CN107298184A - A kind of protection type unmanned plane draw off gear - Google Patents
A kind of protection type unmanned plane draw off gear Download PDFInfo
- Publication number
- CN107298184A CN107298184A CN201710470582.3A CN201710470582A CN107298184A CN 107298184 A CN107298184 A CN 107298184A CN 201710470582 A CN201710470582 A CN 201710470582A CN 107298184 A CN107298184 A CN 107298184A
- Authority
- CN
- China
- Prior art keywords
- draw
- gear
- unmanned plane
- protective plate
- groove
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F3/00—Ground installations specially adapted for captive aircraft
- B64F3/02—Ground installations specially adapted for captive aircraft with means for supplying electricity to aircraft during flight
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Studio Devices (AREA)
Abstract
The invention discloses a kind of protection type unmanned plane draw off gear, for being tethered at unmanned plane, the device includes chassis, draw off gear base, draw off gear, protective cover unit, draw off gear base is located above chassis and can be with respect to chassis rotary motion, protective cover unit is fixed on draw off gear base, draw off gear is fixed on draw off gear base and inside protective cover unit, the protective cover unit includes the side plate of its side and the protective plate of upside, and the protective plate is provided with for being tethered at groove or through hole that the tether cable of unmanned plane is passed.The present invention is protected for draw off gear, can be applied to various complicated, improves the reliability and security for being tethered at unmanned plane retractable operation.
Description
Technical field
The invention belongs to the draw off gear in unmanned plane field, more particularly to unmanned plane.
Background technology
Unmanned plane, is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself, its is excellent
Point is, novel, manufacture simple in construction and all relatively low and flying quality is good with cost.In recent years, the army of occurring gradually over is used to
And civilian association area.But as the field of its application is more and more wider, its shortcoming is also gradually highlighted, that is, is battery powered
Its structure size is limited, causes payload small and can not long time continuous working.
It is that unmanned plane and tether cable are combined into realization to be tethered at unmanned plane, is tethered at unmanned plane and is passed by tether cable
Transmission of electricity can, its structure size, making material can be designed according to application demand will not be by larger limitation, and mobility
By force.It is tethered at unmanned plane and is mainly used in continual aerial monitoring and emergency communication for a long time, special visible ray can be carried and taken the photograph
Camera and infrared thermography, can also carry special emergency communication trunking.Therefore, be tethered at unmanned plane fire-fighting, military affairs,
Multiple professional domain extensive uses such as oil, ocean, mapping and traffic.It is tethered at when unmanned plane is flown and landed, it is necessary to right
Unmanned plane carries out the cooperation of the draw off gear of folding and unfolding cable operational.
In the wild, it may appear that the various complicated such as wind, sand, rain, snow, prior art is to being tethered at the draw off gear of unmanned plane
Lack protection, it is low to directly result in draw off gear reliability affected by environment, is difficult to be tethered at the fast of unmanned plane in emergency
Speed is reclaimed, and influences security.
The content of the invention
The present invention makes improvements for existing technical problem, i.e., the technical problems to be solved by the invention are to provide protection type
Unmanned plane draw off gear, solves the low deficiency of existing unmanned plane device context bad adaptability, reliability.
To solve the above problems, the invention provides a kind of protection type unmanned plane draw off gear, for being tethered at unmanned plane, bag
Chassis, draw off gear base, draw off gear, protective cover unit are included, draw off gear base is located above chassis and can be with respect to chassis
Rotary motion, protective cover unit is fixed on draw off gear base, and draw off gear is fixed on draw off gear base and positioned at anti-
Inside shield unit, the protective cover unit includes the side plate of its side and the protective plate of upside, and the protective plate is provided with for being
Stay groove or through hole that the tether cable of unmanned plane is passed.
Further, the protective plate is that drawing and pulling type is connected with protective cover side plate, groove direction and draw off gear on protective plate
The direction of winding displacement is consistent.
Further, protective plate lower end is also equipped with two reels, and reel is located at the both sides of groove, and the axis direction of reel
It is parallel with groove.
Further, protective plate upper surface is also flexibly connected one piece of groove protective plate, and the groove protective plate covers groove simultaneously
Along groove direction and protective plate be additionally provided with the through hole passed for tether cable on relative motion, the protective plate.
Further, two fixed blocks positioned at draw off gear both sides, the energy of two fixed block 21 are provided with draw off gear base
Slide, and draw off gear is fixed on draw off gear base in enough directions along away from or close to draw off gear.
Compared with prior art, the invention has the advantages that：
Realize the sealing in existing each orientation for being tethered at unmanned plane, effectively it protected, it is to avoid its by
The influence of surrounding enviroment, improves the reliability and security of draw off gear.
Brief description of the drawings
Fig. 1 is the front view of the present invention；
Fig. 2 is the top view of protective plate and groove protective plate.
Embodiment
Describe to be used to disclose the present invention below so that those skilled in the art can realize the present invention.It is excellent in describing below
Embodiment is selected to be only used as citing, it may occur to persons skilled in the art that other obvious modifications.
As depicted in figs. 1 and 2, the protection type unmanned plane draw off gear in the present embodiment includes chassis 10, draw off gear bottom
Seat 20, draw off gear 30, protective cover unit 40.Draw off gear base 20 is located at the top of chassis 10 and lived by bearing with chassis 10
Dynamic connection, draw off gear base 20 can be rotated in the horizontal plane relative to chassis.Draw off gear 30 is fixed on draw off gear chassis
On.Draw off gear 30 and one closing space of composition of protective cover unit 40 positioned at the top of draw off gear 30, are pointed to the space
Internal draw off gear 30 is protected.Protective cover unit 40 includes its left, right, front and rear, the side plate 42 of side and the protection of upside
Plate 41.Protective plate 41 carries out drawing and pulling type with protective cover side plate 42 and is connected, i.e., protective plate front and rear pull can be moved in the horizontal plane, real
The opening of existing protective cover unit 40 and closing.The left and right sides of protective plate 41 is provided with sealing strip, to preferably with protective cover
The better seal of side plate 42 coordinates.Under normal operating conditions, protective cover unit 40 is in closed state, is protected.As in it
Portion's protective plate, which breaks down, need to carry out maintenance and repair, and protective cover unit 40 is in open mode.
Protective plate 41 is provided with groove 44, is stretched out for the tether cable for being tethered at unmanned plane from protective cover unit 40.It is existing
Winding displacement need to be carried out to tether cable by being tethered at the draw off gear 30 of unmanned plane.Due to needing to carry out winding displacement operation, therefore tether cable is simultaneously
The non-fixed position along draw off gear 30 is stretched out from below, and tether cable certainly will be caused to be produced with the groove 44 on protective plate 41
Interference, influences to damage tether cable under folding and unfolding effect, serious conditions, causes security incident.In the present embodiment, the direction of groove 44
It is consistent with the direction of draw off gear winding displacement.The length of groove is the length of the line storage wheel of draw off gear with the distance of draw off gear winding displacement
Degree matches.
Further, the lower end of protective plate 41 is also equipped with two reels 50, and reel is located at the both sides of groove 44, and the axle of reel
Line direction is parallel with groove.Reel 50 can choose to install around its axis direction.By installing two reels 50, it can further limit and be
Stay the contact of hawser and protective plate 41, it is to avoid the scraping of hawser.
Further, also it is flexibly connected one piece of groove protective plate 43 in the top of protective plate 41, the groove protective plate 43 can be along logical
Groove direction carries out relative motion with protective plate 41, and groove protective plate 43 covers groove 44, and is also set on the groove protective plate 43
There is the through hole passed for tether cable.By this way, further whole protective cover unit 40 can be protected, it is to avoid logical
The ill effect of sealing effectiveness difference near groove 44.
Two fixed blocks 21 positioned at the left and right sides of draw off gear 30, two fixed blocks 21 are provided with draw off gear base 20
It can be slided along the direction away from or close to draw off gear 30.Specifically, be provided with draw off gear base 20 along
The conduit that direction away from or close to draw off gear 30 extends, through hole (not shown), bolt are provided with two fixed blocks 21
Coordinate through through hole, conduit and the nut for being arranged on the lower section of draw off gear base 20, when needing to move fixed block 21 by nut
Fixed block can be moved along groove by unscrewing, and when needing to fix draw off gear base 20, fixed block 21 is moved to suitably
Then nut is tightened in position.Also, can also be set in the front and rear sides of draw off gear base 20 same fixed block with
And conduit is draw off gear base 20 to be fixed.
General principle, principal character and the advantages of the present invention of the present invention has been shown and described above.The technology of the industry
Personnel are it should be appreciated that the present invention is not limited to the above embodiments, and that described in above-described embodiment and specification is the present invention
Principle, various changes and modifications of the present invention are possible without departing from the spirit and scope of the present invention, these change and
Improvement is both fallen within the range of claimed invention.The protection domain of application claims by appended claims and its
Equivalent is defined.
Claims (5)
1. a kind of protection type unmanned plane draw off gear, for being tethered at unmanned plane, it is characterised in that including chassis, draw off gear bottom
Seat, draw off gear, protective cover unit, draw off gear base are located above chassis and can be with respect to chassis rotary motions, protective cover list
Member is fixed on draw off gear base, and draw off gear is fixed on draw off gear base and inside protective cover unit, described
Protective cover unit includes the side plate of its side and the protective plate of upside, and the protective plate is provided with the tether cable for being tethered at unmanned plane
The groove or through hole passed.
2. according to the protection type unmanned plane draw off gear described in claim 1, it is characterised in that the protective plate and protective cover side plate
Connected for drawing and pulling type, the groove direction on protective plate is consistent with the direction of draw off gear winding displacement.
3. according to the protection type unmanned plane draw off gear described in claim 2, it is characterised in that protective plate lower end is also equipped with two
Individual reel, reel is located at the both sides of groove, and the axis direction of reel is parallel with groove.
4. according to the protection type unmanned plane draw off gear any one of claims 1 to 3, it is characterised in that on protective plate
Surface is also flexibly connected one piece of groove protective plate, and groove is covered and carries out phase with protective plate along groove direction by the groove protective plate
To motion, the through hole passed for tether cable is additionally provided with the protective plate.
5. according to the protection type unmanned plane draw off gear any one of claims 1 to 3, it is characterised in that in folding and unfolding dress
Two fixed blocks positioned at draw off gear both sides are provided with bottom set seat, two fixed blocks 21 can be filled along away from or close to folding and unfolding
The direction put is slided, and draw off gear is fixed on draw off gear base.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710470582.3A CN107298184A (en) | 2017-06-20 | 2017-06-20 | A kind of protection type unmanned plane draw off gear |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710470582.3A CN107298184A (en) | 2017-06-20 | 2017-06-20 | A kind of protection type unmanned plane draw off gear |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107298184A true CN107298184A (en) | 2017-10-27 |
Family
ID=60136380
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710470582.3A Pending CN107298184A (en) | 2017-06-20 | 2017-06-20 | A kind of protection type unmanned plane draw off gear |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107298184A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108821036A (en) * | 2018-07-02 | 2018-11-16 | 合肥瀚翔智能科技有限公司 | One kind being tethered at unmanned plane with full-automatic hawser draw off gear |
| CN108910624A (en) * | 2018-06-05 | 2018-11-30 | 中国人民解放军第六九O五工厂 | It is tethered at unmanned plane folding and unfolding line method |
| CN109179090A (en) * | 2018-11-06 | 2019-01-11 | 安徽云翼航空技术有限公司 | A kind of outdoor optical cable automatic retraction device |
| CN109748158A (en) * | 2017-11-02 | 2019-05-14 | 天津职业技术师范大学 | A kind of unmanned plane cable automatic retraction device |
| CN110304266A (en) * | 2019-07-05 | 2019-10-08 | 智飞智能装备科技东台有限公司 | A kind of captive unmanned plane ground retractable cable case |
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| CN204999444U (en) * | 2015-08-04 | 2016-01-27 | 徐州创航科技有限公司 | Automatic coiling and uncoiling device of unmanned aerial vehicle aircraft |
| CN205257856U (en) * | 2015-12-07 | 2016-05-25 | 捷胜海洋装备股份有限公司 | Row's cable device of deep sea ocean scientific investigation pulling winch |
| CN106058783A (en) * | 2016-07-06 | 2016-10-26 | 合肥通鼎光电科技有限公司 | Communication cable coiling/uncoiling system for low-altitude sensing unmanned aerial vehicle |
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| CN205932769U (en) * | 2016-08-22 | 2017-02-08 | 合肥瀚翔智能科技有限公司 | Staying unmanned aerial vehicle's automatic coiling and uncoiling device |
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| CN204999444U (en) * | 2015-08-04 | 2016-01-27 | 徐州创航科技有限公司 | Automatic coiling and uncoiling device of unmanned aerial vehicle aircraft |
| CN105217382A (en) * | 2015-10-09 | 2016-01-06 | 东莞三联热缩材料有限公司 | A kind of heat-shrinkable T bush S. A. coils machine |
| CN205257856U (en) * | 2015-12-07 | 2016-05-25 | 捷胜海洋装备股份有限公司 | Row's cable device of deep sea ocean scientific investigation pulling winch |
| CN106058783A (en) * | 2016-07-06 | 2016-10-26 | 合肥通鼎光电科技有限公司 | Communication cable coiling/uncoiling system for low-altitude sensing unmanned aerial vehicle |
| CN205863877U (en) * | 2016-07-06 | 2017-01-04 | 合肥通鼎光电科技有限公司 | A kind of low-altitude detection unmanned plane communication cable extension and retraction system |
| CN205932769U (en) * | 2016-08-22 | 2017-02-08 | 合肥瀚翔智能科技有限公司 | Staying unmanned aerial vehicle's automatic coiling and uncoiling device |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109748158A (en) * | 2017-11-02 | 2019-05-14 | 天津职业技术师范大学 | A kind of unmanned plane cable automatic retraction device |
| CN108910624A (en) * | 2018-06-05 | 2018-11-30 | 中国人民解放军第六九O五工厂 | It is tethered at unmanned plane folding and unfolding line method |
| CN108821036A (en) * | 2018-07-02 | 2018-11-16 | 合肥瀚翔智能科技有限公司 | One kind being tethered at unmanned plane with full-automatic hawser draw off gear |
| CN109179090A (en) * | 2018-11-06 | 2019-01-11 | 安徽云翼航空技术有限公司 | A kind of outdoor optical cable automatic retraction device |
| CN110304266A (en) * | 2019-07-05 | 2019-10-08 | 智飞智能装备科技东台有限公司 | A kind of captive unmanned plane ground retractable cable case |
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|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20171027 |