CN208947596U - Connector, dynamical system and unmanned plane - Google Patents
Connector, dynamical system and unmanned plane Download PDFInfo
- Publication number
- CN208947596U CN208947596U CN201821578488.6U CN201821578488U CN208947596U CN 208947596 U CN208947596 U CN 208947596U CN 201821578488 U CN201821578488 U CN 201821578488U CN 208947596 U CN208947596 U CN 208947596U
- Authority
- CN
- China
- Prior art keywords
- piece
- connector
- face
- conduct piece
- interconnecting piece
- 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
- 238000005183 dynamical system Methods 0.000 title claims abstract description 30
- 238000004806 packaging method and process Methods 0.000 claims abstract description 32
- 238000007789 sealing Methods 0.000 claims description 12
- 230000005611 electricity Effects 0.000 claims description 7
- 238000009434 installation Methods 0.000 description 7
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 239000000428 dust Substances 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 239000004020 conductor Substances 0.000 description 2
- 239000004033 plastic Substances 0.000 description 2
- 229920003023 plastic Polymers 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910000881 Cu alloy Inorganic materials 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 230000004308 accommodation Effects 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000033228 biological regulation Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000003990 capacitor Substances 0.000 description 1
- 239000004568 cement Substances 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 238000005538 encapsulation Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000003384 imaging method Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 238000002386 leaching Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 235000015097 nutrients Nutrition 0.000 description 1
- 239000000575 pesticide Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K11/00—Structural association of dynamo-electric machines with electric components or with devices for shielding, monitoring or protection
- H02K11/30—Structural association with control circuits or drive circuits
- H02K11/33—Drive circuits, e.g. power electronics
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Power Engineering (AREA)
- Motor Or Generator Frames (AREA)
Abstract
The utility model discloses a kind of connectors.Connector is for being electrically connected motor and electron speed regulator.Connector includes conduct piece and packaging body.Conduct piece is electrically connected with one end of triple line, and the other end of triple line is electrically connected with motor.Packaging body is formed with opposite the first face and the second face.Interconnecting piece is formed on first face.Conduct piece is encapsulated in packaging body, and conduct piece at least partly exposes from interconnecting piece, to allow fastener to be mounted on interconnecting piece and be electrically connected conduct piece and electron speed regulator.The invention also discloses a kind of dynamical system and unmanned planes.Conduct piece is encapsulated in packaging body and exposes from interconnecting piece, and since interconnecting piece is formed in the first face, and fastener is only mounted on interconnecting piece by user, could be electrically connected conduct piece and electron speed regulator, is prevented the anti-loaded connector of user and is led to triple line connection error.
Description
Technical field
The utility model relates to technical field of motors, in particular to a kind of connector, dynamical system and unmanned plane.
Background technique
In more rotor unmanned aircraft fields, more rotor unmanned aircrafts in terms of agricultural are especially applied to, motor
Frequency of use is high, it is often necessary to overhaul, safeguards or replace, therefore motor needs often remove and install.Motor passes through three-phase
Line is connect with electron speed regulator, in general, on more rotor unmanned aircrafts, the steering of the motor of different location it is different (clockwise or
Counterclockwise), therefore the connection type of motor triple line needs are connected in strict accordance with pre-provisioning request, just can guarantee each correspondence
The steering of the motor of position turns to rotation by original, makes to guarantee unmanned vehicle smooth flight when multiple rotor wing rotations with this.So
And the triple line of traditional motor is three conducting wires being scattered, there is no special design anti-misoperation devices, therefore, motor triple line
When connecting with electron speed regulator, the easy sequence by the triple line of motor of user is wrongly installed, and makes the motor steering after installation
It is different from original steering, or can not rotate, it can not normal flight so as to cause unmanned vehicle, in some instances it may even be possible to aircraft bombing occur.
Utility model content
The utility model embodiment provides a kind of connector, dynamical system and unmanned plane.
The connector of the utility model embodiment includes leading for being electrically connected motor and electron speed regulator, the connector
Electric part and packaging body.The conduct piece is electrically connected with one end of triple line, and the other end of the triple line is electrically connected with the motor
It connects.The packaging body is formed with opposite the first face and the second face, and interconnecting piece, the conduct piece envelope are formed on first face
In the packaging body, the conduct piece at least partly exposes from the interconnecting piece, to allow fastener to be mounted on the company
In socket part and it is electrically connected the conduct piece and the electron speed regulator.
In some embodiments, the interconnecting piece includes the mounting groove being formed on first face, the mounting groove
For at least partly accommodating the fastener.
In some embodiments, the packaging body further includes the side wall for connecting first face and second face, institute
It states packaging body and is formed on the side wall jagged, the notch is connected to the mounting groove.
In some embodiments, along the direction that second face is directed toward in first face, the depth of the notch is big
In or equal to the mounting groove depth.
In some embodiments, the quantity of the conduct piece is multiple, and the quantity of the interconnecting piece is multiple, Mei Gesuo
Conduct piece is stated to expose from corresponding one interconnecting piece.
In some embodiments, the conduct piece includes being formed with the conductive ring of mounting hole and fixing with the conductive ring
The connector of connection, the connector are electrically connected with the triple line, and the conductive ring at least partly exposes from the interconnecting piece.
In some embodiments, the connector further includes fixing piece, and the fixing piece is connect with the triple line, institute
Fixing piece is stated for the triple line to be fixed on external equipment by preset order.
The dynamical system of the utility model embodiment includes described in motor, electron speed regulator and any of the above-described embodiment
Connector.The electron speed regulator is used to control the working condition of the motor.The electron speed regulator and the conduct piece
It is electrically connected by the fastener.
In some embodiments, the electron speed regulator includes shell and electric tuned plate.It is empty that the shell is formed with receiving
Between, and the through-hole of the connection accommodating space, the connector is arranged in outside the accommodating space and the position of the interconnecting piece
With the through-hole alignment.The electricity tuned plate is housed in the accommodating space, and the fastener passes through the interconnecting piece and described
Through-hole, to be electrically connected the conduct piece and the electric tuned plate.
In some embodiments, the shell includes upper casing and lower casing.The through-hole is provided on the upper casing, and institute
The second face is stated to support on the upper casing.The lower casing forms the accommodating space in conjunction with the upper casing.
In some embodiments, it is provided with conductive column on the electric tuned plate, the fastener is connect with the conductive column
To connect the conduct piece and the electric tuned plate.
In some embodiments, sealing ring is provided between the conductive column and the upper casing, the sealing ring can
Seal the gap between the through-hole and the fastener.
The unmanned plane of the utility model embodiment includes fuselage, dynamical system described in horn and any of the above-described embodiment
System.The horn is connected on the fuselage.The dynamical system is mounted on the horn.
In the connector of the utility model embodiment, dynamical system and unmanned plane, conduct piece be encapsulated in packaging body and
Expose from interconnecting piece, since interconnecting piece is formed in the first face, and fastener is only mounted on interconnecting piece by user, can be just electrically connected
Conduct piece and electron speed regulator are connect, the sequence of user's wrong even triple line due to not having connector is prevented, or anti-loaded connection occurs
Device and lead to triple line connection error.
The additional aspect and advantage of the embodiments of the present invention will be set forth in part in the description, partially will be from
Become obvious in following description, or is recognized by the practice of the embodiments of the present invention.
Detailed description of the invention
In description of the above-mentioned and/or additional aspect and advantage of the utility model from combination following accompanying drawings to embodiment
It will be apparent and be readily appreciated that, in which:
Fig. 1 is the three-dimensional assembling schematic diagram of the unmanned plane of the utility model embodiment；
Fig. 2 is the dynamical system of the utility model embodiment and the three-dimensional assembling schematic diagram of horn；
Fig. 3 is the electron speed regulator of the utility model embodiment and the perspective exploded view of connector；
Fig. 4 is the floor map of the connector of the utility model embodiment；
Fig. 5 is the stereoscopic schematic diagram of the connector of the utility model embodiment；
Fig. 6 is the partial sectional schematic view of the connector of the utility model embodiment；
Fig. 7 is the stereoscopic schematic diagram of the conduct piece of the utility model embodiment.
Main element symbol description:
Unmanned plane 1000, dynamical system 100, motor 10, electron speed regulator 20, shell 21, accommodating space 211, through-hole
212, upper casing 213, radiating fin 2131, lower casing 214, electric tuned plate 22, electronic component 221, conductive column 23, sealing ring 24, company
Connect device 30, conduct piece 31, conductive ring 311, mounting hole 3111, connector 312, connection space 3121, packaging body 32, the first face 321,
Second face 322, interconnecting piece 323, side wall 324, notch 325, fixing piece 33, fuselage 200, horn 300, triple line 400, fastener
500, propeller 600.
Specific embodiment
The embodiments of the present invention is described further below in conjunction with attached drawing.Same or similar label in attached drawing
Same or similar element or element with the same or similar functions are indicated from beginning to end.
In addition, the embodiments of the present invention described with reference to the accompanying drawing is exemplary, it is only used for explaining this reality
With novel embodiment, and should not be understood as limiting the present invention.
In the present invention unless specifically defined or limited otherwise, fisrt feature is in the second feature " on " or " down "
It can be that the first and second features directly contact or the first and second features are by intermediary mediate contact.Moreover, first is special
Sign can be fisrt feature above the second feature " above ", " above " and " above " and be directly above or diagonally above the second feature, or only
Indicate that first feature horizontal height is higher than second feature.Fisrt feature under the second feature " below ", " below " and " below " can be with
It is that fisrt feature is directly under or diagonally below the second feature, or is merely representative of first feature horizontal height less than second feature.
Embodiment one
Fig. 1 and Fig. 2 is please referred to, the unmanned plane 1000 of the utility model embodiment includes fuselage 200, horn 300 and moves
Force system 100.Unmanned plane 1000 can be the moveable platforms such as unmanned vehicle, unmanned vehicle, unmanned boat, and the utility model is implemented
Example is illustrated so that unmanned plane 1000 is unmanned vehicle as an example, it will be understood that the type of unmanned plane 1000 can be with
It is other, should not be understood as the limitation of the utility model.Specifically, unmanned plane 1000 can be more rotor unmanned aircrafts, example
Such as quadrotor unmanned vehicle, six rotor unmanned aircrafts, eight rotor unmanned aircrafts, 12 rotor unmanned aircrafts, nothing
Man-machine 1000 can be used for carrying load to complete scheduled task, such as carry imaging device to be shot, carry pesticide,
Nutrient solution and flusher are to carry out plant protection task dispatching.
Fuselage 200, which can be used as, can install horn outside the installation carrier of the functional component of unmanned plane 1000, such as fuselage 200
300, it loads, rack, power module, flight control system etc. can be installed in fuselage 200.Fuselage 200 can also be to be mounted on fuselage
Functional component in 200 provides the protection of waterproof and dustproof etc..Horn 300 is mounted on fuselage 200, and horn 300 connects in other words
On fuselage 200.The quantity of horn 300 can be multiple, and multiple horns 300 radial centered on fuselage 200 can be set
It sets, in one example, horn 300 can be folded and is housed on fuselage 200 in order to carry, in another example, machine
Arm 300 can also be connected on fuselage 200 by quick-disassembly structure, in order to which user dismantles or replace horn 300.
Dynamical system 100 is mounted on horn 300.Specifically, dynamical system 100 may be mounted at the separate of horn 300
On one end of fuselage 200.Dynamical system 100 can be controlled by the flight control system of unmanned plane 1000, and for unmanned plane 1000
Power is provided.In one example, the quantity of dynamical system 100 can be multiple, and each dynamical system 100 can be controlled independently
System, such as the open and close of each dynamical system 100, the transmission direction of each dynamical system 100, each dynamical system 100
Output power etc. can be with independent control.Power can be transferred to actuating member by dynamical system 100, in example as shown in Figure 1
In, actuating member can be propeller 600, and the rotation of propeller 600 can provide lift and pulling force, each power for unmanned plane 1000
System 100 can be connect with a propeller 600.Certainly, in other embodiments, according to the type of unmanned plane 1000 and need
Ask different, actuating member is also possible to other specific forms, such as can be wheel, cursor etc..
Embodiment two
The structure of dynamical system 100 will be described further below:
Fig. 2 to Fig. 5 is please referred to, dynamical system 100 includes motor 10, electron speed regulator 20 and connector 30.Electronic speed regulation
Device 20 is used to control the working condition of motor 10.Connector 30 is for being electrically connected motor 10 and electron speed regulator 20.Connector 30
Including conduct piece 31 and packaging body 32.Conduct piece 31 is electrically connected with one end of triple line 400, the other end and electricity of triple line 400
Machine 10 is electrically connected.Packaging body 32 is formed with opposite the first face 321 and the second face 322.Interconnecting piece is formed on first face 321
323.Conduct piece 31 is encapsulated in packaging body 32, and conduct piece 31 at least partly exposes from interconnecting piece 323, to allow fastener 500
It is mounted on interconnecting piece 323 and is electrically connected conduct piece 31 and electron speed regulator 20.Electron speed regulator 20 and conduct piece 31 pass through tight
Firmware 500 is electrically connected.
In the unmanned plane 1000 of the utility model embodiment, conduct piece 31 is encapsulated in packaging body 32 and from interconnecting piece
323 expose, and since interconnecting piece 323 is formed in the first face 321, and fastener 500 is only mounted on interconnecting piece 323 by user,
It could be electrically connected conduct piece 31 and electron speed regulator 20, the anti-loaded connector 30 of user is prevented and lead to 400 connection error of triple line.
Specifically, Fig. 1 and Fig. 2 is please referred to, motor 10 can be three-phase motor, and motor 10 can be in the control of electron speed regulator 20
Make lower work.Motor 10 may be mounted on one end of horn 300.It is appreciated that the different mode of connection meetings of motor 10
The steering for influencing motor 10, in the unmanned vehicle of the utility model embodiment, the different motors 10 of different dynamic system 100
It may need to rotate with different direction of rotation, so that the whole smooth flight of unmanned plane 1000, such as turn of adjacent motor 10
Move it is contrary so that the torque that multiple dynamical systems 100 are applied on fuselage 200 is cancelled out each other.Therefore, the steering of motor 10
It is of great significance for the smooth flight of unmanned plane 1000, and the steering of motor 10 can pass through motor 10 and triple line 400
Different connection types be arranged accordingly.
Please refer to figs. 2 and 3, and electron speed regulator 20 can be used for controlling the working condition of motor 10, such as control motor
10 rotate forward, invert, acceleration rotates etc..Electron speed regulator 20 may be mounted on horn 300 and connect with flight control system, electricity
Sub- governor 20 receives the working condition that motor 10 is controlled after the control command of flight control system.Electron speed regulator 20 includes
Shell 21 and electric tuned plate 22.
Shell 21 can be used as the shell of electron speed regulator 20.Shell 21 is formed with accommodating space 211 and connection receiving is empty
Between 211 through-hole 212.Accommodating space 211 can be used for accommodating electric tuned plate 22 so that electric the invading from dust, steam etc. of tuned plate 22
Erosion.Through-hole 212 can be used for passing through for fastener 500 with connecting connector 30 and the electric tuned plate 22 of being electrically connected.
Specifically, shell 21 includes upper casing 213 and lower casing 214.Upper casing 213 is combined with lower casing 214 receiving is collectively formed
Space 211, upper casing 213 and lower casing 214 can be by engaging, screwing togather, weld etc. in conjunction with modes.Upper casing 213 offers above-mentioned
Through-hole 212, connector 30 may be mounted on upper casing 213.In the utility model embodiment, upper casing 213 is also formed with heat dissipation
Fin 2131, the heat that the electric work of tuned plate 22 generates can quickly be transmitted to the external world by radiating fin 2131.Lower casing 214 can be with
It is fixedly mounted on horn 300, entire electron speed regulator 20 is fixed on horn 300.It can also be formed on lower casing 214
Fixed structure for fixed electric tuned plate 22.
Electric tuned plate 22 is mounted in accommodating space 211.Specifically, electric tuned plate 22 can be carried on lower casing 214.Electric tuned plate
Control route union can be equipped on 22 at there is an electronic component 221, electronic component 221 for example can be capacitor, inductance,
Diode etc..Electric tuned plate 22 is connect with flight control system, and electric tuned plate 22 is also used to connect with motor 10.
Embodiment three
Please refer to figs. 2 and 3, and connector 30 is for connecting motor 10 and electron speed regulator 20.Specifically, connector 30 can
Motor 10 and electron speed regulator 20 are connected by triple line 400.Incorporated by reference to Fig. 4 and Fig. 5, connector 30 includes conduct piece 31 and envelope
Fill body 32.
Conduct piece 31 is electrically connected with one end of triple line 400.Conduct piece 31 can use copper, copper alloy, aluminium alloy, conduction
The conductive materials such as plastics, conductive rubber are made.Conduct piece 31 is encapsulated in packaging body 32, and conduct piece 31 is at least partly from encapsulation
Body 32 exposes, and since conduct piece 31 is electrically connected with triple line 400, the other end of triple line 400 is electrically connected with motor 10, therefore,
User only needs that the conduct piece 31 of exposing is connected with electron speed regulator 20 by conductive fastener 500 during installation
Realize the purpose of connection motor 10 and electron speed regulator 20.
Please refer to Fig. 6 and Fig. 7, in the utility model embodiment, conduct piece 31 includes conductive ring 311 and connector 312.It is conductive
Circle 311 is fixedly connected with connector 312, and conductive ring 311 and connector 312 can be integrally formed.Mounting hole is formed on conductive ring 311
3111, mounting hole 3111 can be used for passing through for fastener 500, such as when fastener 500 is screw, the stud of fastener 500
Mounting hole 3111 can be passed through and be further electrically connected with electron speed regulator 20, the nut of fastener 500 can be with conductive ring 311
It offsets to be electrically connected with conductive ring 311.Connector 312 can be used for being electrically connected triple line 400, and specifically, connector 312 can be formed
There is connection space 3121.Triple line 400 can be protruded into connection space 3121 and be connect with connector 312, such as will by welding
Triple line 400 is electrically connected with connector 312.
Fig. 4 to fig. 6 is please referred to, for packaging body 32 for encapsulating conduct piece 31, packaging body 32 can be with the three-phase of packed part
Line 400.During making packaging body 32, the triple line 400 connected and conduct piece 31 first can be fixed on note together
In mould, it can be molded to obtain packaging body 32 by techniques such as encapsulated injection moldings.Packaging body 32 can be made of insulating material, example
As the material of packaging body 32 can be plastic cement.The global shape of packaging body 32 such as can be square, is round, trapezoidal at the shapes, herein
With no restriction.When connecting motor 10 and electron speed regulator 20, packaging body 32 be can be set on upper casing 213.
Packaging body 32 is formed with the first face 321 and the second face 322.First face 321 is opposite with the second face 322.Connect in installation
When connecing device 30, the second face 322 can be combined with upper casing 213, specifically can be the second face 322 and support on upper casing 213.First
Interconnecting piece 323 is formed on face 321, fastener 500 is mounted on interconnecting piece 323 and is electrically connected conduct piece 31 and electron speed regulator
20.During installation, fastener 500 can pass through interconnecting piece 323 and through-hole 212, be adjusted with being electrically connected conduct piece 31 and electricity
Plate 22.Specifically, conduct piece 31 can expose from interconnecting piece 323, more specifically, conductive ring 311 can reveal from interconnecting piece 323
Out.Interconnecting piece 323 can be formed on the first face 321, and the cross sectional dimensions of interconnecting piece 323 and the maximum of fastener 500 are transversal
Face size is adapted, specifically, the size of interconnecting piece 323 can accommodate the head of screw just when fastener 500 is screw,
And interconnecting piece 323 is then not formed on the second face 322, the accommodation space of screw head can not be also provided on the second face 322.Therefore
When user needs installs connector 30, only makes connector 30 be in the second face 322 and combined with upper casing 213 and the first face 321
The state that the interconnecting piece 323 of upper formation exposes, user could be fixed by connector 30 and electron speed regulator 20 by fastener 500
Connection.Therefore, user will not be anti-loaded by connector 30, guarantees that motor 10 and electron speed regulator 20 connect according to scheduled connection type
It connects.
In the utility model embodiment, interconnecting piece 323 includes the mounting groove 323 being formed on the first face 321.Mounting groove
323 at least partly accommodating fastener 500.Conduct piece 31 can be used as the slot bottom of mounting groove 323, and conduct piece 31 is from mounting groove
323 expose, fastener 500 pass through conduct piece 31, and can partial receipt in mounting groove 323.In one example, work as fastener
500 when being screw, and after fastener 500 is installed in place, fastener 500 can all be accommodated in mounting groove 323, without from the
It 321 protrudes above on one side, user can also judge whether to pacify by further judging whether fastener 500 protrudes from the first face 321
Dress is correct and is installed in place.
In some embodiments, packaging body 32 further includes side wall 324.Side wall 324 connects the first face 321 and the second face
322.Packaging body 32 forms jagged 325 on side wall 324, and notch 325 is connected to mounting groove 323.It is appreciated that unmanned plane
1000 in the process of work, and the foreign matters such as rainwater, dust may be fallen into mounting groove 323, and these foreign matters may will affect
The switching performance of connector 30 is even on electric tuned plate 22.Notch 325 is provided with side wall 324 and is connected to mounting groove 323,
Convenient for the foreign matter in mounting groove 323 is discharged, such as can be directly from notch 325 into liquid such as rainwater in mounting groove 323
Outflow is to prevent from accumulating in mounting groove 323.
Further, in certain embodiments, along the direction that the second face 322 is directed toward in the first face 321, notch 325
Depth is greater than or equal to the depth of mounting groove 323.In this way, being further ensured that the foreign matters such as rainwater can flow completely from notch 325
Out, without being remained in the bottom of mounting groove 323.
Fig. 3 and Fig. 4 is please referred to, in some embodiments, the quantity of conduct piece 31 is multiple, the quantity of interconnecting piece 323
To be multiple, each conduct piece 31 exposes from a corresponding interconnecting piece 323.In the utility model embodiment, conduct piece 31
Quantity is three, and each conduct piece 31 is connect with one in triple line 400, and multiple conduct pieces 31 are mutually encapsulated into the same envelope
It fills in body 32, triple line 400 will not be compact-sized in the state being scattered.The quantity of interconnecting piece 323 is multiple, each conduct piece
31 expose from a corresponding interconnecting piece 323, multiple fasteners 500 can be set, each fastener 500 is each passed through a company
Socket part 323 and conduct piece 31 are to be electrically connected electron speed regulator 20 and connector 30.Corresponding, the quantity of notch 325 is also possible to
Multiple, each notch 325 is connected to a corresponding interconnecting piece 323 (mounting groove 323)；The quantity of through-hole 212 is also possible to more
A, each through-hole 212 is aligned with an interconnecting piece 323.Certainly, the quantity of conduct piece 31 is not limited to three of the example above, also
Different quantity can be set according to different demands, such as the quantity of conduct piece 31 is two, four, five, six etc..
Fig. 4 and Fig. 5 is please referred to, in some embodiments, connector 30 further includes fixing piece 33, fixing piece 33 and three-phase
Line 400 connects, and fixing piece 33 is used to triple line 400 being fixed on external equipment by preset sequence.Triple line 400 can be consolidated
Be scheduled on fixing piece 33, then fixing piece 33 be fixed on external equipment again, for example, by fixing piece 33 be fixed on horn 300 or
In motor 10, so that triple line 400 will not be wound mutually in the motion process of unmanned plane 1000.Also, triple line 400
It puts in order also critically important, triple line 400 is corresponding with the electric corresponding position of tuned plate 22 by correct preset order, could make electricity
It adjusts 20 correctly to control motor 10 to rotate by preset correct direction.Therefore, fixing piece 33 can prevent user during installation by three
The sequence of phase line 400 is wrongly installed, and makes the motor steering after installation different from original steering, or can not rotate.
Referring to Fig. 3, in some embodiments, being provided with conductive column 23 on electric tuned plate 22.Fastener 500 and conductive column
23 connections are to connect conduct piece 31 and electric tuned plate 22.Sealing ring 24 is provided between conductive column 23 and upper casing 213.
Specifically, conductive column 23 can be fixedly connected with electric tuned plate 22, and conductive column 23 is made of an electrically conducting material.Conductive column 23
On could be formed with mounting structure for cooperating with fastener 500, mounting structure is, for example, the peace being provided on conductive column 23
Hole is filled, fastener 500 passes through the through-hole 212 on upper casing 213, and is electrically connected after passing through mounting hole with conductive column 23.Sealing ring 24
Setting can seal the gap between through-hole 212 and fastener 500 between upper casing 213 and electric tuned plate 22.Sealing ring 24 can
Rainwater, dust, other impurity or foreign matter is stopped to enter on electric tuned plate 22 from through-hole 212, to prevent them from making to electric tuned plate 22
At influence, or even electric tuned plate 22 is damaged, can be effectively reduced mechanical disorder, improve the service life of electron speed regulator 20.At this
In embodiment, sealing ring 24 can achieve IPX7 grades of waterproofs, i.e. sealing ring 24 can be IPX7 grades of sealing rings, belong to anti-leaching type,
Even if it is under water to can protect electron speed regulator 20, water will not enter inside, it is to be understood that in other embodiments
In, sealing ring 24 can also be other ranks, will not repeat them here.
In the description of this specification, reference term " certain embodiments ", " embodiment ", " some embodiment party
The description of formula ", " exemplary embodiment ", " example ", " specific example " or " some examples " means in conjunction with the embodiment
Or example particular features, structures, materials, or characteristics described are contained at least one embodiment of the utility model or show
In example.In the present specification, schematic expression of the above terms are not necessarily referring to identical embodiment or example.And
And particular features, structures, materials, or characteristics described can be in any one or more embodiments or example to close
Suitable mode combines.
In addition, term " first ", " second " are used for descriptive purposes only and cannot be understood as indicating or suggesting relative importance
Or implicitly indicate the quantity of indicated technical characteristic.Define " first " as a result, the feature of " second " can be expressed or
Implicitly include at least one described feature.The meaning of " plurality " is at least two, such as two in the description of the present invention,
It is a, three, unless otherwise specifically defined.
Although the embodiments of the present invention have been shown and described above, it is to be understood that above-described embodiment is
Illustratively, it should not be understood as limiting the present invention, those skilled in the art are in the scope of the utility model
It inside can make changes, modifications, alterations, and variations to the above described embodiments, the scope of the utility model is by claim and its is equal
Object limits.
Claims (13)
1. a kind of connector, for being electrically connected motor and electron speed regulator, which is characterized in that the connector includes:
Conduct piece, the conduct piece are electrically connected with one end of triple line, and the other end of the triple line is electrically connected with the motor；
And
Packaging body, the packaging body is formed with opposite the first face and the second face, is formed with interconnecting piece on first face, described
Conduct piece is encapsulated in the packaging body, and the conduct piece at least partly exposes from the interconnecting piece, to allow fastener to install
On the interconnecting piece and it is electrically connected the conduct piece and the electron speed regulator.
2. connector according to claim 1, which is characterized in that the interconnecting piece includes being formed on first face
Mounting groove, the mounting groove is at least partly accommodating the fastener.
3. connector according to claim 2, which is characterized in that the packaging body further includes connection first face and institute
State the side wall in the second face, the packaging body forms jagged on the side wall, and the notch is connected to the mounting groove.
4. connector according to claim 3, which is characterized in that be directed toward the direction in second face along first face
On, the depth of the notch is greater than or equal to the depth of the mounting groove.
5. connector according to claim 1, which is characterized in that the quantity of the conduct piece is multiple, the interconnecting piece
Quantity be it is multiple, each conduct piece exposes from corresponding one interconnecting piece.
6. connector according to claim 1, which is characterized in that the conduct piece includes the conductive ring for being formed with mounting hole
The connector being fixedly connected with the conductive ring, the connector are electrically connected with the triple line, the conductive ring at least partly from
The interconnecting piece exposes.
7. connector according to claim 1, which is characterized in that the connector further includes fixing piece, the fixing piece
It is connect with the triple line, the fixing piece is used to the triple line being fixed on external equipment by preset order.
8. a kind of dynamical system characterized by comprising
Motor；
Electron speed regulator, the electron speed regulator are used to control the working condition of the motor；And
Connector described in claim 1 to 7 any one, the electron speed regulator and the conduct piece pass through the fastener
Electrical connection.
9. dynamical system according to claim 8, which is characterized in that the electron speed regulator includes:
Shell, the shell are formed with accommodating space, and the through-hole of the connection accommodating space, the connector are arranged described
Outside the accommodating space and position of the interconnecting piece and the through-hole alignment；And
Electric tuned plate, the electricity tuned plate are housed in the accommodating space, and the fastener passes through the interconnecting piece and the through-hole,
To be electrically connected the conduct piece and the electric tuned plate.
10. dynamical system according to claim 9, which is characterized in that the shell includes:
Upper casing, the through-hole are provided on the upper casing, and second face supports on the upper casing；And
Lower casing, the lower casing form the accommodating space in conjunction with the upper casing.
11. dynamical system according to claim 10, which is characterized in that it is provided with conductive column on the electricity tuned plate, it is described
Fastener is connect to connect the conduct piece and the electric tuned plate with the conductive column.
12. dynamical system according to claim 11, which is characterized in that be provided between the conductive column and the upper casing
Sealing ring, the sealing ring can seal the gap between the through-hole and the fastener.
13. a kind of unmanned plane characterized by comprising
Fuselage；
The horn being connected on the fuselage；And
Dynamical system described in claim 8 to 12 any one, the dynamical system are mounted on the horn.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821578488.6U CN208947596U (en) | 2018-09-26 | 2018-09-26 | Connector, dynamical system and unmanned plane |
| CN201880088685.6A CN111684690A (en) | 2018-09-26 | 2018-12-06 | Connector, driving system and unmanned aerial vehicle |
| PCT/CN2018/119475 WO2020062574A1 (en) | 2018-09-26 | 2018-12-06 | Connector, power systems and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821578488.6U CN208947596U (en) | 2018-09-26 | 2018-09-26 | Connector, dynamical system and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208947596U true CN208947596U (en) | 2019-06-07 |
Family
ID=66739644
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821578488.6U Expired - Fee Related CN208947596U (en) | 2018-09-26 | 2018-09-26 | Connector, dynamical system and unmanned plane |
| CN201880088685.6A Pending CN111684690A (en) | 2018-09-26 | 2018-12-06 | Connector, driving system and unmanned aerial vehicle |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201880088685.6A Pending CN111684690A (en) | 2018-09-26 | 2018-12-06 | Connector, driving system and unmanned aerial vehicle |
Country Status (2)
| Country | Link |
|---|---|
| CN (2) | CN208947596U (en) |
| WO (1) | WO2020062574A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112823575A (en) * | 2020-04-27 | 2021-05-18 | 深圳市大疆创新科技有限公司 | Radiator, heat radiation structure and unmanned aerial vehicle |
| CN114845934A (en) * | 2019-12-27 | 2022-08-02 | Wing航空有限责任公司 | System and method for stopping movement of an operating member |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2100695U (en) * | 1991-05-15 | 1992-04-01 | 王文超 | Power coupler |
| US6210215B1 (en) * | 1999-11-24 | 2001-04-03 | Hon Hai Precision Ind. Co., Ltd. | Panel mount electrical connector assembly |
| JP2009021094A (en) * | 2007-07-12 | 2009-01-29 | Yazaki Corp | Connector |
| US7632148B1 (en) * | 2009-02-18 | 2009-12-15 | J.S.T. Corporation | Sealed and grounded electrical connector and sealed and grounded electrical connector assembly |
| CN101814895A (en) * | 2009-02-24 | 2010-08-25 | 上海雷诺尔科技股份有限公司 | Copper bar assembly structure for variable frequency speed adjustor for replacing cable |
| CN202206259U (en) * | 2011-08-25 | 2012-04-25 | 深圳市易能电气技术有限公司 | Speed regulation frequency converter and motor integrated apparatus |
| CN203135129U (en) * | 2012-08-16 | 2013-08-14 | 富士康(昆山)电脑接插件有限公司 | Electric connector |
| CN103928812B (en) * | 2014-03-14 | 2015-10-21 | 余姚市惠美电器有限公司 | A kind of special cleaning machine of electrical automobile charging plug |
| CN104409906B (en) * | 2014-11-25 | 2016-06-22 | 上海航天科工电器研究院有限公司 | A kind of light in inserting/pulling force high speed transmission electric connector |
| CN204304107U (en) * | 2014-12-30 | 2015-04-29 | 海信（山东）空调有限公司 | The online line Quick Connect Kit of air-conditioning |
| CN204793276U (en) * | 2015-07-27 | 2015-11-18 | Tcl通力电子（惠州）有限公司 | Adapter |
| CN205178043U (en) * | 2015-11-20 | 2016-04-20 | 苏州欧普照明有限公司 | Electric connector , electric connector combination and illumination lamps and lanterns |
| CN205385382U (en) * | 2016-01-22 | 2016-07-13 | 深圳市大疆创新科技有限公司 | Connector, driving system and unmanned vehicles of electronic governor and motor |
| CN205960263U (en) * | 2016-07-25 | 2017-02-15 | 上海合璧电子电器有限公司 | Improved electric connector |
| CN206524322U (en) * | 2016-12-28 | 2017-09-26 | 深圳市大疆创新科技有限公司 | Electron speed regulator and moveable platform |
| CN207450265U (en) * | 2017-10-31 | 2018-06-05 | 上海拓攻机器人有限公司 | A kind of multi-rotor unmanned aerial vehicle of motor cabinet and the application motor cabinet |
| CN108539933B (en) * | 2018-06-06 | 2024-09-06 | 深圳市道通智能航空技术股份有限公司 | Motor, power device and unmanned vehicles |
-
2018
- 2018-09-26 CN CN201821578488.6U patent/CN208947596U/en not_active Expired - Fee Related
- 2018-12-06 CN CN201880088685.6A patent/CN111684690A/en active Pending
- 2018-12-06 WO PCT/CN2018/119475 patent/WO2020062574A1/en active Application Filing
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114845934A (en) * | 2019-12-27 | 2022-08-02 | Wing航空有限责任公司 | System and method for stopping movement of an operating member |
| CN112823575A (en) * | 2020-04-27 | 2021-05-18 | 深圳市大疆创新科技有限公司 | Radiator, heat radiation structure and unmanned aerial vehicle |
| WO2021217366A1 (en) * | 2020-04-27 | 2021-11-04 | 深圳市大疆创新科技有限公司 | Radiator, heat dissipation structure and unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2020062574A1 (en) | 2020-04-02 |
| CN111684690A (en) | 2020-09-18 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US10523090B2 (en) | Inverter terminal block installed in a motor case | |
| CN105960748B (en) | In-vehicle electronic control unit and in-vehicle electromechanical integrated electric motor | |
| US6882072B2 (en) | Energy storage flywheel system with a power connector that integrally mounts one or more controller circuits | |
| CN208947596U (en) | Connector, dynamical system and unmanned plane | |
| US20110316373A1 (en) | Inverter terminal board installed in motor case | |
| US10779444B2 (en) | Control boxes and system-on-module circuit boards for unmanned vehicles | |
| US10264695B2 (en) | Power converter | |
| CN202601769U (en) | Battery module | |
| JP2014164875A (en) | Terminal board and electronic apparatus including the same | |
| US10122313B2 (en) | Power conversion device | |
| US11465776B2 (en) | Charging system for autonomous drones | |
| CN206480722U (en) | Integrated BDU for power battery pack and power battery pack with same | |
| CN208923759U (en) | A kind of high pressure junction box and electric machine controller | |
| CN214954697U (en) | Unmanned aerial vehicle avionics system and unmanned aerial vehicle | |
| WO2022036517A1 (en) | Conducting member, liquid-cooled conductive structure, motor, and electric car power assembly | |
| CN203353030U (en) | ESC heat dissipation device for aircraft | |
| EP4458616A1 (en) | Power distribution unit capable of being multidirectionally matched and mounted, system, and electric vehicle | |
| CN214189555U (en) | Fuse box assembly and vehicle | |
| CN213043426U (en) | Wire harness waterproof plug-in device and power supply conveying equipment | |
| CN207947969U (en) | Speed setting controller packaging system | |
| CN107887548A (en) | Battery box | |
| CN211046698U (en) | Brushless motor of electricity accent motor integral type | |
| JP7310593B2 (en) | power converter | |
| US20220294360A1 (en) | Power converter | |
| CN209169209U (en) | Battery component, battery modules and unmanned plane |
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: 20190607 |