CN210912918U - Unmanned aerial vehicle recovery unit - Google Patents
Unmanned aerial vehicle recovery unit Download PDFInfo
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- CN210912918U CN210912918U CN201921119562.2U CN201921119562U CN210912918U CN 210912918 U CN210912918 U CN 210912918U CN 201921119562 U CN201921119562 U CN 201921119562U CN 210912918 U CN210912918 U CN 210912918U
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- aerial vehicle
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- protective frame
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Abstract
The utility model discloses an unmanned aerial vehicle recovery unit belongs to the unmanned aerial vehicle field, including retrieving the storehouse, retrieve the storehouse including retrieving the mechanism and locating the closing mechanism who retrieves the mechanism top, retrieve the mechanism and catch the screen cloth cover outside the protective frame including catching net, protective frame and lift platform, the protective frame bottom is equipped with supporting baseplate, and lift platform establishes the intracavity that holds that forms at protective frame and supporting baseplate. The utility model has the advantages that: can install unmanned aerial vehicle recovery unit on each high-voltage power tower, unmanned aerial vehicle can not need to patrol the line personnel and carry to the place that needs patrol the line specially, and unmanned aerial vehicle can directly take off from unmanned aerial vehicle recovery unit, also can fly back unmanned aerial vehicle recovery unit standby after taking off, the work load of patrolling the line personnel that has significantly reduced.
Description
Technical Field
The utility model belongs to the unmanned aerial vehicle field especially relates to an equipment for unmanned aerial vehicle retrieves.
Background
The unmanned aerial vehicle taking the battery as power has excellent performances such as lightness, flexibility, acceleration and the like, but the unmanned aerial vehicle taking the battery as power is often much weaker in cruising ability than a fuel oil unmanned aerial vehicle. High tension line need often patrol the line, but a lot of high tension line erect in chongshan mountain and steep hill, and it is big to patrol the line difficult way, if adopt unmanned aerial vehicle to patrol the line, will greatly alleviate the burden of patrolling the line personnel, but because the problem that unmanned aerial vehicle continued the journey, traditional unmanned aerial vehicle patrols the line still needs to patrol the line personnel and take the unmanned aerial vehicle to the scene, patrols the work load of line personnel and still exists.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problem, the utility model discloses an erect unmanned aerial vehicle recovery unit on high tension tower can charge to the unmanned aerial vehicle in retrieving the storehouse, need not from this point on line patrol personnel journey and send unmanned aerial vehicle to appointed line patrol place, alleviates line patrol personnel's work burden.
The technical scheme of the utility model as follows:
the utility model provides an unmanned aerial vehicle recovery unit, is including retrieving the storehouse, retrieve the storehouse including retrieving the mechanism and locating the switching mechanism who retrieves the mechanism top, retrieve the mechanism and catch net, protective frame and lift platform including catching, catch the net cover outside the protective frame, the protective frame bottom is equipped with supporting baseplate, and lift platform establishes the appearance intracavity that forms at protective frame and supporting baseplate.
Further, the opening and closing mechanism comprises an outer supporting ring, a main driving wheel, a plurality of closing plates, a pull arm and a main driving gear, wherein the driving gear is arranged on the periphery of the main driving wheel, the main driving gear is meshed with the driving gear, the outer supporting ring is fixed at the top of the recovery mechanism, the closing plates are rotatably installed on the outer supporting ring through rotating pivots, the closing plates are connected with the main driving wheel through the pull arm, the main driving gear drives the main driving wheel to rotate, and the main driving wheel pulls the closing plates through the pull arm to enable the closing plates to rotate relative to the rotating pivots.
Furthermore, the opening and closing mechanism further comprises a rotary supporting ring, and the main driving wheel carrier is arranged on the supporting ring.
Furthermore, a solar electric plate is arranged on the upper surface of the closed plate and provides electric energy for the whole device.
Furthermore, the recovery mechanism further comprises a capturing cylinder, the top of the capturing net is fixedly connected with a connecting ring, and the connecting ring ascends or descends under the action of the capturing cylinder.
Further, the capture net is connected with the connecting ring through a fixing rubber ring.
Furthermore, still include main lift cylinder among the recovery mechanism, the lift cylinder control supporting baseplate's lift.
Furthermore, still include vice lift cylinder in retrieving the mechanism, vice lift cylinder control lift platform's lift.
Furthermore, the pull arm is connected with the main driving wheel through a connecting pin A, and the pull arm is connected with the closing plate through a connecting pin B.
The utility model has the advantages that: can install unmanned aerial vehicle recovery unit on each high-voltage power tower, unmanned aerial vehicle can not need to patrol the line personnel and carry to the place that needs patrol the line specially, and unmanned aerial vehicle can directly take off from unmanned aerial vehicle recovery unit, also can fly back unmanned aerial vehicle recovery unit standby after taking off, the work load of patrolling the line personnel that has significantly reduced.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is an overall schematic view of a solar closure panel;
1. a recovery bin; 2. an opening and closing mechanism; 2-1, an outer support ring; 2-2, main driving wheels; 2-3, closing the plate; 2-4, pulling arms; 2-5, rotating the pivot; 2-6, connecting pin A; 2-7, connecting pin B; 2-8, driving a gear ring; 2-9, a main drive gear; 2-10, rotating the support ring; 3. a recovery mechanism; 3-1, capturing a cylinder; 3-2, connecting rings; 3-3, fixing a rubber ring; 3-4, capturing a net; 3-5, a protective frame; 3-6, supporting the bottom plate; 3-7, a lifting platform; 3-8, an auxiliary lifting cylinder; 3-9, a switching sleeve; 3-10 parts of main lifting cylinder.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
As shown in fig. 1 and 2, an unmanned aerial vehicle recovery device comprises a recovery bin 1, wherein the recovery bin 1 comprises a recovery mechanism 3 and an opening and closing mechanism 2 arranged at the top of the recovery mechanism 3, the recovery mechanism 3 comprises a capture net 3-4, a protective frame 3-5 and a lifting platform 3-7, the capture net 3-4 is sleeved outside the protective frame 3-5, a supporting bottom plate 3-6 is arranged at the bottom of the protective frame 3-5, and the lifting platform 3-7 is arranged in a containing cavity formed by the protective frame 3-5 and the supporting bottom plate 3-6. The opening and closing mechanism 2 comprises an outer supporting ring 2-1, a main driving wheel 2-2, a plurality of closing plates 2-3, a pull arm 2-4 and a main driving gear 2-9, the periphery of the main driving wheel 2-2 is provided with a driving gear 2-8, the main driving gear 2-9 is meshed with the driving gear 2-8, the outer supporting ring 2-1 is fixed at the top of the recovery mechanism 3, the closing plate 2-3 is rotatably mounted on the outer supporting ring 2-1 through a rotating pivot 2-5, the closing plate 2-3 is connected with the main driving wheel 2-2 through a pull arm 2-4, the main driving gear 2-9 drives the main driving wheel 2-2 to rotate, and the main driving wheel 2-2 pulls the closing plate 2-3 through the pull arm 2-4, so that the closing plate 2-3 rotates relative to the rotating pivot 2-5. The opening and closing mechanism 2 further comprises a rotary supporting ring 2-10, and the main driving wheel 2-2 is erected on the supporting ring 2-10. And a solar electric plate is arranged on the upper surface of the closed plate 2-3 and provides electric energy for the whole device. The recovery mechanism 3 further comprises a capturing cylinder 3-1, the top of the capturing net 3-4 is fixedly connected with a connecting ring 3-2, and the connecting ring 3-2 ascends or descends under the action of the capturing cylinder 3-1. The capture net 3-4 is connected with the connecting ring 3-2 through a fixing rubber ring 3-3. The recovery mechanism 3 also comprises a main lifting cylinder 3-10, and the lifting cylinder 3-10 controls the lifting of the supporting bottom plate 3-6. The recovery mechanism 3 further comprises an auxiliary lifting cylinder 3-8, and the auxiliary lifting cylinder 3-8 controls the lifting of the lifting platform 3-7. The pull arm 2-4 is connected with the main driving wheel 2-2 through a connecting pin A2-6, and the pull arm 2-4 is connected with the closing plate 2-3 through a connecting pin B2-7.
The operation mode of the unmanned aerial vehicle recovery device is as follows:
when the unmanned aerial vehicle comes back, the main driving gear 2-9 is driven by the motor to rotate to drive the driving gear ring 2-8 to rotate, so that the main driving wheel 2-2 rotates, the main driving wheel 2-2 pulls the closing plate 2-3 through the pull arm 2-4, the closing plate 2-3 rotates relative to the rotating pivot 2-5, a closing space between the closing plates 2-3 is opened, a closing gap is enlarged, and the unmanned aerial vehicle enters the recovery mechanism 3 from the opened closing plates 2-3.
The main lifting cylinder 3-10 starts to retract when the main driving gear 2-9 starts to rotate, the auxiliary lifting cylinder 3-8 also starts to retract, the capturing cylinder 3-1 is lifted, the connecting ring 3-2 rises, the capturing net 3-4 is unfolded along with the rising of the connecting ring 3-2, the blades of the unmanned aerial vehicle stop rotating after the unmanned aerial vehicle passes through the closing plate 2-3, and then the blades of the unmanned aerial vehicle can be captured by the capturing net 3-4. After the grabbing is finished, the main lifting cylinder 3-10 rises to enable the protective frame 3-5 on the whole supporting bottom plate 3-6 to rise, the unmanned aerial vehicle is extruded by the edge of the protective frame 3-5 through the relative sliding of the rising of the protective frame 3-5 and the capturing net 3-4, so that the unmanned aerial vehicle is separated from the capturing net 3-4 and falls into the protective frame 3-5, meanwhile, the auxiliary lifting cylinder 3-8 expands maximally to enable the lifting platform 3-7 to rise to the upper half part of the protective frame 3-5, the unmanned aerial vehicle falls on the lifting platform 3-7 at the moment, the unmanned aerial vehicle is centered and parked, after the unmanned aerial vehicle is parked, the main lifting cylinder 3-10 and the auxiliary lifting cylinder 3-8 are contracted to enable the unmanned aerial vehicle to be parked at the bottom of the recovery mechanism 3, and the capturing cylinder 3-1 is contracted at the same time, the capture net 3-4 is folded, and the capture net 3-4 can not influence the fly-back of the unmanned aerial vehicle during fly-back. The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (9)
1. The utility model provides an unmanned aerial vehicle recovery unit which characterized in that: the device comprises a recovery bin (1), wherein the recovery bin (1) comprises a recovery mechanism (3) and an opening and closing mechanism (2) arranged at the top of the recovery mechanism (3), the recovery mechanism (3) comprises a capture net (3-4), a protective frame (3-5) and a lifting platform (3-7), the capture net (3-4) is sleeved outside the protective frame (3-5), a supporting bottom plate (3-6) is arranged at the bottom of the protective frame (3-5), and the lifting platform (3-7) is arranged in a containing cavity formed by the protective frame (3-5) and the supporting bottom plate (3-6).
2. An unmanned aerial vehicle recovery device as claimed in claim 1, wherein: the opening and closing mechanism (2) comprises an outer supporting ring (2-1), a main driving wheel (2-2), a plurality of closing plates (2-3), a pull arm (2-4) and a main driving gear (2-9), the driving gear (2-8) is arranged on the periphery of the main driving wheel (2-2), the main driving gear (2-9) is meshed with the driving gear (2-8), the outer supporting ring (2-1) is fixed to the top of the recovery mechanism (3), the closing plates (2-3) are rotatably mounted on the outer supporting ring (2-1) through rotating pivots (2-5), the closing plates (2-3) are connected with the main driving wheel (2-2) through the pull arm (2-4), the main driving gear (2-9) drives the main driving wheel (2-2) to rotate, and the main driving wheel (2-2) pulls the closing plates (2-3) through the pull arm (2-4) ) So that the closing plate (2-3) is turned relative to the turning pivot (2-5).
3. An unmanned aerial vehicle recovery device as claimed in claim 2, wherein: the opening and closing mechanism (2) further comprises a rotary supporting ring (2-10), and the main driving wheel (2-2) is erected on the supporting ring (2-10).
4. An unmanned aerial vehicle recovery device as claimed in claim 2, wherein: and a solar panel is arranged on the upper surface of the closed plate (2-3) and provides electric energy for the whole device.
5. An unmanned aerial vehicle recovery device as claimed in claim 1, wherein: the recovery mechanism (3) further comprises a capturing cylinder (3-1), the top of the capturing net (3-4) is fixedly connected with a connecting ring (3-2), and the connecting ring (3-2) ascends or descends under the action of the capturing cylinder (3-1).
6. An unmanned aerial vehicle recovery device as claimed in claim 5, wherein: the capture net (3-4) is connected with the connecting ring (3-2) through a fixed rubber ring (3-3).
7. An unmanned aerial vehicle recovery device as claimed in claim 1, wherein: the recovery mechanism (3) further comprises a main lifting cylinder (3-10), and the lifting cylinder (3-10) controls the lifting of the supporting bottom plate (3-6).
8. An unmanned aerial vehicle recovery device as claimed in claim 1, wherein: the recovery mechanism (3) further comprises an auxiliary lifting cylinder (3-8), and the auxiliary lifting cylinder (3-8) controls the lifting of the lifting platform (3-7).
9. An unmanned aerial vehicle recovery device as claimed in claim 2, wherein: the pull arm (2-4) is connected with the main driving wheel (2-2) through a connecting pin A (2-6), and the pull arm (2-4) is connected with the closing plate (2-3) through a connecting pin B (2-7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921119562.2U CN210912918U (en) | 2019-07-16 | 2019-07-16 | Unmanned aerial vehicle recovery unit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921119562.2U CN210912918U (en) | 2019-07-16 | 2019-07-16 | Unmanned aerial vehicle recovery unit |
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| Publication Number | Publication Date |
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| CN210912918U true CN210912918U (en) | 2020-07-03 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201921119562.2U Active CN210912918U (en) | 2019-07-16 | 2019-07-16 | Unmanned aerial vehicle recovery unit |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112623135A (en) * | 2020-12-25 | 2021-04-09 | 上海大学 | Unmanned aerial vehicle cloth puts recovery unit based on flexible mechanism of catching |
| CN112793800A (en) * | 2021-02-03 | 2021-05-14 | 南京安元科技有限公司 | Multi-functional unmanned aerial vehicle flight platform |
-
2019
- 2019-07-16 CN CN201921119562.2U patent/CN210912918U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112623135A (en) * | 2020-12-25 | 2021-04-09 | 上海大学 | Unmanned aerial vehicle cloth puts recovery unit based on flexible mechanism of catching |
| CN112793800A (en) * | 2021-02-03 | 2021-05-14 | 南京安元科技有限公司 | Multi-functional unmanned aerial vehicle flight platform |
| CN112793800B (en) * | 2021-02-03 | 2022-05-13 | 南京安元科技有限公司 | Multi-functional unmanned aerial vehicle flight platform |
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