CN215043654U - Integrated undercarriage of inspection unmanned aerial vehicle - Google Patents
Integrated undercarriage of inspection unmanned aerial vehicle Download PDFInfo
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- CN215043654U CN215043654U CN202121684728.2U CN202121684728U CN215043654U CN 215043654 U CN215043654 U CN 215043654U CN 202121684728 U CN202121684728 U CN 202121684728U CN 215043654 U CN215043654 U CN 215043654U
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Abstract
The utility model provides an integrated undercarriage for inspection unmanned aerial vehicle, which relates to the technical field of undercarriage for unmanned aerial vehicle, comprising an integrated undercarriage for inspection unmanned aerial vehicle, comprising a frame body, a support rod, an installation cavity and an installation mechanism, wherein the support rod is arranged inside the frame body, one end of the support rod extends to the outer side of the frame body, a dismounting mechanism is arranged above the frame body, one end of a reset spring is connected with a hinged rod, an installation component is arranged inside the installation cavity, and dismounting components are arranged on two sides outside the installation cavity; the utility model discloses be provided with dismouting mechanism on the installation cavity, utilize mutually supporting of erection column, reset spring, hinge bar and the dismantlement subassembly of dismouting mechanism, can carry out convenient dismantlement to the undercarriage, install the inside at the installation cavity with new undercarriage efficient again, practiced thrift the time of this undercarriage when changing to the high efficiency of this undercarriage when using has been improved.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle undercarriage technical field especially relates to patrol and examine unmanned aerial vehicle integral type undercarriage.
Background
With the development of economy and continuous progress of science and technology, the development of the unmanned aerial vehicle is very rapid, the unmanned aerial vehicle is an unmanned aerial vehicle which is operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, and the unmanned aerial vehicle makes a great breakthrough in the field of inspection and inspection;
patrol and examine unmanned aerial vehicle and all have the undercarriage when production, but the current unmanned aerial vehicle of patrolling and examining has the local environment comparatively abominable when using, and the undercarriage uses easy damage for a long time, and inconvenient carries out convenient dismouting to the undercarriage, changes, and has reduced the high efficiency of this unmanned aerial vehicle when using, consequently the utility model provides a patrol and examine the problem that unmanned aerial vehicle integral type undercarriage exists in order to solve prior art.
SUMMERY OF THE UTILITY MODEL
To the above problem, the utility model provides a patrol and examine unmanned aerial vehicle integral type undercarriage, this patrol and examine unmanned aerial vehicle integral type undercarriage and be provided with dismouting mechanism on the installation cavity, utilize the erection column of dismouting mechanism, reset spring, hinge bar and the mutually supporting of detaching assembly, can carry out convenient dismantlement to the undercarriage, install the inside at the installation cavity with new undercarriage efficient again, practiced thrift the time of this undercarriage when changing to the high efficiency of this undercarriage when using has been improved.
For realizing the purpose of the utility model, the utility model discloses a following technical scheme realizes: an integrated inspection unmanned aerial vehicle undercarriage comprises a frame body, a support rod, an installation cavity and an installation mechanism, wherein the support rod is arranged inside the frame body, one end of the support rod extends to the outer side of the frame body, a dismounting mechanism is arranged above the frame body, an adjusting mechanism is arranged on the outer side of the frame body, and the installation cavity is installed below an unmanned aerial vehicle;
the dismouting mechanism is including installation component and dismantlement subassembly, the installation component includes erection column, reset spring and hinge bar, the erection column is installed in the top of support body, reset spring is installed to the both sides of erection column, the top of erection column articulates there is the hinge bar, reset spring's one end is connected with the hinge bar, the installation component sets up in the inside of installation cavity, the outside both sides of installation cavity are provided with the dismantlement subassembly.
The further improvement lies in that: the hinge rod is obliquely designed with the mounting column through the reset spring, the spring extension portion is arranged on the outer side of the mounting column, the reset spring is close to one end of the mounting column and is fixed on the spring extension portion, and the hinge rod is driven to move in a telescopic mode through the reset spring.
The further improvement lies in that: the disassembly component comprises a cavity, an expansion spring and a movable rod, the cavity is installed on two sides of the outside of the installation cavity, the movable rod is arranged inside the cavity, two ends of the movable rod all extend to the outside of the cavity, one end of the movable rod extends to the inside of the installation cavity, and the expansion spring is sleeved on the outer side of the movable rod inside the cavity.
The further improvement lies in that: buffer gear is installed to the below of bracing piece, the below of undercarriage is provided with buffer gear, buffer gear is including fixed chamber, buffer spring, mounting panel and stop gear, fixed chamber sets up in the below of undercarriage, buffer spring is installed to the below of fixed intracavity portion, buffer spring's top is provided with the mounting panel, the inside in fixed chamber is provided with stop gear.
The further improvement lies in that: the limiting mechanism comprises a limiting rod, the limiting rod is installed inside the fixed cavity, the limiting rod is provided with two limiting rods, sliding sleeves are installed at two ends of the mounting plate, the diameter of each sliding sleeve is consistent with that of the limiting rod, and the mounting plate is connected with the limiting rods in a sliding mode through the sliding sleeves.
The further improvement lies in that: adjustment mechanism includes the bolt, be provided with a plurality of through-holes on the bracing piece, it is a plurality of the through-hole is equidistant distribution on the bracing piece, the bolt sets up in the outside of support body, the one end of bolt extends to the inside of support body to with the mutual adaptation of through-hole on the bracing piece.
The utility model discloses beneficial effect:
1. the utility model discloses be provided with dismouting mechanism on the installation cavity, utilize mutually supporting of erection column, reset spring, hinge bar and the dismantlement subassembly of dismouting mechanism, can carry out convenient dismantlement to the undercarriage, install the inside at the installation cavity with new undercarriage efficient again, practiced thrift the time of this undercarriage when changing to the high efficiency of this undercarriage when using has been improved.
2. The utility model discloses be provided with buffer gear in the below of undercarriage, utilize buffer gear decide chamber, buffer spring, mounting panel and gag lever post mutually support, the impact force that unmanned aerial vehicle produced when descending can be greatly reduced the damage that the inside accurate electrical component of unmanned aerial vehicle caused because of the vibration, also make the undercarriage not fragile to unmanned aerial vehicle's life has been prolonged.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a schematic side view of the present invention.
Fig. 3 is a schematic diagram of a partially enlarged structure at a in fig. 1 according to the present invention.
Fig. 4 is a schematic diagram of the local enlarged structure at B in fig. 2 according to the present invention.
Wherein: 1. a frame body; 2. a support bar; 3. a mounting cavity; 4. mounting a column; 5. a return spring; 6. a hinged lever; 7. a cavity; 8. a tension spring; 9. a movable rod; 10. a fixed cavity; 11. a buffer spring; 12. mounting a plate; 13. a limiting rod; 14. a bolt; 15. and a through hole.
Detailed Description
In order to deepen the understanding of the present invention, the following embodiments will be combined to make the present invention do further details, and the present embodiment is only used for explaining the present invention, and does not constitute the limitation of the protection scope of the present invention.
Example one
According to the figures 1-4, the embodiment provides an integrated undercarriage for an inspection unmanned aerial vehicle, which comprises a frame body 1, a support rod 2, an installation cavity 3 and an installation mechanism, wherein the support rod 2 is arranged inside the frame body 1, one end of the support rod 2 extends to the outer side of the frame body 1, a dismounting mechanism is arranged above the frame body 1, an adjusting mechanism is arranged on the outer side of the frame body 1, and the installation cavity 3 is installed below the unmanned aerial vehicle;
dismouting mechanism is including installation component and dismantlement subassembly, the installation component includes erection column 4, reset spring 5 and hinge bar 6, erection column 4 is installed in the top of support body 1, reset spring 5 is installed to the both sides of erection column 4, the top of erection column 4 articulates there is hinge bar 6, reset spring 5's one end is connected with hinge bar 6, the installation component sets up in the inside of installation cavity 3, the outside both sides of installation cavity 3 are provided with the dismantlement subassembly, during the use, press hinge bar 6, place hinge bar 6 into the inside of installation cavity 3, and reset spring 5 receives the effect of elasticity and drives hinge bar 6 and reset this moment, hinge bar 6 and 3 blocks of installation cavity this moment, accomplish the installation of undercarriage, then start unmanned aerial vehicle and patrol and examine.
Hinge rod 6 is the slope design through reset spring 5 and erection column 4, the outside of erection column 4 is provided with the spring extension, and reset spring 5 is close to the one end of erection column 4 is fixed on the spring extension, drives hinge rod 6 through reset spring 5 and carries out concertina movement, can carry out convenient installation to the undercarriage.
The disassembly component comprises a cavity 7, an expansion spring 8 and a movable rod 9, the cavity 7 is installed on two sides of the outer portion of the installation cavity 3, the movable rod 9 is arranged inside the cavity 7, two ends of the movable rod 9 extend to the outer portion of the cavity 7, one end of the movable rod 9 extends to the inner portion of the installation cavity 3, the expansion spring 8 is sleeved on the outer side of the movable rod 9 inside the cavity 7, the movable rod 9 is pressed, the movable rod 9 moves towards the inner portion of the installation cavity 3 to abut against the hinge rod 6, the reset spring 5 drives the hinge rod 6 to shrink, and the undercarriage can be conveniently disassembled.
Adjustment mechanism includes bolt 14, be provided with a plurality of through-holes 15 on bracing piece 2, it is a plurality of through-hole 15 is equidistant distribution on bracing piece 2, bolt 14 sets up in the outside of support body 1, the one end of bolt 14 extends to the inside of support body 1 to with the mutual adaptation of through-hole 15 on bracing piece 2, utilize mutually supporting of bolt 14 and through-hole 15, can adjust the height of bracing piece 2, patrol and examine that unmanned aerial vehicle also can stably descend in the ground of high ground injustice, can adapt to the topography of multiple complicacy.
Example two
According to the figures 1-4, the embodiment provides an integrated undercarriage for an inspection unmanned aerial vehicle, which comprises a frame body 1, a support rod 2, an installation cavity 3 and an installation mechanism, wherein the support rod 2 is arranged inside the frame body 1, one end of the support rod 2 extends to the outer side of the frame body 1, a dismounting mechanism is arranged above the frame body 1, an adjusting mechanism is arranged on the outer side of the frame body 1, and the installation cavity 3 is installed below the unmanned aerial vehicle;
dismouting mechanism is including installation component and dismantlement subassembly, the installation component includes erection column 4, reset spring 5 and hinge bar 6, erection column 4 is installed in the top of support body 1, reset spring 5 is installed to the both sides of erection column 4, the top of erection column 4 articulates there is hinge bar 6, reset spring 5's one end is connected with hinge bar 6, the installation component sets up in the inside of installation cavity 3, the outside both sides of installation cavity 3 are provided with the dismantlement subassembly, during the use, press hinge bar 6, place hinge bar 6 into the inside of installation cavity 3, and reset spring 5 receives the effect of elasticity and drives hinge bar 6 and reset this moment, hinge bar 6 and 3 blocks of installation cavity this moment, accomplish the installation of undercarriage, then start unmanned aerial vehicle and patrol and examine.
Hinge rod 6 is the slope design through reset spring 5 and erection column 4, the outside of erection column 4 is provided with the spring extension, and reset spring 5 is close to the one end of erection column 4 is fixed on the spring extension, drives hinge rod 6 through reset spring 5 and carries out concertina movement, can carry out convenient installation to the undercarriage.
The disassembly component comprises a cavity 7, an expansion spring 8 and a movable rod 9, the cavity 7 is installed on two sides of the outer portion of the installation cavity 3, the movable rod 9 is arranged inside the cavity 7, two ends of the movable rod 9 extend to the outer portion of the cavity 7, one end of the movable rod 9 extends to the inner portion of the installation cavity 3, the expansion spring 8 is sleeved on the outer side of the movable rod 9 inside the cavity 7, the movable rod 9 is pressed, the movable rod 9 moves towards the inner portion of the installation cavity 3 to abut against the hinge rod 6, the reset spring 5 drives the hinge rod 6 to shrink, and the undercarriage can be conveniently disassembled.
Buffer gear is installed to the below of bracing piece 2, the below of undercarriage is provided with buffer gear, buffer gear includes fixed chamber 10, buffer spring 11, mounting panel 12 and stop gear, fixed chamber 10 sets up in the below of undercarriage, buffer spring 11 is installed to the below of fixed chamber 10 inside, buffer spring 11's top is provided with mounting panel 12, the inside of fixed chamber 10 is provided with stop gear, drives mounting panel 12 and undercarriage through buffer spring 11 and stretches out and draws back to slow down the impact force that the undercarriage received, protect unmanned aerial vehicle and undercarriage with this.
Stop gear includes gag lever post 13, gag lever post 13 is installed in the inside of fixed chamber 10, gag lever post 13 is provided with two, the sliding sleeve is installed at the both ends of mounting panel 12, the diameter of sliding sleeve with gag lever post 13's diameter is unanimous, mounting panel 12 passes through sliding sleeve and gag lever post 13 sliding connection, and gag lever post 13's use can be spacing buffer spring 11 for buffer spring 11 is more stable when flexible.
Adjustment mechanism includes bolt 14, be provided with a plurality of through-holes 15 on bracing piece 2, it is a plurality of through-hole 15 is equidistant distribution on bracing piece 2, bolt 14 sets up in the outside of support body 1, the one end of bolt 14 extends to the inside of support body 1 to with the mutual adaptation of through-hole 15 on bracing piece 2, utilize mutually supporting of bolt 14 and through-hole 15, can adjust the height of bracing piece 2, patrol and examine that unmanned aerial vehicle also can stably descend in the ground of high ground injustice, can adapt to the topography of multiple complicacy.
When the landing gear is used, a worker takes out the landing gear, then presses the hinge rod 6, places the mounting column 4, the reset spring 5 and the hinge rod 6 into the mounting cavity 3, at the moment, the reset spring 5 is acted by elastic force to drive the hinge rod 6 to reset, at the moment, the hinge rod 6 is clamped with the mounting cavity 3 to complete the mounting of the landing gear, takes out the bolt 14 and then adjusts the support rod 2 to a proper position, then the bolt 14 penetrates through the frame body 1 and is clamped with the through hole 15 on the support rod 2, then the unmanned aerial vehicle is started to carry out inspection, when the unmanned aerial vehicle descends, the landing gear is acted by downward impact force, the buffer spring 11 is utilized to drive the mounting plate 12 to extend under the action of the limiting rod 13, the impact force applied to the landing gear is buffered, when the landing gear needs to be replaced, the worker presses the movable rod 9, at the moment, the movable rod 9 moves towards the inside the mounting cavity 3 to abut against the hinge rod 6, reset spring 5 drives the shrink of hinge bar 6, can dismantle the undercarriage this moment, and expanding spring 8 drives the movable rod 9 and resets, then takes out new undercarriage, repeats above-mentioned operating procedure and installs the undercarriage.
The utility model discloses be provided with dismouting mechanism on installation cavity 3, utilize the mutual cooperation of dismouting mechanism's erection column 4, reset spring 5, hinge bar 6 and dismantlement subassembly, can carry out convenient dismantlement to the undercarriage, install the inside at installation cavity 3 with new undercarriage efficient again, practiced thrift the time of this undercarriage when changing to the high efficiency of this undercarriage when using has been improved; the utility model discloses be provided with buffer gear in the below of undercarriage, utilize buffer gear decide chamber, buffer spring 11, mounting panel 12 and gag lever post 13 mutually support, the impact force that unmanned aerial vehicle produced when descending can be greatly reduced the damage that the inside accurate electrical component of unmanned aerial vehicle caused because of the vibration, also make the undercarriage not fragile to unmanned aerial vehicle's life has been prolonged.
The foregoing illustrates and describes the principles, general features, and advantages of the present invention. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (6)
1. Patrol and examine unmanned aerial vehicle integral type undercarriage, including support body (1), bracing piece (2), installation cavity (3) and installation mechanism, its characterized in that: a support rod (2) is arranged in the frame body (1), one end of the support rod (2) extends to the outer side of the frame body (1), a dismounting mechanism is arranged above the frame body (1), an adjusting mechanism is arranged on the outer side of the frame body (1), and the installation cavity (3) is installed below the unmanned aerial vehicle;
dismouting mechanism is including installation component and dismantlement subassembly, the installation component includes erection column (4), reset spring (5) and hinge bar (6), install in the top of support body (1) erection column (4), reset spring (5) are installed to the both sides of erection column (4), the top of erection column (4) articulates there is hinge bar (6), the one end and the hinge bar (6) of reset spring (5) are connected, the installation component sets up in the inside of installation cavity (3), the outside both sides of installation cavity (3) are provided with the dismantlement subassembly.
2. The inspection unmanned aerial vehicle integral type undercarriage of claim 1, characterized in that: articulated rod (6) are the slope design through reset spring (5) and erection column (4), the outside of erection column (4) is provided with the spring extension, and reset spring (5) are close to the one end of erection column (4) is fixed on the spring extension, drives articulated rod (6) through reset spring (5) and carries out concertina movement.
3. The inspection unmanned aerial vehicle integral type undercarriage of claim 1, characterized in that: the disassembly component comprises a cavity (7), an expansion spring (8) and a movable rod (9), the cavity (7) is installed on two sides of the outside of the installation cavity (3), the movable rod (9) is arranged inside the cavity (7), two ends of the movable rod (9) extend to the outside of the cavity (7), one end of the movable rod (9) extends to the inside of the installation cavity (3), and the expansion spring (8) is sleeved on the outer side of the movable rod (9) inside the cavity (7).
4. The inspection unmanned aerial vehicle integral type undercarriage of claim 1, characterized in that: buffer gear is installed to the below of bracing piece (2), the below of undercarriage is provided with buffer gear, buffer gear is including fixed chamber (10), buffer spring (11), mounting panel (12) and stop gear, fixed chamber (10) set up in the below of undercarriage, buffer spring (11) are installed to the inside below in fixed chamber (10), the top of buffer spring (11) is provided with mounting panel (12), the inside in fixed chamber (10) is provided with stop gear.
5. The inspection unmanned aerial vehicle integral type undercarriage of claim 4, characterized in that: stop gear includes gag lever post (13), gag lever post (13) are installed in the inside of fixed chamber (10), gag lever post (13) are provided with two, the sliding sleeve is installed at the both ends of mounting panel (12), the diameter of sliding sleeve with the diameter of gag lever post (13) is unanimous, mounting panel (12) pass through sliding sleeve and gag lever post (13) sliding connection.
6. The inspection unmanned aerial vehicle integral type undercarriage of claim 1, characterized in that: adjustment mechanism includes bolt (14), be provided with a plurality of through-holes (15) on bracing piece (2), it is a plurality of through-hole (15) are equidistant distribution on bracing piece (2), bolt (14) set up in the outside of support body (1), the one end of bolt (14) extends to the inside of support body (1) to with through-hole (15) mutual adaptation on bracing piece (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121684728.2U CN215043654U (en) | 2021-07-23 | 2021-07-23 | Integrated undercarriage of inspection unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121684728.2U CN215043654U (en) | 2021-07-23 | 2021-07-23 | Integrated undercarriage of inspection unmanned aerial vehicle |
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| CN215043654U true CN215043654U (en) | 2021-12-07 |
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| CN202121684728.2U Active CN215043654U (en) | 2021-07-23 | 2021-07-23 | Integrated undercarriage of inspection unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117246549A (en) * | 2023-11-20 | 2023-12-19 | 江苏汉科航空科技有限公司 | Unmanned aerial vehicle with prevent mechanism of turning on one's side |
-
2021
- 2021-07-23 CN CN202121684728.2U patent/CN215043654U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117246549A (en) * | 2023-11-20 | 2023-12-19 | 江苏汉科航空科技有限公司 | Unmanned aerial vehicle with prevent mechanism of turning on one's side |
| CN117246549B (en) * | 2023-11-20 | 2024-01-30 | 江苏汉科航空科技有限公司 | Unmanned aerial vehicle with prevent mechanism of turning on one's side |
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Address after: 241000 building 27, Wuhu navigation Innovation Park, Beihang, Xinwu Avenue, Wanhe Town, Wuhu County, Wuhu City, Anhui Province Patentee after: Anhui Weiyuan Intelligent Technology Co.,Ltd. Address before: 241000 building 27, Wuhu navigation Innovation Park, Beihang, Xinwu Avenue, Wanhe Town, Wuhu County, Wuhu City, Anhui Province Patentee before: Wuhu Weiyuan Intelligent Technology Co.,Ltd. |