CN215436975U - Navigation lens suspension mechanism for unmanned aerial vehicle - Google Patents
Navigation lens suspension mechanism for unmanned aerial vehicle Download PDFInfo
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- CN215436975U CN215436975U CN202121983867.5U CN202121983867U CN215436975U CN 215436975 U CN215436975 U CN 215436975U CN 202121983867 U CN202121983867 U CN 202121983867U CN 215436975 U CN215436975 U CN 215436975U
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- aerial vehicle
- unmanned aerial
- connecting piece
- suspension mechanism
- fixedly connected
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- 230000007246 mechanism Effects 0.000 title claims abstract description 21
- 239000000725 suspension Substances 0.000 title claims abstract description 19
- 125000006850 spacer group Chemical group 0.000 claims abstract description 7
- 238000009434 installation Methods 0.000 claims description 12
- 230000008859 change Effects 0.000 abstract description 5
- 238000000034 method Methods 0.000 description 7
- 230000008878 coupling Effects 0.000 description 4
- 238000010168 coupling process Methods 0.000 description 4
- 238000005859 coupling reaction Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 3
- 230000009471 action Effects 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004590 computer program Methods 0.000 description 1
- 230000003750 conditioning effect Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
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Abstract
The utility model belongs to the field of aerial lens suspension, and particularly relates to an aerial lens suspension mechanism for an unmanned aerial vehicle, which comprises the unmanned aerial vehicle, an aerial lens positioned at the bottom of the unmanned aerial vehicle, a supporting leg used for supporting the unmanned aerial vehicle, a connecting component fixedly connected at the bottom end of the unmanned aerial vehicle and an adjusting component fixedly connected at the bottom end of the connecting component; this have unmanned aerial vehicle camera lens suspension mechanism, the spacing lock of face of the round platform on wedge and the connecting piece is died, and then can be with the camera lens fixed mounting in unmanned aerial vehicle's bottom, during the dismantlement, the manual connecting piece that upwards promotes, utilize the cooperation between the slider and the wedge of the last slip setting of connecting piece, dismantle the camera lens of navigating, be convenient for install and dismantle, and can prevent through the spacer pin and the setting up of spacing hole that the camera lens of navigating from taking place to rotate when using, and then cause and shoot picture poor stability, utilize servo motor's rotation, adjust the position that the camera lens was shot through the gear, and then can make the change to the angle of shooing.
Description
Technical Field
The utility model belongs to the technical field of aerial lens suspension, and particularly relates to an aerial lens suspension mechanism for an unmanned aerial vehicle.
Background
The unmanned aerial vehicle aerial equipment is an unmanned aerial vehicle controlled by radio remote control equipment or an onboard computer program control system, the unmanned aerial vehicle is simple in structure and low in use cost, not only can complete tasks executed by piloted planes, but also is suitable for tasks which cannot be executed by piloted planes, emergency and early warning are very effective in emergencies, the existing unmanned aerial vehicle aerial lens suspension mechanism is provided, the aerial lens is usually fixedly installed at the bottom end of the unmanned aerial vehicle, the unmanned aerial vehicle can inevitably generate vibration in the operation process due to high air flow change and various natural conditions in the aerial photographing process, the connection is unstable, so that the aerial device directly shakes, the aerial lens is fixedly connected, the unmanned aerial vehicle is required to be manually operated to remotely control the aerial vehicle to fly, and the photographed image is poor in stability, The definition of the image is low, and the like.
Therefore, the aerial lens suspension mechanism for the unmanned aerial vehicle is designed to solve the problems.
SUMMERY OF THE UTILITY MODEL
To solve the problems set forth in the background art described above. The utility model provides a navigation lens suspension mechanism for an unmanned aerial vehicle, which has the characteristics of stable connection and capability of adjusting a navigation lens according to requirements.
In order to achieve the purpose, the utility model provides the following technical scheme: an aerial lens suspension mechanism for an unmanned aerial vehicle comprises the unmanned aerial vehicle, an aerial lens positioned at the bottom of the unmanned aerial vehicle, a supporting leg used for supporting the unmanned aerial vehicle, a connecting assembly fixedly connected at the bottom end of the unmanned aerial vehicle and an adjusting assembly fixedly connected at the bottom end of the connecting assembly;
coupling assembling includes the installation cover, the connecting piece, spacing hole, the slider, the spacer pin, a word external screw thread bolt, the telescopic link, a spring, the wedge, the spout, the top fixed connection unmanned aerial vehicle's of installation cover bottom outside symmetry, the spout has been seted up to installation cover bottom outside symmetry, and be equipped with the screw thread on the one end inner wall of spout and with a word external screw thread bolt threaded connection, the one end fixed connection of one side fixed connection telescopic link of a word external screw thread bolt, the other end of telescopic link and the one end fixed connection of wedge, the cover is equipped with the spring on the excircle of telescopic link, unmanned aerial vehicle's one end sliding connection is kept away from to the installation cover is equipped with the connecting piece, the excircle sliding connection of connecting piece is equipped with the slider, the inside top fixed connection of installation cover is equipped with the spacer pin, spacing hole has been seted up on the connecting piece, spacing hole of spacer pin sliding connection.
Preferably, the adjusting assembly comprises a driving gear, a driven gear, a connecting plate, a rotating shaft and a servo motor, one end of the servo motor is fixedly connected with the bottom end of the connecting piece, the output end of the servo motor is rotatably connected with the driving gear, the driving gear is meshed with the driven gear, the driven gear is sleeved on the outer circle of the rotating shaft, the connecting plate is arranged on the outer circle of the rotating shaft and below the driven gear, the connecting plate is fixedly connected with the supporting legs, and one end of the rotating shaft is fixedly connected with the navigation lens.
Preferably, the limiting pin and the limiting hole are arranged in a square shape.
Preferably, one end of the connecting piece is arranged in a circular truncated cone shape, and the sliding piece is arranged in a circular truncated cone shape.
Preferably, the top of the sliding part is provided with an annular groove matched with the groove at the bottom of the connecting part.
Preferably, the connecting plate is arranged in a hollow mode and is fixedly connected with the supporting legs.
Preferably, the driving gear and the driven gear have the same number of teeth and the same modulus.
Compared with the prior art, the utility model has the beneficial effects that:
this have unmanned aerial vehicle camera lens suspension mechanism, the spacing lock of face of round platform on wedge and the connecting piece is utilized through coupling assembling's setting up, and then can be with the bottom of aerial vehicle camera lens fixed mounting at unmanned aerial vehicle, during the dismantlement, the manual connecting piece that upwards promotes, utilize the slider of the last slip setting of connecting piece and the cooperation between the wedge, dismantle the aerial vehicle camera lens, be convenient for installation and dismantlement, and can prevent through the spacer pin and spacing setting up of hole that the aerial vehicle camera lens from taking place to rotate when using, and then cause and shoot picture poor stability, utilize servo motor's rotation through adjusting part's setting, adjust the position that the aerial vehicle camera lens was shot through the gear, and then can make the change to the angle of shooing.
Drawings
The accompanying drawings, which are included to provide a further understanding of the utility model and are incorporated in and constitute a part of this specification, illustrate embodiments of the utility model and together with the description serve to explain the principles of the utility model and not to limit the utility model. In the drawings:
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is an exploded view of the connecting assembly of the present invention;
FIG. 3 is an exploded view of the structure of the conditioning assembly of the present invention;
FIG. 4 is a schematic view of the structural assembly of the connecting assembly and the adjusting assembly of the present invention;
FIG. 5 is a schematic cross-sectional view of the connection assembly of the present invention;
in the figure:
1. an unmanned aerial vehicle; 2. navigating a camera lens; 3. a support leg;
4. a connecting assembly; 41. installing a sleeve; 42. a connecting member; 43. a limiting hole; 44. a slider; 45. a spacing pin; 46. a straight external threaded bolt; 47. a telescopic rod; 48. a spring; 49. a wedge block; 410. a chute;
5. an adjustment assembly; 51. a driving gear; 52. a driven gear; 53. a connecting plate; 54. a rotating shaft; 55. a servo motor.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
As shown in fig. 1;
the utility model provides a mechanism is hung to boat camera lens for unmanned aerial vehicle, includes unmanned aerial vehicle 1 and is located the boat camera lens 2 of 1 bottom of unmanned aerial vehicle and is used for supporting landing leg 3 of unmanned aerial vehicle 1.
In this embodiment: the current aerial camera lens that has for the unmanned aerial vehicle hangs mechanism, fixes aerial camera lens 2 in the bottom of unmanned aerial vehicle 1 and shoots, and unmanned aerial vehicle 1 is at aerial in-process of taking photo by plane in the air, because the restriction of high aerial air current change and various natural conditions to directly lead to the device of taking photo by plane to rock, lead to the picture quality of shooting poor.
It should be noted that: navigation camera lens 2 will firmly be fixed in unmanned aerial vehicle 1's bottom, prevents to connect unstable navigation camera lens 2 and takes place to drop at the shooting in-process.
As shown in fig. 1 and 2 and fig. 3 and 4 and 5:
based on current have for the unmanned aerial vehicle lens mechanism that hangs, on current have for the unmanned aerial vehicle lens mechanism that hangs basis, in 1 bottom fixed connection's of unmanned aerial vehicle coupling assembling 4 and the adjusting part 5 that is located 4 bottom fixed connection of coupling assembling.
Further, the method comprises the following steps:
in combination with the above, the connecting assembly 4 includes a mounting sleeve 41, a connecting member 42, a limiting hole 43, a sliding member 44, a limiting pin 45, a straight-line-shaped external thread bolt 46, a telescopic rod 47, a spring 48, a wedge 49, and a sliding slot 410, the top end of the mounting sleeve 41 is fixedly connected to the bottom end of the unmanned aerial vehicle 1, the outer side of the bottom end of the mounting sleeve 41 is symmetrically provided with the sliding slot 410, the inner wall of one end of the sliding slot 410 is provided with a thread and is in threaded connection with the straight-line-shaped external thread bolt 46, one side of the straight-line-shaped external thread bolt 46 is fixedly connected to one end of the telescopic rod 47, the other end of the telescopic rod 47 is fixedly connected to one end of the wedge 49, the outer circle of the telescopic rod 47 is sleeved with the spring 48, the sliding end of the mounting sleeve 41 away from the unmanned aerial vehicle 1 is provided with the connecting member 42, the outer circle of the connecting member 42 is provided with the sliding member 44, the limiting pin 45 is fixedly connected to the top end of the mounting sleeve 41, the limiting hole 43 is provided on the connecting member 42, the limit pin 45 is slidably connected with the limit hole 43.
In this embodiment: the connecting piece 42 slides up and down in the mounting sleeve 41, when the mounting is carried out, the inclined surface of the circular truncated cone above the connecting piece 42 contacts the wedge block 49 to slide, due to the action of stress, the wedge block 49 slides to one side close to the straight-line-shaped external thread bolt 46 in the sliding groove 410, one side of the straight-line-shaped external thread bolt 46 is fixedly connected with one end of the telescopic rod 47, the other end of the telescopic rod 47 is fixedly connected with one end of the wedge block 49, the outer circle of the telescopic rod 47 is sleeved with the spring 48 to drive the telescopic rod 47 to extend and retract, meanwhile, the spring 48 is stressed and compressed until the wedge block 49 is clamped with the bottom end of the circular truncated cone above the connecting piece 42 to be connected, when the dismounting is carried out, the connecting piece 42 is pushed upwards until the inclined surface of the annular bulge arranged at the top end of the sliding piece 44 slides with the inclined surface of the wedge block 49, until the bottom end of the sliding piece 44 is positioned above the wedge block 49, the connecting piece 42 is pulled downwards, the outer circle of the connecting piece 42 is provided with a sliding piece 44 in a sliding connection mode until the top end of the sliding piece 44 is attached to the ground of the circular truncated cone on the connecting piece 42, and the connecting piece 42 is pulled continuously until the connecting piece 42 is separated from the mounting sleeve 41.
It should be understood that: spacing pin 45 and spacing hole 43 are square setting, prevent through this setting that the boat camera lens from taking place to rotate when using, and then cause and shoot picture poor stability.
It should be noted that: the one end of connecting piece 42 is the setting of round platform shape, and slider 44 is the setting of reverse round platform shape, makes things convenient for the inclined plane of round platform shape and the slip between wedge 49 when the installation through this setting when connecting piece 42, and the top of slider 44 is equipped with the annular groove with connecting piece 42 bottom recess looks adaptation, and wedge 49 blocks card is died on slider 44 when preventing to drop down, causes the unable dismantlement of device.
As shown in fig. 3 and 4:
further, the method comprises the following steps:
in combination with the above, the adjusting assembly 5 includes a driving gear 51, a driven gear 52, a connecting plate 53, a rotating shaft 54, a servo motor 55, one end of the servo motor 55 is fixedly connected to the bottom end of the connecting piece 42, an output end of the servo motor 55 is rotatably connected to the driving gear 51, the driving gear 51 is meshed with the driven gear 52, the driven gear 52 is sleeved on an outer circle of the rotating shaft 54, the connecting plate 53 is arranged on the outer circle of the rotating shaft 54 and below the driven gear 52, the connecting plate 53 is fixedly connected to the supporting legs 3, and one end of the rotating shaft 54 is fixedly connected to the aerial lens 2.
In this embodiment: rotation through control servo motor 55, servo motor 55's output rotates to be connected and is equipped with driving gear 51, and then drive driving gear 51 and rotate, driving gear 51 meshes the connection driven gear 52, and then make driven gear 52 follow the rotation, the excircle at pivot 54 is established to driven gear 52 cover, the excircle of pivot 54 and the below that is located driven gear 52 are equipped with connecting plate 53, connecting plate 53 and 3 fixed connection of landing leg, the one end fixed connection of pivot 54 is equipped with boat camera lens 2, drive through pivot 54, boat camera lens 2 that pivot 54 one end is connected rotates, and then can make the change to the angle of shooting.
It should be understood that: connecting plate 53 is the cavity setting to with landing leg 3 fixed connection, through the cavity setting, the holistic weight when having alleviateed unmanned aerial vehicle 1 and taking off.
It should be noted that: the tooth number of the driving gear 51 is the same as that of the driven gear 52, the modulus is the same, and through the arrangement, the driving gear 51 can drive the driven gear 52 to rotate conveniently, so that the rotating process is stable, and the quality of a shot picture is improved.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that changes may be made in the embodiments and/or equivalents thereof without departing from the spirit and scope of the utility model. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (7)
1. The aerial lens suspension mechanism for the unmanned aerial vehicle comprises the unmanned aerial vehicle (1), an aerial lens (2) positioned at the bottom of the unmanned aerial vehicle (1), supporting legs (3) used for supporting the unmanned aerial vehicle (1), a connecting assembly (4) fixedly connected at the bottom end of the unmanned aerial vehicle (1) and an adjusting assembly (5) fixedly connected at the bottom end of the connecting assembly (4);
the connecting assembly (4) comprises an installation sleeve (41), a connecting piece (42), a limiting hole (43), a sliding piece (44), a limiting pin (45), a straight-line-shaped external thread bolt (46), a telescopic rod (47), a spring (48), a wedge block (49) and a sliding groove (410), the top end of the installation sleeve (41) is fixedly connected with the bottom end of the unmanned aerial vehicle (1), the sliding groove (410) is symmetrically formed in the outer side of the bottom end of the installation sleeve (41), a thread is arranged on the inner wall of one end of the sliding groove (410) and is in threaded connection with the straight-line-shaped external thread bolt (46), one side of the straight-line-shaped external thread bolt (46) is fixedly connected with one end of the telescopic rod (47), the other end of the telescopic rod (47) is fixedly connected with one end of the wedge block (49), and the spring (48) is sleeved on the excircle of the telescopic rod (47), keep away from installation cover (41) the one end sliding connection of unmanned aerial vehicle (1) is equipped with connecting piece (42), the excircle sliding connection of connecting piece (42) is equipped with slider (44), the inside top fixed connection of installation cover (41) is equipped with spacer pin (45), seted up on connecting piece (42) spacing hole (43), spacer pin (45) sliding connection spacing hole (43).
2. The aerial lens suspension mechanism for an unmanned aerial vehicle according to claim 1, characterized in that: adjusting part (5) include driving gear (51), driven gear (52), connecting plate (53), pivot (54), servo motor (55), the one end fixed connection of servo motor (55) the bottom of connecting piece (42), the output of servo motor (55) is rotated and is connected and is equipped with driving gear (51), driving gear (51) meshing is connected driven gear (52), driven gear (52) cover is established the excircle of pivot (54), the excircle of pivot (54) just is located the below of driven gear (52) is equipped with connecting plate (53), connecting plate (53) with landing leg (3) fixed connection, the one end fixed connection of pivot (54) is equipped with boat camera lens (2).
3. The aerial lens suspension mechanism for an unmanned aerial vehicle according to claim 1, characterized in that: the limiting pin (45) and the limiting hole (43) are both arranged in a square shape.
4. The aerial lens suspension mechanism for an unmanned aerial vehicle according to claim 1, characterized in that: one end of the connecting piece (42) is arranged in a circular truncated cone shape, and the sliding piece (44) is arranged in a circular truncated cone shape.
5. The aerial lens suspension mechanism for an unmanned aerial vehicle according to claim 4, characterized in that: the top of the sliding piece (44) is provided with an annular groove matched with the groove at the bottom of the connecting piece (42).
6. The aerial lens suspension mechanism for an unmanned aerial vehicle according to claim 2, characterized in that: the connecting plate (53) is arranged in a hollow mode and is fixedly connected with the supporting legs (3).
7. The aerial lens suspension mechanism for an unmanned aerial vehicle according to claim 2, characterized in that: the driving gear (51) and the driven gear (52) have the same tooth number and the same module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121983867.5U CN215436975U (en) | 2021-08-23 | 2021-08-23 | Navigation lens suspension mechanism for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121983867.5U CN215436975U (en) | 2021-08-23 | 2021-08-23 | Navigation lens suspension mechanism for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215436975U true CN215436975U (en) | 2022-01-07 |
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ID=79695876
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121983867.5U Expired - Fee Related CN215436975U (en) | 2021-08-23 | 2021-08-23 | Navigation lens suspension mechanism for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215436975U (en) |
-
2021
- 2021-08-23 CN CN202121983867.5U patent/CN215436975U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220107 |