CN207902758U - Aircraft harness connection structure, fuselage bottom plate and power supply system and aircraft - Google Patents
Aircraft harness connection structure, fuselage bottom plate and power supply system and aircraft Download PDFInfo
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- CN207902758U CN207902758U CN201820315630.1U CN201820315630U CN207902758U CN 207902758 U CN207902758 U CN 207902758U CN 201820315630 U CN201820315630 U CN 201820315630U CN 207902758 U CN207902758 U CN 207902758U
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- China
- Prior art keywords
- aircraft
- power supply
- motor
- bottom plate
- connecting terminal
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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Abstract
The utility model discloses a kind of aircraft harness connection structure, aircraft fuselage bottom plate, aircraft power supply system and aircraft, are related to electronic technology field.The aircraft harness connection structure includes fast connecting terminal, and fast connecting terminal is embedded on fuselage bottom plate, and the both ends of fast connecting terminal are located at the both sides of fuselage bottom plate.The aircraft fuselage bottom plate is provided with above-mentioned aircraft harness connection structure.Aircraft power supply system includes that above-mentioned aircraft harness connection structure, motor terminals and power supply, motor terminals are connect by fast connecting terminal with power supply.The aircraft is provided with above-mentioned aircraft power supply system.The beneficial effects of the utility model are：Keep the harness of aircraft clear, and avoid being directly connected between each element, convenient for being safeguarded to aircraft.
Description
Technical field
The utility model is related to electronic technology fields, and in particular to a kind of aircraft harness connection structure, aircraft fuselage
Bottom plate, aircraft power supply system and aircraft.
Background technology
Aircraft is a kind of not manned vehicle manipulated using radio robot and the presetting apparatus provided for oneself.
Aircraft has been applied to express transportation, has taken photo by plane, agricultural, plant protection, miniature self-timer, disaster relief, observation wild animal, monitors and infect
The fields such as disease, mapping, news report, electric inspection process, movies-making, and many companies and country are also in actively extension sector application
With development vehicle technology.
Currently, the power supply of aircraft is set on fuselage bottom plate, the connecting terminal of motor and the connection electric wire of power supply need
Fuselage bottom plate is passed through, and the connecting terminal of motor is directly connect with the positive and negative anodes of power supply, in addition, other electric wires of aircraft
And control circuit is arranged in around fuselage bottom plate.
During realizing the utility model, inventor has found that aforesaid operations mode has the following disadvantages：
The electric wire and control circuit of aircraft are complicated, time-consuming and laborious when connecting the connecting terminal and power supply of motor；Such as
When needing to change power supply or motor, power supply or motor, process are further taken out after needing the connection electric wire of dismantling power and motor
It is complicated and not easy to operate.
Utility model content
The conducting wire between power supply and motor to solve aircraft in the prior art is not easy wiring and power supply or electricity
Motivation problem not easy to remove, a kind of aircraft harness connection structure of the utility model offer, aircraft fuselage bottom plate, aircraft
Power supply system and aircraft keep the harness of aircraft clear, and avoid being directly connected between each element, convenient for being carried out to aircraft
It safeguards.
To achieve the above object, one side according to the ... of the embodiment of the present invention provides a kind of aircraft harness connection knot
Structure.
A kind of aircraft harness connection structure of the embodiment of the present invention includes fast connecting terminal, wherein：The fast connecting terminal is embedding
On fuselage bottom plate, and the both ends of the fast connecting terminal are located at the both sides of fuselage bottom plate.
By fast connecting terminal, keep the harness of aircraft clear, and avoid being directly connected between each element, convenient for aircraft
It is safeguarded.
Optionally, the both ends of the fast connecting terminal are respectively arranged with connects external socket and connects interior socket soon soon, wherein：It is described fast
Connect the outside that external socket is located at fuselage bottom plate；The inside for connecing interior socket soon and being located at fuselage bottom plate.
External socket is connect soon and connects interior socket soon and is respectively arranged inside and outside fuselage bottom plate, and the circuit letter of aircraft is made
It is clean, clear, the conducting wire of power supply or motor can be accurately found, efficiently completes to take out stitches or wiring works.
To achieve the above object, other side according to the ... of the embodiment of the present invention provides a kind of aircraft fuselage bottom plate.
A kind of aircraft harness that a kind of aircraft fuselage bottom plate of the embodiment of the present invention is provided with the embodiment of the present invention connects
Binding structure.
By fast connecting terminal, keep the harness of aircraft clear, and avoid being directly connected between each element, convenient for aircraft
It is safeguarded.
To achieve the above object, another aspect according to the ... of the embodiment of the present invention provides a kind of aircraft power supply system.
A kind of aircraft harness that a kind of aircraft power supply system of the embodiment of the present invention is provided with the embodiment of the present invention connects
Binding structure, further includes motor terminals and power supply, wherein：The motor terminals pass through the fast connecting terminal and institute
State power supply connection.
By fast connecting terminal, make to avoid being directly connected between the motor terminals of motor and power supply, only to electricity
It is easy to operate and time saving and energy saving when source or motor are dismantled, replaced or installed, it can efficiently complete to take out stitches or wiring work
Make.
Optionally, the both ends of the fast connecting terminal are respectively arranged with connects external socket and connects interior socket soon soon, wherein described fast
External socket is connect to connect with the power supply；It is described to connect interior socket soon and connect with the motor terminals.
External socket is connect soon and connects interior socket soon and is respectively arranged inside and outside fuselage bottom plate, and the circuit letter of aircraft is made
It is clean, clear, the conducting wire of power supply or motor can be accurately found, efficiently completes to take out stitches or wiring works.
Optionally, the motor terminals include motor wiring plus end and motor wiring negative terminal, wherein：
The motor wiring plus end is connect with the anode of the power supply by a fast connecting terminal；The motor wiring is negative
Terminal is connect with the cathode of the power supply by fast connecting terminal described in another.
Optionally, when the aircraft power supply system includes multiple motor, multiple motor wiring plus ends are simultaneously
Connection, and multiple motor wiring negative terminals are in parallel.
The mode of multiple motor parallel connections can provide rated voltage for each motor, ensure each electricity of aircraft
Motivation being capable of normal operation.
Optionally, when the aircraft power supply system includes multiple power supplys, the anode of multiple power supplys is in parallel, and multiple power supplys
Cathode it is in parallel.
Mode of the partial power as stand-by power supply can make motor keep working condition, and then enable aircraft
Normal operation.
To achieve the above object, according to the other side of the utility model embodiment, a kind of aircraft is provided.
A kind of aircraft of the utility model embodiment is provided with a kind of aircraft power supply system of the utility model embodiment
System.
It is provided with the aircraft of aircraft power supply system, the conducting wire between motor and power supply is convenient for wiring, takes out stitches, and operates
It is simple and time saving and energy saving；It can also ensure that the simple in circuits, clear of aircraft.
One embodiment in above-mentioned utility model has the following advantages that or advantageous effect：By fast connecting terminal, make flight
The harness of device is clear, and avoids being directly connected between each element, convenient for being safeguarded to aircraft.Only to power supply or motor
It is easy to operate and time saving and energy saving when equal elements are dismantled, replaced or installed, it can efficiently complete to take out stitches or wiring works.
Description of the drawings
Fig. 1 is a kind of schematic diagram for aircraft harness connection structure that the utility model embodiment provides；
Fig. 2 is a kind of application schematic diagram for aircraft harness connection structure that the utility model embodiment provides；
Fig. 3 is a kind of circuit diagram for aircraft power supply system that the utility model embodiment provides.
In figure,
1- fast connecting terminals；11- connects external socket soon；12- connects interior socket soon；2- motor terminals；21- motor wirings
Plus end；22- motor wiring negative terminals；3- power supplys.
Specific implementation mode
It explains to the exemplary embodiment of the utility model below in conjunction with attached drawing, implements including the utility model
The various details of example should think them only exemplary to help understanding.Therefore, those of ordinary skill in the art answer
When recognizing, various changes and modifications can be made to the embodiments described herein, without departing from the scope of the utility model
And spirit.Equally, for clarity and conciseness, the description to known function and structure is omitted in following description.
Fig. 1 is a kind of schematic diagram for aircraft harness connection structure that the utility model embodiment provides.
As shown in Figure 1, a kind of aircraft harness connection structure that the utility model embodiment provides includes mainly：End is connect soon
Son 1.
Fast connecting terminal 1 can be embedded on fuselage bottom plate, and the both ends of fast connecting terminal 1 are respectively arranged at fuselage bottom plate
Both sides, fast connecting terminal 1 can make the harness of aircraft clear, and avoid being directly connected between each element, convenient for aircraft into
Row is safeguarded.
In the utility model embodiment, it can be respectively set at the both ends of fast connecting terminal 1 and connect external socket 11 soon and connect soon
Interior socket 12.
External socket 11 is connect soon and connects interior socket 12 soon and is respectively arranged inside and outside fuselage bottom plate, thus winged not dismantling
In the case of row device, the outside wiring of aircraft can also be completed.
In addition, the utility model embodiment additionally provides a kind of aircraft fuselage bottom plate, aircraft fuselage bottom plate setting
There is the aircraft harness connection structure of the utility model embodiment.
The aircraft fuselage bottom plate of the utility model embodiment, by fast connecting terminal 1 by each connection wiring harness of aircraft
It is arranged on aircraft fuselage bottom plate, keeps the harness of aircraft clear, and avoid being directly connected between each element, convenient for flight
Device is safeguarded.
As shown in Figs. 1-3, a kind of aircraft power supply system of the utility model embodiment offer includes mainly：Fast connecting terminal
1, the motor terminals 2 of motor and the power supply 3 for motor.
Fast connecting terminal 1 is embedded on fuselage bottom plate, and motor terminals 2 are connect by the fast connecting terminal 1 with power supply 3,
Make to avoid being directly connected between the motor terminals 2 of motor and power supply 3, only power supply 3 or motor are dismantled,
It is easy to operate and time saving and energy saving when replacing or installing, it can efficiently complete to take out stitches or wiring works.Also, by fast connecting terminal 1
Both ends be respectively arranged at the both sides of fuselage bottom plate, the wiring of fast connecting terminal 1 and motor terminals 2 can be made, connect end soon
Son 1 and the wiring of power supply 3 separate, and make the simple in circuits, clearly of aircraft.
In the utility model embodiment, the both ends of fast connecting terminal 1 are respectively arranged with to be connect external socket 11 and connects interpolation soon soon
Mouth 12.
External socket 11 is connect soon and connects interior socket 12 soon and is respectively arranged inside and outside fuselage bottom plate, and connection motor is made to connect
The conducting wire of line plus end 21 or motor wiring negative terminal 22 exists in the conducting wire of the same side, the positive or negative pole for connecting power supply 3
The other side, that is, be used for connect motor motor wiring plus end 21 or motor wiring negative terminal 22 conducting wire can from fly
The inside of row device and connect 12 grafting of interior socket soon, for connect power supply 3 can with conducting wire can from the outside of aircraft with connect soon
11 grafting of external socket ensures the simple in circuits, clear of aircraft so as to accurately find the conducting wire of power supply or motor, and
And power supply 3 or motor wiring or dismounting conducting wire it is more convenient, it is easy to repair.
In embodiments of the present invention, motor terminals 2 include that motor wiring plus end 21 and motor wiring are negative
Terminal 22.
The anode for connecting power supply 3 is connected to the both ends of the same fast connecting terminal 1 with motor wiring plus end 21, it will even
The cathode for connecing power supply 3 is connected to the both ends of another fast connecting terminal 1 with motor wiring negative terminal 22, makes the motor of motor
It avoids being directly connected between wiring plus end 21 and motor wiring negative terminal 22 and the positive and negative anodes of power supply 3.When mounted, respectively
The motor wiring plus end 21 of motor and motor wiring negative terminal 22 are connected with interior socket 12 is connect soon by conducting wire
It connects, and the positive or negative pole of power supply 3 is attached with external socket 11 is connect soon by conducting wire, you can complete wiring work, connect
Line refers to using wire connecting line road；Similarly, when replacing power supply or motor, power supply or electricity are only dismantled at fast connecting terminal 1
The conducting wire of motivation can remove power supply or motor, easy to operate and time saving and energy saving.
In embodiments of the present invention, when power supply 3 is multiple motors, multiple motor wiring plus ends 21 are in parallel,
And multiple 22 parallel connections of motor wiring negative terminal.
For the rotor craft of a multiaxis, multiple motor drive rotors are needed, when an aircraft is arranged
It, can be by multiple motor by the way of in parallel, to be each electricity after aircraft startup when having multiple motor
Motivation provides rated voltage, ensures that each motor of aircraft being capable of normal operation.
In embodiments of the present invention, when aircraft power supply system includes multiple power supplys 3, the anode of multiple power supplys 3 is in parallel, and
The cathode of multiple power supplys 3 is in parallel.
It, can be by multiple power supplys 3 simultaneously when i.e. an aircraft is with multiple power supplys 3 for power supply 3 of the aircraft with abundance
Connection, one of power supply 3 are motor as main power source, and other power supplys 3 are used as stand-by power supply, in some power supply 3
It breaks down, can continue to power by other power supplys 3, motor is made to remain working condition in aircraft operational process,
And then enable aircraft normal operation.
In addition, the utility model embodiment additionally provides a kind of aircraft, which is provided with aircraft power supply system.
Using the aircraft of the aircraft power supply system, the conducting wire between motor and power supply 3 is convenient for wiring, takes out stitches, and grasps
Make simple and time saving and energy saving；The aircraft powered using multiple power supplys 3 can also improve cruising ability.
As described above as can be seen that by fast connecting terminal 1, keep the harness of aircraft clear, and is kept away between each element
Exempt to be directly connected to, convenient for safeguarding aircraft.Only the elements such as power supply 3 or motor are being dismantled, replaced or installed
When, it is easy to operate and time saving and energy saving, it can efficiently complete to take out stitches or wiring works.
The above is only the preferred embodiments of the present utility model only, is not intended to limit the utility model, all in this practicality
Any modification, equivalent replacement and simple modifications etc., should be included in the protection of the utility model made by novel substantive content
Within the scope of.
Claims (9)
1. a kind of aircraft harness connection structure, which is characterized in that including fast connecting terminal (1), wherein：
The fast connecting terminal (1) is embedded on fuselage bottom plate, and the both ends of the fast connecting terminal (1) are located at fuselage bottom plate
Both sides.
2. aircraft harness connection structure according to claim 1, which is characterized in that the both ends of the fast connecting terminal (1)
It is respectively arranged with and connects external socket (11) soon and connect interior socket (12) soon, wherein：
The outside for connecing external socket (11) soon and being located at fuselage bottom plate；
The inside for connecing interior socket (12) soon and being located at fuselage bottom plate.
3. a kind of aircraft fuselage bottom plate, which is characterized in that be arranged just like the aircraft line described in any one of claim 1-2
Beam connection structure.
4. a kind of aircraft power supply system, including aircraft harness connection structure as described in claim 1, which is characterized in that
Further include motor terminals (2) and power supply (3), wherein：
The motor terminals (2) are connect by the fast connecting terminal (1) with the power supply (3).
5. aircraft power supply system according to claim 4, which is characterized in that distinguish at the both ends of the fast connecting terminal (1)
It is provided with and connects external socket (11) soon and connect interior socket (12) soon, wherein：
The external socket (11) that connects soon is connect with the power supply (3)；
The interior socket (12) that connects soon is connect with the motor terminals (2).
6. aircraft power supply system according to claim 4, which is characterized in that the motor terminals (2) include
Motor wiring plus end (21) and motor wiring negative terminal (22), wherein：
The motor wiring plus end (21) is connect with the anode of the power supply (3) by a fast connecting terminal (1)；
The motor wiring negative terminal (22) is connect with the cathode of the power supply (3) by fast connecting terminal described in another (1).
7. aircraft power supply system according to claim 6, which is characterized in that
When the aircraft power supply system includes multiple motor, multiple motor wiring plus ends (21) are in parallel and more
A motor wiring negative terminal (22) is in parallel.
8. the aircraft power supply system according to any one of claim 4-7, which is characterized in that
When the aircraft power supply system includes multiple power supplys (3), the anode of multiple power supplys (3) is in parallel, and multiple power supplys (3)
Cathode is in parallel.
9. a kind of aircraft, which is characterized in that be arranged and connect knot just like the aircraft harness described in any one of claim 1-2
Structure；Or it is provided with aircraft fuselage bottom plate as claimed in claim 3；Or it is arranged just like described in any one of claim 4-8
Aircraft power supply system.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820315630.1U CN207902758U (en) | 2018-03-07 | 2018-03-07 | Aircraft harness connection structure, fuselage bottom plate and power supply system and aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820315630.1U CN207902758U (en) | 2018-03-07 | 2018-03-07 | Aircraft harness connection structure, fuselage bottom plate and power supply system and aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207902758U true CN207902758U (en) | 2018-09-25 |
Family
ID=63558032
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820315630.1U Active CN207902758U (en) | 2018-03-07 | 2018-03-07 | Aircraft harness connection structure, fuselage bottom plate and power supply system and aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207902758U (en) |
-
2018
- 2018-03-07 CN CN201820315630.1U patent/CN207902758U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210226 Address after: Room a1905, 19 / F, building 2, No. 18, Kechuang 11th Street, Daxing District, Beijing, 100176 Patentee after: Beijing Jingdong Qianshi Technology Co.,Ltd. Address before: 101, 1st floor, building 2, yard 20, Suzhou street, Haidian District, Beijing 100080 Patentee before: Beijing Jingbangda Trading Co.,Ltd. Effective date of registration: 20210226 Address after: 101, 1st floor, building 2, yard 20, Suzhou street, Haidian District, Beijing 100080 Patentee after: Beijing Jingbangda Trading Co.,Ltd. Address before: 100195 Beijing Haidian Xingshikou Road 65 West Cedar Creative Garden 4 District 11 Building East 1-4 Floor West 1-4 Floor Patentee before: BEIJING JINGDONG SHANGKE INFORMATION TECHNOLOGY Co.,Ltd. Patentee before: BEIJING JINGDONG CENTURY TRADING Co.,Ltd. |
|
| TR01 | Transfer of patent right |