CN207466993U - Clamping device and the base station with clamping device and UAV system - Google Patents
Clamping device and the base station with clamping device and UAV system Download PDFInfo
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- CN207466993U CN207466993U CN201721418632.5U CN201721418632U CN207466993U CN 207466993 U CN207466993 U CN 207466993U CN 201721418632 U CN201721418632 U CN 201721418632U CN 207466993 U CN207466993 U CN 207466993U
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- clamping section
- unmanned plane
- landing platform
- inclined plate
- base station
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- 230000007246 mechanism Effects 0.000 claims abstract description 45
- 230000007704 transition Effects 0.000 claims description 15
- 230000005540 biological transmission Effects 0.000 claims description 14
- 230000008878 coupling Effects 0.000 claims description 7
- 238000010168 coupling process Methods 0.000 claims description 7
- 238000005859 coupling reaction Methods 0.000 claims description 7
- 238000005452 bending Methods 0.000 claims description 3
- 238000003825 pressing Methods 0.000 abstract description 3
- 230000007423 decrease Effects 0.000 description 5
- 239000000463 material Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000002093 peripheral effect Effects 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000000903 blocking effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 238000007790 scraping Methods 0.000 description 1
- 239000007779 soft material Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/12—Ground or aircraft-carrier-deck installations for anchoring aircraft
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Accommodation For Nursing Or Treatment Tables (AREA)
- Studio Devices (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model provides a kind of clamping device and the base station with clamping device and UAV system, the UAV system includes unmanned plane (700) and base station, base station is included for carrying the landing platform (100) of unmanned plane and clamping device (200), and clamping device includes clamping section (1) and the driving mechanism (2) being drivingly connected with clamping section；Driving mechanism can drive clamping section to be moved relative to landing platform, so that clamping section is optionally in retracted state or opening state；When unmanned plane is carried on the designated position on landing platform, driving mechanism (2) drives clamping section to be moved to opening state relative to landing platform, and clamping section is used to the foot stool of unmanned plane being pressed on landing platform；When driving mechanism driving clamping section is moved to retracted state relative to landing platform, clamping section is used to unclamp foot stool.Fix the foot stool of unmanned plane automatically by pressing device, it is simple in structure, it is easy to operate.
Description
Technical field
The utility model is related to unmanned plane positioning field more particularly to a kind of clamping device and with clamping device base station
And UAV system.
Background technology
With the development of computer vision technique, unmanned plane technology of landing automatically is also greatly improved.Unmanned plane
Scheduled drop zone can be drop under the guiding for the machine vision sensor being provided thereon.
At present, it after unmanned plane drops to the drop zone of base station, needs further to fix unmanned plane, thus by unmanned plane
The a certain designated position in drop zone is maintained, prevents unmanned plane from moving, is grasped in next step so as to be conducive to perform unmanned plane
Make, for example, performing charging operations to unmanned plane.
Utility model content
The utility model provides a kind of clamping device and the base station with clamping device and UAV system.
Specifically, the utility model is achieved by the following technical solution：
It is according to the present utility model in a first aspect, provide a kind of clamping device, it is described for unmanned plane to be fixed to base station
Base station includes the landing platform for carrying unmanned plane, and the clamping device includes clamping section and drive with the clamping section to connect
The driving mechanism connect；Wherein, the driving mechanism can drive the clamping section to be moved relative to the landing platform, so that institute
It states clamping section and is optionally in retracted state or opening state；When the unmanned plane is carried on the finger on the landing platform
When positioning is put, the driving mechanism drives the clamping section to be moved to the opening state relative to the landing platform, described
Clamping section is used to the foot stool of the unmanned plane being pressed on the landing platform；When the driving mechanism drives the clamping section
When being moved to the retracted state relative to the landing platform, the clamping section is used to unclamp the foot stool.
Optionally, further include transmission mechanism, described transmission mechanism one end is drivingly connected with the driving mechanism, the other end with
The clamping section connection；The driving mechanism rotation, drives the transmission mechanism to push the clamping section relative to the landing
Platform moves.
Optionally, what the transmission mechanism included being connected with the driving mechanism pushes part and connecting rod, the connecting rod
One end pushes part described in abutting, and the other end connects the clamping section；When the driving mechanism rotates, the part that pushes pushes institute
Connecting rod is stated, to drive the clamping section that foot stool pressure is set on the landing platform.
Optionally, for the part that pushes for cam, the main shaft of the driving mechanism connects the cam through a shaft coupling.
Optionally, the connecting rod is double leval jib, opposite including first connecting rod and with the first connecting rod and the second company for setting
Bar；The part that pushes is connected to side of the first connecting rod far from the second connecting rod, and the clamping section is connected to described four
Side far from the first connecting rod on connecting rod.
Second aspect according to the present utility model provides a kind of base station, the landing platform including being used to carry unmanned plane, also
Including above-mentioned clamping device.
Optionally, it further includes on the landing platform and two the first inclined plates that are opposite and setting；When the unmanned plane
During the designated position being carried on the landing platform, two first inclined plates are connected to the both sides of the foot stool respectively.
Optionally, the second inclined plate on the landing platform is further included, wherein, second inclined plate is set on two institutes
The same side of the first inclined plate is stated, two first inclined plates and second inclined plate enclose the landing platform to set to form a landing
Region, and the direction that two first inclined plates and second inclined plate are directed away from the landing platform is gradually opened；It is described
Designated position is located at the drop zone, when the unmanned plane is carried on the drop zone and towards the side of second inclined plate
To when sliding to the designated position, two first inclined plates are connected on the foot stool and are parallel to the two of line of travel respectively
Side, second inclined plate are connected to the other side on the foot stool on line of travel.
Optionally, the clamping device is two, and two first inclined plates are respectively equipped with accommodating groove, two clampings
Device and two accommodating groove corresponding matchings；When the clamping section is moved to the retracted state relative to the landing platform
When, the clamping section is housed in corresponding accommodating groove and coplanar with corresponding first inclined plate；When the unmanned plane is carried on institute
When stating designated position, the clamping section is moved to the opening state relative to the landing platform, and the clamping section is by corresponding to
Accommodating groove stretch out and the foot stool is pressed on the landing platform.
Optionally, the side of two described first inclined plate the same sides is connected to the both sides of second inclined plate.
Optionally, transition inclined plate is further included, the side of two described first inclined plate the same sides is oblique by the transition respectively
Plate is connected to the both sides of second inclined plate.
Optionally, it further includes that the foot stool is guided to slide to the changeover portion of the drop zone, first inclined plate
It is connected on the landing platform by a changeover portion respectively with second inclined plate.
Optionally, the side of the changeover portion towards the drop zone is arc-shaped transitional surface or bending transition face.
Optionally, the designated position is equipped with landing and identifies.
Optionally, first inclined plate is equipped with fluting.
The third aspect according to the present utility model provides a kind of UAV system, including unmanned plane, further includes above-mentioned base
It stands, wherein the unmanned plane is carried on the landing platform of the base station.
The technical solution provided by more than the utility model embodiment is as it can be seen that the utility model is pressed from both sides using driving mechanism driving
Tight portion is moved relative to landing platform so that clamping section can switch between retracted state and opening state.It on the one hand can be
When unmanned plane drops to designated position, the foot stool of unmanned plane is pressed on base station by clamping section, so as to which unmanned plane be clamped
It is fixed on designated position.On the other hand it when unmanned plane needs to leave designated position, can be compressed by operating compressed part
Unclamp the foot stool of unmanned plane in portion.Fix the foot stool of unmanned plane automatically by pressing device, it is simple in structure, it is easy to operate.
It should be understood that above general description and following detailed description are only exemplary and explanatory, not
The utility model can be limited.
Description of the drawings
It is required in being described below to embodiment 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, it should be apparent that, the accompanying drawings in the following description is only some realities of the utility model
Example is applied, it for those of ordinary skill in the art, without having to pay creative labor, can also be attached according to these
Figure obtains other attached drawings.
Fig. 1 is the clamping device stereogram on a direction wherein of one embodiment of the utility model；
Fig. 2 is stereogram of the clamping device of one embodiment of the utility model on other direction；
Fig. 3 is stereogram of the clamping device of one embodiment of the utility model on another direction；
Fig. 4 is that the structure of the clamping device of one embodiment of the utility model splits schematic diagram；
Fig. 5 is stereogram of the clamping device of one embodiment of the utility model on an also direction；
Fig. 6 is the base station stereogram on a direction wherein of one embodiment of the utility model；
Fig. 7 is stereogram of the base station of one embodiment of the utility model on other direction；
Fig. 8 is the stereogram of the UAV system of one embodiment of the utility model.
Reference numeral：
100：Landing platform；101：Drop zone；102：Perforating；
200：Clamping device；1：Clamping section；2：Driving mechanism；3：Transmission mechanism；31：Push part；32：Connecting rod；321：The
One connecting rod；322：Second connecting rod；4：Shaft coupling；5：Supporting rack；
300：First inclined plate；310：Accommodating groove；
400：Second inclined plate
500：Transition inclined plate；
600：Changeover portion；
700：Unmanned plane；710：Fuselage；720：Foot stool；721：First foot stool；722：Second foot stool.
Specific embodiment
Here exemplary embodiment will be illustrated in detail, example is illustrated in the accompanying drawings.Following description is related to
During attached drawing, unless otherwise indicated, the same numbers in different attached drawings represent the same or similar element.Following exemplary embodiment
Described in embodiment do not represent all embodiments consistent with the utility model.On the contrary, they be only with such as
The example of the consistent device and method of some aspects be described in detail in the appended claims, the utility model.
It is only merely for the purpose of description specific embodiment in the term that the utility model uses, and is not intended to be limiting this reality
With novel.In " one kind " of the utility model and singulative used in the attached claims, " described " and "the"
It is intended to include most forms, unless context clearly shows that other meanings.It is also understood that term used herein " and/
Or " refer to and any or all may be combined comprising one or more associated list items purposes.
It will be appreciated that though various information may be described using term first, second, third, etc. in the utility model,
But these information should not necessarily be limited by these terms.These terms are only used for same type of information being distinguished from each other out.For example, not
In the case of being detached from the scope of the utility model, the first information can also be referred to as the second information, and similarly, the second information can also
It is referred to as the first information.Depending on linguistic context, word as used in this " if " can be construed to " ... when " or
" when ... " or " in response to determining ".
Below in conjunction with the accompanying drawings, to the clamping device of the utility model 200 and with clamping device 200 base station and unmanned plane
System is described in detail.In the absence of conflict, the feature in following embodiment and embodiment can be combined with each other.
Embodiment one
With reference to Fig. 1 to Fig. 5, the utility model embodiment provides a kind of clamping device 200.Fig. 8, the clamping device are combined again
200 can be used for unmanned plane 700 being fixed to base station, wherein, the base station may include the landing platform for carrying unmanned plane 700
100。
Referring to Fig. 1 and Fig. 2, the clamping device 200 may include clamping section 1 and driving mechanism 2.Wherein, the driving machine
Structure 2 is drivingly connected with the clamping section 1.The driving mechanism 2 can drive the clamping section 1 relative to the landing platform
100 movements, so that the clamping section 1 is optionally in retracted state or opening state.Optionally, 1 phase of clamping section
Following two situations may include for the landing platform 100 movement：The clamping section 1 is remote relative to the landing platform 100
From so that the clamping section 1 is in retracted state；Or the clamping section 1 is close relative to the landing platform 100 so that
The clamping section 1 is in opening state.
And in practical application scenarios, the driving mechanism 2 can be driven as needed so that clamping section 1, which is in, to be withdrawn
State or opening state, to meet the needs of different.For example, in the present embodiment, when the unmanned plane 700 is carried on the landing
During designated position on platform 100, the driving mechanism 2 drives the clamping section 1 to be moved to relative to the landing platform 100
The opening state, the clamping section 1 are used to the foot stool 720 of the unmanned plane 700 being pressed on the landing platform 100,
So as to prevent unmanned plane 700 from moving.In the present embodiment, in the on-state, foot stool 720 is to be folded in clamping for the clamping section 1
Between portion 1 and landing platform 100.The pressure applied when setting the foot stool 720 for the pressure of clamping section 1 to the foot stool 720 is set
Power size can then be selected according to the firmness demand of fixed unmanned plane 700.
When the driving mechanism 2 drives the clamping section 1 to be moved to the retracted state relative to the landing platform 100
When, the clamping section 1 is used to unclamp the foot stool 720.After foot stool 720 is unclamped in clamping section 1, unmanned plane 700 can be flat from landing
Platform 100 is flown away from.
In the utility model embodiment, clamping section 1 is driven to be moved relative to landing platform 100 using automatic mode, made
Clamping section 1 is obtained between retracted state and opening state to switch.On the one hand can when unmanned plane 700 drops to designated position,
The foot stool 720 of unmanned plane 700 is pressed on base station by clamping section 1, so as to be fixedly clamped unmanned plane 700 in designated position
On.On the other hand when unmanned plane 700 needs to leave designated position, unmanned plane can be unclamped by operating compressed part compressed part
700 foot stool 720.Fix the foot stool 720 of unmanned plane 700 automatically by pressing device, it is simple in structure, it is easy to operate.
Further, the clamping section 1 can be equipped with groove.When clamping section 1 in the open state, the foot stool 720 blocks
It is connected in the groove, so as to which unmanned plane 700 is fixed on designated position more securely, it is fixed to improve unmanned plane 700
Effect.
Soft layer can be equipped on the clamping section 1.When clamping section 1 in the open state, the clamping section 1 is by described
The foot stool 720 is pressed on designated position by soft layer, avoids scraping foot stool 720.The material of the soft layer may be selected to be
Rubber or other soft materials.
In addition, working as clamping section 1 in the open state, the size of clamping section 1 and 720 contact area of foot stool can be according to fixation
The selections such as the firmness demand of unmanned plane 700, the shape and structure of foot stool 720 so that unmanned plane 700 can be fixed tively firm
On designated position.
And the designated position can be a regional location or some positions.In the present embodiment, the designated position is
One regional location.It can be using the center of fuselage 710 as reference, when the center of fuselage 710 is aligned up and down with the center of designated position
When (being carried on the top of landing platform 100 as reference using unmanned plane 700), represent that the unmanned plane 700 is carried on the landing
Designated position on platform 100.Certainly, in other embodiments, the designated position is alternatively a position, when fuselage 710
When center is aligned up and down with designated position and (is carried on the top of landing platform 100 as reference using unmanned plane 700), the nothing is represented
Man-machine 700 are carried on the designated position on the landing platform 100.
Wherein, the driving mechanism 2 can be steering engine or other are capable of providing the structure of driving force.In the present embodiment, with institute
Driving mechanism 2 is stated to be further illustrated for steering engine.
Fig. 1 and Fig. 2 is combined again, which may also include transmission mechanism 3.Described 3 one end of transmission mechanism with it is described
Servo driving connects, and the other end is connect with the clamping section 1.Wherein, the steering engine rotation, drives the transmission mechanism 3 to push
The clamping section 1 is moved relative to the landing platform 100, and the driving force of steering engine is passed to clamping section 1 by transmission mechanism 3, from
And realize movement of the clamping section 1 relative to landing platform 100.
Further, with reference to Fig. 1 to Fig. 5, the transmission mechanism 3 may include pushing part 31 and connecting rod 32.Wherein, it is described to support
Push piece 31 is connected with the steering engine.In the present embodiment, it is described push part 31 can the steering engine connected directly or indirectly, example
Such as, the steering engine can be connected through a shaft coupling 4 it is described push part 31, push part 31 so as to which the driving force of steering engine be passed to.Knot
Fig. 1, Fig. 2 and Fig. 5 are closed, described push can also be equipped with supporting rack 5 between part 31 and the shaft coupling 4, described to push the one of part 31
Part is connected after wearing support frame as described above 5 with the shaft coupling 4.Further, the part 31 that pushes can be cam, described convex
Wheel includes a connecting shaft.The main shaft of the steering engine connects the connecting shaft of the cam through a shaft coupling 4.The peripheral outer wall of cam is supported
Connective pole 32 (in figure, the peripheral outer wall of cam abuts the first connecting rod 321 of connecting rod 32).When steering engine rotates, the cam is driven
Rotation, the peripheral outer wall of cam pushes the connecting rod 32 and moves, so as to which the clamping section 1 be driven to be transported close to landing platform 100
It is dynamic.Certainly, the type for pushing part 31 is not limited to cam.
One end of the connecting rod 32 pushes part 31 described in abutting, and the other end connects the clamping section 1.When the steering engine rotates
When, the part 31 that pushes pushes the connecting rod 32, is put down so that the clamping section 1 is driven to press the foot stool 720 set on the landing
On platform 100, so as to which unmanned plane 700 is fixed on landing platform 100.And when the steering engine stops operating (i.e. steering engine lets out power)
When, the connecting rod 32 can reset under the action of elastic force, so as to which the clamping section 1 be driven to unclamp the foot stool 720.
Optionally, the connecting rod 32 and described push are equipped with elastic component (for example, spring) between part 31, alternatively, the company
Bar 32 is internally provided with elastic component.When the steering engine stops operating, the work of elastic force of the connecting rod 32 in the elastic component
With lower reset.Optionally, the connecting rod 32 includes an elastic portion, and the elastic portion abuts connection with the part 31 that pushes.Institute
When stating steering engine and stopping operating, the connecting rod 32 resets under the resilient force of the elastic component.
Further, with reference to Fig. 1 to Fig. 5, the connecting rod 32 can be double leval jib 32, which may include first connecting rod
321 and second connecting rod 322.Wherein, the first connecting rod 321 is set relatively with the second connecting rod 322.The part 31 that pushes supports
Side of the first connecting rod 321 far from the second connecting rod 322 is connected to, the clamping section 1 is connected on the double leval jib 32
Side far from the first connecting rod 321.Specifically, when steering engine rotates, drive pushes part 31 and pushes the first connecting rod
321, the double leval jib 32 can it is described push part 31 support thrust under deform, so as to drive the clamping section 1 close to drop
Platform 100 is fallen to move.And when steering engine stops operating, the first connecting rod 321 resets in the presence of a tensile force, drives described four
The other parts of connecting rod 32 reset, so that the clamping section 1 moves and (resets) far from the landing platform 100.
In one embodiment, the elastic component be set on the second connecting rod 322 and it is described push part 31 between, alternatively, institute
Elastic component is stated in the second connecting rod 322.When the steering engine stops operating, the second connecting rod 322 is in the elasticity
It is resetted under the action of the elastic force of part, so as to drive 32 integral reset of double leval jib, is further driven to clamping section 1 and resets.Another
In embodiment, the elastic portion is at least part of the second connecting rod 322, and the elastic portion is supported with the part 31 that pushes
It connects in succession.When the steering engine stops operating, the second connecting rod 322 resets under the resilient force of the elastic portion, from
And 32 integral reset of double leval jib is driven, it is further driven to clamping section 1 and resets.
Embodiment two
With reference to Fig. 6 to Fig. 8, the utility model two provides a kind of base station, which may include carrying unmanned plane 700
The clamping device 200 of landing platform 100 and above-described embodiment one.In the present embodiment, designated position is dropped in unmanned plane 700
When, the foot stool 720 of unmanned plane 700 can be pressed on base station by clamping section 1, referred to so as to which unmanned plane 700 be fixedly clamped
Positioning is put.And when unmanned plane 700 needs to leave designated position, unmanned plane can be unclamped by operating compressed part compressed part
700 foot stool 720, realization method is relatively simple.
Fig. 6 to Fig. 8 is combined again, and the base station may also include two the first inclined plates on the landing platform 100
300.Two first inclined plates 300 are opposite and set.When the unmanned plane 700 is carried on specifying on the landing platform 100
During position, two first inclined plates 300 are connected to the both sides of the foot stool 720 respectively, so as to the foot stool of multiple no-manned plane 700
720 are limited, so as to preferably limit unmanned plane 700 in the designated position.
Further, but combine Fig. 6 and Fig. 7, the base station may also include on the landing platform 100 second tiltedly
Plate 400.Specifically, second inclined plate 400 is set on the same side of two first inclined plates 300.In the present embodiment, two institutes
It states the first inclined plate 300 and second inclined plate 400 and encloses the landing platform 100 and set to form a drop zone 101, and two institutes
It states the first inclined plate 300 and second inclined plate 400 is directed away from the direction of the landing platform 100 and gradually opens, described in two
First inclined plate 300 and second inclined plate 400 are similar to radial distribution around the drop zone 101.
The designated position is located at the drop zone 101, when the unmanned plane 700 is carried on the drop zone 101
And towards the direction of second inclined plate 400 slide to the designated position when, two first inclined plates 300 are connected to respectively
Be parallel to the both sides of line of travel on the foot stool 720, second inclined plate 400 be connected on the foot stool 720 perpendicular to
The other side on line of travel.
It should be noted that in the present embodiment, if using the head of unmanned plane 700 and tail as unmanned plane 700
Front-rear direction, the line of travel of unmanned plane 700 are parallel with the front-rear direction of unmanned plane 700.Two first inclined plates 300 are distinguished
It is connected to and the both sides of line of travel are parallel on the foot stool 720 refer to that two the first inclined plates 300 are connected to the foot respectively
The left and right sides of frame 720, so as to by setting two the first inclined plates 300, lateral position of the guiding unmanned plane 700 in descent
It moves, unmanned plane 700 is laterally limited.
The other side that second inclined plate 400 is connected on the foot stool 720 on line of travel refers to described
Second inclined plate 400 is connected to the front end of the foot stool 720, so as to which by setting the second inclined plate 400, guiding unmanned plane 700 is vertical
Anterior displacement on direction limits the front end of unmanned plane 700.
The present embodiment by setting the first inclined plate 300 and the second inclined plate 400, realize respectively to the lateral of unmanned plane 700 with
The limiting of front end, so as to which unmanned plane 700 is located on designated position.After unmanned plane 700 drop to certain altitude, unmanned plane
700 foot stool 720 can touch any block or polylith in the first inclined plate 300 and the second inclined plate 400, therefore in unmanned plane 700
During continuing decline, unmanned plane 700 can lean on the first inclined plate 300 and any block in the second inclined plate 400 or polylith is held
It is continuous to decline, until unmanned plane 700 slides into designated position.
Fig. 6, Fig. 7 and Fig. 8 are combined again, and the clamping device 200 is two.Two first inclined plates 300 are respectively equipped with
Accommodating groove 310, two clamping devices 200 and two 310 corresponding matchings of accommodating groove.Specifically, when the clamping section 1
When being moved to the retracted state relative to the landing platform 100, the clamping section 1 is housed in corresponding accommodating groove 310
And it is coplanar with corresponding first inclined plate 300, it is realized so as to which the function of the first inclined plate 300 will not be destroyed.Wherein, the clamping section 1
It is housed in corresponding accommodating groove 310 and with the coplanar clamping section 1 that refers to of corresponding first inclined plate 300 towards the one of drop zone 101
The side of side and the first inclined plate 300 towards drop zone 101 is coplanar.And when the unmanned plane 700 is carried on the designated position
When, the clamping section 1 is moved to the opening state relative to the landing platform 100, and the clamping section 1 is by corresponding storage
Slot 310 stretches out and the foot stool 720 is pressed on the landing platform 100 so that unmanned plane 700 is clamped and fixed specified
Position.
Certainly, the quantity of clamping device 200 be not limited to two or one or two more than, so as to meet not
Same sandwiched demand.
The position of the clamping device 200 is also not necessarily limited to be set on the first inclined plate 300, for example, in one embodiment, it is described
Drop zone 101 is equipped with container (not shown), and the clamping device 200 coordinates with the container.When 1 phase of clamping section
When being moved to the retracted state for the landing platform 100, the clamping section 1 is housed in corresponding container.Preferentially
Ground, the clamping section 1 and the drop zone 101 are coplanar, and when unmanned plane 700 is slided in drop zone 101, container hinders foot
Frame 720 slides.When the unmanned plane 700 is carried on the designated position, the clamping section 1 is relative to the landing platform
100 are moved to the opening state, and the clamping section 1 is stretched out by corresponding container and is pressed on the foot stool 720 described
On landing platform 100 so that unmanned plane 700 is clamped and fixed in designated position.
In the present embodiment, the side of two described first inclined plate, 300 the same sides is connected to second inclined plate 400
Both sides, so as to ensure the globality and rigidity of the first inclined plate 300 and the second inclined plate 400.For example, in a wherein embodiment,
Two first inclined plates 300 are integrally formed with second inclined plate 400 and set.
In another embodiment, with reference to Fig. 6 and Fig. 7, the base station may also include transition inclined plate 500, two described first
The side of 300 the same side of inclined plate is connected to the both sides of second inclined plate 400 by the transition inclined plate 500 respectively.Wherein, two
A first inclined plate 300, second inclined plate 400 and the transition inclined plate 500 are directed away from the landing platform 100
It gradually opens in direction.
Further, in some embodiments, the base station may also include changeover portion 600,300 He of the first inclined plate
Second inclined plate 400 can be connected to by a changeover portion 600 on the landing platform 100 respectively, so as to pass through changeover portion 600
It guides the foot stool 720 to slide to the drop zone 101, prevents unmanned plane 700 from leaning on the first inclined plate 300 and second tiltedly
Any block or polylith in plate 400 drop to the end of the first inclined plate 300 or the second inclined plate 400, and (the first inclined plate 300 or second is tiltedly
Plate 400 is close to one end of landing platform 100) when blocked by the first inclined plate 300 or the second inclined plate 400.
The changeover portion 600 of the present embodiment is directed towards the side protrusion of the drop zone 101.And the shape of transition can
It is set as needed, for example, in a wherein embodiment, the side of the changeover portion 600 towards the drop zone 101 is circle
Arc transition face reduces the friction between foot stool 720 and transition face, quick that unmanned plane 700 is guided to decline.
In another embodiment, the side of the changeover portion 600 towards the drop zone 101 is bending transition face, from
And unmanned plane 700 can quickly be guided to decline.
The designated position can be equipped with landing mark, for the position that unmanned plane 700 is marked to decline.Wherein, landing mark
Type can select as needed, for example, the layer knot that rubber layer or other materials are formed can be set on the designated position
Structure is identified the layer structure that rubber layer or other materials are formed as the landing.
The base station further includes mechanical arm (not shown), and the mechanical arm is set on the lower section of the landing platform 100.It is described
Landing platform 100 is equipped with perforating 102 and the blocking portion (not shown) with the perforating 102 cooperation.Under normal conditions, institute
The surrounding for stating stopper section is connected to the madial wall of the perforating 102, and the stopper section and the landing platform 100 are coplanar,
It avoids that unmanned plane 700 is hindered to slide.When unmanned plane 700 is carried on designated position, the stopper section is opened, and the mechanical arm can
It stretches out to carry out unmanned plane 700 battery altering or other operations from the perforating 102.
Fluting (not shown) can be equipped on first inclined plate, 300 or second inclined plate 400.When unmanned plane 700 includes spiral
During paddle, in 700 descent of unmanned plane, the downwash flow of propeller can have an impact the gesture stability of unmanned plane 700.
Fluting is set on one inclined plate 300 or the second inclined plate 400 so that downwash flow can discharge in time, so as to reduce to unmanned plane 700
The influence of posture.Certainly, it can not also slot on the first inclined plate 300 and the second inclined plate 400, simplify overall structure and improve first tiltedly
The intensity of 300 and second inclined plate 400 of plate.
Embodiment three
Referring to Fig. 8, the utility model embodiment three provides a kind of UAV system, and the UAV system may include nobody
The base station of machine 700 and above-described embodiment two.Wherein, the unmanned plane 700 is carried on the landing platform 100 of the base station.
The unmanned plane 700 includes fuselage 710 and foot stool 720.The foot stool 720 may include the first foot stool 721 and second
Foot stool 722, the first foot stool 721 and the second foot stool 722 are respectively arranged on the both sides of the fuselage 710.Wherein, first foot stool
721 may include the first supporting rack and the first skid (not shown), and second foot stool 722 may include the second supporting rack and second
Skid (not shown).The side of first supporting rack connects the side of the fuselage 710, first supporting rack it is another
Side connects first skid.The side of second supporting rack connects the opposite side of the fuselage 710, second support
The opposite side of frame connects second skid.First skid and second skid are arranged in parallel, unmanned plane 700
When declining, the first inclined plate and the second inclined plate any block or polylith are contacted by the first skid brackets and the second skid brackets.
And when unmanned plane 700 drops to landing platform 100, the first skid brackets and the second skid brackets are slided with landing platform 100
Cooperation, so as to slide into designated position.
When the unmanned plane 700 drop to designated position, first skid far from second skid one
Side abuts wherein one first inclined plate 300, and 200 meeting of clamping device on the first inclined plate 300 abutted with the first skid brackets
First skid is pressed on landing platform 100, limits the slip of the first skid.Meanwhile second skid far from described
The side of first skid abuts another first inclined plate 300, correspondingly, on the first inclined plate 300 abutted with the second skid
Clamping device 200 second skid can be pressed on landing platform 100, limit the second skid slip, and then by nobody
Machine 700 is fixed on base station.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
The spirit of utility model and any modification, equivalent substitution, improvement and etc. within principle, done, should be included in the utility model
Within the scope of protection.
Claims (16)
1. a kind of clamping device, for unmanned plane to be fixed to base station, the base station includes putting down for carrying the landing of unmanned plane
Platform, which is characterized in that the clamping device includes clamping section and the driving mechanism being drivingly connected with the clamping section；
Wherein, the driving mechanism can drive the clamping section to be moved relative to the landing platform, so that the clamping section
Optionally it is in retracted state or opening state；
When the unmanned plane is carried on the designated position on the landing platform, the driving mechanism drives the clamping section phase
The opening state is moved to for the landing platform, the clamping section is used to the foot stool of the unmanned plane being pressed on described
On landing platform；
When the driving mechanism drives the clamping section to be moved to the retracted state relative to the landing platform, the folder
Tight portion is used to unclamp the foot stool.
2. clamping device as described in claim 1, which is characterized in that further include transmission mechanism, described transmission mechanism one end with
The driving mechanism is drivingly connected, and the other end is connect with the clamping section；
The driving mechanism rotation, drives the transmission mechanism that the clamping section is pushed to be moved relative to the landing platform.
3. clamping device as claimed in claim 2, which is characterized in that the transmission mechanism includes being connected with the driving mechanism
Push part and connecting rod, one end of the connecting rod abut described in push part, the other end connects the clamping section；
When the driving mechanism rotates, the part that pushes pushes the connecting rod, to drive the clamping section by the foot stool pressure
On the landing platform.
4. clamping device as claimed in claim 3, which is characterized in that the part that pushes is cam, the master of the driving mechanism
Axis connects the cam through a shaft coupling.
5. clamping device as claimed in claim 3, which is characterized in that the connecting rod be double leval jib, including first connecting rod and with
The second connecting rod that the first connecting rod is opposite and sets；
The part that pushes is connected to side of the first connecting rod far from the second connecting rod, and the clamping section is connected to described four
Side far from the first connecting rod on connecting rod.
6. a kind of base station, the landing platform including being used to carry unmanned plane, which is characterized in that it is any to further include claim 1 to 5
Clamping device described in.
7. base station as claimed in claim 6, which is characterized in that further include on the landing platform and it is opposite and set two
A first inclined plate；
When the unmanned plane is carried on the designated position on the landing platform, two first inclined plates are connected to institute respectively
State the both sides of foot stool.
8. base station as claimed in claim 7, which is characterized in that the second inclined plate on the landing platform is further included,
In, second inclined plate is set on the same side of two first inclined plates, and two first inclined plates and second inclined plate will
The landing platform, which encloses, to be set to form a drop zone, and two first inclined plates and second inclined plate are directed away from the drop
It gradually opens in the direction for falling platform；
The designated position is located at the drop zone, when the unmanned plane is carried on the drop zone and towards described second
When the direction of inclined plate is slided to the designated position, two first inclined plates, which are connected to be parallel on the foot stool respectively, to be slided
The both sides in direction, second inclined plate are connected to the other side on the foot stool on line of travel.
9. base station as claimed in claim 8, which is characterized in that the clamping device is two, two first inclined plates point
It She You not accommodating groove, two clamping devices and two accommodating groove corresponding matchings；
When the clamping section is moved to the retracted state relative to the landing platform, the clamping section is housed in corresponding
It is in accommodating groove and coplanar with corresponding first inclined plate；
When the unmanned plane is carried on the designated position, the clamping section is moved to described beat relative to the landing platform
Open state, the clamping section are stretched out by corresponding accommodating groove and the foot stool are pressed on the landing platform.
10. base station as claimed in claim 8, which is characterized in that the side of two described first inclined plate the same sides connects respectively
In the both sides of second inclined plate.
11. base station as claimed in claim 10, which is characterized in that further include transition inclined plate, two first inclined plates are same
The side of side is connected to the both sides of second inclined plate by the transition inclined plate respectively.
12. base station as claimed in claim 8, which is characterized in that further include that the foot stool is guided to slide to the landing
The changeover portion in region, first inclined plate and second inclined plate are connected to by a changeover portion on the landing platform respectively.
13. base station as claimed in claim 12, which is characterized in that the side of the changeover portion towards the drop zone is circle
Arc transition face or bending transition face.
14. base station as claimed in claim 8, which is characterized in that the designated position is equipped with landing and identifies.
15. base station as claimed in claim 8, which is characterized in that first inclined plate is equipped with fluting.
16. a kind of UAV system, including unmanned plane, which is characterized in that further include described in 6 to 15 any one of the claims
Base station, wherein the unmanned plane is carried on the landing platform of the base station.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721418632.5U CN207466993U (en) | 2017-10-30 | 2017-10-30 | Clamping device and the base station with clamping device and UAV system |
| CN201780065374.3A CN109890703B (en) | 2017-10-30 | 2017-12-08 | Clamping device and have clamping device's basic station and unmanned aerial vehicle system |
| PCT/CN2017/115249 WO2019085152A1 (en) | 2017-10-30 | 2017-12-08 | Clamping device and a base station having same, and unmanned aerial vehicle system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721418632.5U CN207466993U (en) | 2017-10-30 | 2017-10-30 | Clamping device and the base station with clamping device and UAV system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207466993U true CN207466993U (en) | 2018-06-08 |
Family
ID=62265543
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721418632.5U Expired - Fee Related CN207466993U (en) | 2017-10-30 | 2017-10-30 | Clamping device and the base station with clamping device and UAV system |
| CN201780065374.3A Expired - Fee Related CN109890703B (en) | 2017-10-30 | 2017-12-08 | Clamping device and have clamping device's basic station and unmanned aerial vehicle system |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201780065374.3A Expired - Fee Related CN109890703B (en) | 2017-10-30 | 2017-12-08 | Clamping device and have clamping device's basic station and unmanned aerial vehicle system |
Country Status (2)
| Country | Link |
|---|---|
| CN (2) | CN207466993U (en) |
| WO (1) | WO2019085152A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019127225A1 (en) * | 2017-12-28 | 2019-07-04 | 深圳市大疆创新科技有限公司 | Positioning device for unmanned aerial vehicle |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11279481B2 (en) | 2017-05-12 | 2022-03-22 | Phirst Technologies, Llc | Systems and methods for tracking, evaluating and determining a response to emergency situations using unmanned airborne vehicles |
| CN109703735B (en) * | 2018-10-11 | 2024-04-09 | 深圳市科卫泰实业发展有限公司 | Automatic folding device of unmanned aerial vehicle horn |
| CN111367306B (en) * | 2020-03-19 | 2023-04-14 | 上海陆根智能传感技术有限公司 | Unmanned aerial vehicle positioner |
| KR102389328B1 (en) * | 2020-09-24 | 2022-04-21 | 공주대학교 산학협력단 | drone base station |
| CN113148211B (en) * | 2021-06-03 | 2023-06-13 | 广东省智能机器人研究院 | Unmanned aerial vehicle automatic storage bin with centre gripping fuselage and rotor function that opens and shuts |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104981403B (en) * | 2014-08-08 | 2018-02-13 | 深圳市大疆创新科技有限公司 | Unmanned plane base station and its battery replacement device |
| CN204250382U (en) * | 2014-11-19 | 2015-04-08 | 深圳市大疆创新科技有限公司 | Detent mechanism and adopt the UAV base station of this detent mechanism |
| CN104494503A (en) * | 2014-11-25 | 2015-04-08 | 中国兵器工业计算机应用技术研究所 | Comprehensive shelter system of unmanned aerial vehicle |
| US9527605B1 (en) * | 2014-12-18 | 2016-12-27 | Amazon Technologies, Inc. | Multi-use unmanned aerial vehicle docking station |
| KR101765040B1 (en) * | 2016-02-13 | 2017-08-04 | 김성호 | Auto change system for chemical container with battery built in the uav |
| CN205819583U (en) * | 2016-07-04 | 2016-12-21 | 广东天米教育科技有限公司 | A kind of unmanned plane landing work station |
| CN106564610B (en) * | 2016-10-26 | 2019-02-15 | 中国电子科技集团公司第四十八研究所 | A kind of rotor wing unmanned aerial vehicle auxiliary landing system |
| CN106428538B (en) * | 2016-10-27 | 2018-09-14 | 济南新吉纳远程测控股份有限公司 | A kind of novel gyroplane system and charging method of landing |
| CN206407161U (en) * | 2016-12-16 | 2017-08-15 | 深圳市端方文化科技有限公司 | A kind of unmanned plane fixing device on unmanned plane ground service car |
| CN106864763B (en) * | 2017-03-16 | 2019-09-13 | 山东大学 | A kind of accurate positioning that auxiliary unmanned plane lands and fixed device |
-
2017
- 2017-10-30 CN CN201721418632.5U patent/CN207466993U/en not_active Expired - Fee Related
- 2017-12-08 CN CN201780065374.3A patent/CN109890703B/en not_active Expired - Fee Related
- 2017-12-08 WO PCT/CN2017/115249 patent/WO2019085152A1/en active Application Filing
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019127225A1 (en) * | 2017-12-28 | 2019-07-04 | 深圳市大疆创新科技有限公司 | Positioning device for unmanned aerial vehicle |
| CN110382362A (en) * | 2017-12-28 | 2019-10-25 | 深圳市大疆创新科技有限公司 | A kind of positioning device of unmanned plane |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109890703A (en) | 2019-06-14 |
| WO2019085152A1 (en) | 2019-05-09 |
| CN109890703B (en) | 2022-08-19 |
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