56, be convenient for control fixture block 55 and remove, improve whole ease for use.
Specifically, the surface of the pull rod 56 is sleeved with the first spring 57, two ends of the first spring 57 are respectively and fixedly connected with the inner walls of the fixture block 55 and the hollow block 53, and the first spring 57 is arranged, so that the fixture block 55 can be conveniently controlled to reset, and the binding effect of the fixture block 55 is improved.
In this embodiment: anticreep device 6 is connected with the fixed surface of organism 1 including solid fixed ring 61, and the ring channel has been seted up on solid fixed ring 61's surface, and the inner wall of ring channel rotates and is connected with control ring 62, and control ring 62's fixed surface is connected with two kellies 63, and circuit 4's fixed surface is connected with spacing ring 64, and two recesses, kellies 63 and groove joint have been seted up on spacing ring 64's surface.
In this embodiment: cooperate through kelly 63 and spacing ring 64, can reduce the condition that drops appears in the circuit 4 atress, influence the normal charging of equipment.
Specifically, the connecting hole has been seted up on the surface of control ring 62, and the inner wall sliding connection of connecting hole has inserted bar 65, and the slot has been seted up on the surface of solid fixed ring 61, and inserted bar 65 and slot joint through setting up inserted bar 65, can restrict control ring 62 and kelly 63, improve holistic stability.
Specifically, the surface of the insertion rod 65 is sleeved with a second spring 66, and two ends of the second spring 66 are respectively fixedly connected with the insertion rod 65 and the control ring 62.
In this embodiment: through setting up second spring 66, can control inserted bar 65 and reset, improve inserted bar 65's constraint effect.
The working principle is as follows: by arranging the adjusting device 5, when the equipment needs to be used, the pull rod 56 is pulled, the pull rod 56 drives the clamping block 55 to move, the first spring 57 is stressed and deformed to generate elastic force, the clamping block 55 loses the constraint on the clamping groove on the surface of the fixed rod 54, the position of the supporting rod 52 is adjusted in the placing sleeve 51, when the adjustment is completed, the pull rod 56 is loosened, the first spring 57 releases the elastic force, the clamping block 55 is inserted into the clamping groove on the surface of the fixed rod 54, the adjustment and the placement of the equipment are facilitated by arranging the adjusting device 5, the phenomenon that the equipment is placed unevenly on a low-lying ground can be effectively reduced, the influence of the equipment on the recovery of the unmanned aerial vehicle is reduced, the integral stability of the equipment is further improved, by arranging the anti-falling device 6, when the clamping rod 63 passes through the groove on the surface of the limiting ring 64, the control ring 62 is rotated, the control ring 62 drives the clamping rod 63 to rotate, rotate to a certain position, second spring 66 releases elasticity, drives inserted bar 65 and resets and inserts and establish in solid fixed ring 61 surface slot, makes kelly 63 offset with spacing ring 64's surface, can accomplish and use, through setting up anticreep device 6, is convenient for consolidate the protection to equipment wire connection department, can reduce the phenomenon that equipment connection department atress appears droing effectively, has reduced the unable normal circumstances of charging of equipment, and then has improved the holistic protectiveness of equipment.
Claims (7)
1. The utility model provides an automatic quick-witted nest that charges of retrieving of VTOL fixed wing unmanned aerial vehicle, includes organism (1) and adjusting device (5), its characterized in that: the inner wall of the machine body (1) is provided with a placing plate (2), the upper surface of the machine body (1) is provided with two machine covers (3), one side of the machine body (1) is provided with a circuit (4), the adjusting device (5) is arranged on the surface of the machine body (1), the adjusting device (5) comprises four placing sleeves (51), the number of the placing sleeves (51) is four, the placing sleeves (51) are fixedly connected with the surface of the machine body (1), the inner wall of the placing sleeves (51) is slidably connected with a supporting rod (52), the surface of the placing sleeves (51) is provided with a sliding hole, the surface of the supporting rod (52) is fixedly connected with a hollow block (53), the hollow block (53) is slidably connected with the inner wall of the sliding hole, the inner wall of the surface sliding hole of the placing sleeves (51) is fixedly connected with a fixing rod (54), and the surface of the clamping block (55) is provided with a round hole, the fixing rod (54) is connected with the inner wall of the round hole in a sliding mode, the inner wall of the hollow block (53) is connected with a clamping block (55) in a sliding mode, a clamping groove is formed in the surface of the fixing rod (54), and the clamping block (55) is clamped with the clamping groove.
2. The automatic recycling charger nest of VTOL fixed wing unmanned aerial vehicle of claim 1, characterized by: the number of the clamping grooves on the surface of the fixing rod (54) is multiple, and the clamping grooves are arranged at equal intervals.
3. The automatic recycling charger nest of VTOL fixed wing unmanned aerial vehicle of claim 1, characterized by: a circular hole is formed in one side of the hollow block (53), a pull rod (56) is fixedly connected to one side of the clamping block (55), and the pull rod (56) is connected with the inner wall of the circular hole in a sliding mode.
4. The automatic recycling charger nest of VTOL fixed wing unmanned aerial vehicle of claim 3, characterized by: the surface of the pull rod (56) is sleeved with a first spring (57), and two ends of the first spring (57) are fixedly connected with the inner walls of the clamping block (55) and the hollow block (53) respectively.
5. The automatic recycling charger nest of VTOL fixed wing unmanned aerial vehicle of claim 1, characterized by: organism (1) is close to one side of circuit (4) and is provided with anticreep device (6), anticreep device (6) are including solid fixed ring (61), gu fixed ring (61) is connected with the fixed surface of organism (1), the ring channel has been seted up on the surface of solid fixed ring (61), the inner wall of ring channel rotates and is connected with control ring (62), the fixed surface of control ring (62) is connected with two kellies (63), the fixed surface of circuit (4) is connected with spacing ring (64), two recesses have been seted up on the surface of spacing ring (64), kellies (63) and groove joint.
6. The automatic recycling charger nest of VTOL fixed wing unmanned aerial vehicle of claim 5, characterized by: the connecting hole has been seted up on the surface of control ring (62), the inner wall sliding connection of connecting hole has inserted bar (65), the slot has been seted up on the surface of solid fixed ring (61), inserted bar (65) and slot joint.
7. The automatic recycling charger nest of the vertical take-off and landing fixed-wing unmanned aerial vehicle according to claim 6, characterized in that: the surface cover of inserted bar (65) is equipped with second spring (66), the both ends of second spring (66) respectively with inserted bar (65) and control ring (62) fixed connection.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202220608631.1U CN216994885U (en) | 2022-03-18 | 2022-03-18 | Automatic quick-witted nest that charges of retrieving of VTOL fixed wing unmanned aerial vehicle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN202220608631.1U CN216994885U (en) | 2022-03-18 | 2022-03-18 | Automatic quick-witted nest that charges of retrieving of VTOL fixed wing unmanned aerial vehicle |
Publications (1)
Publication Number | Publication Date |
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CN216994885U true CN216994885U (en) | 2022-07-19 |
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Application Number | Title | Priority Date | Filing Date |
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CN202220608631.1U Active CN216994885U (en) | 2022-03-18 | 2022-03-18 | Automatic quick-witted nest that charges of retrieving of VTOL fixed wing unmanned aerial vehicle |
Country Status (1)
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CN (1) | CN216994885U (en) |
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2022
- 2022-03-18 CN CN202220608631.1U patent/CN216994885U/en active Active
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