CN212530081U - Unmanned aerial vehicle load interface - Google Patents
Unmanned aerial vehicle load interface Download PDFInfo
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- CN212530081U CN212530081U CN202021442697.5U CN202021442697U CN212530081U CN 212530081 U CN212530081 U CN 212530081U CN 202021442697 U CN202021442697 U CN 202021442697U CN 212530081 U CN212530081 U CN 212530081U
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- casing
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- shell
- aerial vehicle
- unmanned aerial
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- 230000007246 mechanism Effects 0.000 claims abstract description 14
- 230000003028 elevating effect Effects 0.000 claims abstract description 5
- 238000009434 installation Methods 0.000 claims description 8
- 230000005611 electricity Effects 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle load interface, including panel, interface and more than one casing, the opening of casing sets up relatively, all is equipped with the gag lever post more than in the opening of casing, and the centre department of upper end casing is equipped with a square mouth, and the panel sets up in the casing upper end, and the bottom surface of panel just forms a fixed part to square mouth department downward protrusion, is equipped with a recess on the bottom surface of fixed part, and the interface is embedded to be installed in the recess, and the angle adjustment mechanism who is connected with the casing is installed to the both sides of panel, installs elevating system between casing and the casing. The utility model discloses simple structure accomplishes the electricity between load and the unmanned aerial vehicle through the mode of pegging graft and is connected, and load self then compresses tightly through elevating system and is fixed in between the casing to can be spacing with different structure loads through the gag lever post that can move backward in the casing, increased stability, and then can adjust the angle of load through angle adjustment mechanism, increased adaptability.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, concretely relates to unmanned aerial vehicle load interface.
Background
Along with the development of unmanned aerial vehicle technique and the continuous expansion of market demand, more and more unmanned aerial vehicle related load has appeared, and the unmanned aerial vehicle load is connected with unmanned aerial vehicle through the connector wiring at present mostly and is carried out data transmission, also adopts the screw snap-on's method with unmanned aerial vehicle is fixed mostly. When unmanned aerial vehicle need change the load, can't change the load fast convenient, work efficiency is low, and can not carry the thing phase-match with the load of difference.
Disclosure of Invention
The utility model aims to solve the technical problem that an unmanned aerial vehicle load interface is provided to solve the problem of proposing in the above-mentioned background art.
The utility model discloses a realize through following technical scheme: the utility model provides an unmanned aerial vehicle load interface, which comprises a pane, interface and more than one casing, the opening of casing sets up relatively, all be equipped with the gag lever post more than in the opening of casing, all be equipped with the locating hole on the opposite face of gag lever post, all be equipped with the locating lever in the locating hole, locating lever one end is all installed on the internal face of casing, all the cover has the spring on the locating lever, spring one end is all installed on the gag lever post, the other end is all installed on the internal face of casing, the centre department of upper end casing is equipped with a square mouth, the panel sets up in the casing upper end, the bottom surface of panel just to square mouth department downwardly protruding formation fixed part, be equipped with a recess on the bottom surface of fixed part, the embedded installation of interface is in the recess, the angle adjusting mechanism who is connected with.
As preferred technical scheme, angle adjusting mechanism is equipped with two, angle adjusting mechanism includes the axostylus axostyle, the locating plate, the bolt is twisted to fixed plate and hand, fixed plate one end is all installed on the bottom surface of panel, the centre department of fixed plate all is equipped with first mounting hole, all install first bearing in the first mounting hole, axostylus axostyle one end is all installed in the inner ring of first bearing, the other end is all installed on the outer wall of upper end casing, the locating plate is all installed on the axostylus axostyle, it has more than one first screw hole all to be annular structure distribution on the locating plate, all be equipped with the second screw hole on the fixed plate, the equal threaded connection of bolt and second screw hole are twisted to the hand, bolt one end is twisted to the hand all insert in the corresponding first screw hole.
As preferred technical scheme, elevating system includes four second bearings and hand wheels and four screw rods, all outwards the protrusion forms more than one installation department on the open-ended lateral surface of casing, all be equipped with the third screw hole on the installation department of upper end casing, all be equipped with a second mounting hole on the installation department of lower extreme casing, the second bearing is all installed in the second mounting hole, the screw rod is installed respectively in the inner ring of second bearing, the screw rod upper end all passes the setting of third screw hole, screw rod and third screw hole threaded connection, the hand wheel is all installed in the screw rod lower extreme.
As the preferred technical scheme, install the rubber tube on the top surface of upper end casing, the rubber tube upper end is installed on the bottom surface of panel.
As a preferred technical scheme, more than one fixing hole is arranged on the top surface of the panel.
The utility model has the advantages that: the utility model discloses simple structure accomplishes the electricity between load and the unmanned aerial vehicle through the mode of pegging graft and is connected, and load self then compresses tightly through elevating system and is fixed in between the casing, has made things convenient for fixedly and dismantlement, has increased efficiency to can be spacing with different structure loads through the gag lever post that can move backward in the casing, increased stability, and then can adjust the angle of load through angle adjustment mechanism, increased adaptability.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a schematic structural view of a fixing plate of the present invention;
fig. 3 is a schematic structural view of the middle positioning plate of the present invention.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present invention, and should not be construed as limiting the present invention.
In the description of the present invention, it is to be understood that the terms "center", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are merely for convenience of description and for simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
In the description of the present invention, it should be noted that unless otherwise explicitly stated or limited, the terms "mounted," "connected" and "disposed" are to be construed broadly, and may for example be fixedly connected, disposed, detachably connected, disposed, or integrally connected and disposed. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
As shown in fig. 1, fig. 2 and fig. 3, the unmanned aerial vehicle load interface of the present invention comprises a panel 1, an interface 2 and more than one housing 6, wherein the openings of the housing 6 are oppositely arranged, more than one limiting rod 16 is arranged in each opening of the housing 6, positioning holes are arranged on opposite surfaces of the limiting rods 16, positioning rods are arranged in the positioning holes, one ends of the positioning rods are all arranged on the inner wall surface of the housing, springs 15 are sleeved on the positioning rods, one ends of the springs 15 are all arranged on the limiting rods 16, the other ends of the springs are all arranged on the inner wall surface of the housing 6, a square opening 3 is arranged in the middle of the upper housing 6, the panel 1 is arranged at the upper end of the housing 6, the bottom surface of the panel 1 protrudes downwards relative to the square opening 3 to form a fixing portion 4, a groove is arranged on the bottom surface of the fixing portion 4, the interface 2 is embedded in the groove, angle, a lifting mechanism is arranged between the shell 6 and the shell 6.
In this embodiment, angle adjusting mechanism is equipped with two, angle adjusting mechanism includes axostylus axostyle 12, locating plate 8, fixed plate 17 and hand screw bolt 11, fixed plate 17 one end is all installed on the bottom surface of panel 1, the centre department of fixed plate 17 all is equipped with first mounting hole, all install first bearing 9 in the first mounting hole, axostylus axostyle 12 one end is all installed in the inner ring of first bearing 9, the other end is all installed on the outer wall of upper end casing 6, locating plate 8 is all installed on axostylus axostyle 12, it has more than one first screw hole 7 all to be the annular structure distribution on the locating plate 8, all be equipped with the second screw hole on the fixed plate 17, hand screw bolt 11 is in equal threaded connection and the second screw hole, hand screw bolt 11 one end all inserts in the corresponding first screw hole 7, and all with first screw hole 7 threaded connection.
In this embodiment, the lifting mechanism includes four second bearings 13, a hand wheel and four screw rods 14, the outer side surface of the opening of the housing 6 is outwardly protruded to form more than one mounting portion 18, the mounting portion 18 of the upper housing 6 is provided with a third screw hole, the mounting portion 18 of the lower housing 6 is provided with a second mounting hole, the second bearings 13 are mounted in the second mounting holes, the screw rods 14 are mounted in the inner rings of the second bearings 13 respectively, the upper ends of the screw rods 14 pass through the third screw holes, the screw rods 14 are in threaded connection with the third screw holes, and the hand wheel is mounted at the lower end of the screw rods 14.
In this embodiment, install rubber tube 5 on the top surface of upper end casing 6, rubber tube 5 upper end is installed on the bottom surface of panel 1, can effectually cover follow-up joint of pegging graft with the interface through the rubber tube, great reduction the probability of dust and rainwater contact interface.
In this embodiment, be equipped with more than one fixed orifices on the top surface of panel 1, the screw can pass the fixed orifices, fixes panel lock on unmanned aerial vehicle.
During the installation, place the load between upper and lower casing, the joint on the volume load then passes square mouthful and inserts the interface, accomplish the back, rotate the hand wheel, the rotation of hand wheel has driven the screw rod, make the screw rod along third screw hole rebound, the removal of screw rod has driven the casing of lower extreme, can inwards press from both sides tightly between the casing about making, at the tight in-process of clamp, the gag lever post that contacts with the load can retreat, and the gag lever post that does not contact with the load then motionless, the gag lever post that does not move just in time wraps the outside at the load, thereby it is effectual spacing with the load, the rocking has been avoided.
After accomplishing, can twist out the hand earlier and twist the bolt, make the hand twist the bolt and twist out from first screw hole, at this moment, just can the axostylus axostyle be the rotation casing at center, the rotation of casing has driven inside load, make the angle of load change, if need adjust the shooting angle of camera or detector etc. when angle adjustment is accomplished, the back is accomplished to angular adjustment, the hand is twisted the bolt in the reverse rotation, make the hand twist the bolt in the first screw hole of inserting again, it can effectually be fixed with the axostylus axostyle to twist the bolt through the hand, make the casing with carry cargo the angle that can keep after the adjustment. The fixing and the disassembly are convenient, the efficiency is increased,
the above description is only for the specific embodiments of the present invention, but the scope of the present invention is not limited thereto, and any changes or substitutions that are not thought of through the creative work should be covered within the scope of the present invention. Therefore, the protection scope of the present invention should be subject to the protection scope defined by the claims.
Claims (5)
1. An unmanned aerial vehicle load interface which characterized in that: comprises a panel (1), an interface (2) and more than one shell (6), the openings of the shells (6) are arranged oppositely, more than one limiting rod (16) is arranged in each opening of the shell (6), positioning holes are arranged on opposite surfaces of the limiting rods (16), positioning rods are arranged in the positioning holes, one ends of the positioning rods are all arranged on the inner wall surface of the shell, springs (15) are sleeved on the positioning rods, one ends of the springs (15) are all arranged on the limiting rods (16), the other ends of the springs are all arranged on the inner wall surface of the shell (6), a square opening (3) is arranged in the middle of the upper end shell (6), the panel (1) is arranged at the upper end of the shell (6), the bottom surface of the panel (1) protrudes downwards relative to the square opening (3) to form a fixing part (4), a groove is arranged on the bottom surface of the fixing part (4), the interface (2), an angle adjusting mechanism connected with the shell (6) is installed on two sides of the panel (1), and a lifting mechanism is installed between the shell (6) and the shell (6).
2. The unmanned aerial vehicle load interface of claim 1, wherein: the angle adjusting mechanisms are two, each angle adjusting mechanism comprises a shaft lever (12), a positioning plate (8), a fixing plate (17) and a hand-screwed bolt (11), one end of each fixing plate (17) is arranged on the bottom surface of the panel (1), the middle of each fixing plate (17) is provided with a first mounting hole, each first mounting hole is internally provided with a first bearing (9), one end of each shaft lever (12) is arranged in an inner ring of the first bearing (9), the other end of each shaft lever is arranged on the outer wall surface of the upper end shell (6), the positioning plates (8) are arranged on the shaft levers (12), more than one first screw holes (7) are distributed on the positioning plates (8) in an annular structure, each fixing plate (17) is provided with a second screw hole, the hand-screwed bolts (11) are in threaded connection with the second screw holes, one end of the hand-screwed bolts (11) is inserted into the corresponding first screw holes (7), and are all in threaded connection with the first screw holes (7).
3. The unmanned aerial vehicle load interface of claim 1, wherein: elevating system includes four second bearings (13) and hand wheel and four screw rods (14), all outwards bulge on casing (6) open-ended lateral surface and form more than one installation department (18), all be equipped with the third screw hole on installation department (18) of upper end casing (6), all be equipped with a second mounting hole on installation department (18) of lower extreme casing (6), second bearing (13) are all installed in the second mounting hole, install respectively in the inner ring of second bearing (13) screw rod (14), the third screw hole setting is all passed to screw rod (14) upper end, screw rod (14) and third screw hole threaded connection, the hand wheel is all installed in screw rod (14) lower extreme.
4. The unmanned aerial vehicle load interface of claim 1, wherein: the top surface of the upper end shell (6) is provided with a rubber tube (5), and the upper end of the rubber tube (5) is arranged on the bottom surface of the panel (1).
5. The unmanned aerial vehicle load interface of claim 1, wherein: the top surface of the panel (1) is provided with more than one fixing hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021442697.5U CN212530081U (en) | 2020-07-21 | 2020-07-21 | Unmanned aerial vehicle load interface |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021442697.5U CN212530081U (en) | 2020-07-21 | 2020-07-21 | Unmanned aerial vehicle load interface |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212530081U true CN212530081U (en) | 2021-02-12 |
Family
ID=74518397
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021442697.5U Active CN212530081U (en) | 2020-07-21 | 2020-07-21 | Unmanned aerial vehicle load interface |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212530081U (en) |
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2020
- 2020-07-21 CN CN202021442697.5U patent/CN212530081U/en active Active
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Effective date of registration: 20231108 Address after: Room 610, Middle Building, Ruiyun Hotel, No. 117 Zhengning Road, Chengguan District, Lanzhou City, Gansu Province, 730030 Patentee after: Gansu Feituo Intelligent Technology Co.,Ltd. Address before: 730050 No.200, third village, yanjiaping, Qilihe district, Lanzhou City, Gansu Province Patentee before: GANSU CONSTRUCTION VOCATIONAL TECHNICAL College |