CN206471891U - A kind of electric supply installation of aircraft - Google Patents
A kind of electric supply installation of aircraft Download PDFInfo
- Publication number
- CN206471891U CN206471891U CN201720119812.7U CN201720119812U CN206471891U CN 206471891 U CN206471891 U CN 206471891U CN 201720119812 U CN201720119812 U CN 201720119812U CN 206471891 U CN206471891 U CN 206471891U
- Authority
- CN
- China
- Prior art keywords
- circuit board
- magnet
- positive
- pad
- aircraft
- 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.)
- Active
Links
Landscapes
- Coupling Device And Connection With Printed Circuit (AREA)
- Multi-Conductor Connections (AREA)
Abstract
The utility model discloses a kind of electric supply installation of aircraft, the circuit board is provided with pad, the circuit board also includes the first magnet and is located at the positive pole of circuit board and on the pad, the circuit board also includes the second magnet and is located at the negative pole of the circuit board and on the pad, with this so that forming magnet contact on the circuit board, the soft contact of spring is powered with the circuit board by magnet contact portion, and by the way that the magnet same sex is attracting, the different in nature principle error connection proof repelled each other, fault-tolerant position Position Design, it is ensured that the accurate connection of both positive and negative polarity.
Description
Technical field
The utility model belongs to military spacecraft field, more particularly to a kind of electric supply installation of military spacecraft.
Background technology
Now, the use of many military spacecrafts is more and more, could be reached when simultaneously also very high to military aircraft requirements
To military requirement, but in the market have the electric supply installation of many aircraft be inconvenient to dismount, it is unreliable to be powered.
Therefore, it is necessary to a kind of electric supply installation of new aircraft be designed, to overcome above mentioned problem.
Utility model content
In view of this, to be to provide a kind of dismounting convenient for the purpose of this utility model, is powered reliable, the sufficient flight of nargin
The electric supply installation of device.
The technical scheme that the utility model solution above-mentioned technical problem is used is as follows：A kind of electric supply installation of aircraft,
It includes：One battery is fixed in the aircraft；One circuit board is used to be connected with the battery, and the circuit board is provided with
Both positive and negative polarity corresponds to the both positive and negative polarity of the battery respectively, and the circuit board is provided with pad, and the circuit board also includes the first magnetic
Iron is located at the positive pole of circuit board and on the pad, and the circuit board also includes the second magnet and is located at the negative of the circuit board
Pole and on the pad；The soft contact of one spring, described soft contact one end of spring is used to be used for an external power source, the other end
It is connected with the circuit board, the positive pole of the soft contact of spring is provided with the 3rd magnet for attracting with first magnet, described
The negative pole of the soft contact of spring is provided with the 4th magnet for attracting with second magnet, with this so that the both positive and negative polarity of the circuit board
Conducting is connected with the soft contact both positive and negative polarity of the spring, so that the external power source charges to the battery.
Alternatively, the circuit board is oval, and the ellipse of the circuit board is surrounded by multiple gluing positioning holes.
Alternatively, the circuit board is located at below the pad provided with square frame endoporus, provided with external in the square frame endoporus
Equipment line solder joint.
According to above technical scheme, a kind of electric supply installation of aircraft of the present utility model at least has advantages below：
The circuit board is provided with pad, and the circuit board also includes the first magnet and is located at the positive pole of circuit board and positioned at institute
State on pad, the circuit board also includes the second magnet and is located at the negative pole of the circuit board and on the pad, is made with this
Obtain and magnet contact is formed on the circuit board, the soft contact of spring is powered with the circuit board by magnet contact portion, and
By the way that the magnet same sex is attracting, the different in nature principle error connection proof repelled each other, fault-tolerant position Position Design, it is ensured that the accurate connection of both positive and negative polarity.
Brief description of the drawings
Fig. 1 is the stereogram of the electric supply installation of the aircraft of the utility model embodiment；
Fig. 2 leads for the soft contact of the spring of the electric supply installation of the aircraft of the utility model embodiment with the circuit board
Logical schematic diagram；
Fig. 3 is the schematic diagram of the circuit board of the electric supply installation of the aircraft of the utility model embodiment.
Realization, functional characteristics and the advantage of the utility model purpose will be described further referring to the drawings in conjunction with the embodiments.
Embodiment
In order that technical problem to be solved in the utility model, technical scheme and beneficial effect are clearer, clear, with
Under in conjunction with the accompanying drawings and embodiments, the utility model is further elaborated.It should be appreciated that specific reality described herein
Example is applied only to explain the utility model, is not used to limit the utility model.
As shown in Figure 1 to Figure 3, a kind of electric supply installation of aircraft, it includes：One battery 4 is fixed on the aircraft 1
It is interior；One circuit board 3 is used to be connected with the battery 4, and the circuit board 3 corresponds to the battery 4 respectively provided with both positive and negative polarity
Both positive and negative polarity, the circuit board 3 is provided with pad, and the circuit board 3 also includes the first magnet and is located at the positive pole of circuit board 3 and is located at
On the pad, the circuit board 3 also includes the second magnet and is located at the negative pole of the circuit board 3 and on the pad；One
The soft contact 4 of spring, described soft one end of contact 4 of spring is used to be used to be connected with the circuit board 3 with an external power source, the other end,
The positive pole of the soft contact 4 of spring is used for first magnet attracting, the negative pole of the soft contact 4 of spring provided with the 3rd magnet
Provided with the 4th magnet for attracting with second magnet, with this so that the both positive and negative polarity of the circuit board 3 is soft tactile with the spring
The both positive and negative polarity of piece 4 connection conducting, so that the external power source charges to the battery 4.
As shown in Figure 1 to Figure 3, the circuit board 3 is oval, and the ellipse of the circuit board 3 is surrounded by multiple gluing
Positioning hole.The circuit board 3 is located at below the pad provided with square frame endoporus, and external equipment line is provided with the square frame endoporus
Solder joint.
The electric supply installation of the aircraft 1 of utility model, the circuit board 3 is provided with pad, and pad uses turmeric technique,
Can effectively anticorrosion, anti-oxidant, the circuit board 3 also includes the first magnet and is located at the positive pole of circuit board 3 and positioned at the pad
On, the circuit board 3 also includes the second magnet and is located at the negative pole of the circuit board 3 and on the pad, with this so that institute
State and magnet contact is formed on circuit board 3, the soft contact 4 of spring is powered with the circuit board 3 by magnet contact portion, and is led to
Cross the attracting magnet same sex, the different in nature principle error connection proof repelled each other, fault-tolerant position Position Design, it is ensured that the accurate connection of both positive and negative polarity.
Above by reference to preferred embodiment of the present utility model has been illustrated, not thereby limit to right of the present utility model
Scope.Those skilled in the art do not depart from scope and spirit of the present utility model, can have a variety of flexible programs to realize this practicality
New, the feature for example as one embodiment can be used for another embodiment and obtain another embodiment.It is all to use this practicality
Any modifications, equivalent substitutions and improvements made within new technical concept, all should interest field of the present utility model it
It is interior.
Claims (3)
1. a kind of electric supply installation of aircraft, it is characterised in that it includes：
One battery is fixed in the aircraft；
One circuit board is used to be connected with the battery, and the circuit board corresponds to the positive and negative of the battery respectively provided with both positive and negative polarity
Pole, the circuit board is provided with pad, and the circuit board also includes the first magnet and is located at the positive pole of circuit board and positioned at the weldering
On disk, the circuit board also includes the second magnet and is located at the negative pole of the circuit board and on the pad；
The soft contact of one spring, described soft contact one end of spring is used to be used to connect with the circuit board with an external power source, the other end
Connect, the positive pole of the soft contact of spring be used for provided with the 3rd magnet it is attracting with first magnet, the soft contact of spring it is negative
Pole is provided with the 4th magnet for attracting with second magnet, with this so that the both positive and negative polarity of the circuit board is soft tactile with the spring
Piece both positive and negative polarity connection conducting, so that the external power source charges to the battery.
2. a kind of electric supply installation of aircraft according to claim 1, it is characterised in that：The circuit board is oval,
The ellipse of the circuit board is surrounded by multiple gluing positioning holes.
3. a kind of electric supply installation of aircraft according to claim 2, it is characterised in that：The circuit board is provided with square frame
Hole position is provided with external equipment line solder joint below the pad in the square frame endoporus.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720119812.7U CN206471891U (en) | 2017-02-09 | 2017-02-09 | A kind of electric supply installation of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720119812.7U CN206471891U (en) | 2017-02-09 | 2017-02-09 | A kind of electric supply installation of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206471891U true CN206471891U (en) | 2017-09-05 |
Family
ID=59704156
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720119812.7U Active CN206471891U (en) | 2017-02-09 | 2017-02-09 | A kind of electric supply installation of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206471891U (en) |
-
2017
- 2017-02-09 CN CN201720119812.7U patent/CN206471891U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN201887290U (en) | Universal debugging pinboard | |
| CN206471891U (en) | A kind of electric supply installation of aircraft | |
| CN202679451U (en) | Cellphone circuit board for surface adhesion | |
| WO2017193697A1 (en) | Magnetopause type power obtaining system | |
| CN109494848A (en) | A kind of general magnetic charging paster apparatus | |
| CN201378376Y (en) | Teaching electrical module | |
| CN219204110U (en) | Wireless magnetic attraction charging frame of wireless magnetic attraction mobile power supply | |
| CN206388953U (en) | High-tension connector | |
| CN205846286U (en) | Electronic equipment | |
| CN205385317U (en) | Charging system | |
| CN210015426U (en) | Passive capacitance pen | |
| CN207368152U (en) | A kind of battery management system gathers balancing disk | |
| CN206195117U (en) | Wireless charger connection piece | |
| CN205208188U (en) | LED fluorescent tube of simple and easy equipment | |
| CN218939422U (en) | Integrated 1394B transformer aviation plug | |
| CN204257620U (en) | The auxiliary terminal syndeton of power model | |
| CN211017671U (en) | Data line is inhaled to magnetism that fills soon | |
| JP2017121039A (en) | Antenna assembly | |
| CN205658474U (en) | Intelligence bracelet with conversation function | |
| CN203467058U (en) | Heat radiator of power switch | |
| CN106549274B (en) | Electronic device and its electronic system with improvement connection structure | |
| CN217214476U (en) | Capacitor applied to circuit board | |
| CN205123423U (en) | Wireless dash receiver that charges of silica gel antiskid | |
| CN202058796U (en) | Battery assembly structure of circuit board and consumable chip of printer | |
| CN207652766U (en) | A kind of hanging printed circuit board of high heat conduction of thermoelectricity separation |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |