CN106184703A - Attachment means and multi-rotor aerocraft - Google Patents
Attachment means and multi-rotor aerocraft Download PDFInfo
- Publication number
- CN106184703A CN106184703A CN201610618629.1A CN201610618629A CN106184703A CN 106184703 A CN106184703 A CN 106184703A CN 201610618629 A CN201610618629 A CN 201610618629A CN 106184703 A CN106184703 A CN 106184703A
- Authority
- CN
- China
- Prior art keywords
- terminal
- plug connector
- attachment means
- button
- plug
- 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
- 238000009434 installation Methods 0.000 claims abstract description 34
- 230000015572 biosynthetic process Effects 0.000 claims abstract description 3
- 230000003467 diminishing effect Effects 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 12
- 238000003032 molecular docking Methods 0.000 abstract description 8
- 230000005611 electricity Effects 0.000 description 5
- 238000004806 packaging method and process Methods 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000008859 change Effects 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000000284 extract Substances 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connector Housings Or Holding Contact Members (AREA)
Abstract
nullThe open a kind of attachment means of the present invention and multi-rotor aerocraft，This attachment means includes one first plug connector and one second plug connector，It is formed with Plug Division at the front end of the first plug connector，Plug Division is formed with the first terminal installation portion and at least one button installation position in its outer surface，The first terminal installation portion is fixed with the first terminal，Each button installation position is provided with a button by a spring，Second plug connector is formed with one and plugs chamber，Plug and at the inner surface in chamber, be formed with the second terminal mount being matched with the first terminal installation portion，And formation is matched with the button mouth of button in its cavity wall，Second terminal mount is fixed with the second terminal，Plug Division is inserted within plugging chamber，The first terminal installation portion and the assembling of the second terminal mount，The first terminal and the second terminal are electrically connected with，Button is placed in corresponding button mouth under the action of the spring.The present invention has terminal docking precision height, the Advantageous Effects of good connecting effect.
Description
Technical field
The present invention relates to a kind of attachment means and use the multi-rotor aerocraft of this attachment means.
Background technology
Existing multi-rotor aerocraft mainly includes fuselage, multiple with the integrated horn of fuselage and multiple be divided into machine
The propeller of arm end, owing to horn and horn are formed in one preparation, although this kind of structure is simply, but, when being pointed to
When the motor of horn end and the electron speed regulator being positioned at fuselage interior are electrically connected, the connecting line of motor needs from machine
Arm is internal to be adjusted through the electricity being connected to fuselage, and the grafting horn the most again that power line docking got up of must checking the number one by one, this
Planting connected mode process the most loaded down with trivial details, work efficiency is low, and adds the probability made mistakes.
Summary of the invention
The technical problem to be solved is to provide a kind of terminal docking precision height, the connection of good connecting effect
Device.
Another technical problem to be solved of the present invention be to provide a kind of lifting motor and electricity adjust docking precision and
Connect effect, be easy to product packaging and the multi-rotor aerocraft of transport.
For solving above-mentioned technical problem, the present invention provides employing technical scheme as described below: a kind of attachment means, it includes
Have one first plug connector and one with the second plug connector of described first plug connector grafting, formed at the front end of described first plug connector
Having Plug Division, described Plug Division is formed with the first terminal installation portion and at least one button installation position in its outer surface, and described
One terminal mount is fixed with the first terminal, each button installation position is provided with a button by a spring, described second
Plug connector is formed with one and plugs chamber for what described Plug Division plugged, described in plug be formed at the inner surface in chamber be matched with described
Second terminal mount of the first terminal installation portion, and formed in its cavity wall and be matched with the button mouth of described button, described the
Two-terminal installation portion is fixed with the second terminal mated with described the first terminal, described Plug Division be inserted in described in plug chamber it
In, the first terminal installation portion and the assembling of the second terminal mount, the first terminal and the second terminal are electrically connected with, and button is at spring
Corresponding button mouth it is placed under effect.
In above-mentioned attachment means, described Plug Division is respectively formed with a button installation position at the opposite sides of its outer surface.
In above-mentioned attachment means, described the first terminal installation portion is the recessed axle formed of the outer surface from described Plug Division
To groove, described second terminal mount is to protrude, from the described inner surface plugging chamber, the hollow axial boss formed, described
Boss is placed in described groove.
In above-mentioned attachment means, described groove is the diminishing structure of notch, and described boss is that platform top gradually expands
Structure.
In above-mentioned attachment means, at the bottom of described Plug Division, it is formed with the step around described Plug Division, when first inserts
When fitting is inserted in the second plug connector, described in plug the top in chamber and contact at described step.
In above-mentioned attachment means, described the first terminal installation portion is provided with a terminal clamp gripping member, described terminal clamp gripping member
Including one first grip block and second grip block docked with described first grip block, the first terminal is clamped by described first
Plate and the second grip block clamp and are fixed among described the first terminal installation portion.
In above-mentioned attachment means, described first grip block is formed with the first groove of multiple semicircle shape, described second folder
Hold the second groove being formed with multiple semicircle shape on plate, described first groove and the second groove fit and by spacing for the first terminal also
Fixing.
In above-mentioned attachment means, described second terminal mount is provided with a terminal fixing plate, described terminal fixing plate
On be formed with some circular ports, the second terminal through described circular port and be fixed on described terminal fixing plate.
In above-mentioned attachment means, described Plug Division is the structure of cross section ovalize, described in plug chamber be cross section in
Oval structure.
A kind of multi-rotor aerocraft, includes a fuselage and multiple horn, and described fuselage interior is provided with electron speed regulator, institute
State the end of horn to be provided with motor, described horn and fuselage and be attached by above-mentioned attachment means, described first grafting
Part is located at one end of described horn, and its interior the first terminal is electrically connected with described motor, and described second plug connector is located at described
The side of fuselage, its second interior terminal is electrically connected with described electron speed regulator.
The Advantageous Effects of the present invention is: this attachment means include one first plug connector and one can with this first insert
The second plug connector that fitting grafting coordinates, and the first terminal, the second terminal are divided into the first plug connector, the phase of the second plug connector
Answer position, by the grafting of the first plug connector and the second plug connector to realize the first terminal and the electrical connection of the second terminal,
So, it is ensured that the accuracy of terminal docking and connection effect, it is to avoid the chance that terminal grafting makes mistakes；This multi-rotor aerocraft will
Horn and fuselage are divided into independent parts, re-use attachment means and are attached, so, in the production and sales process of product
In, horn can be separated with fuselage, thus reduce the packaging volume of product, it is simple to pack and transport, transport sky can be made full use of
Between, reduce cost of transportation, can coordinate with this first plug connector grafting additionally, this attachment means includes one first plug connector and
The second plug connector, and the second terminal that the first terminal being electrically connected with motor and electron speed regulator are electrically connected with is set up separately
In the first plug connector, the corresponding position of the second plug connector, by the grafting of the first plug connector and the second plug connector to realize
One terminal and the electrical connection of the second terminal, thus realize the electrical connection of electron speed regulator and motor, so, it is ensured that motor
Adjust docking precision with electricity and connect effect.
Accompanying drawing explanation
Fig. 1 is the perspective view of attachment means of the present invention.
Fig. 2 is the decomposition texture schematic diagram of attachment means of the present invention.
Fig. 3 is the structural representation of another embodiment of attachment means of the present invention.
Detailed description of the invention
For making those of ordinary skill in the art be more clearly understood from the object, technical solutions and advantages of the present invention, with
Under the present invention is further elaborated in conjunction with the accompanying drawings and embodiments.
Attachment means disclosed in this invention can be as the building block of multi-rotor aerocraft, for multi-rotor aerocraft
Horn and the connection of fuselage, in the following description, also illustrate attachment means, so as a example by multi-rotor aerocraft
And, it will be appreciated by those skilled in the art that ground, attachment means disclosed in this invention does not limit and is applied to multi-rotor aerocraft,
Also apply be applicable to, on other equipment, to realize the connection of two parts, such as, be electrically connected.Refering to shown in Fig. 1 to Fig. 2, it is somebody's turn to do
Attachment means include one first plug connector 10 and one with the second plug connector 20 of this first plug connector 10 grafting.Wherein, this
Being formed with Plug Division 100 at the front end of one plug connector 10, this Plug Division 100 is formed with the first terminal installation portion in its outer surface
101, and at the opposite sides of outer surface, respectively it is formed with a button installation position 102, this first terminal installation portion 101 is fixed with
The first terminal (not shown in FIG.), and each button installation position 102 is provided with a button 104 by a spring 103.This is years old
Two plug connectors 20 are formed with one and plug chamber 200 for what this Plug Division 100 plugged, and this plugs and is formed at the inner surface in chamber 200
It is matched with the second terminal mount 201 of this first terminal installation portion 101, and formation is matched with button 104 in its cavity wall
Button mouth 202, is fixed with the second terminal (not shown in FIG.) mated with the first terminal in this second terminal mount 201.
This Plug Division 100 is inserted within this plugs chamber 200, and its first terminal installation portion 101 assembles with the second terminal mount 201,
The first terminal and the second terminal are electrically connected with, and button 104 is then placed in corresponding button mouth 202 under the effect of spring 103,
Thus realize the first plug connector 10 and firm grafting of the second plug connector 20.Preferably, this Plug Division 100 be designed as cross section in
Oval structure, this plugs chamber 200 and is also configured as the structure of the cross section ovalize coordinated with this Plug Division 100.
During insertion, first press with finger two buttons 104, the second grafting is inserted in the Plug Division 100 of the first plug connector 10
Part 20 plug chamber 200, and unclamp finger after being pushed to the end, button 104 is upspring under the elastic force effect of spring 103 and is inserted
In the two corresponding button mouths 202 of plug connector 20, realize the first plug connector 10 He by button 104 and the cooperation of button mouth 202
Fixing of second plug connector 20, now the first terminal and the second terminal constitute electrical connection；When extracting, make to press with finger two
Button 104 to button 104 end face, less than plugging the internal face in chamber 200, the most outwards extracts the first plug connector 10, can realize the
One plug connector 10 and the separation of the second plug connector 20.
What this attachment means included that one first plug connector 10 and can coordinate with this first plug connector 10 grafting second inserts
Fitting 20, and the first terminal, the second terminal are divided into the corresponding position of first plug connector the 10, second plug connector 20, pass through
The grafting of the first plug connector 10 and the second plug connector 20, to realize the first terminal and the electrical connection of the second terminal, so, can be protected
The accuracy of card terminal docking and connection effect, it is to avoid the chance that terminal grafting makes mistakes.
As shown in drawings, in this preferred embodiment, this first terminal installation portion 101 is the appearance from this Plug Division 100
The axial notch that face is recessed and is formed, this second terminal mount 201 protrudes for the inner surface plugging chamber 200 from this and is formed
Hollow axial boss, this boss is placed in corresponding groove.Preferably, this groove is the diminishing structure of notch, and is somebody's turn to do
Boss is the structure that platform top gradually expands, so, it is ensured that this first terminal installation portion 101 and second terminal mount 201 liang
Being accurately positioned between person, improves the first terminal and the accuracy of the second terminal connection further.
In the example shown in accompanying drawing 1～2, two buttons 104 are set on the Plug Division 100 of this first plug connector 10,
And corresponding two the button mouths 202 in position are set in plugging of this second plug connector 20, by two button 104 Hes on chamber 200
The corresponding matching of two button mouths 202 and realize the first plug connector 10 and firm connection of the second plug connector 20.And such as Fig. 3 institute
In the embodiment shown, a button 104 is only set on this Plug Division 100, and plugs chamber 200 in this button mouth 202 is set,
The first plug connector 10 and connection of the second plug connector 20 is fixed with coordinating of a button mouth 202 by a button 104, certainly,
The embodiment of the stable connection of this kind of embodiment the most as above embodiment.
Preferably, the step 105 around this Plug Division 100 it is formed with at the bottom of this Plug Division 100, when the first plug connector
10 when being inserted in the second plug connector 20, and the top plugging chamber 200 of this second plug connector 20 can contact at this step 105.So,
During grafting, push this first plug connector 10 to this step 105 and contact at this second plug connector 20 and can make both
It is accurately positioned, it is simple to the operation of user.
In certain embodiments, this first terminal installation portion 100 is provided with a terminal clamp gripping member 106 for gripping
The first terminal, this terminal clamp gripping member 106 includes that one first grip block 1060 and docks with this first grip block 1060
Two grip blocks 1061, the first terminal is clamped by this first grip block 1060 and the second grip block 1061 and is fixed on this first terminal
Among installation portion 100.Refering to shown in Fig. 2, this first grip block 1060 is formed with the first groove 1062 of multiple semicircle shape, should
Being formed with the second groove 1063 of multiple semicircle shape on second grip block 1061, this first groove 1062 and the second groove 1063 are joined
Close and by spacing for the first terminal and fix.
As in figure 2 it is shown, in some preferred embodiments, the second terminal is arranged at second by a terminal fixing plate 107
In terminal mount 201, this terminal fixing plate 107 being formed with some circular ports 1070, the second terminal passes this circular port
1070 and be fixed on this terminal fixing plate 107.
The invention also discloses a kind of multi-rotor aerocraft, it includes and is provided with the fuselage of electron speed regulator and multiple end in one
Being provided with the horn of motor at end, each horn is attached with this fuselage by an attachment means, wherein, and this attachment means
First plug connector 10 is located at one end of this horn, and its interior the first terminal is electrically connected with motor, and the second of this attachment means inserts
Fitting 20 is located at the side of this fuselage, and its second interior terminal is electrically connected with electron speed regulator.
Horn and fuselage are divided into independent parts by this multi-rotor aerocraft, re-use attachment means and are attached, as
This, during the production and sales of product, can separate horn with fuselage, thus reduce the packaging volume of product, it is simple to packaging
And transport, transport space can be made full use of, reduce cost of transportation.Additionally, this attachment means includes one first plug connector 10 He
One the second plug connector 20 that can coordinate with this first plug connector 10 grafting, and by the first terminal being electrically connected with motor and electricity
The second terminal that sub-speed regulator is electrically connected with is divided into the corresponding position of first plug connector the 10, second plug connector 20, by the
The grafting of one plug connector 10 and the second plug connector 20 is to realize the first terminal and the electrical connection of the second terminal, thus realizes electronics
Speed regulator and the electrical connection of motor, so, it is ensured that motor and electricity are adjusted docking precision and connect effect.
The foregoing is only the preferred embodiments of the present invention, rather than the present invention is done any pro forma restriction.This area
Technical staff can impose change and the improvement of various equivalent, all institutes within the scope of the claims on the basis of above-described embodiment
The equivalent variations done or modification, all should fall under the scope of the present invention.
Claims (10)
1. an attachment means, include one first plug connector and one with the second plug connector of described first plug connector grafting, its
Being characterised by: be formed with Plug Division at the front end of described first plug connector, described Plug Division is formed with first in its outer surface
Terminal mount and at least one button installation position, be fixed with the first terminal in described the first terminal installation portion, each button is installed
In Wei, a spring being provided with a button, described second plug connector is formed with one and plugs chamber for what described Plug Division plugged,
The second terminal mount being matched with described the first terminal installation portion it is formed with at the described inner surface plugging chamber, and in its cavity wall
Upper formation is matched with the button mouth of described button, is fixed with mated with described the first terminal in described second terminal mount
Two-terminal, described Plug Division be inserted in described in plug chamber within, the first terminal installation portion and the second terminal mount assembling, first
Terminal and the second terminal are electrically connected with, and button is placed in corresponding button mouth under the action of the spring.
2. attachment means as claimed in claim 1, it is characterised in that: described Plug Division is each at the opposite sides of its outer surface
It is formed with a button installation position.
3. attachment means as claimed in claim 1, it is characterised in that: described the first terminal installation portion is from described Plug Division
The axial notch that outer surface is recessed and is formed, described second terminal mount is to protrude from the described inner surface plugging chamber to be formed
Hollow axial boss, described boss is placed in described groove.
4. attachment means as claimed in claim 3, it is characterised in that: described groove is the diminishing structure of notch, described
Boss is the structure that platform top gradually expands.
5. attachment means as claimed in claim 1, it is characterised in that: it is formed at the bottom of described Plug Division and inserts around described
Connect the step in portion, when the first plug connector is inserted in the second plug connector, described in plug the top in chamber and contact at described step.
6. attachment means as claimed in claim 1, it is characterised in that: described the first terminal installation portion is provided with a terminal clamp
Gripping member, described terminal clamp gripping member includes one first grip block and second grip block docked with described first grip block, the
One terminal is clamped by described first grip block and the second grip block and is fixed among described the first terminal installation portion.
7. attachment means as claimed in claim 6, it is characterised in that: it is formed with multiple semicircle shape on described first grip block
First groove, described second grip block is formed the second groove of multiple semicircle shape, and described first groove and the second groove are joined
Close and by spacing for the first terminal and fix.
8. attachment means as claimed in claim 1, it is characterised in that: described second terminal mount is provided with a terminal solid
Determining plate, described terminal fixing plate is formed some circular ports, the second terminal is fixed on described terminal through described circular port
In fixed plate.
9. attachment means as claimed in claim 1, it is characterised in that: described Plug Division is the structure of cross section ovalize,
Described plug the structure that chamber is cross section ovalize.
10. a multi-rotor aerocraft, includes a fuselage and multiple horn, and described fuselage interior is provided with electron speed regulator, institute
The end stating horn is provided with motor, it is characterised in that: described horn and fuselage are by as described in any one of claim 1～9
Attachment means be attached, described first plug connector is located at one end of described horn, its interior the first terminal and described motor
Being electrically connected with, described second plug connector is located at the side of described fuselage, and its second interior terminal is electrical with described electron speed regulator
Connect.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610618629.1A CN106184703A (en) | 2016-07-29 | 2016-07-29 | Attachment means and multi-rotor aerocraft |
| PCT/CN2017/093265 WO2018019153A1 (en) | 2016-07-29 | 2017-07-18 | Connection device and multi-rotor aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610618629.1A CN106184703A (en) | 2016-07-29 | 2016-07-29 | Attachment means and multi-rotor aerocraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106184703A true CN106184703A (en) | 2016-12-07 |
Family
ID=57497591
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610618629.1A Pending CN106184703A (en) | 2016-07-29 | 2016-07-29 | Attachment means and multi-rotor aerocraft |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN106184703A (en) |
| WO (1) | WO2018019153A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107150802A (en) * | 2017-05-23 | 2017-09-12 | 广州星晖智能科技有限公司 | A kind of adjustable for height unmanned plane of motor |
| WO2018019153A1 (en) * | 2016-07-29 | 2018-02-01 | 深圳亿天航科技有限公司 | Connection device and multi-rotor aircraft |
| WO2018113480A1 (en) * | 2016-12-21 | 2018-06-28 | 深圳市道通智能航空技术有限公司 | Detachable arm assembly and aircraft |
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| WO2018019153A1 (en) * | 2016-07-29 | 2018-02-01 | 深圳亿天航科技有限公司 | Connection device and multi-rotor aircraft |
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| CN107150802A (en) * | 2017-05-23 | 2017-09-12 | 广州星晖智能科技有限公司 | A kind of adjustable for height unmanned plane of motor |
| CN107150802B (en) * | 2017-05-23 | 2019-06-11 | 广州星晖智能科技有限公司 | A kind of height-adjustable unmanned plane of motor |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2018019153A1 (en) | 2018-02-01 |
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Effective date of abandoning: 20191227 |
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