CN108045186A - Electromagnetic type separable device - Google Patents
Electromagnetic type separable device Download PDFInfo
- Publication number
- CN108045186A CN108045186A CN201810015723.7A CN201810015723A CN108045186A CN 108045186 A CN108045186 A CN 108045186A CN 201810015723 A CN201810015723 A CN 201810015723A CN 108045186 A CN108045186 A CN 108045186A
- Authority
- CN
- China
- Prior art keywords
- plug
- socket
- electromagnet
- spring
- electromagnetic type
- 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.)
- Pending
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
- 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
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B2200/00—Constructional details of connections not covered for in other groups of this subclass
- F16B2200/83—Use of a magnetic material
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Transportation (AREA)
- Remote Sensing (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
Abstract
The present invention provides a kind of electromagnetic type separable device, the plug and socket including being provided with mounting hole is respectively fixed with electromagnet 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.Spring is provided among plug, the groove being used cooperatively with spring is provided on socket, spring provides pre-pressing force as damping device.Present invention could apply to the fields such as hovercar, air-ground amphibious unmanned plane, rotorcycle, pass through special electromagnetic separation, land mobile devices and flight instruments are separated, 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 present invention relates to aviation flight field of power machinery, are specifically a kind of electromagnetic type separable device.
Background technology
At present, it is a variety of new to have developed a variety of hovercars, air-ground amphibious unmanned plane, rotorcycle etc. for domestic and international many companies
The type vehicles can carry out land traveling and airflight function, and that improves people goes out line efficiency.New land and air double-used traffic
Instrument is one of hot fields of new era research, and application prospect is very extensive.New traffic tool when driving, flies on land
Device becomes load, reduces payload, meanwhile, the loss of energy can be increased.And during 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 separate the land mobile devices and flight instruments of new traffic tool, is made new
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.
The content of the invention
The present invention provides a kind of electromagnetic type separable device, can be applied to fly to solve problem of the prior art
The fields such as row automobile, air-ground amphibious unmanned plane, rotorcycle, by special electromagnetic separation, to land mobile devices and
Flight instruments is separated, and makes new traffic tool under two kinds of use states, can improve payload, reduces energy damage
Consumption, it is cost-effective.
The present invention includes being provided with the plug and socket of mounting hole, and electromagnet is respectively fixed on the plug and socket,
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
Current inverters are connected 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, by the use of safety bolt as spare gripping mechanism, plug is provided through between plug and socket
With the safety bolt of socket.
Advantageous effect of the present invention is：
1. pair land mobile devices and flight instruments separate, make new traffic tool under a certain use state, it can
Mitigate self structure weight, 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 overall structure diagram of the present invention.
Fig. 2 is front view of the present invention.
Fig. 3 applies the schematic diagram in flight instruments for the present invention.
Specific embodiment
The invention will be further described below in conjunction with the accompanying drawings.
Structure of the present invention as depicted in figs. 1 and 2, including being provided with the plug 1 of mounting hole and socket 4, the plug 1 and is inserted
Electromagnet 3 is respectively fixed on seat 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 with what is be used cooperatively with spring 6 on socket 4
Groove, spring provide pre-pressing force as damping device.
For the sake of security, by the use of safety bolt as spare gripping mechanism, it is provided through inserting between plug 1 and socket 4
First 1 and the safety bolt 5 of socket 4.
The present invention applies the schematic diagram in flight instruments as shown in figure 3, a kind of air-ground amphibious vehicles, are omitted driving
Cabin and power set only retain dominant structural moieties, and land travels part and the script of flight instruments is connected using mechanical,
Assembly and disassembly is extremely not easy.According to the present invention as land traveling part and the separator of flight instruments, can realize fast
The separated function of speed.Four electromagnetic type separable devices are needed, plug is mounted on flight instruments bottom, and floor installation is in land row
Sail device top., it is necessary to extract safety bolt during separation, then starting current phase inverter so that generated between plug and pedestal
Repulsive force, assisting in flying device and land mobile devices are separated.After task has been performed, it can reinstall.The electromagnetic type
Separable device is reusable.
It is similar can also be applied to the fields such as air-ground amphibious unmanned plane, rotorcycle and it is separable use other
Weight light-duty machinery.
There are many concrete application approach of the present invention, and the above is only the preferred embodiment of the present invention, it is noted that for
For those skilled in the art, without departing from the principle of the present invention, several improvement can also be made, this
A little improve also should be regarded as protection scope of the present invention.
Claims (4)
1. a kind of electromagnetic type separable device, the plug including being provided with 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 set
There is 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 provided through plug（1）And socket（4）Safety bolt（5）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810015723.7A CN108045186A (en) | 2018-01-08 | 2018-01-08 | Electromagnetic type separable device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810015723.7A CN108045186A (en) | 2018-01-08 | 2018-01-08 | Electromagnetic type separable device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108045186A true CN108045186A (en) | 2018-05-18 |
Family
ID=62126892
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810015723.7A Pending CN108045186A (en) | 2018-01-08 | 2018-01-08 | Electromagnetic type separable device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108045186A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110239297A (en) * | 2019-05-27 | 2019-09-17 | 中国民航大学 | One kind separating air-ground amphibious robot and separation combination control method |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150276353A1 (en) * | 2014-03-28 | 2015-10-01 | Mitsubishi Heavy Industries, Ltd. | Modularized armor structure with unmanned aerial vehicle loaded and armored vehicle using the same |
| CN205131676U (en) * | 2015-11-26 | 2016-04-06 | 中国人民解放军军事交通学院 | On -vehicle flying device |
| DE102015207979A1 (en) * | 2015-04-30 | 2016-11-03 | Bayerische Motoren Werke Aktiengesellschaft | Land vehicle with unmanned aerial vehicle and switching station to it |
| CN106921203A (en) * | 2017-05-10 | 2017-07-04 | 韩烨 | A kind of floated Self-disconnecting charger and its power-off method |
| CN107226191A (en) * | 2017-06-19 | 2017-10-03 | 浙江科技学院 | A kind of many rotor unmanned aircraft chargings are tethered at line automatic releasing device |
| CN206759086U (en) * | 2017-04-11 | 2017-12-15 | 歌尔科技有限公司 | Airborne charging connector, base station charging structure and unmanned plane automatic charging system |
| CN208085428U (en) * | 2018-01-08 | 2018-11-13 | 南京航空航天大学 | Electromagnetic type separable device |
-
2018
- 2018-01-08 CN CN201810015723.7A patent/CN108045186A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150276353A1 (en) * | 2014-03-28 | 2015-10-01 | Mitsubishi Heavy Industries, Ltd. | Modularized armor structure with unmanned aerial vehicle loaded and armored vehicle using the same |
| DE102015207979A1 (en) * | 2015-04-30 | 2016-11-03 | Bayerische Motoren Werke Aktiengesellschaft | Land vehicle with unmanned aerial vehicle and switching station to it |
| CN205131676U (en) * | 2015-11-26 | 2016-04-06 | 中国人民解放军军事交通学院 | On -vehicle flying device |
| CN206759086U (en) * | 2017-04-11 | 2017-12-15 | 歌尔科技有限公司 | Airborne charging connector, base station charging structure and unmanned plane automatic charging system |
| CN106921203A (en) * | 2017-05-10 | 2017-07-04 | 韩烨 | A kind of floated Self-disconnecting charger and its power-off method |
| CN107226191A (en) * | 2017-06-19 | 2017-10-03 | 浙江科技学院 | A kind of many rotor unmanned aircraft chargings are tethered at line automatic releasing device |
| CN208085428U (en) * | 2018-01-08 | 2018-11-13 | 南京航空航天大学 | Electromagnetic type separable device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110239297A (en) * | 2019-05-27 | 2019-09-17 | 中国民航大学 | One kind separating air-ground amphibious robot and separation combination control method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180518 |
|
| WD01 | Invention patent application deemed withdrawn after publication |