CN206759086U - Airborne charging connector, base station charging structure and unmanned plane automatic charging system - Google Patents
Airborne charging connector, base station charging structure and unmanned plane automatic charging system Download PDFInfo
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- CN206759086U CN206759086U CN201720378226.4U CN201720378226U CN206759086U CN 206759086 U CN206759086 U CN 206759086U CN 201720378226 U CN201720378226 U CN 201720378226U CN 206759086 U CN206759086 U CN 206759086U
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- unmanned plane
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Abstract
The utility model discloses a kind of airborne charging connector, base station charging structure and unmanned plane automatic charging system.The airborne charging connector includes the first plug division, first plug division includes elastic telescopic part and is connected to the plug of described elastic telescopic part one end, the elastic telescopic part, which is configured the other end, to be connected on unmanned aerial vehicle body, the plug is configured to the remote elastic telescopic part direction movement to be plugged in external receptacle, when the elastic telescopic part is configured in the plug to away from elastic telescopic part direction movement, the plug can be supplied to towards the elastic force of the elastic telescopic part.A technical problem to be solved in the utility model is that unmanned plane can not realize that automatic charging is continued a journey during long-range flight.
Description
Technical field
Charging technique field is the utility model is related to, specifically, the utility model is related to a kind of airborne charging connector, base station
Charging structure and unmanned plane automatic charging system.
Background technology
Unmanned plane is as the industry risen suddenly in recent years, and its growth momentum is swift and violent, and various unmanned planes are not
It is disconnected to emerge in large numbers.Such as the charge machine unmanned plane for taking photo by plane, for prospecting or unmanned plane etc. of agricultural, commodities market.
In the unmanned plane of remote flying distance with, its flying distance and flight time are longer.Such as surveyed for coastal waters
Examine or the unmanned plane of the purposes such as highway, railroad maintenance, be respectively provided with longer flying distance.In such unmanned plane, unlike disappearing
It is the same to take machine unmanned plane, is operated all the time by manual remote control device.Their takeoff and landing is typically automatic.In flight course
Each place, the ground base station provided with cooperation, which takes off and navigated for it, provides guiding.In such unmanned plane, due to flight away from
From longer, the electricity under original state can not meet the needs of relatively long distance flight, need to fill it in flight course
Electricity continuation of the journey.But in the prior art, it can not realize that automatic charging is continued a journey under the interference of no artificial disturbance, meet middle-long distance
The needs of flight.
Therefore, it is necessary to existing unmanned plane and its related charging unit, method are improved.
Utility model content
A purpose of the present utility model is to provide a kind of airborne charging connector, base station charging structure and unmanned plane and filled automatically
The new solution of electric system.
According to first aspect of the present utility model, there is provided a kind of airborne charging connector.The airborne charging connector includes the
One plug division, first plug division includes elastic telescopic part and is connected to the plug of described elastic telescopic part one end, described
Elastic telescopic part, which is configured the other end, to be connected on unmanned aerial vehicle body, and the plug is configured to stretch to away from the elasticity
For the direction movement of contracting part to be plugged in external receptacle, the elastic telescopic part is configured in the plug to away from the elastic telescopic
When part direction is moved, the plug can be supplied to towards the elastic force of the elastic telescopic part.
Alternatively, it is located remotely from the plug on the surface of the elastic telescopic part direction side and is provided with positioning mark,
The positioning mark is configured to be set by outside positioning shooting head.
Alternatively, the other end of the elastic telescopic part is connected in fixed plate, and the fixed plate is configured to be bonded
In on unmanned aerial vehicle body；Or the other end of the elastic telescopic part is connected on magnet, the magnet is configured to adsorb
In on unmanned aerial vehicle body.
Alternatively, in addition to first plug division the second plug division being electrically connected, second plug division
It is configured to be plugged in unmanned plane charging inlet.
According to second aspect of the present utility model, there is provided a kind of base station charging structure.The base station charging structure includes electricity
Magnet, socket and positioning shooting head, the positioning shooting head are configured to by identifying outside positioning mark come localized external
The position of plug division, the electromagnet be configured as the positioning shooting head navigate to external plug be located at the socket just on
Fang Houneng is powered is plugged in the socket with magnetic-adsorption external plug, and magnetic force disappears when power is off.
Alternatively, in addition to the installing plate on the ground base station, the electromagnet, socket and positioning shooting head are arranged on
The installing plate is located remotely from the surface of ground base station direction side, and ground base station direction one is located towards in the installing plate
The surface of side is provided with roller or guide rail, so that the base station charging structure moves on ground base station.
According to the third aspect of the present utility model, there is provided a kind of unmanned plane automatic charging system.The unmanned plane fills automatically
Electric system includes：Unmanned plane；Airborne charging connector, the airborne charging connector include the first plug division, first plug division
It is connected on the fuselage of the unmanned plane；At least one base station charging structure, the base station charging structure include socket, the nothing
It is man-machine be configured as when being triggered can finding nearby base station charging structure position and landing, first plug division be configured
To recognize first plugging position behind the surface of the socket, the socket can be plugged in to the unmanned plane
Charging, can be separated after charging complete with the socket.
Alternatively, first plug division includes elastic telescopic part and is connected to inserting for described elastic telescopic part one end
Head, the elastic telescopic part other end are connected on the unmanned aerial vehicle body, and the base station charging structure also includes electromagnet, institute
Electromagnet is stated to be configured as the magnetic force when being powered and attract the plug to be moved downward to being plugged in the socket and the elasticity is stretched
Contracting part is stretched, and magnetic force disappears when power is off, and the elastic telescopic part, which shrinks, drives the plug to move up and divide with the socket
From.
Alternatively, it is fixed to be provided with the airborne charging connector on the surface to the base station charging structure direction side
Bit identification, the base station charging structure also include being used for the positioning shooting head for identifying the positioning mark, the positioning shooting head
It is configured to position the position of first plug division by identifying the positioning mark, first plug division is configured
To be plugged in the socket being navigated to by the positioning shooting head behind the surface of the socket.
Alternatively, charging inlet is provided with the unmanned plane, the airborne charging connector also includes and described first
The second plug division that plug division is electrically connected, second plug division are configured to be plugged in the charging inlet.
Inventor of the present utility model has found that in the unmanned plane of long-range flight, the electricity under original state can not meet
The demand of relatively long distance flight, needs to carry out charging continuation of the journey to it in flight course.But prior art can not be inartificial
Such unmanned plane automatic charging is continued a journey under the interference of interference.
In unmanned plane and unmanned plane charging assembly provided by the utility model, automatic recharging method, nobody can be realized
The automatic charging continuation of the journey of machine, meet the needs of long-range flight.Airborne charging connector can be applied to the unmanned plane of different model, peace
It is convenient to fill.Electrically connected by airborne charging connector with the cooperation of base station charging structure, charging modes are simple, and reliability is high.
It is of the present utility model other by referring to the drawings to the detailed description of exemplary embodiment of the present utility model
Feature and its advantage will be made apparent from.
Brief description of the drawings
It is combined in the description and the accompanying drawing of a part for constitution instruction shows embodiment of the present utility model, and
And it is used to explain principle of the present utility model together with its explanation.
Fig. 1 is the structural representation of the airborne charging connector provided in a kind of embodiment of the utility model；
Fig. 2 is the structural representation of the base station charging structure provided in a kind of embodiment of the utility model；
Fig. 3 is charged state schematic diagram in the unmanned plane charging system provided in a kind of embodiment of the utility model；
The schematic diagram of the unmanned plane charging method provided in a kind of embodiment of Fig. 4 the utility model.
Wherein, 10：First plug division；100：Plug；101：Positioning mark；102：Elastic telescopic part；103：Fixed plate；
11：Charging wire；12：Second plug division；20：Socket；21：Electromagnet；22：Positioning shooting head；24：Installing plate；30：Unmanned owner
Body；40:Ground base station.
Embodiment
Various exemplary embodiments of the present utility model are described in detail now with reference to accompanying drawing.It should be noted that：It is unless another
Illustrate outside, the part and the positioned opposite of step, numerical expression and numerical value otherwise illustrated in these embodiments is unlimited
The scope of the utility model processed.
The description only actually at least one exemplary embodiment is illustrative to be never used as to this practicality below
New and its application or any restrictions used.
It may be not discussed in detail for technology, method and apparatus known to person of ordinary skill in the relevant, but suitable
In the case of, the technology, method and apparatus should be considered as part for specification.
In shown here and discussion all examples, any occurrence should be construed as merely exemplary, without
It is as limitation.Therefore, other examples of exemplary embodiment can have different values.
It should be noted that：Similar label and letter represents similar terms in following accompanying drawing, therefore, once a certain Xiang Yi
It is defined, then it need not be further discussed in subsequent accompanying drawing in individual accompanying drawing.
The utility model provides a kind of unmanned plane charging assembly, referring to figs. 1 to Fig. 3, the unmanned plane charging assembly bag
Include airborne charging connector and base station charging structure.Wherein, the airborne charging connector includes the first plug division 10.Unmanned plane bag
Fuselage and foot stool are included, foot stool is used to support fuselage.First plug division 10 is connected on unmanned aerial vehicle body.The base station charging
Structure includes socket 20.Such as the base station charging structure may be mounted on ground base station 40.Unmanned plane is in long-range flight one
Come after the section time to ground base station 40, to realize charging continuation of the journey.With reference to the state after unmanned plane landing in figure 3, nothing is defined
Under the direction of man-machine fuselage towards base station charging structure is, otherwise it is upper.First plug division 10 is being navigated to positioned at described
Behind the surface of socket 20, first plug division 10 is plugged in the socket 20.The base station charging structure passes through the machine
Charging connector and unmanned mechatronics are carried, to realize that the charging to unmanned plane is continued a journey.After charging complete, first plug division
10 move up to be separated with the socket 20, and unmanned plane takes off again.
First plug division 10 can be with the grafting of socket 20 and separating.Fig. 1, which shows that the utility model is a kind of, to be implemented
Airborne charging connector in example, first plug division 10 include elastic telescopic part 102 and are connected to the elastic telescopic part
The plug 100 of 102 one end.The other end of the elastic telescopic part 102 can be connected on unmanned aerial vehicle body.The plug 100 exists
External force effect is lower to be moved to the direction away from the elastic telescopic part 102, until being plugged in the socket 20.In the plug
100 to away from the elastic telescopic part 102 direction move when, the elastic telescopic part 102 is elongated, be supplied to it is described insert
First 100 towards the elastic telescopic part 102 elastic force.In outer power event resolves, the elastic force pulls the plug 100
It is reset to the position before being stretched.It is appreciated that first plug division 10 be located at the socket 20 surface refer to it is described
Plug 100 is located at the surface of the socket 20.
The external force can be realized when automatically generating, disappearing, the plug 100 can autopatching in or be located away from outside insert
Seat 20.Fig. 2 shows the base station charging structure in a kind of embodiment of the utility model, and the base station charging structure also includes electromagnet
21.When navigating to first plug division 10 and being located at the surface of the socket 20, the electromagnet 21, which is powered, produces magnetic force,
To attract the plug 100 to be moved towards the socket 20 until being plugged in the socket 20.In this way, the socket 20 and nobody
Mechatronics, charging continuation of the journey is carried out to unmanned plane.After charging complete, the electromagnet 21 powers off, and magnetic force disappears, the plug
100 reset.In this way, magnetic force caused by the electromagnet 21 is the external force, can be controlled by the energization of coil, power-off described
The generation of external force, disappear.It should be noted that the concrete structure for the part for being used to charge inside the base station charging structure is existing
There is technology, will not be described here.Alternatively, the base station charging structure also includes the installing plate 24 on ground base station 40,
The electromagnet 21, the socket 20 may be mounted at the installing plate 24 and be located remotely from the direction side of ground base station 40
On surface.Such as the socket 20 can be set around the electromagnet 21.
The connected mode of first plug division 10 and unmanned plane has a variety of.Alternatively, the elastic telescopic part 102 is another
One end is detachably connected on unmanned aerial vehicle body.In one example, with reference to figure 1, the other end of the elastic telescopic part 102
It is connected in fixed plate 103, the fixed plate 103 can be bonded on unmanned aerial vehicle body by double faced adhesive tape.In another example
In, the other end of the elastic telescopic part 102 is connected on magnet, and the magnet adsorption is on unmanned aerial vehicle body.Certainly, it is described
Elastic telescopic part 102 can also be wholely set with the unmanned aerial vehicle body, non-dismountable.
The airborne charging connector and unmanned mechatronics, to realize the charging to unmanned plane.The airborne charging connector
There can be various ways with the mode of unmanned mechatronics.In one example, also wrapped with reference to figure 1, the airborne charging connector
Include the second plug division 12 being electrically connected with first plug division 10.Such as first plug division 10 can be by filling
Electric wire 11 electrically connects with second plug division 12.Second plug division 12 is plugged in unmanned plane charging inlet, to realize
State the electrical connection of airborne charging connector and unmanned plane.Certainly, second plug division 12 and unmanned plane charging inlet can also one
Body is set, non-dismountable.
The airborne charging connector is connected on unmanned plane.Positioning mark can be provided with first plug division 10
101.Specifically, it can be arranged on the plug 100 with reference to figure 1, the positioning mark 101 and be located remotely from the elastic telescopic part
On the bottom surface in 102 directions side.Accordingly, the base station charging structure can also include being used to identify the fixation and recognition 101
To realize the positioning shooting of positioning function first 22.Such as shown in Fig. 2, the positioning shooting first 22 may be mounted at the installing plate
On 24 surfaces away from the direction side of ground base station 40, the positioning shooting first 22 can be located at the electromagnet 21 and insert
The side of seat 20.The positioning shooting first 22 positions the position of first plug division 10 by identifying the positioning mark 101
Put.Navigated in the positioning shooting first 22 behind the surface of the socket 20, first plug division 10 is plugged in institute
State socket 20.It so, it is possible to ensure that first plug division 10 is corresponding with the position of socket 20, avoid in the electromagnet
After 21 energizations inhale first plug division 10 down, first plug division 10 can not be plugged in the socket 20.
It should be noted that particular location of the positioning shooting first 22 on the installing plate 24 and unrestricted.It is described
For the camera lens of positioning shooting first 22 towards also being limited without specific, it can be according to the positioning shooting first 22 and the socket 20 described
Particular location on installing plate 24 is set.The positioning shooting first 22 and positioning chip be wired or wireless connection, with reality
Existing positioning function.
Unmanned plane there may be landing place deviation, cannot be guaranteed that first plug division 10 is certain when unmanned plane lands
Positioned at the surface of the socket 20.Alternatively, the surface of the direction side of ground base station 40 is located towards in the installing plate 24
Roller or guide rail are provided with, so that the base station charging structure moves on ground base station 40.In the positioning shooting first 22
Positioning action under, the base station charging structure can automatically move so that first plug division 10 is located at the socket 20
Surface.
The utility model additionally provides a kind of unmanned plane, reference picture 1, Fig. 3, the unmanned plane include unmanned plane main body 30 and
Above-mentioned airborne charging connector.The unmanned plane main body 30 includes fuselage and foot stool, and the foot stool is used to support the fuselage.It is described
One end of elastic telescopic part 102 is connected on the plug 100.The other end of the elastic telescopic part 102 is connected to the nothing
On the fuselage of man-machine main body 30.
Alternatively, the other end of the elastic telescopic part 102 is removably attachable to the fuselage position of unmanned plane main body 30
In on the surface towards ground side.Or the elastic telescopic part 102 can also be with the fuselage of unmanned plane main body 30 one
Set, it is non-dismountable.
Charging inlet can be provided with the fuselage of the unmanned plane main body 30.As above-mentioned, when the airborne charging
When joint also includes the second plug division 12 being electrically connected with first plug division 10, second plug division 12 can be with
It is plugged in the charging inlet.In this way, external charging structure is entered by the airborne charging connector to the unmanned plane main body 30
Row charging.
The utility model additionally provides a kind of unmanned plane charging system, and referring to figs. 1 to Fig. 4, the man-machine charging system includes
Unmanned plane, above-mentioned airborne charging connector and at least one above-mentioned base station charging structure.When the unmanned plane is awing touched
During hair can finding nearby base station charging structure position and land.Such as the unmanned plane can pass through GPS or image recognition
Etc. the position that function searches out neighbouring base station charging structure.It is being located at the socket 20 just navigating to first plug division 10
Behind top, first plug division 10 is plugged in the socket 20, to be charged to the unmanned plane.It is described after charging complete
First plug division 10 separates with the socket 20.
The utility model additionally provides a kind of unmanned plane charging method, referring to figs. 1 to Fig. 4, the unmanned plane automatic charging side
Method includes：
First, there is provided be connected with the unmanned plane of the first plug division 10, at least one base station charging structure, the base station charging
Structure includes socket 20.Such as the base station charging structure may be mounted on ground base station 40.
In the flight course after unmanned plane takes off, when the unmanned plane is triggered, the unmanned plane finding nearby
Simultaneously land base station charging structure position.During landing, the foot stool of the unmanned plane can be supported on ground base station.The unmanned plane
It can be triggered under numerous conditions, such as the dump energy of the unmanned plane is less than particular value.The unmanned plane can pass through
The function such as GPS or image recognition searches out the position of neighbouring base station charging structure.
After the unmanned plane landing, after navigating to first plug division 10 and being located at the surface of the socket 20, institute
State the socket 20 that the first plug division 10 is plugged on the base station charging structure.The base station charging structure enters to the unmanned plane
Row charging.
After charging complete, first plug division 10 separates with the socket 20 on the base station charging structure.It is described nobody
Machine can take off again.
, it is necessary to position the position of first plug division 10 after unmanned plane landing.In one example, described
First plug division 10 is provided with positioning mark 101.The base station charging structure also includes positioning shooting first 22.The positioning shooting
First 22 position the position of first plug division 10 by identifying the positioning mark 101.After unmanned plane landing, institute
State the position that positioning shooting first 22 positions first plug division 10, the base station charging structure is to the side of the first plug division 10
To mobile until first plug division 10 is located at the surface of the socket 20.
After navigating to first plug division 10 and being located at the surface of the socket 20, first plug division 10 needs
The socket 20 being plugged on the base station charging structure.Specifically, first plug division 10 can include elastic telescopic part 102
And it is connected to the plug 100 of described one end of elastic telescopic part 102.The other end of elastic telescopic part 102 is connected to the nothing
On man-machine fuselage.The base station charging structure also includes electromagnet 21.Inserted navigating to first plug division 10 positioned at described
Behind the surface of seat 20, the electromagnet 21, which is powered to being moved downward to the magnetic force attraction plug 100, is plugged in the socket
On 20, the elastic telescopic part 102 is stretched.After charging complete, the electromagnet 21 powers off, and magnetic force disappears.The elasticity
Extensible member 102 is shunk so that the plug 100 to be separated with the socket 20., can be with this way, the unmanned plane completes charging continuation of the journey
Again take off.
It should be noted that it can be special time set in advance that charging, which started to the time needed for charging complete,；
The charge condition of unmanned plane by the information exchange of the base station charging structure and unmanned plane, can be perceived, is charged in unmanned plane
After amount reaches particular value, the electromagnet 21 is controlled to power off.
The upper and inferior orientation term mentioned in this manual is defined relative to the construction shown in each accompanying drawing
, they are relative concepts, and it is therefore possible to can correspondingly be become according to its residing diverse location, different use states
Change.So these or other orientation terms should not be construed to restricted term.
Although some specific embodiments of the present utility model are described in detail by example, this area
It is to be understood by the skilled artisans that example above merely to illustrate, rather than in order to limit the scope of the utility model.This
Field it is to be understood by the skilled artisans that can not depart from the scope of the utility model and spirit in the case of, to above example
Modify.The scope of the utility model is defined by the following claims.
Claims (10)
1. a kind of airborne charging connector, it is characterised in that including the first plug division (10), first plug division (10) includes bullet
Property extensible member (102) and the plug for being connected to described elastic telescopic part (102) one end, the elastic telescopic part (102) by with
Putting the other end can be connected on unmanned aerial vehicle body, and the plug (100) is configured to away from the elastic telescopic part (102)
To be plugged in external receptacle, the elastic telescopic part (102) is configured in the plug (100) to away from the bullet for direction movement
Property extensible member (102) direction movement when, the plug (100) can be supplied to towards the elastic force of the elastic telescopic part (102).
2. airborne charging connector according to claim 1, it is characterised in that be located remotely from the plug (100) described
The surface of elastic telescopic part (102) direction side is provided with positioning mark (101), and the positioning mark (101) is configured to
Set by outside positioning shooting head.
3. airborne charging connector according to claim 1, it is characterised in that the other end of the elastic telescopic part (102)
It is connected in fixed plate, the fixed plate is configured to be adhered on unmanned aerial vehicle body；Or the elastic telescopic part (102)
The other end be connected on magnet, the magnet is configured to be adsorbed on unmanned aerial vehicle body.
4. the airborne charging connector according to claim 1 or 3, it is characterised in that also include and first plug division
(10) the second plug division (12) being electrically connected, second plug division (12) are configured to be plugged in unmanned plane charging
Interface.
5. a kind of base station charging structure, it is characterised in that including electromagnet (21), socket (20) and positioning shooting head (22), institute
Positioning shooting head (22) is stated to be configured to by identifying outside positioning mark come the position of localized external plug division, the electromagnetism
Iron (21) is configured as navigating to after external plug is located at directly over the socket (20) and leading in the positioning shooting head (22)
Electricity is plugged in the socket (20) with magnetic-adsorption external plug, and magnetic force disappears when power is off.
6. base station charging structure according to claim 5, it is characterised in that also include the installing plate on ground base station
(24), the electromagnet (21), socket (20) and positioning shooting head (22) are located remotely from ground installed in the installing plate (24)
On the surface of base station direction side, it is located towards being provided with roller on the surface of ground base station direction side in the installing plate (24)
Or guide rail, so that the base station charging structure moves on ground base station.
A kind of 7. unmanned plane automatic charging system, it is characterised in that including：
Unmanned plane, the unmanned plane include fuselage and foot stool；
Airborne charging connector, the airborne charging connector include the first plug division (10), and first plug division (10) is connected to
On the fuselage of the unmanned plane；
At least one base station charging structure, the base station charging structure include socket (20), and the unmanned plane is configured as in quilt
During triggering can finding nearby base station charging structure position and landing, first plug division (10) be configured as being positioned to
The socket (20) can be plugged in behind the surface of the socket (20) to be charged to the unmanned plane, after charging complete
It can be separated with the socket (20).
8. unmanned plane automatic charging system according to claim 7, it is characterised in that first plug division (10) includes
Elastic telescopic part (102) and the plug for being connected to described elastic telescopic part (102) one end, the elastic telescopic part (102) are another
One end is connected on the unmanned aerial vehicle body, and the base station charging structure also includes electromagnet (21), electromagnet (21) quilt
It is configured to the magnetic force when being powered and attracts the plug (100) to be moved downward to be plugged in the socket (20) and the elastic telescopic
Part (102) is stretched, and magnetic force disappears when power is off, and the elastic telescopic part (102), which is shunk, drives the plug (100) to move up simultaneously
Separated with the socket (20).
9. unmanned plane automatic charging system according to claim 7, it is characterised in that be located in the airborne charging connector
Positioning mark (101) is provided with to the surface of the base station charging structure direction side, the base station charging structure also includes using
In the positioning shooting head (22) for identifying the positioning mark (101), the positioning shooting head (22) is configured to pass through identification
The positioning identifies (101) to position the position of first plug division (10), and first plug division (10) is configured as
Navigated to by the positioning shooting head (22) behind the surface of the socket (20) and be plugged in the socket (20).
10. the unmanned plane automatic charging system according to any one in claim 7, it is characterised in that it is described nobody
It is provided with charging inlet on machine, the airborne charging connector also includes the to be electrically connected with first plug division (10)
Two plug divisions (12), second plug division (12) are configured to be plugged in the charging inlet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720378226.4U CN206759086U (en) | 2017-04-11 | 2017-04-11 | Airborne charging connector, base station charging structure and unmanned plane automatic charging system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720378226.4U CN206759086U (en) | 2017-04-11 | 2017-04-11 | Airborne charging connector, base station charging structure and unmanned plane automatic charging system |
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| CN206759086U true CN206759086U (en) | 2017-12-15 |
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ID=60613729
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108045186A (en) * | 2018-01-08 | 2018-05-18 | 南京航空航天大学 | Electromagnetic type separable device |
-
2017
- 2017-04-11 CN CN201720378226.4U patent/CN206759086U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108045186A (en) * | 2018-01-08 | 2018-05-18 | 南京航空航天大学 | Electromagnetic type separable device |
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| GR01 | Patent grant | ||
| GR01 | Patent grant |