CN104097787B - Mooring grille, onboard mooring mast and quick mooring device - Google Patents
Mooring grille, onboard mooring mast and quick mooring device Download PDFInfo
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- CN104097787B CN104097787B CN201410352874.3A CN201410352874A CN104097787B CN 104097787 B CN104097787 B CN 104097787B CN 201410352874 A CN201410352874 A CN 201410352874A CN 104097787 B CN104097787 B CN 104097787B
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- mooring
- tethered
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- 230000001413 cellular effect Effects 0.000 claims description 9
- 230000007306 turnover Effects 0.000 claims description 9
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 4
- 238000013519 translation Methods 0.000 claims description 2
- 230000000875 corresponding effect Effects 0.000 description 7
- 238000003780 insertion Methods 0.000 description 5
- 230000037431 insertion Effects 0.000 description 5
- 241001466460 Alveolata Species 0.000 description 2
- 230000009471 action Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000004083 survival effect Effects 0.000 description 1
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Abstract
An embodiment of the invention discloses a mooring grille, an onboard mooring mast and a quick mooring device. The quick mooring device comprises the onboard mooring mast and the mooring grille. The onboard mooring mast comprises a connecting device, an elastic rod and a ball, wherein the connecting device is used for mounting the onboard mooring mast on a mounting base of an unmanned aerial vehicle. The mooring grille comprises an upper grille plate, a lower grille plate, a support and a driving component, wherein the upper grille plate is fixed on the support, the lower grille plate is arranged below the upper grille plate, the upper grille plate is provided with a plurality of leading-in holes, and the lower grille plate is provided with a plurality of clamping holes; when the mooring grille is in a first working state, the driving component drives the lower grille plate to run, and the leading-in holes and the clamping holes form channels meeting the requirements on entering and exiting of the onboard mooring mast; when the mooring grille is in a second working state, the driving component drives the lower grille plate to run, and the leading-in holes and the clamping holes clamp the onboard mooring mast to enable the same not to be pulled out.
Description
Technical field
The present invention relates to airborne vehicle technical field, more particularly, it relates to one kind is tethered at grid, airborne mooring mast and fast
Fast mooring device.
Background technology
Mooring device includes airborne mooring mast and is tethered at grid.Wherein, airborne mooring mast is arranged on unmanned plane, and is tethered at
Grid is arranged on flight-deck (airplane parking area or the platform being capable of unmanned plane shutdown).Mooring device rises for unmanned plane
Fall is most important, this device can make that unmanned plane is quick, safety warship (land) it is reliably fixing.
At present, the mooring mast that mooring device adopts is expansion link, and the head of mooring mast is provided with fork-shaped latch-up structure.Unmanned
When warship (land), mooring mast insertion is tethered at grid locking to machine, is produced with avoiding unmanned plane and break away and topple during warship；Unmanned plane
When taking off, this device ensures that unmanned plane reaches maximum lift, and ensures to discharge unmanned plane under the conditions of survival wind speed, wind direction,
To ensure that it safely leaves warship (land) area.
But, using above-mentioned be tethered at mode when, the main fork-shaped latch-up structure passing through on operation mooring mast completes unmanned plane
Be tethered at.Therefore, the design requirement of mooring mast is higher, needs to complete " stretch out-lock " and " unblock-retract " action supporting phase
The driving answered and control device.This technical scheme, increased the complexity of unmanned plane, reduces the reliability of unmanned plane.In addition,
The volume of mooring mast is relatively large, and action is complicated, and weight is also larger, thus decreasing the payload of unmanned plane.
Therefore, how to increase the payload of unmanned plane, raising unmanned plane safety and reliability during warship (land), become
For those skilled in the art's technical problem urgently to be resolved hurrily.
Content of the invention
In view of this, first purpose of the present invention is to provide one kind to be tethered at grid, to improve the security of unmanned plane
And reliability, increase the payload of unmanned plane；Second object of the present invention is to provide a kind of airborne mooring mast；The present invention
The 3rd purpose be to provide a kind of quick mooring device.
For realizing above-mentioned first purpose, the present invention following technical scheme of offer:
One kind is tethered at grid, and the described grid that is tethered at includes upper grid plate, lower grid plate, support and drive component.Its
In, described upper grid plate is fixing on the bracket, and described lower grid plate is arranged on the lower section of described upper grid plate；Institute
State upper grid plate and be provided with multiple entrance holes, described entrance hole is in cellular arrangement, the aperture of described entrance hole is along near institute
The direction stating lower grid plate tapers into；It is provided with multiple hole clippings on described lower grid plate.When being in the first working condition
When, described drive component drives described lower grid plate to run, and forms the spheroid turnover requirement meeting described airborne mooring mast
Passage；When being in the second working condition, described drive component drives described lower grid plate to run, by described airborne mooring mast
Spheroid be stuck in described hole clipping.
Preferably, in above-mentioned mooring device, between described lower grid plate and described support, be provided with guide rail, described under
Portion's flase floor can move on described guide rail, and the linear motion output end of described drive component is connected simultaneously with described lower grid plate
Drive described lower grid plate translation；When being in the first working condition, described entrance hole is formed completely with corresponding described hole clipping
The passage that the spheroid turnover of the airborne mooring mast of foot requires；When being in the second working condition, described entrance hole and corresponding described card
The spheroid of described airborne mooring mast can be stuck in described hole clipping for hole.
Preferably, in above-mentioned mooring device, described hole clipping is in cellular arrangement, and its aperture is along away from described upper grid
The direction of plate becomes larger.
Preferably, in above-mentioned mooring device, described hole clipping is in cellular arrangement, and described hole clipping is straight hole.
Preferably, in above-mentioned mooring device, when being in the first working condition, described lower grid plate is in described driving
Under the driving of assembly, the aperture of described hole clipping is variable big；When being in the second working condition, described lower grid plate is in described drive
Under the driving of dynamic assembly, the aperture of described hole clipping can diminish.
Preferably, in above-mentioned mooring device, described drive component is cylinder, hydraulic cylinder or electric cylinder.
When unmanned plane warship (land), this is tethered at grid and is in the first working condition, is provided with the mooring mast insertion of spheroid
In entrance hole, the spheroid of airborne mooring mast passes through passage, enters in hole clipping, now this mooring device switches to the second work shape
State, the spheroid of airborne mooring mast is stuck in corresponding hole clipping for hole clipping motion, completes being tethered at of unmanned plane；When unmanned plane takes off
When, this mooring device switches to the first working condition by the second working condition, and entrance hole meets spheroid turnover with hole clipping formation will
The passage asked, airborne mooring mast is extracted in the presence of unmanned plane lift from honeycomb hole, thus realizing letting fly away of unmanned plane.By
In using the mooring device in the present invention, the cooperation of upper grid plate and lower grid plate can complete the fixation of airborne mooring mast
With release, therefore, relatively low for the requirement of the airborne mooring mast being arranged on unmanned plane using the mooring device in the present invention, be
Stay the function phase of bar to single, structure is simple, thus improve the reliability of unmanned plane, increased the payload of unmanned plane.
Second object of the present invention is to provide a kind of airborne mooring mast, described airborne mooring mast with including but not limited on
State the grid that is tethered at described in either a program to use cooperatively, described airborne mooring mast includes attachment means, elastic rod and spheroid；Its
In, attachment means are used for elastic rod is arranged on the pedestal of unmanned plane, and elastic rod connects spheroid and attachment means.
Third object of the present invention is to provide a kind of quick mooring device, including being tethered at grid and airborne mooring mast, institute
State airborne mooring mast and include attachment means, elastic rod and spheroid；Attachment means are used for for airborne mooring mast being arranged on unmanned plane
In installation pedestal；The described grid that is tethered at is using being tethered at grid described in any of the above-described technical scheme.
Brief description
In order to be illustrated more clearly that the embodiment of the present invention or technical scheme of the prior art, below will be to embodiment or existing
Have technology description in required use accompanying drawing be briefly described it should be apparent that, drawings in the following description be only this
Some embodiments of invention, for those of ordinary skill in the art, on the premise of not paying creative work, acceptable
Other accompanying drawings are obtained according to these accompanying drawings.
Side-looking structural representation during a kind of the first working condition of mooring device that Fig. 1 is provided by the embodiment of the present invention
Figure；
Side-looking structural representation during a kind of the second working condition of mooring device that Fig. 2 is provided by the embodiment of the present invention
Figure；
Side-looking structural representation during the first working condition of the second mooring device that Fig. 3 is provided by the embodiment of the present invention
Figure；
Side-looking structural representation during the second working condition of the second mooring device that Fig. 4 is provided by the embodiment of the present invention
Figure；
Side-looking structural representation during the first working condition of the third mooring device that Fig. 5 is provided by the embodiment of the present invention
Figure；
Side-looking structural representation during the second working condition of the third mooring device that Fig. 6 is provided by the embodiment of the present invention
Figure；
A kind of overlooking the structure diagram of upper grid plate that Fig. 7 is provided by the embodiment of the present invention；
The overlooking the structure diagram of another kind of upper grid plate that Fig. 8 is provided by the embodiment of the present invention.
Wherein: 1 is unmanned plane, 211 is support, 212 is guide rail, 213 is upper grid plate, 214 is lower grid plate,
215 is entrance hole, 216 is hole clipping, 217 is driving means, 221 is elastic rod, 222 is spheroid, 223 is attachment means, 3 is first
Plate (airplane parking area).
Specific embodiment
For this reason, first core of the present invention is open one kind is tethered at grid, with improve the security of unmanned plane, reliability and
For the purpose of increasing the effective mission payload of unmanned plane；Second core of the present invention is to disclose a kind of airborne mooring mast；The present invention the 3rd
Individual core is to disclose a kind of quick mooring device.Hereinafter, referring to the drawings embodiment is illustrated.Additionally, reality shown below
Apply example and any restriction effect is not played to the content of the invention described in claim.In addition, composition represented by example below
Full content is not limited to as necessary to the solution of the invention described in claim.
As shown in Figures 1 to 8, it is tethered at grid to include upper grid plate 213, lower grid plate 214, support 211 and drive
Assembly 217；Wherein, upper grid plate 213 is fixed on support 211, and lower grid plate 214 is arranged on upper grid plate 213
Lower section；Upper grid plate 213 is provided with multiple entrance holes 215, and entrance hole 215 is in cellular arrangement；The aperture edge of entrance hole 215
Direction near lower grid plate 214 tapers into；Lower grid plate 214 is provided with multiple hole clippings 216.When being in the first work
During state, drive component drives lower grid plate 214 to run, and is formed and meets the passage that spheroid 222 turnover requires；When being in second
During working condition, drive component drives lower grid plate 214 to run, and spheroid 222 is stuck in hole clipping 216.
When unmanned plane warship (land), this is tethered at grid and is in the first working condition, and the mooring mast being provided with spheroid 222 is inserted
Enter in any entrance hole 215, the spheroid 222 of airborne mooring mast enters in hole clipping 216 by passage, now this mooring device switching
To the second working condition, the spheroid 222 of airborne mooring mast is stuck in corresponding hole clipping 216, completes being tethered at of unmanned plane；When unmanned
When machine takes off, this mooring device switches to the first working condition by the second working condition, and entrance hole 215 and hole clipping 216 form full
The passage that spheroid 222 turnover of the airborne mooring mast of foot requires, airborne mooring mast, in the presence of unmanned plane lift, is tethered at airborne
The spheroid 222 of bar is extracted from honeycomb hole, it is achieved thereby that the letting fly away of unmanned plane.Due to using the mooring device in the present invention,
Lower grid plate 214 can complete being tethered at of mooring mast, therefore, using the mooring device in the present invention for being arranged on unmanned plane
On mooring mast requirement relatively low, to single, structure is simple for the function phase of mooring mast, thus improve the reliability of unmanned plane,
Increased the payload of unmanned plane.
In one embodiment of the present of invention, lower grid plate 214 and support 211 are provided with guide rail 212, lower grid plate
214 are slidably disposed on guide rail 212, and the linear motion output end of drive component is connected with lower grid plate 214 and drives
Described lower grid plate 214 translates；When being in the first working condition, entrance hole 215 is formed with corresponding hole clipping 216 and meets machine
Carry the passage that spheroid 222 turnover of mooring mast requires；When being in the second working condition, hole clipping 216 is moved airborne mooring mast
Spheroid 222 be stuck in hole clipping 216.
In embodiments of the present invention, arrangement on upper grid plate 213 for the entrance hole 215 have multiple, for example be in square
Configuration arrangement, cellular arrangement.As shown in fig. 7, entrance hole 215 is cellular in the arrangement form of upper grid plate 213.Its
In, the projection of shape of entrance hole 215 is regular polygon or circle, and the aperture of entrance hole 215 is along away from lower grid plate 214
Direction become larger (hole that can be understood as entrance hole 215 tapers into) radially adjacent to the direction of lower grid plate 214, such as
This setting ensure that in any entrance hole of spheroid 222 radom insertion on mooring mast.As shown in figure 8, entrance hole 215 is in matrix
Structure is arranged, and the aperture of entrance hole 215 tapers into along the direction near lower grid plate 214 and (can be understood as entrance hole
215 aperture becomes larger along the direction away from lower grid plate 214), it is arranged such the spheroid that ensure that on mooring mast
In any entrance hole of 222 radom insertions.
The arrangement of hole clipping 216 of lower grid plate 214 and the arrangement of the entrance hole 215 of upper grid plate 213
Identical；When the entrance hole 215 of upper grid plate 213 is arranged for matrix structure, the hole clipping 216 of lower grid plate 214 corresponds to square
Battle array shape structure arrangement.When the entrance hole 215 of upper grid plate 213 is arranged for alveolate texture, the hole clipping of lower grid plate 214
216 corresponding alveolate texture arrangements, the cross sectional shape of hole clipping 216 is circle.It is arranged so that spheroid 222 insertion is tethered at grid
Probability greatly increase.
The aperture of the hole clipping 216 of middle and lower part of the present invention flase floor 214 gradually becomes along the direction away from upper grid plate 213
Greatly, as depicted in figs. 1 and 2.That is, the entrance hole 215 of upper grid plate 213 is bellmouth (or approximate bellmouth),
And the hole clipping 216 of lower grid plate 214 is reverse taper hole (or approximate reverse taper hole).When being in the first working condition, ball
When body 222 enters to hole clipping 216 by entrance hole 215, because the aperture of hole clipping 216 is along the direction away from upper grid plate 213
Become larger, therefore, the hole wall of hole clipping 216 acts on the power less (or no active force) of spheroid 222；When being in the second work shape
During state, spheroid 222 is located in hole clipping 216, and hole clipping 216 forms wedge structure with spheroid 222, and therefore spheroid 222 moves downward
Trend, thus further strain unmanned plane.
Or, the aperture of the hole clipping 216 of middle and lower part of the present invention flase floor 214 is constant, be straight hole as shown in Figure 3 to Figure 4.
In still another embodiment of the process, lower grid plate 214 is to have independent, the clip-bore device of variable-diameter, such as
Shown in Fig. 5 and Fig. 6, wherein, the axis of hole clipping 216 is alignd with the axis of entrance hole 215, and each hole clipping 216 is set by multiple inclinations
The clamp put constitutes an incomplete bellmouth, and multiple clamp is under the drive of drive component, to close to each other or phase
Mutually away from direction move, the movement close to each other of multiple clamps is so that the aperture of hole clipping 216 tapers into；It is located remotely from each other
Direction is moved so that the aperture of hole clipping 216 becomes larger, so that hole clipping 216 is formed under the cooperation of entrance hole 215 blocking
The screens of spheroid 222 and the passage of spheroid turnover.
Drive component is the actuating unit that can export desired movement, for example, cylinder, hydraulic cylinder, electric cylinder, straight-line electric
Machine etc., the embodiment of the present invention is not limited only to above-mentioned form.
Act on resistance on unmanned plane in order to reduce unmanned plane this mooring device in takeoff condition, when being in the first work
When making state, on both composition surfaces, the diameter of hole clipping 216 should be equal to entrance hole 215 diameter for entrance hole 215 and hole clipping 216；
When being in the second working condition, on both composition surfaces, the diameter of hole clipping 216 should be less than ball for entrance hole 215 and hole clipping 216
The maximum gauge of body 222.
The invention also discloses a kind of airborne mooring mast, this mooring mast and including but not limited to any of the above-described technical scheme institute
The grid that is tethered at stated uses cooperatively, and this airborne mooring mast includes attachment means 223, elastic rod 221 and spheroid 222；Wherein, connect
Device 223 is used for elastic rod is arranged on the installation pedestal of unmanned plane, and elastic rod 221 connects spheroid 222 and attachment means
223.Airborne mooring mast using present configuration can significantly reduce the weight of unmanned plane, therefore, it can accordingly improve no
Man-machine payload.
The invention also discloses a kind of quick mooring device, including being tethered at grid and airborne mooring mast, wherein, it is tethered at grid
Being arranged on unmanned plane can be able to be for example deck 3, high building, automobile, train etc. with the place of take-off and landing.Wherein, it is tethered at lattice
Grid are the grid that is tethered at described in any of the above-described technical scheme, and described airborne mooring mast is airborne described in any of the above-described technical scheme
Mooring mast.It is tethered at grid due to above-mentioned and airborne mooring mast has the effect above, the quick mooring device in the embodiment of the present invention
Also there is corresponding effect, here is omitted.
Described above to the disclosed embodiments, makes professional and technical personnel in the field be capable of or uses the present invention.
Multiple modifications to these embodiments will be apparent from for those skilled in the art, as defined herein
General Principle can be realized without departing from the spirit or scope of the present invention in other embodiments.Therefore, the present invention
It is not intended to be limited to the embodiments shown herein, and be to fit to and principles disclosed herein and features of novelty phase one
The scope the widest causing.
Claims (9)
1. one kind is tethered at grid it is characterised in that the described grid that is tethered at includes upper grid plate, lower grid plate, support and drive
Dynamic assembly；Wherein, described upper grid plate is fixing on the bracket, and described lower grid plate is arranged on described upper grid plate
Lower section；Described upper grid plate is provided with multiple entrance holes, and described entrance hole is in cellular arrangement, the aperture of described entrance hole
Taper in the direction near described lower grid plate；Described lower grid plate is provided with multiple hole clippings, when being in the first work
When making state, described drive component drives described lower grid plate to run, and forms the spheroid turnover requirement meeting airborne mooring mast
Passage；When being in the second working condition, described drive component drives described lower grid plate to run, and airborne is tethered at described
The spheroid of bar is stuck in described hole clipping.
2. it is tethered at grid as claimed in claim 1 it is characterised in that being provided between described lower grid plate and described support
Guide rail, described lower grid plate can move on described guide rail, and described drive component is connected and drives with described lower grid plate
Described lower grid plate translation；When being in the first working condition, described entrance hole is formed with corresponding described hole clipping and meets machine
Carry the passage that the spheroid turnover of mooring mast requires；When being in the second working condition, described entrance hole will with corresponding described hole clipping
The spheroid of described airborne mooring mast is stuck in described hole clipping.
3. be tethered at grid as claimed in claim 2 it is characterised in that described hole clipping is in cellular arrangement, its aperture along away from
The direction of described upper grid plate becomes larger.
4. it is tethered at grid as claimed in claim 2 it is characterised in that described hole clipping is in cellular arrangement, described hole clipping is straight
Hole.
5. be tethered at grid as claimed in claim 4 it is characterised in that described hole clipping and described entrance hole contact surface diameter
Equal.
6. it is tethered at grid as claimed in claim 5 it is characterised in that described drive component adopts cylinder or hydraulic cylinder or electronic
Relative motion realized by cylinder.
7. it is tethered at grid as claimed in claim 1 it is characterised in that when being in the first working condition, described lower grid
Under the driving of described drive component, the aperture of described hole clipping becomes big to plate, when being in the second working condition, described lower grid
Under the driving of described drive component, the aperture of described hole clipping diminishes plate.
8. a kind of airborne mooring mast is it is characterised in that be tethered at lattice any one of this airborne mooring mast and claim 1-7
Grid use cooperatively, and described airborne mooring mast includes attachment means, elastic rod and spheroid；Wherein, attachment means are used for elastic rod
It is arranged on the pedestal of unmanned plane, elastic rod connects spheroid and attachment means.
9. a kind of quick mooring device, including be tethered at grid and airborne mooring mast it is characterised in that described be tethered at grid be right
Require 1 to 7 any one of be tethered at grid, described airborne mooring mast be airborne mooring mast described in claim 8.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410352874.3A CN104097787B (en) | 2014-07-24 | 2014-07-24 | Mooring grille, onboard mooring mast and quick mooring device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410352874.3A CN104097787B (en) | 2014-07-24 | 2014-07-24 | Mooring grille, onboard mooring mast and quick mooring device |
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| Publication Number | Publication Date |
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| CN104097787A CN104097787A (en) | 2014-10-15 |
| CN104097787B true CN104097787B (en) | 2017-01-18 |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN104527993A (en) * | 2014-12-31 | 2015-04-22 | 郑州德莱孚科技有限公司 | Grating cover plate fixing device |
| CN109592023B (en) * | 2016-07-05 | 2022-01-07 | 王晓飞 | Intelligent unmanned aerial vehicle capable of realizing remote control communication and working method thereof |
| CN106184799B (en) * | 2016-07-25 | 2018-02-23 | 中国人民解放军总参谋部第六十研究所 | A kind of carrier-borne depopulated helicopter harpoon system |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN103332295A (en) * | 2013-06-27 | 2013-10-02 | 厦门天圣能源科技有限公司 | Novel helicopter carrier landing system |
| CN103942085B (en) * | 2013-12-31 | 2017-06-23 | 中国人民解放军空军航空大学军事仿真技术研究所 | A kind of carrier-based helicopter flight simulator warship emulation mode |
| CN203996922U (en) * | 2014-07-24 | 2014-12-10 | 郑州德莱孚科技有限公司 | A kind of mooring grid, airborne mooring mast and quick mooring gear |
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Inventor after: Meng Qiang Inventor after: Liu Donglei Inventor after: Tao Shili Inventor after: Zhou Liang Inventor before: Meng Qiang Inventor before: Liu Donglei Inventor before: Zhou Liang |
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