CN208085428U - Electromagnetic type separable device - Google Patents
Electromagnetic type separable device Download PDFInfo
- Publication number
- CN208085428U CN208085428U CN201820026307.2U CN201820026307U CN208085428U CN 208085428 U CN208085428 U CN 208085428U CN 201820026307 U CN201820026307 U CN 201820026307U CN 208085428 U CN208085428 U CN 208085428U
- Authority
- CN
- China
- Prior art keywords
- plug
- socket
- electromagnet
- spring
- utility
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 238000013016 damping Methods 0.000 abstract description 3
- 238000000926 separation method Methods 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 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 description 1
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- Electric Propulsion And Braking For Vehicles (AREA)
Abstract
The utility model provides a kind of electromagnetic type separable device, including is provided with the plug and socket of mounting hole, and electromagnet is respectively fixed on the plug and socket, and two electromagnet contact surface magnetic poles are opposite.Electromagnet on the plug and socket is respectively connected with battery, is wherein connected with current inverters between any one electromagnet and battery, and additional electromagnetic repulsion force can be provided when taking off using current inverters.It is provided with spring among plug, the groove being used cooperatively with spring is provided on socket, spring provides pre-pressing force as damping device.The utility model can be applied to the fields such as hovercar, air-ground amphibious unmanned plane, rotorcycle, pass through special electromagnetic separation, land mobile devices and flight instruments are detached, make new traffic tool under two kinds of use states, payload can be improved, reduce energy loss, it is cost-effective.
Description
Technical field
The utility model is related to aviation flight field of power machinery, specifically a kind of electromagnetic type separable device.
Background technology
Currently, to have developed a variety of hovercars, air-ground amphibious unmanned plane, rotorcycle etc. a variety of new for many companies both at home and abroad
The type vehicles can carry out land traveling and airflight function, and that improves people goes out line efficiency.Novel land and air double-used traffic
Tool is one of the hot fields of new era research, and application prospect is very extensive.New traffic tool land when driving, flight
Device becomes load, reduces payload, meanwhile, the loss of energy can be increased.And when flight in the air, land mobile devices
Become to load, can also reduce payload, reduce the duration performance of new traffic tool, the cost of new traffic tool is caused to become
It is high.
A solution is to detach the land mobile devices and flight instruments of new traffic tool, is made novel
The vehicles lose land mobile devices under state of flight, improve payload, reduce energy loss, cost-effective.Tradition
Be mechanically decoupled apparatus structure complexity, and be not easily accomplished fast quick-detach.
Utility model content
The utility model in order to solve problems in the prior art, provides a kind of electromagnetic type separable device, can apply
Land is travelled and is filled by special electromagnetic separation in fields such as hovercar, air-ground amphibious unmanned plane, rotorcycles
It sets and is detached with flight instruments, make new traffic tool under two kinds of use states, payload can be improved, reduce energy
Loss, it is cost-effective.
The utility model includes the plug and socket for being provided with mounting hole, and electromagnetism is respectively fixed on the plug and socket
Iron, two electromagnet contact surface magnetic poles are opposite.
It is further improved, the electromagnet on the plug and socket is respectively connected with battery, wherein any one electromagnet
It is connected with current inverters between battery, additional electromagnetic repulsion force can be provided when taking off using current inverters.
It is further improved, spring is provided among the plug, the groove being used cooperatively with spring, bullet are provided on socket
Spring provides pre-pressing force as damping device.
For the sake of security, it using safety bolt as spare gripping mechanism, is equipped with across plug between plug and socket
With the safety bolt of socket.
The utility model advantageous effect is：
1. pair land mobile devices and flight instruments detach, make new traffic tool under a certain use state,
Self structure weight can be mitigated, increase payload.
2. the electromagnetic type separable device is simple in structure, securely and reliably, it is easy to accomplish quick disassembling function.
3. the electromagnetic type separable device is reversed using the reversed magnetic force of electric current, additional electromagnetic repulsion force can be provided and helped
It takes off, reduces the power termination of engine when taking off.
4. the electromagnetic type separable device is versatile, can also be applied to heavy duty crane, land sky combined transportation etc. its
His field.
Description of the drawings
Fig. 1 is the utility model overall structure diagram.
Fig. 2 is the utility model front view.
Fig. 3 is that the utility model applies the schematic diagram in flight instruments.
Specific implementation mode
The utility model is described in further detail below in conjunction with the accompanying drawings.
The utility model structure is as depicted in figs. 1 and 2, including is provided with the plug 1 and socket 4 of mounting hole, the plug 1
With electromagnet 3 is respectively fixed on socket 4, two 3 contact surface magnetic poles of electromagnet are opposite.
It is further improved, the electromagnet 3 on the plug 1 and socket 4 is respectively connected with battery 2, wherein any one electricity
Current inverters 7 are connected between magnet 3 and battery 2, additional electromagnetism can be provided when taking off using current inverters 7 denounces
Power.
Be further improved, be provided with spring 6 among the plug 1, be provided on socket 4 and be used cooperatively with spring 6
Groove, spring provide pre-pressing force as damping device.
For the sake of security, it using safety bolt as spare gripping mechanism, is equipped with across slotting between plug 1 and socket 4
First 1 and socket 4 safety bolt 5.
The utility model applies the schematic diagram in flight instruments as shown in figure 3, a kind of air-ground amphibious vehicles, are omitted
Cockpit and power plant only retain dominant structural moieties, and land traveling is partly and the script of flight instruments is using mechanical
Connection, assembly and disassembly are extremely not easy.Separator according to the utility model as land traveling part and flight instruments, both
It can realize the function of quick separating.Four electromagnetic type separable devices, plug are needed to be mounted on flight instruments bottom, floor installation
On land mobile devices top.When separation, need to extract safety bolt, then starting current phase inverter so that plug and pedestal
Between generate repulsive force, assisting in flying device and land mobile devices are detached.After having executed task, it can reinstall.
The electromagnetic type separable device is reusable.
It is similar to be applied to the fields such as air-ground amphibious unmanned plane, rotorcycle, and can be used separately other
Weight light-duty machinery.
There are many utility model concrete application approach, and the above is only the preferred embodiment of the utility model, should
It points out, for those skilled in the art, without departing from the principle of this utility model, can also make
Go out several improvement, these improvement also should be regarded as the scope of protection of the utility model.
Claims (4)
1. a kind of electromagnetic type separable device, including it is provided with the plug of mounting hole（1）And socket（4）, it is characterised in that：Described
Plug（1）And socket（4）On be respectively fixed with electromagnet（3）, two electromagnet（3）Contact surface magnetic pole is opposite.
2. electromagnetic type separable device according to claim 1, it is characterised in that：The plug（1）And socket（4）On
Electromagnet（3）It is respectively connected with battery（2）, wherein any one electromagnet（3）And battery（2）Between be connected with current inverters
（7）.
3. electromagnetic type separable device according to claim 1, it is characterised in that：The plug（1）Centre is provided with
Spring（6）, socket（4）On be provided with and spring（6）The groove being used cooperatively.
4. electromagnetic type separable device according to claim 1, it is characterised in that：The plug（1）And socket（4）It
Between be equipped with across plug（1）And socket（4）Safety bolt（5）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820026307.2U CN208085428U (en) | 2018-01-08 | 2018-01-08 | Electromagnetic type separable device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820026307.2U CN208085428U (en) | 2018-01-08 | 2018-01-08 | Electromagnetic type separable device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208085428U true CN208085428U (en) | 2018-11-13 |
Family
ID=64065571
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820026307.2U Expired - Fee Related CN208085428U (en) | 2018-01-08 | 2018-01-08 | Electromagnetic type separable device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208085428U (en) |
Cited By (3)
| 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 |
| CN110861454A (en) * | 2019-11-29 | 2020-03-06 | 吉林大学 | Reconfigurable air-submersible amphibious robot |
| CN111158290A (en) * | 2019-12-31 | 2020-05-15 | 埃游科技（深圳）有限公司 | Multi-modal control method and device for unmanned equipment |
-
2018
- 2018-01-08 CN CN201820026307.2U patent/CN208085428U/en not_active Expired - Fee Related
Cited By (3)
| 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 |
| CN110861454A (en) * | 2019-11-29 | 2020-03-06 | 吉林大学 | Reconfigurable air-submersible amphibious robot |
| CN111158290A (en) * | 2019-12-31 | 2020-05-15 | 埃游科技（深圳）有限公司 | Multi-modal control method and device for unmanned equipment |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181113 |