CN208963332U - A kind of fixed-wing unmanned plane interception recovery system - Google Patents
A kind of fixed-wing unmanned plane interception recovery system Download PDFInfo
- Publication number
- CN208963332U CN208963332U CN201821301660.3U CN201821301660U CN208963332U CN 208963332 U CN208963332 U CN 208963332U CN 201821301660 U CN201821301660 U CN 201821301660U CN 208963332 U CN208963332 U CN 208963332U
- Authority
- CN
- China
- Prior art keywords
- fixed
- mounting blocks
- unmanned plane
- wing unmanned
- recovery system
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Abstract
The utility model discloses a kind of fixed-wing unmanned planes to intercept recovery system, including pedestal, several groups stretching device is provided on the pedestal, the stretching device includes the cross tube and sheer pole stretched out to outer, and the interception rope of tensioning is provided between the cross tube and sheer pole；It is provided with multiple groups stretching device to tense more interception ropes, this system structure is simple, facilitates installation application that quick, safe recycling fixed-wing unmanned plane may be implemented；Package unit is removable, with using upper flexibility；More interceptions are restricted while being intercepted, and can be applied to the recycling of a large amount of fixed-wing unmanned planes, especially suitable for unmanned plane cluster operation.
Description
Technical field
The utility model relates to unmanned plane fields more particularly to a kind of fixed-wing unmanned plane to intercept recovery system.
Background technique
When existing fixed-wing unmanned plane lands, usual way of recycling has hook to take, parachuting, net formula stop landing etc., and hook is fetched
Receipts are that recycling machine tool is served as using helicopter, and unmanned plane is hooked up capture in the sky, then carry unmanned plane return of carrier pedestal.
This way of recycling needs the participation of helicopter, and removal process is extremely complex, and parachuting and the opportunity hooked up cooperation must be very quasi-
Really, difficulty is costly greatly.Although parachuting structure is simple, influenced by weather, after wind speed is more than allowed band, landing
Unmanned plane is easily damaged, and very high to the reliability requirement of system.The obstruction of net formula is by installing arresting net for unmanned plane
It catches, but this method needs to have biggish space on moving base to install braced frame and arresting net, is on the other hand easy to make
At the damage of unmanned plane or net.And common recovery system is typically only capable to recycle single unmanned plane, to a large amount of
Efficiency is too slow when unmanned plane is recycled, and cost is too high.
Utility model content
In order to overcome the above-mentioned deficiencies of the prior art, the utility model provide in a kind of confined space can to it is a nobody
Machine is intercepted, and safety coefficient is high, and fixed-wing unmanned plane at low cost intercepts recovery system.
To achieve the goals above, the technical solution adopted in the utility model is:
A kind of fixed-wing unmanned plane intercepts recovery system, including pedestal, is provided with several groups stretching device on the pedestal,
The stretching device includes the cross tube and sheer pole stretched out to outer, is provided with tensioning between the cross tube and sheer pole
Intercept rope.
As a further improvement of the foregoing solution, at least one column, the upper end of the column are provided on the pedestal
Upper mounting blocks and lower mounting blocks are respectively arranged with lower end, are respectively arranged with jack on the upper mounting blocks and lower mounting blocks, institute
It states cross tube to be plugged in mounting blocks respectively, the sheer pole is plugged in respectively in lower mounting blocks.
As a further improvement of the foregoing solution, the stretching device includes several fixed pulleys, and the fixed pulley setting exists
On cross tube and/or sheer pole, every intercepts rope and keeps tensioning by the fixed pulley of every group of stretching device.
As a further improvement of the foregoing solution, restraining position ring block, the interception rope are set on the cross tube or sheer pole
End be fixed on the stop collar.
As a further improvement of the foregoing solution, the upper mounting blocks are identical as lower installation block structure, and upper mounting blocks are under
The surrounding of mounting blocks is provided with several convex blocks, and the side of the convex block is that the opening other side is limit side wall, a cross tube or one
Sheer pole is inserted into respectively in a convex block.
As a further improvement of the foregoing solution, the rope recyclable device that storage intercepts rope, institute are provided on the column
Stating interception rope is elastic string.
As a further improvement of the foregoing solution, the connection of the cross tube or sheer pole and upper mounting blocks or lower mounting blocks
Mode is connected using ball-joint or cross axis joint.
The utility model has the beneficial effects that
A kind of fixed-wing unmanned plane of the utility model intercepts recovery system, is provided with multiple groups stretching device on a pedestal
More interceptions rope is tensed, this system structure is simple, facilitate installation application may be implemented quick, safe recycling fixed-wing nobody
Machine；Package unit is removable, with using upper flexibility；More interceptions rope while intercepting, can be applied to a large amount of fixed-wings without
Man-machine recycling, especially suitable for unmanned plane cluster operation.
Detailed description of the invention
It, below will be to required in embodiment description in order to illustrate more clearly of the technical scheme in the embodiment of the utility model
Attached drawing to be used is briefly described.Obviously, described attached drawing is a part of the embodiment of the utility model, rather than complete
Portion's embodiment, those skilled in the art without creative efforts, can also be obtained according to these attached drawings
Other design schemes and attached drawing:
Fig. 1 is the structural schematic diagram one when the utility model preferred embodiment uses；
Fig. 2 is the utility model preferred embodiment structural schematic diagram two.
Specific embodiment
It is carried out below with reference to technical effect of the embodiment and attached drawing to the design of the utility model, specific structure and generation
It clearly and completely describes, to be completely understood by the purpose of this utility model, feature and effect.Obviously, described embodiment
It is a part of the embodiment of the utility model, rather than whole embodiments, it is based on the embodiments of the present invention, the skill of this field
Art personnel other embodiments obtained without creative efforts belong to the model of the utility model protection
It encloses.
Referring to Fig.1 with Fig. 2, a kind of fixed-wing unmanned plane intercepts recovery system, including pedestal 1, is provided on the pedestal 1
Several groups stretching device, the stretching device include the cross tube 3 and sheer pole 4 stretched out to outer, the cross tube 3 and lower cross
The interception rope 5 of tensioning is provided between bar 4, the interception rope 5 is elastic string, has certain elasticity, is avoided that stress is bent.
Restraining position ring block 9 is set on the cross tube 3 or sheer pole 4, and the end for intercepting rope 5 is fixed on the stop collar 9.Solid
Determine to increase hooking device on wing unmanned plane wing, in unmanned plane landing, hooking device is contacted with interception rope 5 is recycled, due to
There are more interception ropes 5 while intercepting, can be applied to the recycling of a large amount of fixed-wing unmanned planes, make especially suitable for a unmanned plane group of planes
Industry.
It is provided at least one column 2 on the pedestal 1, the rope recycling that storage intercepts rope 5 is provided on the column 2
Device 11, the top and bottom of the column 2 are respectively arranged with mounting blocks 6 and lower mounting blocks 7, and the upper mounting blocks 6 are under
Jack is respectively arranged on mounting blocks 7, the cross tube 3 is plugged in respectively in mounting blocks 6, and the sheer pole 4 plugs respectively
In lower mounting blocks 7.The connection type of the cross tube 3 or sheer pole 4 and upper mounting blocks 6 or lower mounting blocks 7 uses ball-joint
Or cross axis joint connection.Upper mounting blocks 6 and lower mounting blocks 7 in the present embodiment are squashed structure, described in actual production
Upper mounting blocks 6 and lower mounting blocks 7 can be the different shapes such as spherical or rectangular.
The stretching device includes several fixed pulleys 8, and the fixed pulley 8 is arranged on cross tube 3 and/or sheer pole 4, often
Root intercepts rope 5 and keeps tensioning by the fixed pulley 8 of every group of stretching device.Fixed pulley 8 in the present embodiment is arranged in cross tube 3
On, stop collar 9 is arranged on sheer pole 4, and according to demand, the position of the fixed pulley 8 and stop collar 9 can be replaced.
The upper mounting blocks 6 are identical as lower 7 structure of mounting blocks, and the surrounding of upper mounting blocks 6 and lower mounting blocks 7 is provided with several
Convex block 10, the side of the convex block 10 are that the opening other side is limit side wall, and a cross tube 3 or a sheer pole 4 are inserted into one respectively
In convex block 10.Limit side wall can be supported effect to cross tube 3 and sheer pole 4, and unmanned plane is avoided to push away to 5 generations of rope are intercepted
Power is excessive, and torque is excessive so that cross tube 3 or sheer pole 4 fracture on cross tube 3 or sheer pole 4, can play preferably connection and make
With so that structure is more stable.
It is to be illustrated to the preferred embodiment of the utility model, but the utility model creation is not limited to above
The embodiment, those skilled in the art can also make various etc. without departing from the spirit of the present invention
Same variation or replacement, these equivalent variation or replacement are all included in the scope defined by the claims of the present application.
Claims (7)
1. a kind of fixed-wing unmanned plane intercepts recovery system, it is characterised in that: including pedestal (1), be provided on the pedestal (1)
Several groups stretching device, the stretching device include the cross tube (3) and sheer pole (4) stretched out to outer, the cross tube (3)
The interception rope (5) of tensioning is provided between sheer pole (4).
2. fixed-wing unmanned plane according to claim 1 intercepts recovery system, it is characterised in that: set on the pedestal (1)
It is equipped at least one column (2), the top and bottom of the column (2) are respectively arranged with mounting blocks (6) and lower mounting blocks
(7), it is respectively arranged with jack on the upper mounting blocks (6) and lower mounting blocks (7), the cross tube (3) is plugged in peace respectively
It fills in block (6), the sheer pole (4) is plugged in respectively in lower mounting blocks (7).
3. fixed-wing unmanned plane according to claim 1 intercepts recovery system, it is characterised in that: the stretching device includes
Several fixed pulleys (8), the fixed pulley (8) are arranged on cross tube (3) and/or sheer pole (4), and every interception rope (5) passes through
The fixed pulley (8) of every group of stretching device keeps tensioning.
4. fixed-wing unmanned plane according to claim 1 intercepts recovery system, it is characterised in that: the cross tube (3) or
Restraining position ring block (9) are set on sheer pole (4), the end for intercepting rope (5) is fixed on the stop collar (9).
5. fixed-wing unmanned plane according to claim 2 intercepts recovery system, it is characterised in that: the upper mounting blocks (6)
Identical as lower mounting blocks (7) structure, the surrounding of upper mounting blocks (6) and lower mounting blocks (7) is provided with several convex blocks (10), described convex
The side of block (10) is that the opening other side is limit side wall, and a cross tube (3) or a sheer pole (4) are inserted into a convex block (10) respectively
It is interior.
6. fixed-wing unmanned plane according to claim 2 intercepts recovery system, it is characterised in that: set on the column (2)
It is equipped with the rope recyclable device (11) that storage intercepts rope (5), the interception rope (5) is elastic string.
7. fixed-wing unmanned plane according to claim 1 intercepts recovery system, it is characterised in that: the cross tube (3) or
Sheer pole (4) is connect with the connection type of upper mounting blocks (6) or lower mounting blocks (7) using ball-joint or cross axis joint.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821301660.3U CN208963332U (en) | 2018-08-13 | 2018-08-13 | A kind of fixed-wing unmanned plane interception recovery system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821301660.3U CN208963332U (en) | 2018-08-13 | 2018-08-13 | A kind of fixed-wing unmanned plane interception recovery system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208963332U true CN208963332U (en) | 2019-06-11 |
Family
ID=66752949
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821301660.3U Active CN208963332U (en) | 2018-08-13 | 2018-08-13 | A kind of fixed-wing unmanned plane interception recovery system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208963332U (en) |
-
2018
- 2018-08-13 CN CN201821301660.3U patent/CN208963332U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104266856A (en) | Method for two-stage fairing-mounted rocket body free boundary implementation and fairing fixed-end boundary implementation in vibration tower | |
| CN109960204A (en) | Sling of suspension bridge Suo Li intelligent controlling device | |
| CN208963332U (en) | A kind of fixed-wing unmanned plane interception recovery system | |
| CN206218246U (en) | Portable full landform multi-rotor unmanned aerial vehicle landing platform | |
| CN104420656A (en) | Traction tension forming mounting method of spherical rib annular type cable dome structure | |
| CN107069533B (en) | A kind of super UHV Overhead Transmission Line tangent tower ground wire lifting tool | |
| CN108945513B (en) | Movable helicopter mooring hovering test device | |
| CN209389677U (en) | A kind of rolling small lightning arrester for communication tower | |
| CN205349623U (en) | A device that is used for changing fan gear box in air | |
| CN208516764U (en) | A kind of protection hanging basket for photovoltaic module distribution, lifting | |
| CN107069535B (en) | A kind of high-altitude coaster sets up component | |
| CN207346969U (en) | Fan blade, which is put down, hangs and replaces suspender | |
| CN205346645U (en) | A device that is used for changing fan gear box fast axis in air | |
| CN201358764Y (en) | Balance weight structure of vertical oil extractor | |
| CN208548847U (en) | It is a kind of to facilitate installation and the frequency converter with shock-absorbing function | |
| CN208748517U (en) | A kind of bridge cable device for expelling ice and snow | |
| CN203589426U (en) | Lifting device for mounting grounding wire hanging hook | |
| CN208258871U (en) | A kind of vision wind-force bird repellent instrument | |
| CN208228188U (en) | A kind of easy-to-mount electric power scarer | |
| CN204675624U (en) | Falling tup machine suspension hook automatic decoupling device | |
| CN205654064U (en) | Aerial work platform of extra -high voltage framework | |
| CN206412695U (en) | A kind of high-altitude coaster | |
| CN203549313U (en) | Wind resistance support of high-altitude test robot | |
| CN203983858U (en) | A kind of UHV transmission line steel tower cross-arm aerial ladder | |
| CN206169975U (en) | Fan wheel demolishs device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP02 | Change in the address of a patent holder | ||
| CP02 | Change in the address of a patent holder |
Address after: Room 102, floor 1, 3 workshop, No. 6898, Zhuhai Avenue, Hongqi Town, Jinwan District, Zhuhai City, Guangdong Province Patentee after: ZHUHAI TIANQING AEROSPACE TECHNOLOGY Co.,Ltd. Address before: 519000 Guangdong Province, Zhuhai city planning exhibition hall on the third floor of the aviation city Jinwan District 312-30 room Patentee before: ZHUHAI TIANQING AEROSPACE TECHNOLOGY Co.,Ltd. |