CN207889999U - A kind of carry for unmanned plane and hit net integral type retracting device - Google Patents
A kind of carry for unmanned plane and hit net integral type retracting device Download PDFInfo
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- CN207889999U CN207889999U CN201721876389.1U CN201721876389U CN207889999U CN 207889999 U CN207889999 U CN 207889999U CN 201721876389 U CN201721876389 U CN 201721876389U CN 207889999 U CN207889999 U CN 207889999U
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- carry
- principal arm
- cantilever
- unmanned plane
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Abstract
The utility model discloses a kind of carry for unmanned plane and hit net integral type retracting device, it includes principal arm, Erecting organ, Zhuan Wang mechanisms, carry mechanism, controller and vehicular platform, principal arm is inclined on vehicular platform, Erecting organ is fixed on vehicular platform and connect the angle for being used to support and adjusting principal arm and vehicular platform with principal arm, Zhuan Wang mechanisms and the carry mechanism are arranged on principal arm, controller is arranged on vehicular platform for controlling the flexible of principal arm, the setting that the utility model passes through carry mechanism and Zhuan Wang mechanisms, it can be recycled in different ways, applicability is more extensive；Zhuan Wang mechanisms can be shunk automatically by contraction pole, while damping mechanism is arranged can slowly slow down during whole wire side retreats, safe retrieving unmanned plane；The setting of multiple carry mechanisms can improve the efficiency of recycling；The utility model is installed and arrangement is simple, and recycling precision is high, greatly improves the application range of small and medium size unmanned aerial vehicles.
Description
Technical field
The utility model belongs to unmanned plane retracting device technical field, and in particular to a kind of carry for unmanned plane and hits
Net integral type retracting device.
Background technology
Unmanned plane is the not manned vehicle manipulated by radio robot or airborne computer stored program controlled,
Unmanned plane can not only complete the task of manned aircraft execution, be more suitable for the task that someone's aircraft should not execute.
In the prior art, the mode of unmanned plane recycling is usually：Automatic Landing first, landing mission with it is manned
Aircraft is identical, is landed on runway by remote control or machine internal program control device operating aircraft by ground controlling personnel；Its
Secondary is parachute recycling, carries parachute on unmanned plane, landing period automatically opens, or is opened according to telecommand, parachute
Unmanned plane is suspended on slowly to descend slowly and lightly landing；There is aerial recycling again, the program of beginning is identical as parachute way of recycling, when nobody
Machine releases a parachute when descending slowly and lightly in the air, is in the air recycled unmanned plane with the recycling machine tool such as helicopter, and carries go back to field and land；
In addition, it is net collision recovery to also have, one vertical of leader is flown to by unmanned plane, unmanned plane hits leader according to guiding, head,
And knocking in a flash, leader locks in body mechanism, prevents unmanned plane from falling.Leader moves after passing through, and absorbs impact energy, from
And reaching the target of recycling unmanned plane, which hits to site requirements very little and nets and can move, so as to aboard ship adopt
With still, the area for hitting net is larger, and expansion is more difficult.This method is also restricted to the type of unmanned plane, can not be applicable in propeller
Preceding pull-type unmanned plane.Meanwhile the impact for hitting net is huge, is easy to cause aircraft and protrudes object, such as pitot, communication day
Line, even wing are damaged.
Utility model content
For overcome the deficiencies in the prior art, the purpose of the utility model is to provide a kind of carry for unmanned plane and
Hit net integral type retracting device.
What the technical solution of the utility model was realized in：
The utility model embodiment provides a kind of carry for unmanned plane and hits net integral type retracting device comprising main
Arm, Erecting organ, Zhuan Wang mechanisms, carry mechanism, controller and vehicular platform, the principal arm are inclined on vehicular platform,
The Erecting organ is fixed on vehicular platform and is connect with principal arm the angle for being used to support and adjusting principal arm and vehicular platform,
The Zhuan Wang mechanisms and the carry mechanism are arranged on principal arm, and the controller is arranged on vehicular platform for controlling master
Arm stretches.
In said program, the principal arm includes sequentially connected first telescopic arm and at least one second telescopic arm, described
First telescopic arm is arranged on vehicular platform, and first telescopic arm and at least one second telescopic arm are both provided with electronic gas
Cylinder, the electric cylinder are connect with controller for controlling the flexible of principal arm；The Zhuan Wang mechanisms are arranged on the first telescopic arm；
At least one second telescopic arm is respectively provided with carry mechanism.
In said program, the Zhuan Wang mechanisms include recycling network, shrink bar assembly and two supporting rods, the contraction pole group
There are two the left and right sides for being located at recycling network, the both sides that described two supporting rods are symmetricly set on principal arm are used respectively for part setting
Contraction bar assembly in the left and right sides of connection recycling network, one end of the supporting rod are connect with principal arm, the other end and contraction pole
Component connects；Electric cylinder is set between the supporting rod and principal arm, and the electric cylinder is connect with controller.
In said program, the contraction bar assembly includes vertical supporting rod, cantilever group, the first swing rod, the second swing rod；The branch
One end of support montant is connect with supporting rod, and the other end is connect with cantilever group；The cantilever group include the first cantilever, connecting cantilever and
Second cantilever, first cantilever and the second cantilever are connect by shaft with vertical supporting rod respectively, one end of first cantilever
By the connection of connecting cantilever and the second cantilever, the other end is connect with the first swing rod, and second cantilever also connects with the second swing rod
It connects.
In said program, one end of the connecting cantilever is connected to the middle part of the second cantilever.
In said program, the Zhuan Wang mechanisms further include damping mechanism, and the damping mechanism is connect with cantilever group.
In said program, the carry mechanism includes mobile jib, rope and carry bar, and one end and the principal arm of the mobile jib connect
It connects, the other end is connect by rope with carry bar；The mobile jib and principal arm are angled, and the rope surrounds triangle with carry bar
Shape.
In said program, electric cylinder is set, the electric cylinder is connect with controller between the mobile jib and principal arm.
In said program, the carry mechanism further includes sensor, and the sensor is connect with controller.
In said program, the carry mechanism further includes the hook for coordinating with unmanned plane.
Compared with prior art, the utility model embodiment provides a kind of carry for unmanned plane and hits net integral type and returns
Receiving apparatus comprising principal arm, Erecting organ, Zhuan Wang mechanisms, carry mechanism, controller and vehicular platform, the principal arm inclination are set
Set on vehicular platform, the Erecting organ be fixed on vehicular platform and connect with principal arm be used to support and adjust principal arm with
The angle of vehicular platform, the Zhuan Wang mechanisms and the carry mechanism are arranged on principal arm, and the controller is arranged vehicle-mounted
For controlling the flexible of principal arm on platform, in this way, setting of the utility model by carry mechanism and Zhuan Wang mechanisms, can use
Different modes are recycled, and applicability is more extensive；The Zhuan Wang mechanisms of the utility model can be shunk automatically by contraction pole, be set simultaneously
Setting damping mechanism can slowly slow down during whole wire side retreats, safe retrieving unmanned plane；Multiple carry mechanisms are set
The efficiency of recycling can be improved by setting；The utility model floor space is small, not high to site requirements, and installation and arrangement are simple, recycling
Precision is high, and recycling reliability is high, greatly improves the application range of small and medium size unmanned aerial vehicles.
Description of the drawings
Fig. 1 is a kind of carry for unmanned plane of the utility model embodiment and hits the structure of net integral type retracting device and show
It is intended to；
Fig. 2 is a kind of carry for unmanned plane of the utility model embodiment and hits in net integral type retracting device and hit net
The structural schematic diagram of mechanism；
Fig. 3 is a kind of carry for unmanned plane of the utility model embodiment and hits carry in net integral type retracting device
The structural schematic diagram of mechanism.
Reference numeral is as follows：
1 --- --- --- the second telescopic arm, 2 --- Erecting organ, 3 --- hit net machine for the first telescopic arm, 12 for principal arm, 11
--- bar assembly, 321 --- vertical supporting rod, 322 --- the first swing rod, 323 --- second --- are shunk in recycling network, 32 for structure, 31
--- --- --- the second cantilever, 33 --- supporting rod, 34 --- damp for connecting cantilever, 326 for the first cantilever, 325 for swing rod, 324
--- --- --- --- carry bar, 5 --- controller, 6 --- are vehicle-mounted flat for rope, 43 for mobile jib, 42 for carry mechanism, 41 for mechanism, 4
Platform.
Specific implementation mode
In order to make the purpose of the utility model, technical solutions and advantages more clearly understood, below in conjunction with attached drawing and implementation
Example, the present invention will be further described in detail.It should be appreciated that specific embodiment described herein is only used to explain
The utility model is not used to limit the utility model.
The utility model embodiment provides a kind of carry for unmanned plane and hits net integral type retracting device, such as Fig. 1-3
It is shown comprising principal arm 1, Erecting organ 2, Zhuan Wang mechanisms 3, carry mechanism 4, controller 5 and vehicular platform 6, the principal arm 1 incline
Tiltedly it is arranged on vehicular platform 6, the Erecting organ 2 is fixed on vehicular platform 6 and is connect with principal arm 1 and is used to support and adjusts
The angle of whole principal arm 1 and vehicular platform 6, the Zhuan Wang mechanisms 3 and carry mechanism 4 are arranged on principal arm 1, the controller 5
It is arranged on vehicular platform 6 for controlling the flexible of principal arm 1.
The utility model can be recycled in different ways by the setting of carry mechanism and Zhuan Wang mechanisms, be applicable in
Property is more extensive；The Zhuan Wang mechanisms of the utility model can be shunk automatically by contraction pole, while damping mechanism is arranged can be in entirety
Wire side slowly slows down during retreating, safe retrieving unmanned plane；The setting of multiple carry mechanisms can improve the efficiency of recycling；
The utility model floor space is small, not high to site requirements, and installation and arrangement are simple, and recycling precision is high, and recycling reliability is high, pole
The earth improves the application range of small and medium size unmanned aerial vehicles.
The principal arm 1 includes sequentially connected first telescopic arm 11 and at least one second telescopic arm 12, and described first stretches
Contracting arm 11 is arranged on vehicular platform 6, and first telescopic arm 11 and at least one second telescopic arm 12 are both provided with electronic gas
Cylinder, the electric cylinder are connect with controller 5 for controlling the flexible of principal arm 1；The Zhuan Wang mechanisms 3 are arranged in the first telescopic arm
On 11；At least one second telescopic arm is respectively provided with carry mechanism 4.
Principal arm 1 is retractable structure, including the first telescopic arm 11 and at least one second telescopic arm 12, the first telescopic arm 11
It is arranged on vehicular platform 6 by Erecting organ 2, Erecting organ 2 includes pedestal and electric cylinder, the first telescopic arm 11 and pedestal
It is hinged, and connect with the electric cylinder of Erecting organ 2, electric cylinder is controlled by controller 5, can adjust the first telescopic arm
Angle between 11 and vehicular platform 6；
First telescopic arm 11 and at least one second telescopic arm 12 are socketed successively from the bottom to top, and 11 He of the first telescopic arm
At least one second telescopic arm 12 is socketed successively from the bottom to top, and the first telescopic arm 11 and at least one second telescopic arm 12 are respectively provided with
Electric cylinder, controller 5 can control the first telescopic arm 11 and at least one second telescopic arm respectively by controlling electric cylinder
12 collapsing length.
The Zhuan Wang mechanisms 3 are arranged on the first telescopic arm 11；The Zhuan Wang mechanisms 3 include recycling network 31, contraction pole group
Part 32 and two supporting rods 33, the bar assembly 32 of shrinking is arranged there are two the left and right sides for being located at recycling network 31, described
The both sides that two supporting rods 33 are symmetricly set on principal arm 1 are respectively used to the contraction bar assembly of the left and right sides of connection recycling network 31
32, one end of the supporting rod 33 is connect with principal arm 1, and the other end is connect with bar assembly 32 is shunk；The supporting rod 33 and principal arm 1
Between electric cylinder is set, the electric cylinder is connect with controller 5.
Bar assembly 32 is shunk to be arranged in the both sides of recycling network 31 for by 31 support exhibition of recycling network, supporting rod 33 to be symmetricly set on
The both sides of principal arm 1 are used to open the contraction bar assembly 32 of recycling network both sides, to support exhibition recycling network 31.
The contraction bar assembly 32 includes vertical supporting rod 321, cantilever group, the first swing rod 322, the second swing rod 323；The branch
One end of support montant 321 is connect with supporting rod 33, and the other end is connect with cantilever group；The cantilever group includes the first cantilever 324, connects
Cantilever 325 and the second cantilever 326 are connect, first cantilever, 324 and second cantilever 326 passes through shaft and vertical supporting rod 321 respectively
Connection, one end of first cantilever 324 pass through the connection of connecting cantilever 325 and the second cantilever 326, the other end and the first swing rod
322 connections, second cantilever 326 are also connect with the second swing rod 323.
Wherein, one end of the connecting cantilever 325 is connected to the middle part of the second cantilever 326.
The Zhuan Wang mechanisms 3 further include damping mechanism 34, and the damping mechanism 34 is connect with cantilever group.
It shrinks bar assembly 32 and is mainly used to the unmanned plane that recycling bangs into net, its working principle is that：When unmanned plane bangs into back
Net 31 is received, the impact force of unmanned plane passes to recycling network 31, and the wing of unmanned plane generates pulling force to recycling network 31, due to the first pendulum
Bar 322 is in the upside of the second swing rod 323, since the first swing rod 322 and the second swing rod 323 pass through the first cantilever 324 and respectively
Two cantilevers 326 connect, and the first cantilever 324 and the second cantilever 326 are connect by shaft with vertical supporting rod 321, therefore, nothing
Man-machine wing generates pulling force to recycling network 31, to drive the first swing rod 322 and 323 relative motion of the second swing rod, due to the
One swing rod 322 and the second swing rod 323 are connected by the first cantilever 324 and the second cantilever 326 respectively, and pass through connecting cantilever
325 ensure (general 10 ° to the 70 °) symmetric motion in certain angular range of the first cantilever 324 and the second cantilever 326, to
Ensure that the first swing rod 322 and the second swing rod 323 do symmetric motion, preferably completes recycling action；And the first swing rod 322 and
Two swing rods 323 transmit the force to damping mechanism 34 by cantilever group, and damping mechanism 34 completes energy-absorbing, by unmanned plane safe retrieving.
The carry mechanism 4 includes mobile jib 41, rope 42 and carry bar 43, and one end of the mobile jib 41 is connect with principal arm 1,
The other end is connect by rope 42 with carry bar 43；The mobile jib 41 and principal arm 1 are angled, and the rope 42 is enclosed with carry bar 43
At triangle.
Wherein, electric cylinder is set between the mobile jib 41 and principal arm 1, and the electric cylinder is connect with controller 5.
The carry mechanism 4 further includes sensor, and the sensor is connect with controller 5.
The carry mechanism 4 further includes the hook for coordinating with unmanned plane.
Carry mechanism 4 is also equipped with damping mechanism.
The course of work of carry component 4 is：Hook is installed on unmanned plane, unmanned plane puts down hook in landing, dropping
During falling, carry bar 43 is tangled, pulling force is transferred to damping mechanism by carry bar 43, and damping mechanism completes energy-absorbing, then
The sensor of mobile jib 41 sends out signal to controller 5, and controller 5 can control principal arm contraction, recycle unmanned plane.
The utility model embodiment provides a kind of carry for unmanned plane and hits net integral type retracting device comprising main
Arm, Erecting organ, Zhuan Wang mechanisms, carry mechanism, controller and vehicular platform, the principal arm are inclined on vehicular platform,
The Erecting organ is fixed on vehicular platform and is connect with principal arm the angle for being used to support and adjusting principal arm and vehicular platform,
The Zhuan Wang mechanisms and the carry mechanism are arranged on principal arm, and the controller is arranged on vehicular platform for controlling master
Arm stretches, in this way, setting of the utility model by carry mechanism and Zhuan Wang mechanisms, can be returned in different ways
It receives, applicability is more extensive；The Zhuan Wang mechanisms of the utility model can be shunk automatically by contraction pole, while damping mechanism is arranged can
Slowly slow down during whole wire side retreats, safe retrieving unmanned plane；The setting of multiple carry mechanisms can improve recycling
Efficiency；The utility model floor space is small, not high to site requirements, and installation and arrangement are simple, and recycling precision is high, and recycling is reliable
Property it is high, greatly improve the application range of small and medium size unmanned aerial vehicles.
The above, the only preferred embodiment of the utility model, are not intended to limit the protection of the utility model
Range.
Claims (10)
1. a kind of carry for unmanned plane and hitting net integral type retracting device, which is characterized in that it includes principal arm (1), it is perpendicular to rise
Mechanism (2), Zhuan Wang mechanisms (3), carry mechanism (4), controller (5) and vehicular platform (6), the principal arm (1) are inclined at
On vehicular platform (6), the Erecting organ (2) is fixed on vehicular platform (6) and is connect with principal arm (1) and is used to support and adjusts
The angle of whole principal arm (1) and vehicular platform (6), the Zhuan Wang mechanisms (3) and carry mechanism (3) are arranged on principal arm (1), institute
Controller (5) is stated to be arranged on vehicular platform (6) for controlling the flexible of principal arm (1).
2. a kind of carry for unmanned plane according to claim 1 and hitting net integral type retracting device, which is characterized in that
The principal arm (1) includes sequentially connected first telescopic arm (11) and at least one second telescopic arm (12), and described first is flexible
Arm (11) is arranged on vehicular platform (6), and first telescopic arm (11) and at least one second telescopic arm (12) are both provided with
Electric cylinder, the electric cylinder are connect with controller (5) for controlling the flexible of principal arm (1)；The setting of Zhuan Wang mechanisms 3 exists
On first telescopic arm (11)；At least one second telescopic arm is respectively provided with carry mechanism (4).
3. a kind of carry for unmanned plane according to claim 2 and hitting net integral type retracting device, which is characterized in that
The Zhuan Wang mechanisms (3) include recycling network (31), shrink bar assembly (32) and two supporting rods (33), the contraction bar assembly
(32) there are two the left and right sides for being located at recycling network (31), described two supporting rods (33) to be symmetricly set on principal arm for setting
(1) both sides be respectively used to connection recycling network (31) the left and right sides contraction bar assembly (32), the one of the supporting rod (33)
End is connect with principal arm (1), and the other end is connect with bar assembly (32) is shunk；It is arranged between the supporting rod 33 and principal arm (1) electronic
Cylinder, the electric cylinder are connect with controller (5).
4. a kind of carry for unmanned plane according to claim 3 and hitting net integral type retracting device, which is characterized in that
The contraction bar assembly (32) includes vertical supporting rod (321), cantilever group, the first swing rod (322), the second swing rod (323)；The branch
One end of support montant (321) is connect with supporting rod (33), and the other end is connect with cantilever group；The cantilever group includes the first cantilever
(324), connecting cantilever (325) and the second cantilever (326), first cantilever (324) and the second cantilever (326) are respectively by turning
Axis is connect with vertical supporting rod (321), and one end of first cantilever (324) passes through connecting cantilever (325) and the second cantilever (326)
Connection, the other end connect with the first swing rod (322), and second cantilever (326) also connect with the second swing rod (323).
5. a kind of carry for unmanned plane according to claim 4 and hitting net integral type retracting device, which is characterized in that
One end of the connecting cantilever (325) is connected to the middle part of the second cantilever (326).
6. a kind of carry for unmanned plane according to claim 5 and hitting net integral type retracting device, which is characterized in that
The Zhuan Wang mechanisms (3) further include damping mechanism (34), and the damping mechanism (34) connect with cantilever group.
7. a kind of carry for unmanned plane according to claim 6 and hitting net integral type retracting device, which is characterized in that
The carry mechanism (4) includes mobile jib (41), rope (42) and carry bar (43), one end and the principal arm (1) of the mobile jib (41)
Connection, the other end are connect by rope (42) with carry bar (43)；The mobile jib (41) and principal arm (1) are angled, the rope
(42) triangle is surrounded with carry bar (43).
8. a kind of carry for unmanned plane according to claim 7 and hitting net integral type retracting device, which is characterized in that
Electric cylinder is set between the mobile jib (41) and principal arm (1), and the electric cylinder is connect with controller (5).
9. a kind of carry for unmanned plane according to claim 7 and hitting net integral type retracting device, which is characterized in that
The carry mechanism (4) further includes sensor, and the sensor is connect with controller (5).
10. a kind of carry for unmanned plane according to claim 7 and hitting net integral type retracting device, feature exists
In the carry mechanism (4) further includes the hook for coordinating with unmanned plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721876389.1U CN207889999U (en) | 2017-12-28 | 2017-12-28 | A kind of carry for unmanned plane and hit net integral type retracting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721876389.1U CN207889999U (en) | 2017-12-28 | 2017-12-28 | A kind of carry for unmanned plane and hit net integral type retracting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207889999U true CN207889999U (en) | 2018-09-21 |
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ID=63550130
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721876389.1U Active CN207889999U (en) | 2017-12-28 | 2017-12-28 | A kind of carry for unmanned plane and hit net integral type retracting device |
Country Status (1)
| Country | Link |
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| CN (1) | CN207889999U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109502042A (en) * | 2018-11-26 | 2019-03-22 | 南京林业大学 | A kind of unmanned plane acquisition equipment |
| CN109883737A (en) * | 2019-01-02 | 2019-06-14 | 中南大学 | The lossless train acquisition equipment of air damping speed reduction screen driving system two-stage |
| CN110775216A (en) * | 2019-10-31 | 2020-02-11 | 杭州流富科技有限公司 | Unmanned aerial vehicle offshore take-off and landing platform applying internet communication technology |
-
2017
- 2017-12-28 CN CN201721876389.1U patent/CN207889999U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109502042A (en) * | 2018-11-26 | 2019-03-22 | 南京林业大学 | A kind of unmanned plane acquisition equipment |
| CN109883737A (en) * | 2019-01-02 | 2019-06-14 | 中南大学 | The lossless train acquisition equipment of air damping speed reduction screen driving system two-stage |
| CN110775216A (en) * | 2019-10-31 | 2020-02-11 | 杭州流富科技有限公司 | Unmanned aerial vehicle offshore take-off and landing platform applying internet communication technology |
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